SCROLL COMPRESSOR WITH INTERMEDIATE INJECTION

Abstract

A scroll compressor includes a compressor housing containing an orbiting scroll member, a non-orbiting scroll member, bands disposed between the non-orbiting scroll member and the compressor housing, a suction chamber, a discharge chamber, and one or more intermediate injection chamber defined by the bands. The non-orbiting scroll member includes one or more intermediate injection ports fluidly connecting the one or more intermediate injection chambers to at least one compression pocket formed by the intermeshed scroll members. A heating, ventilation, air conditioning, and refrigeration system includes a refrigerant circuit with a condenser, an expander, an evaporator, and the scroll compressor fluidly connected. A method of making a scroll compressor includes placing an upper portion of a compressor housing over a non-orbiting scroll member with bands disposed therebetween, and interference fitting the upper portion onto the non-orbiting scroll member via the bands.

Claims

1. A scroll compressor, comprising: a compressor housing containing a suction chamber, a discharge chamber, and intermediate injection chambers; an orbiting scroll member and a non-orbiting scroll member intermeshed to form compression pockets within the compressor housing, the compression pockets configured to suction from the suction chamber and discharge into the discharge chamber, the non-orbiting scroll member including intermediate injection ports fluidly connecting the intermediate injection chambers to the compression pockets; and at least three bands disposed within the compressor housing, each of the at least three bands extending between the non-orbiting scroll member and the compressor housing, the intermediate injection chambers being defined by pairs of the three or more bands.

2. The scroll compressor of claim 1, wherein the intermediate injection chambers include a first intermediate injection chamber and a second intermediate injection chamber, and the intermediate injection ports include: a first intermediate injection port fluidly connecting the first intermediate injection chamber to at least one of the compression pockets, and a second intermediate injection port fluidly connecting the second intermediate injection chamber to at least one of the compression pockets.

3. The scroll compressor of claim 2, wherein the pairs of the three or more bands include: a first pair of the bands, the first intermediate injection chamber defined by the first pair of bands, and a second pair of the bands, the second intermediate injection chamber defined by the second pair of bands.

4. The scroll compressor of claim 3, wherein the at least three bands include a first band, the first pair of the bands and the second pair of the bands each include the first band.

5. The scroll compressor of claim 3, wherein the at least three bands include a second band and a third band, the first pair of the bands including the second band, and the second pair of the bands including the third band.

6. The scroll compressor of claim 2, further comprising: a suction inlet in the compression housing, the suction chamber fluidly connecting the suction inlet to an inlet of the compression pockets, a discharge outlet in the compression housing, the discharge chamber fluidly connecting an outlet of the compression pockets to the discharge outlet, a first intermediate injection inlet in the compression housing, the first intermediate injection chamber fluidly connecting the first intermediate injection inlet to the first intermediate injection port in the non-orbiting scroll member, and a second intermediate injection inlet in the compression housing, the second intermediate injection chamber fluidly connecting the second intermediate injection inlet to the second intermediate injection port in the non-orbiting scroll member.

7. The scroll compressor of claim 1, wherein the at least three bands include: a first band that forms a seal between the intermediate injection chambers and the discharge chamber, and a second band that forms a seal between the intermediate injection chambers and the suction chamber.

8. The scroll compressor of claim 1, wherein each of the at least three bands extends from the non-orbiting scroll member to the compressor housing.

9. The scroll compressor of claim 1, wherein each of the at least three bands contacts the non-orbiting scroll member and the compressor housing.

10. The scroll compressor of claim 1, wherein one or more of the at least three bands encircles the non-orbiting scroll member, and one or more of the intermediate injection chambers encircles the non-orbiting scroll member and has an annular shape.

11. The scroll compressor of claim 1, wherein the compressor housing includes an upper portion and a lower portion, the three or more bands including a first band extending from the non-orbiting scroll member to the upper portion of the compressor housing, and the intermediate injection chambers including a first intermediate injection chamber defined by the first band, the upper portion of the compressor housing, and the non-orbiting scroll member.

12. The scroll compressor of claim 11, wherein the upper portion of the compressor housing is shrink fitted onto the non-orbiting scroll member via the three or more bands.

13. A heating, ventilation, air conditioning, and refrigeration (HVACR) system, comprising: a refrigerant circuit including a condenser, an expander, an evaporator, and a scroll compressor fluidly connected, a working fluid flowing through the refrigerant circuit, wherein the scroll compressor includes: a compressor housing containing a suction chamber, a discharge chamber, and intermediate injection chambers, an orbiting scroll member and a non-orbiting scroll member intermeshed to form compression pockets within the compressor housing, the compression pockets configured to suction from the suction chamber and discharge into the discharge chamber, the non-orbiting scroll member including intermediate injection ports fluidly connecting the intermediate injection chambers to the compression pockets, and at least three bands disposed within the compressor housing, each of the at least three bands extending between the non-orbiting scroll member and the compressor housing, and the intermediate injection chambers being defined by pairs of the three or more bands.

14. The HVACR system of claim 13, wherein the pairs of the three or more bands include: a first pair of the bands, the intermediate injection chambers including a first intermediate injection chamber defined by the first pair of bands, and a second pair of the bands, the intermediate injection chambers including a second intermediate injection chamber defined by the second pair of bands.

15. The HVACR system of claim 13, wherein the intermediate injection chambers include a first intermediate injection chamber and a second intermediate injection chamber, and the intermediate injection ports include: a first intermediate injection port fluidly connecting the first intermediate injection chamber to at least one of the compression pockets, and a second intermediate injection port fluidly connecting the second intermediate injection chamber to at least one of the compression pockets.

16. The HVACR system of claim 13, wherein the suction chamber is configured to receive a suction flow of the working fluid, the discharge chamber is configured to receive a discharge flow of the working fluid from compression pockets, and the intermediate injection chambers including a first intermediate injection chamber configured to receive a first intermediate injection flow of the working fluid and a second intermediate injection chamber configured to receive a second intermediate injection flow of the working fluid.

17. The HVACR system of claim 16, further comprising: a suction inlet in the compression housing configured to direct the suction flow of the working fluid into the suction chamber, the suction chamber fluidly connecting the suction inlet to an inlet of the compression pockets, a discharge outlet in the compression housing configured to direct the discharge flow of the working fluid from the discharge chamber out of the compressor, the discharge chamber fluidly connecting an outlet of the compression pockets to the discharge outlet, a first intermediate injection inlet in the compression housing configured to direct the first intermediate injection flow of the working fluid into the first intermediate injection chamber, the first intermediate injection chamber fluidly connecting the first intermediate injection inlet to the first intermediate injection port in the non-orbiting scroll member, and a second intermediate injection inlet in the compression housing configured to direct the second intermediate injection flow of the working fluid into the second intermediate injection chamber, the second intermediate injection chamber fluidly connecting the second intermediate injection inlet to the second intermediate injection port in the non-orbiting scroll member.

18. The HVACR system of claim 16, wherein the suction chamber is configured to receive a suction flow of the working fluid, the discharge chamber is configured to receive a discharge flow of the working fluid from compression pockets, and the intermediate injection chambers including a first intermediate injection chamber configured to receive a first intermediate injection flow of the working fluid and a second intermediate injection chamber configured to receive a second intermediate injection flow of the working fluid.

19. A method of making a scroll compressor, comprising: placing an upper portion of a compressor housing over a non-orbiting scroll member, the upper portion of the compressor housing surrounding the non-orbiting scroll member, and at least three bands being disposed between the upper portion of the compressor housing and the non-orbiting scroll member; and interference fitting the upper portion of the compressor housing onto the non-orbiting scroll member via the at least three bands, wherein the interference fitting forms intermediate injection chambers defined by pairs of the at least three bands, the upper portion of the compressor housing, and the non-orbiting scroll member, the intermediate injection chambers fluidly connecting intermediate injection inlets in the compressor housing to intermediate injection ports in the non-orbiting scroll member.

20. The method of claim 19, further comprising: heating of the upper portion of the compressor housing, prior to placing the upper portion of the compressor housing onto the non-orbiting scroll member, wherein the interference fitting is a shrinking fitting that includes cooling of the upper portion of the compressor housing, which results in the upper portion of the compressor housing being shrink fit onto the non-orbiting scroll member via the at least three bands, the at least three bands being shrink bands.

Description

DRAWINGS

[0043] FIG. 1A is a schematic diagram of an embodiment of a refrigerant circuit in a heating, ventilation, air conditioning, and refrigeration (HVACR) system.

[0044] FIG. 1B is a schematic diagram of an embodiment of a refrigerant circuit in a HVACR system.

[0045] FIG. 1C is a schematic diagram of an embodiment of a refrigerant circuit in a HVACR system.

[0046] FIG. 1D is a schematic diagram of an embodiment of a refrigerant circuit in a HVACR system.

[0047] FIG. 2 is a front perspective view of an embodiment of a scroll compressor.

[0048] FIG. 3 is a vertical cross-sectional view of the scroll compressor as indicated in FIG. 2, according to an embodiment.

[0049] FIG. 4 is a partial vertical cross-sectional view of the scroll compressor in FIG. 2, according to an embodiment.

[0050] FIG. 5 is a horizontal cross-sectional view of the scroll compressor as indicated in FIG. 3, according to an embodiment.

[0051] FIG. 6 is a partial front perspective view of the scroll compressor in FIG. 2 with a top portion of a compressor housing of the scroll compressor omitted, according to an embodiment.

[0052] FIG. 7 is a vertical cross-sectional view of an embodiment of a scroll compressor.

[0053] FIG. 8 is a partial vertical cross-sectional view of the scroll compressor in FIG. 7, according to an embodiment.

[0054] FIG. 9 is a block flow diagram of an embodiment of making a scroll compressor.

[0055] Like numbers represent like features.

DETAILED DESCRIPTION

[0056] FIG. 1 is a schematic diagram of an embodiment of a refrigerant circuit 5 in a heating, ventilation, air conditioning, and refrigeration (HVACR) system 1. In an embodiment, the HVACR system 1 may be an industrial, commercial, or residential HVACR system 1 configured to condition the inside of a building (e.g., office space, residential house, or the like). In an embodiment, the HVACR system 1 may be a transport HVACR used for cooling the inside of a transport unit (e.g., shipping container, transport/trucking container, reefer, or the like) and/or a passenger vehicle (e.g., a bus, a plane, or the like).

[0057] The refrigerant circuit 5 includes a compressor 10, a condenser 20, a first expansion device 30, a second expansion device 32, and an evaporator 50 that are fluidly connected. In an embodiment, the refrigerant circuit 5 can be modified to include additional components. For example, the refrigerant circuit 5 in an embodiment can include one or more flow control devices, a receiver tank, a dryer, a suction-liquid heat exchanger, or the like. The components of the refrigerant circuit 5 are fluidly connected. Dotted lines and dotted-dashed lines are provided in FIGS. 1A-1C to indicate fluid flows through some components (e.g., compressor 10, condenser 20, evaporator 50) for clarity, and should be understood as not specifying a specific route within each component. Dashed lines are provided in FIGS. 1A-1D to indicate features that may be different in other embodiments. It should be appreciated differences in other embodiments are not limited to those indicated in dashed lines.

[0058] The refrigerant circuit 5 can be configured as a cooling system (e.g., a fluid chiller of an HVACR, an air conditioning system, or the like) that can be operated in a cooling mode, and/or the refrigerant circuit 5 can be configured to operate as a heat pump system that can run in a cooling mode and a heating mode.

[0059] The refrigerant circuit 5 applies known principles of gas compression and heat transfer. The refrigerant circuit 5 can be configured to heat or cool a process fluid (e.g., water, air, chiller fluid, or the like). In an embodiment, the refrigerant circuit 5 may represent a chiller that cools a process fluid such as water or the like. In an embodiment, the refrigerant circuit 5 may represent an air conditioner and/or a heat pump that cools and/or heats a process fluid such as air, water, or the like.

[0060] During the operation of the refrigerant circuit 5, a working fluid (e.g., containing refrigerant, a refrigerant mixture, or the like) flows into the compressor 10 from the evaporator 50 in a gaseous state at a relatively lower pressure. The compressor 10 compresses the gaseous working fluid into a high pressure state, which also heats the gas. The compressor 10 includes a suction inlet 12, a discharge outlet 14, one or more intermediate injection inlets 16A, 16B, and a compression mechanism 18 configured to move within the compressor 10 to compress the gas into the high pressure state. The lower pressure gaseous working fluid flows from the evaporator 50 into the suction inlet 12 of the compressor 10 and is discharged from the discharge outlet 14 of the compressor 10 after being compressed by the compression mechanism 18. The working fluid flows from the suction inlet 12 into the compression mechanism 18 and then from the compression mechanism 18 to and out of the compressor 10 through the discharge outlet 14.

[0061] In an embodiment, the compressor 10 is a type that utilizes injection of intermediate pressure working fluid into the compression mechanism 18 (e.g., economizer injection or the like). In an embodiment, the compressor 10 is a scroll compressor and the compression mechanism 18 is a pair of intermeshed scroll members (e.g., intermediate pressure gaseous working fluid is injected into a formed intermediate compression pocket between the intermeshed scroll members). The intermediate pressure working fluid flows into the intermediate injection inlet(s) 16A, 16B of the compressor 10, and from the intermediate injection inlets 16A, 16B into the compression mechanism 18. The intermediate pressure working fluid mixes with the gaseous working fluid being compressed within the compression mechanism 18 (e.g., mixes with the gaseous working fluid already partially compressed within the compression mechanism 18), is further compressed within the compression mechanism 18, and is then discharged from the compression mechanism 18 to and out of the compressor 10 through the discharge outlet 14. After being compressed, the relatively higher pressure and higher temperature gaseous working fluid flows from the discharge outlet 14 of the compressor 10 to the condenser 20. The working fluid flows through the condenser 20. In addition to the working fluid flowing through the condenser 20, a first process fluid PF.sub.1 (e.g., external air, external water, cooling/heater water, glycol, combinations thereof, or the like) also separately flows through the condenser 20. The first process fluid PF.sub.1 absorbs heat from the working fluid as the first process fluid PF.sub.1 flows through the condenser 20, which cools the working fluid as the working fluid flows through the condenser 20. The working fluid condenses to liquid within the condenser 20. The liquid working fluid then flows from the condenser 20 to the expansion devices 30, 32.

[0062] A first portion of the relatively cooler, relatively higher pressure liquid working fluid discharged from the condenser 20 flows from the condenser 20 into the first expansion device 30. A second portion of the relatively cooler, relatively higher pressure liquid working fluid discharged from the condenser 20 flows into the second expansion device 32. As shown in FIG. 1A, the first expansion device 30 and the second expansion device 32 are disposed in parallel downstream of the condenser 20.

[0063] The first expansion device 30 allows the working fluid to expand, which converts the working fluid to a mixed vapor and liquid state. The expansion also causes further cooling of the working fluid. An expansion device as described herein may also be referred to as an expander. In an embodiment, the expander may be an expansion valve, expansion plate, expansion vessel, orifice, or the like, or other such types of expansion mechanisms. It should be appreciated that the expander may be any type of expansion device used in the field for expanding a working fluid to cause the gaseous working fluid to decrease in pressure and temperature. The first expander 30 and the second expander 32 may be the same type of expansion device or may be different types of expansion devices. In an embodiment, one or both of the expanders 30, 32 are an adjustable type of expansion device. For example, the expanders 30, 32 may each be an expansion valve. For example, one or both of the expanders 30, 32 may be adjusted to control the amount of the working fluid that will flow into the suction inlet 12 and the intermediate injection inlet 16A of the compressor.

[0064] The further relatively lower temperature, vapor/liquid working fluid then flows from the second expander 32 into the evaporator 50. A second process fluid PF.sub.2 (e.g., air, chiller liquid, water, glycol, combinations thereof, or the like) also flows through the evaporator 50. The working fluid absorbs heat from the second process fluid PF.sub.2 as it flows through the evaporator 50, which cools the second process fluid PF.sub.2 as it flows through the evaporator 50. As the working fluid absorbs heat, the working fluid evaporates to vapor. The gaseous/mostly gaseous working fluid then returns to the compressor 10 from the evaporator 50.

[0065] The second portion of the relatively cooler, relatively higher pressure liquid working fluid discharged from the condenser 20 flows to the second expander 32. The second expander 32 allows the working fluid to expand, which converts the working fluid to a vapor state. The expansion also causes further cooling of the working fluid. The relatively lower temperature, intermediate pressure gaseous working fluid then flows from the second expander 32 to the intermediate injection inlet 16A of the compressor 10.

[0066] In an embodiment, the compressor 10 may include multiple intermediate injection inlets 16A, 16B. As shown in FIG. 1A, the compressor 10 can include a first intermediate injection inlet 16A and a second intermediate injection inlet 16B. Respective flows of the working fluid are injected through the intermediate injection inlets 16A, 16B. In the illustrated embodiment, the intermediate pressure working fluid is injected through the intermediate injection inlets 16A, 16B at different pressures (e.g., at different intermediate pressures, a first flow of working fluid at a first intermediate pressure injected through the first intermediate inlet 16A, a second flow of working fluid at a second intermediate pressure injected through the first intermediate inlet 16B, or the like). In another embodiment, the intermediate working fluid injected through the intermediate injection inlets 16A, 16B may be at the same pressure. For example, the streams of intermediate working fluid injected through the intermediate injection inlets 16A, 16B may be at the same pressure while differing in another property (e.g., being different phases, being at different temperatures, having different compositions, or the like). For example, in an embodiment, the refrigerant circuit 5 may include a flash tank (not shown), and a liquid stream of intermediate working fluid and a gaseous stream of intermediate working fluid may be respectively supplied from the flash tank to the intermediate injection inlets 16A, 16B of the compressor 10.

[0067] In an embodiment, the first intermediate injection inlet 16A can be a gaseous intermediate inlet configured to receive/inject the gaseous intermediate pressure working fluid, and the second intermediate injection inlet 16B can be liquid intermediate inlet configured to receive/inject liquid working fluid (e.g., at least partially liquid, mixed phase, at or about fully liquid, or the like). For example, as shown in FIG. 1A, a (third) portion of the (relatively lower temperature) liquid working fluid discharged from the condenser 20 may flow from the condenser 20 to the second intermediate injection inlet 16B of the compressor 10. The liquid working fluid can evaporate as its injected into the compression mechanism 18 into a gaseous state (e.g., evaporates and mixes with the gaseous working fluid within the compression mechanism 18), is further compressed within the compression mechanism 18, and is then discharged from the compression mechanism 18 out of the compressor 10 through the discharge outlet 14. The evaporation of the injected liquid working fluid can provide cooling (e.g., cooling of the working fluid, cooling of the compression mechanism 18, and the like).

[0068] The above-described process continues while the refrigerant circuit 5 is operated, for example, in a cooling mode. In an embodiment, the HVACR system 1 may include a controller (not shown) that controls operation of the expanders 30, 32. The controller may control the expanders 30, 32 (e.g., the degree each expansion valve is open) so that the desired amount (e.g., percentage, or the like) of the working fluid discharged from the condenser flows through the first expander 30 and the second expander 32.

[0069] FIG. 1B is a schematic diagram of another embodiment of a refrigerant circuit 5 in a HVACR system 1. The refrigerant circuit 5 includes similar components to the refrigerant circuit 5 in FIG. 1A, except for the position and configuration of the expanders 30, 32. For example, the refrigerant circuit 5 includes a compressor 10, a condenser 20, a first expander 30, a second expander 32, and an evaporator 50 that are fluidly connected. Unless described otherwise, the refrigerant circuit 5 and its individual components operate in a similar manner to the refrigerant circuit 5 in FIG. 1A as described above. The refrigerant circuit 5 may be modified as similarly discussed above with respect to the refrigerant circuit 5 in FIG. 1 (e.g., to include additional components, or the like).

[0070] During the operation of the refrigerant circuit 5, the working fluid flows from the evaporator 50 into the suction inlet 12 of the compressor 10, is compressed and mixes with intermediate pressure working fluid within the compression mechanism 18, is discharged from the discharge outlet 14 of the compressor 10, and is then cooled/condensed within the condenser 20, as similarly discussed for the refrigerant circuit 5 in FIG. 1A.

[0071] The cooler, relatively higher pressure liquid working fluid discharged from the condenser 20 flows into the first expander 30. The first expansion device 30 causes/allows the working fluid to partially expand, which converts the working fluid to a mixed vapor and liquid state. The working fluid also cools as it expands. A first portion of the relatively lower temperature, intermediate pressure working fluid (e.g., a liquid portion or a mixed vapor and liquid portion of the relatively lower temperature intermediate pressure working fluid) flows form the first expander 30 to the second expander 32. A second portion of the relatively lower temperature, intermediate pressure working fluid (e.g., a gaseous portion of the relatively lower temperature intermediate pressure working fluid) flows from the first expander 30 to the intermediate injection inlet 16A of the compressor 10.

[0072] As shown in FIG. 1B, the first expander 30 and the second expander 32 are disposed in series downstream of the condenser 20. In an embodiment, the refrigerant circuit 5 may include an economizer 40 disposed between the first expander 30 and the second expander 32 (e.g., the first expander 32, the economizer 40, and the second expander 32 disposed in series downstream of the condenser 20). In the illustrated embodiment, the economizer 40 is a liquid/gas separator. The first portion of the relatively lower temperature, intermediate pressure working fluid flows from the economizer 40 to the second expander 32, and the second portion of the relatively lower temperature, intermediate pressure working fluid flows from the economizer to the intermediate injection inlet 16A of the compressor 10. The economizer 40 can be configured to ensure that the second portion of intermediate pressure working fluid flowing to intermediate injection inlet 16A of the compressor 10 is in a gaseous state.

[0073] The first portion of intermediate pressure working fluid is further expanded by the expander 32, which causes liquid in the first portion to become gaseous. This also causes further cooling of the working fluid. The further relatively lower temperature, vapor/liquid working fluid then flows from the second expander 32 into the evaporator 50. As similarly discussed above for the refrigerant circuit 5 in FIG. 1A, the working fluid then cools a process fluid PF.sub.2 within the evaporator 50, and then flows from the evaporator 50 back to the compressor 10.

[0074] In an embodiment, the compressor 10 may include the multiple intermediate injection inlets 16A, 16B, as similarly discussed above. For example, as shown in FIG. 1B, a (third) portion of the (relatively lower temperature) liquid working fluid discharged from the condenser 20 may flow from the condenser 20 to the second intermediate injection inlet 16B of the compressor 10. In another embodiment, the liquid working fluid may be a portion of the working fluid discharged from the economizer 40 (e.g., a first portion of the cooled liquid working fluid discharged from the economizer 40 flows to the first expander 30 and a second portion of the cooled liquid working fluid discharged from economizer 40 flows to the second intermediate injection inlet 16B of the compressor 10).

[0075] FIG. 1C is a schematic diagram of another embodiment of a refrigerant circuit 5 in a HVACR system 1. The refrigerant circuit 5 includes similar components to the refrigerant circuit 5 in FIG. 1A, except for the inclusion of an economizer 40. For example, the refrigerant circuit 5 includes a compressor 10, a condenser 20, a first expander 30, a second expander 32, an economizer 40, and an evaporator 50 that are fluidly connected. Unless described otherwise, the refrigerant circuit 5 operates in a similar manner to the refrigerant circuit 5 in FIG. 1A as described above. The refrigerant circuit 5 may be modified as similarly discussed above with respect to the refrigerant circuit 5 in FIG. 1 (e.g., to include additional components, or the like).

[0076] During the operation of the refrigerant circuit 5, the working fluid flows from the evaporator 50 into the suction inlet 12 of the compressor 10, is compressed and mixes with intermediate pressure working fluid within the compression mechanism 18, is discharged from the discharge outlet 14 of the compressor 10, and is then cooled/condensed within the condenser 20, as similarly discussed for the refrigerant circuit 5 in FIG. 1A. As shown in FIG. 1C, the expanders 30, 32 are disposed in parallel downstream of the condenser 20.

[0077] A first portion of the liquid working fluid discharged from the condenser 20 flows through the economizer 40 to a first expander 30. A second portion of the liquid working fluid discharged from the condenser 20 flows through a second expander 32 and the economizer 40 to the intermediate injection inlet 16A of the compressor 10. The first expansion device 30 causes/allows the working fluid to partially expand, which converts the working fluid to a gas state or to a vapor and liquid mixed state. The relatively cooler, intermediate pressure working fluid then flows from the second expander 32 to the economizer 40.

[0078] In the illustrated embodiment, the economizer 40 is a heat exchanger that allows the first portion of working fluid and the second portion of working fluid to exchange heat without physically mixing. As both portions of the working fluid flow through the economizer 40, the relatively cooler, intermediate pressure working fluid (i.e., the second portion of the working fluid) absorbs heat from the first portion of the working fluid. In an embodiment, this may also convert liquid in the second portion into gaseous working fluid. The gaseous intermediate pressure working fluid (i.e., the second portion of the working fluid) then flows from the economizer 40 to the intermediate injection inlet 16A of the compressor 10.

[0079] The first portion of working fluid is cooled within the economizer 40 and then flows from the economizer 40 to the first expander 30. The cooled first portion of working fluid is then expanded by the expander 32, which causes liquid in the first portion to become gaseous. This also causes further cooling of the working fluid. The further relatively lower temperature, vapor/liquid working fluid then flows from the first expander 30 into the evaporator 50. As similarly discussed above for the refrigerant circuit 5 in FIG. 1A, the working fluid then cools a process fluid PF.sub.2 within the evaporator 50, and then flows from the evaporator 50 back to the compressor 10.

[0080] In an embodiment, the compressor 10 may include the multiple intermediate injection inlets 16A, 16B, as similarly discussed above. For example, as shown in FIG. 1C, a (third) portion of the (relatively lower temperature) liquid working fluid discharged from the condenser 20 may flow from the condenser 20 to the second intermediate injection inlet 16B of the compressor 10. In another embodiment, the liquid working fluid may be a portion of the working fluid discharged from the economizer 40 (e.g., a first part of the first portion of the cooled liquid working fluid after flowing through the economizer 40 flows to the first expander 30 and a second part of the first portion of the cooled liquid working fluid after passing through the economizer 40 flows to the second intermediate injection inlet 16B of the compressor 10).

[0081] FIG. 1D is a schematic diagram of another embodiment of a refrigerant circuit 5 in a HVACR system 1. The refrigerant circuit 5 includes similar components to the refrigerant circuit 5 in FIG. 1A, except for not including the second expander 32. For example, the refrigerant circuit 5 includes a compressor 10, a condenser 20, a first expander 30, and an evaporator 50 that are fluidly connected. Unless described otherwise, the refrigerant circuit 5 operates in a similar manner to the refrigerant circuit 5 in FIG. 1A as described above. The refrigerant circuit 5 may be modified as similarly discussed above with respect to the refrigerant circuit 5 in FIG. 1 (e.g., to include additional components, or the like).

[0082] During the operation of the refrigerant circuit 5, the working fluid flows from the evaporator 50 into the suction inlet 12 of the compressor 10, is compressed and mixes with injected working fluid from the intermediate inlet 16A within the compression mechanism 18, is discharged from the discharge outlet 14 of the compressor 10, and is then cooled/condensed within the condenser 20, as similarly discussed for the refrigerant circuit 5 in FIG. 1A. As discussed below, the working fluid flowing into the compressor 10 through the intermediate inlet 16A and injected into the compression mechanism 18 contains liquid working fluid (e.g., is liquid working fluid, is a mixed phase liquid and vapor liquid working fluid).

[0083] A first portion of the liquid working fluid condensed in the condenser 20 flows to the expander 30. The expander 30 causes/allows the working fluid to partially expand, which converts the working fluid to a gas state or to a vapor and liquid mixed state. The relatively lower temperature, vapor/liquid working fluid then flows from the expander 30 into the evaporator 50. As similarly discussed above for the refrigerant circuit 5 in FIG. 1A, the working fluid then cools a process fluid PF.sub.2 within the evaporator 50, and then flows from the evaporator 50 back to the compressor 10.

[0084] A second portion of the liquid working fluid flows from the condenser 20 to the intermediate injection inlet 16A of the compressor 10. As shown in FIG. 1D, the second portion of liquid working fluid may be provided separately from the condenser 20 or may be provided from liquid working fluid discharged of the condenser 20 (e.g., from the working fluid as it flows from the condenser 20 to the expander 30).

[0085] In FIG. 1D, the liquid working fluid is at the discharge pressure of the compressor. In an embodiment, the liquid working fluid may be an intermediate pressure liquid portion of the working fluid (e.g., refrigerant circuit 5 in FIG. 1A in which the second expander 32 discharges a mixed liquid and vapor intermediate pressure working fluid, refrigerant circuit 5 in FIG. 1B in which intermediate liquid working fluid or a mixed liquid and vapor intermediate pressure working fluid is supplied to the intermediate injection inlet 16A of the compressor 10, or the like). The injection of liquid working fluid can provide cooling to the compressor 10. In one example, the liquid working fluid evaporates within the compressor 10 (e.g., within the compression mechanism 18) which provides cooling to the compressor 10.

[0086] In an embodiment, the compressor 10 may include the multiple intermediate injection inlets 16A, 16B, as similarly discussed above. For example, as shown in FIG. 1D, after pass through the expander 30 and being expanded therein, a first part of the first portion of the working fluid flows from the expander 30 to the evaporator 50 and a second part of the first portion of the working fluid flows from the expander 30 to the second intermediate injection inlet 16B of the compressor 10.

[0087] In some embodiments, the working fluid may include refrigerant and lubricant (e.g., oil or the like). In such embodiments, the intermediate liquid working fluid supplied to an intermediate injection inlet 16A, 16B can be liquid lubricant (e.g., includes liquid lubricant, a flow of working fluid that is a majority lubricant, or the like). For example, intermediate liquid lubricant may be supplied/injected through the first intermediate injection inlet 16A and intermediate refrigerant (e.g., gaseous refrigerant, liquid refrigerant, or mixed phase refrigerant; a flow of working fluid that is a majority refrigerant, or the like) may be supplied through the second intermediate injection inlet 16B. In an embodiment, the supplied intermediate lubricant may be at discharge pressure or at an intermediate pressure. For example, said intermediate lubricant may be supplied from a lubricant separator (not shown) in the refrigerant circuit 5 (e.g., lubricant separator disposed between the discharge outlet 14 of the compressor 14 and the condenser 20, or the like), from the evaporator 50 (e.g., from a bottom of the evaporator 50, or the like), or the like. For example, when supplied from the evaporator 50, a pump (not shown) may be used to supply the intermediate lubricant to the first intermediate injection inlet 16B (e.g., at an intermediate or higher pressure).

[0088] FIG. 2 is a front perspective view of a scroll compressor 100, according to an embodiment. In an embodiment, the scroll compressor may be the compressor 10 in the refrigerant circuit 5 in FIG. 1A, in the refrigerant circuit 5 in FIG. 1B, in the refrigerant circuit 5 in FIG. 1C, or in the refrigerant circuit 5 in FIG. 1D. The compressor 100 includes a compressor housing 102 that contains components of the compressor 100. As shown in FIG. 2, the compressor housing 102 is the outer housing of the compressor 100.

[0089] The compressor 100 includes a plurality of fluid ports that extend through the housing 102 for supplying working fluid into and discharging working fluid from the compressor 100. The working fluid enters and exits the compressor 100 by flowing through the fluid ports in the housing 102. The fluid ports include a suction inlet 104A, a discharge outlet 104B, and an intermediate injection inlet 104C. A suction flow f.sub.S of the working fluid to be compressed flows into the compressor 100 though the suction inlet 104A in the housing 102 at a relatively lower pressure (e.g., at a first pressure P.sub.1). A discharge flow f.sub.D of the compressed working fluid is discharged from the discharge outlet 104B of the compressor 100 at a relatively higher pressure (e.g., at a second pressure P.sub.2 greater than the first pressure P.sub.1). An intermediate flow f.sub.i of the working fluid flows into the compressor 100 through the intermediate injection inlet 104C in the housing 102. This flow f.sub.i can also be referred to as economizer injection, intermediate injection flow, or economizer injection flow. The intermediate injection working fluid in the flow f.sub.i may be a liquid working fluid at the relatively higher pressure or a working fluid at an intermediate pressure (e.g., at a third pressure P.sub.3 greater than the first pressure P.sub.1 and less than the second pressure P.sub.2). For example, the working fluid at the intermediate pressure can be a gaseous working fluid at the intermediate pressure or a mixed phase liquid and vapor working fluid at the intermediate pressure.

[0090] In one example, the intermediate injection working fluid is at the intermediate pressure. In an embodiment, the intermediate pressure working fluid is a gaseous working fluid. In an embodiment, the intermediate pressure working fluid may be a liquid working fluid or a mixed phase liquid and vapor working fluid. For example, the intermediate injection working fluid is an intermediate pressure working fluid supplied from an expander in the refrigerant circuit of the compressor 100 (e.g., from the second expander 32 in FIG. 1A, from the first expander 30 in FIG. 1B, from the second expander 32 in FIG. 1C) to the intermediate injection inlet 106C of the compressor 100. For example, the intermediate injection working fluid in the flow f.sub.i is a portion of the compressed working fluid in the discharge flow f.sub.D after being cooled in a condenser in the refrigerant circuit of the compressor 100 (e.g., condenser 20 in each of FIGS. 1A-1C) and then expanded by the expander in the refrigerant circuit of the compressor 100. For example, the relatively lower pressure working fluid in the suction flow f.sub.S is a different portion of the working fluid in the discharge flow that is supplied to the suction inlet 104A after being cooled in the condenser, further expanded by a different expander in the refrigerant circuit (e.g., by the first expander 30 in FIG. 1A, by the second expander 32 in FIG. 1B, by the first expander 30 in FIG. 1C), and then heated in an evaporator in the refrigerant circuit of the compressor 100 (e.g., evaporator 50 in FIGS. 1A-1C).

[0091] In one example, the intermediate injection working fluid can be a liquid working fluid at the relatively higher pressure. For example, the liquid intermediate injection working fluid is a portion of the liquid working fluid provided from a condenser (e.g., directly from the condenser or as the liquid working fluid flows from the condenser to an expander) of the refrigerant circuit of the compressor 100 (e.g., from the condenser 20 in FIG. 1D). For example, the intermediate injection working fluid in the flow f.sub.i is a portion of the compressed working fluid in the discharge flow f.sub.D after being cooled in a condenser in the refrigerant circuit of the compressor 100 (e.g., condenser 20 in FIG. 1D) and prior to being expanded by the expander (e.g., expander 30 in FIG. 1D) in the refrigerant circuit of the compressor 100. For example, the relatively lower pressure working fluid in the suction flow f.sub.S is a different portion of the working fluid in the discharge flow that is supplied to the suction inlet 104A after being cooled in the condenser, expanded by the expander in the refrigerant circuit, and then heated in an evaporator in the refrigerant circuit of the compressor 100 (e.g., evaporator 50 in FIG. 1D).

[0092] FIG. 3 is a cross-sectional view of the scroll compressor 100 in FIG. 2, according to an embodiment. The view in FIG. 3 is a vertical cross-sectional view of the scroll compressor 100, as indicated in FIG. 2. Dashed arrows are provided in FIG. 3 to indicate the flow of working fluid within the scroll compressor 100. As described above, the lower pressure fluid working fluid in the suction flow f.sub.S (i.e., the working fluid to be compressed) flows into the scroll compressor 100 through the suction inlet 104A, the higher pressure (compressed) working fluid in discharge flow f.sub.D is discharged from the compressor 100 through the discharge outlet 104B, and the intermediate/higher pressure working fluid in the injection flow f.sub.i flows into the compressor 100 through the intermediate injection inlet port 104C.

[0093] The illustrated compressor 100 is a single-stage scroll compressor. More specifically, the illustrated compressor 100 is a single-stage vertical scroll compressor. It is to be appreciated that the principles described herein are not limited to single-stage scroll compressors and can be applied to multi-stage scroll compressors having two or more compression stages. The embodiments are described herein for a compressor with a vertical or a near vertical crankshaft (e.g., as shown in FIG. 3). In other embodiments, the concepts described herein for the compressor 100 may be applied and/or adapted to a compressor with a non-vertical or a horizontal crankshaft. In such embodiments, it should be appreciated that relative spatial terms used herein, such as but not limited to upper, lower, vertical, horizontal, would be interpreted with the compressor being positioned with its crankshaft in a vertical position.

[0094] The scroll compressor 100 includes a non-orbiting scroll member 112 and an orbiting scroll member 114. Applying known aspects of scroll compressor compression, the scroll compressor 100 utilizes the intermeshing of the two scroll members 112, 114 to form a plurality of compression pockets 116 in which gas is trapped and then compressed. The non-orbiting scroll 112 has a baseplate 113 and a spiral wrap 118 that projects from the baseplate 113 in a direction towards the orbiting scroll member 114. The orbiting scroll member 114 has a baseplate 115 and a spiral wrap 120 that projects from the baseplate 115 in a direction towards the non-orbiting scroll member 112. The spiral wrap 118 of the non-orbiting scroll 112 is intermeshed with the spiral wrap 120 of the orbiting scroll member 114 forming the compression pockets 116 there between. In an embodiment, the axial end of one or both of the spiral wraps 118, 120 may include a tip seal (not shown) to help encourage sealing between each spiral wraps 118, 120 and the opposing baseplate 113, 115.

[0095] The non-orbiting scroll member 112 is a scroll member that is in a fixed position within the compressor housing 102 and is not configured to be moved (e.g., orbited, rotated) relative to the compressor housing 102 during the operation of the scroll compressor 100. The non-orbiting scroll member 112 may be referred to as a non-orbiting scroll, a fixed scroll, a stationary scroll, a first scroll member, or the like. In an embodiment, the non-orbiting scroll 112 can be directly attached to the compressor housing 102 of the scroll compressor 100. For example, in the illustrated embodiment, the non-orbiting scroll 112 is interference fit into the compressor housing 102. This fit between the non-orbiting scroll 112 and the housing 102 is discussed in more detail below.

[0096] The orbiting scroll member 114 is a scroll member engaged with an end of a crankshaft 160. During operation of the scroll compressor 100, the orbiting scroll member 114 is moved (e.g., orbited, rotated) relative to the non-orbiting scroll member 112. The orbiting scroll member 114 is configured to be moved relative to the compressor housing 102 during operation of the compressor 100. The orbiting scroll member 114 may also be referred to as an orbiting scroll, a moving scroll, a second scroll member, or the like.

[0097] The orbiting scroll 114 is moved (e.g., orbited, rotated) by the crankshaft 160. As the orbiting scroll member 114 is engaged with the end of the crankshaft 160, rotation of the crankshaft 160 causes the moving of the orbiting scroll 114. The crankshaft 160 can be rotated by, for example, an electric motor 162. The electric motor 162 includes a rotor and a stator. The rotor and the crankshaft 160 are affixed together such that they rotate together (e.g., the rotor and the crankshaft 160 can be affixed together using an interference fit or other type of fit). The electric motor 162 may operate using known principles to rotate the crankshaft 160. In an embodiment, the crankshaft 160 may be rotated by other mechanisms other than the electric motor 162, such as, for example, an external electric motor, an external combustion engine, or other such mechanisms. Accordingly, such embodiments may not include the electric motor 162 as shown in FIG. 3. The scroll compressor 100 may include an alignment coupler for maintaining alignment of the intermeshed scrolls 112, 114, such as an Oldham coupling 164.

[0098] The compressor 100 includes a bearing support 134. The bearing support 134 can be affixed to the housing 102 and/or the non-orbiting scroll 112. The orbiting scroll 114 is disposed between the non-orbiting scroll 112 and the bearing support 134. The bearing support 134 can provide bearing(s)/bearing surface(s) for supporting the orbiting scroll 114 (e.g., a thrust bearing for axially supporting the orbiting scroll 114, or the like) and/or for supporting the crankshaft 160 (e.g., radial bearings for radially supporting the crankshaft 160, or the like).

[0099] The compressor housing 102 of the scroll compressor 100 includes an upper portion 108A and a lower portion 108B. As shown in FIG. 3, the suction inlet 104A extends through the lower portion 108B of the compressor housing 102. The intermediate injection inlet 104C extends through the upper portion 108B of the compressor housing 102. The discharge outlet 104B also extends through the upper portion 108B of the compressor housing 102. In the illustrated embodiment, the upper portion 108A is the uppermost portion of the compressor housing 102 and the lower portion 108B is the lowermost portion of the compressor housing 102. In other embodiments, the upper portion 108A may not be the uppermost portion of the housing 102 and/or the lower portion 108B may not be the lowermost portion of the compressor housing 102. In such embodiments, the intermediate injection inlet 104B and the discharge outlet 104C may extend through different portions of the compressor housing 102. As shown in FIG. 3, the upper portion 108A can be a cap of the scroll compressor housing 102.

[0100] The compressor housing 102 contains an internal volume that includes a suction chamber 140, a discharge chamber 142, and an intermediate injection chamber 144 of the compressor 100. The discharge chamber 142, the suction chamber 140, and the intermediate injection chamber 144 are at different pressures. For example, the suction chamber 140 is at the suction pressure (e.g., the first pressure P.sub.1), the discharge chamber 142 is at the discharge pressure (e.g., the second pressure P.sub.2), and the intermediate injection chamber 144 is at the discharge pressure or the intermediate pressure (e.g., the third pressure P.sub.3). In an embodiment, the intermediate injection chamber 144 is at the intermediate pressure. The intermediate injection chamber 144 is discussed in more detail below with respect to FIG. 4.

[0101] The discharge chamber 142 is disposed between the compressor housing 102 and the non-orbiting scroll member 112 (e.g., between the upper portion 108A of the compressor housing 102 and the non-orbiting scroll member 112). As shown in FIG. 3, the discharge chamber 142 is a volume defined by the compressor housing 102 and the non-orbiting scroll member 112 (e.g., defined by the upper portion 108A of the compressor housing 102 and the non-orbiting scroll member 112). The discharge chamber 142 may also be referred to as an upper volume of the compressor 100.

[0102] The suction chamber 140 is disposed between the compressor housing 102 and the non-orbiting scroll member 112 (e.g., between the lower portion 108B of the compressor housing 102 and the non-orbiting scroll member 112). The suction chamber 140 is disposed opposite to the discharge chamber 142 with respect to the non-orbiting scroll 112. For example, the suction chamber 140 and the discharge chamber 142 are disposed on opposite sides of the non-orbiting scroll 112. As shown in the illustrated embodiment, the discharge chamber 142 and the suction chamber 140 are fluidly separated by the non-orbiting scroll 112. As shown in FIG. 3, the suction chamber 140 is a volume defined by the compressor housing 102 and the non-orbiting scroll member 112 (e.g., defined by the lower portion 108A of the compressor housing 102 and the non-orbiting scroll member 112). The suction chamber 140 may also be referred to as a lower volume of the compressor 100.

[0103] As shown in FIG. 3, the intermeshed scrolls 112, 114 have an inlet 124 through which gas flows into the intermeshed scrolls 112, 114. The inlet 124 is formed by/at an outer radius of the spiral wraps 118, 120 (e.g., at the outermost spiral of each spiral wrap 118, 120, at the start of the compression process, not at an intermediate location/compression pocket, or the like). For example, the inlet 124 is at a location at which the compression pockets 116 are initially being formed.

[0104] The intermeshed spiral wraps 118, 120 also have outlet 122. The outlet 122 is a port that allows the compressed gas to flow out from between the intermeshed spiral wraps 118, 120. As shown in the illustrated embodiment, the outlet 122 is formed in the baseplate 113 of the non-orbiting scroll. For example, the outlet 122 is located at or near the axial center of the intermeshed spiral wraps 118, 120 (e.g., at or near where the intermeshed spiral wraps 118, 120 end). The outlet 122 is fluidly connected to the discharge chamber 142 of the scroll compressor 100. The compressor 100 may include a valve (e.g., a check valve, a valve plate, or the like) (not shown) to regulate the flow of pressurized gas through the outlet 122.

[0105] The compressor 100 includes one or more intermediate injection ports 150 formed in the non-orbiting scroll 112 for injecting intermediate working fluid into the intermeshed scrolls 112, 114. The intermediate injection port(s) 150 fluidly connects the intermediate injection chamber 144 to one or more of the intermediate compression pockets 117 of the intermeshed scrolls 112, 114. The intermediate injection port(s) 150 are configured to inject/direct the intermediate working fluid (i.e., in flow f.sub.i) into the intermeshed scrolls 112, 114. An intermediate compression pocket 117 is one of the compression pockets 116 that is partially through the compression process (e.g., at a pressure between the inlet pressure P.sub.1 and the discharge pressure P.sub.2, has travelled part way and is disposed at an intermediate position between the inlet 124 and the outlet 122). The gaseous and/or liquid intermediate injection working fluid is added to the working fluid already within the intermediate compression pocket 117, which is then further compressed (e.g., to the discharge pressure P.sub.2). When the injection working fluid contains liquid working fluid, the liquid working can undergo a pressure drop as its injected into the intermediate compression pocket 117 (e.g., as it flows to the intermediate compression pocket 117, within the intermediate compression pocket 117 that is at relatively lower pressure). The pressure drop can cause evaporation of the working fluid, which provides cooling.

[0106] The specific location(s) of the intermediate inlet port(s) 150 with respect to the compression process can be varied. In an embodiment, a location of an intermediate injection port 150 can be located so that the pressure of the intermediate compression pocket 117 is relatively near the suction pressure (e.g., at a location in which compression is just beginning). In the illustrated embodiment, this is a location at a relatively outer extent of the intermeshed scrolls 112, 114 (e.g., relatively closer to the inlet 124, closer to the inlet 124 than the outlet 122). In an embodiment, a location of the intermediate injection port 150 can be selected so that the pressure in the intermediate compression pocket 117 is relatively near the discharge pressure (e.g., at a location near the discharge). In the illustrated embodiment, this is a location at a relatively inner extent of the intermeshed scrolls 112, 114 (e.g., relatively closer to the outlet 122, closer to the outlet 122 than the inlet 124).

[0107] For example, the selection of the location(s) of the intermediate inlet port(s) 150 may be selected based on balanced between providing cooling to the compressor 100, increasing capacity of the HVACR system of the compressor 100, and/or maintaining efficiency of the HVACR system of the compressor 100. Such location(s) may be selected based on, for example, modeling the anticipated efficiency and capacity changes, testing to determine the optimal location, or combinations thereof.

[0108] The working fluid is compressed by the intermeshed scrolls 112, 114 as the working fluid travels between the intermeshed scrolls 112, 114. The compressed working fluid flows out of the scroll compressor 100 by flowing from the outlet 122 of the intermeshed scrolls 112, 114 to and through the discharge outlet 104B. The working fluid enters the intermeshed scrolls 112, 114 at the relatively lower pressure (e.g., at suction pressure, at the first pressure P.sub.1), and is discharged from intermeshed scrolls 112, 114 at a relative higher pressure (e.g., at discharge pressure, at the second pressure P.sub.2). The intermediate working fluid at the relatively higher pressure or at the intermediate pressure (e.g., at a pressure between the suction pressure and the discharge pressure, at the third pressure P.sub.3) also flows into the intermeshed scrolls 112, 114.

[0109] The suction inlet 104A is fluidly connected to the inlet 124 of the intermeshed scrolls 112, 114. The suction flow f.sub.S of the working fluid flows from the suction inlet 104A into the inlet 124 of the intermeshed scrolls 112, 114. As shown in FIG. 3, the suction chamber 140 fluidly connects the suction inlet 104A to the inlet 124 of the intermeshed scrolls 112, 114. For example, the suction inlet 104A fluidly connects to the suction chamber 140, and the suction chamber 140 fluidly connects to the inlet 124 of the intermeshed scrolls 112, 114. The suction chamber 140 is at the suction/inlet pressure of the suction flow f.sub.S (e.g., the working fluid within the suction chamber 140 is at the suction/inlet pressure of the suction flow f.sub.S. The intermeshed scrolls 112, 114 configured to suction the working fluid from the suction chamber 140.

[0110] The discharge outlet 104B is fluidly connected to the outlet 122 of the intermeshed scrolls 112, 114. The discharge flow f.sub.D of the compressed working fluid flows from outlet 122 of the intermeshed scrolls 112, 114 to and through the discharge outlet 104B of the compressor 100. As shown in FIG. 3, the discharge chamber 142 fluidly connects the outlet 122 of the intermeshed scrolls 112, 114 to the discharge outlet 104B of the compressor 100. For example, the outlet 122 of the intermeshed scrolls 112, 114 fluidly connects to the discharge chamber 142, and the discharge chamber 142 fluidly connects to the discharge outlet 104B of the compressor 100. The compressed working fluid flows from the intermeshed scrolls 112, 114 through the discharge chamber 142 to the discharge outlet 104B of the compressor 100. The discharge chamber 142 is at the discharge pressure (e.g., the working fluid within the discharge chamber 142 is at the discharge pressure of the discharge flow f.sub.D).

[0111] FIG. 4 is a partial cross-sectional view of the compressor 100 in FIG. 2, according to an embodiment. For example, FIG. 4 is an enlarged portion of the view in FIG. 3. Dashed lines indicate a cutoff of the compressor 100 in the view of FIG. 4. The intermediate injection inlet 104C fluidly connects to the intermediate injection chamber 144. The economizer injection flow f.sub.i (of the intermediate injection working fluid) is directed from the intermediate injection inlet 104C to and through the intermediate injection port 150 into the intermediate compression pocket 117.

[0112] As shown in FIG. 4, the intermediate injection chamber 144 fluidly connects the intermediate injection inlet 104C of the compressor 100 to the intermediate injection port 150 in the non-orbiting scroll 112. For example, the intermediate injection inlet 104C fluidly connects to the intermediate injection chamber 144, and the intermediate injection chamber 144 fluidly connects to the intermediate injection port 150 in the non-orbiting scroll 112. The intermediate injection chamber 144 directs the intermediate injection working fluid from the intermediate injection inlet 104C into the intermediate injection port(s) 150 in the non-orbiting scroll 112. The intermediate injection chamber 144 is at the intermediate injection (e.g., the working fluid within the intermediate injection chamber 144 is at the intermediate injection pressure of the economizer injection flow f.sub.i).

[0113] As shown in FIG. 4, the compressor 100 includes a pair of bands 180, 182 disposed within the housing 102 of the compressor 100. The bands 180, 182 include a first band 180 and a second band 182. The first band 180 may also be referred to as an upper band, and the second band 182 may also be referred to as a lower band. The bands 180, 182 each extend between the non-orbiting scroll 112 and the compressor housing 102. For example, each band 180, 182 extends from the compressor housing 108 to the non-orbiting scroll 112. For example, each band 180, 182 extends from the non-orbiting scroll 112 to the compressor housing 102. In the illustrated embodiment, each band 180, 182 extends between/to the upper portion 108A of the compressor housing 102. Each band 180, 182 forms a respective seal between the upper portion 108A of the compressor housing 102 and the non-orbiting scroll 112.

[0114] Each of the bands 180, 182 extends around a circumference of the non-orbiting scroll 112 (e.g., as shown in FIG. 6). The bands 180, 182 are spaced apart from each other in the axial direction (e.g., in axial direction D.sub.1, vertically spaced apart). The intermediate injection chamber 144 is formed by the gap between the bands 180, 182. Said gap is also between the compressor housing 102 and the non-orbiting scroll 112 (e.g., the intermediate injection chamber 114 is formed between the bands 180, 182 and between the compressor housing 102 and the non-orbiting scroll 112).

[0115] The intermediate injection chamber 144 is disposed between the compressor housing 102 and the non-orbiting scroll member 112 (e.g., between the upper portion 108A of the compressor housing 102 and the non-orbiting scroll member 112). The intermediate injection chamber 144 is also disposed between the bands 180, 182. The intermediate injection chamber 144 is a volume defined by the compressor housing 102, the non-orbiting scroll member 112, the first band 180 and the second band 182 (e.g., defined by the upper portion 108A of the compressor housing 102, the non-orbiting scroll member 112, the first band 180, and the second band 182). The intermediate injection chamber 144 connects to the intermediate injection port 150 that extends through the non-orbiting scroll member 122 (e.g., intermediate injection port 150 being a passageway/port that extends all the way through the non-orbiting scroll).

[0116] The first band 180 forms a seal between the intermediate injection chamber 144 and the suction chamber 140. For example, the first band 180 prevents the working fluid from flowing between the intermediate injection chamber 144 and the suction chamber 140 (e.g., prevents working fluid from flowing directly between the intermediate injection chamber 144 and the suction, prevents the working fluid from flowing directly from the suction chamber 140 into the intermediate injection chamber 140). The first band 180 defines the suction chamber 140.

[0117] The second band 182 forms a seal between the intermediate injection chamber 144 and the discharge chamber 142. For example, the second band 182 prevents the working fluid from flowing between the intermediate injection chamber 144 and the discharge chamber 142 (e.g., prevents working fluid from flowing directly between the intermediate injection chamber 144 and discharge chamber 142, prevents the working fluid from flowing directly from the discharge chamber 142 into the intermediate injection chamber 144). The second band 182 defines the discharge chamber 142.

[0118] The upper portion 108A of the compressor housing 102 is interference fit onto the non-orbiting scroll 112 via the bands 180, 182. For example, interference fit refers to fit between features/components in which the friction between the components prevents movement of the features/components relative to each other. In an embodiment, the interference fit of the upper portion 108A onto the non-orbiting scroll 112 is a shrink fit (e.g., formed by shrink fitting). Shrink fitting is an example of one manner of forming the interference fit. The interference/friction fit is formed by shrink fitting the upper portion 108A of the compressor housing 102 onto the non-orbiting scroll 112 via the bands 180, 182. In such an embodiment, the bands 180, 182 are shrink bands. For example, the upper portion 108A is heated to fit onto/around the non-orbiting scroll 112 (e.g., the heated upper portion 108A is placed over/onto/around the non-orbiting scroll 112), and then is cooled (e.g., air cooled, cooled using cooled air/gas, or the like) causing shrinking of the upper portion 108A and onto the shrink bands 180, 182. The shrinking/cooling of the upper portion 108A causing an interference fit between the upper portion 108A of the compressor housing 102 and the non-orbiting scroll 112 via the shrink bands 180, 182. Shrink fitting can advantageously form the interference fit without generating debris (e.g., scraping of surfaces against each other generates debris) that can damage the compressor. Shrink fitting can also advantageously ensure a seal is formed at each of the bands 180, 182 between the upper portion 108A of the compressor housing 102 and the non-orbiting scroll 112.

[0119] In an embodiment, the interference fit of the upper portion 108A is a press fit onto the upper portion 108A onto the non-orbiting scroll 112. For example, press fitting may include the upper portion 108A being molded/deformed (e.g., radially inward) onto the non-orbiting scroll 112. The compressor 100 may also include fasteners (e.g., bolts, screws, or the like) (not shown) that help maintain the position of the upper portion 108A of compressor housing 102 (e.g., prevent axial movement, prevent upwards) on the non-orbiting scroll member 112.

[0120] FIG. 5 is a cross-sectional view of the compressor 100, according to an embodiment. For example, the cross-sectional view is a horizontal cross-sectional view of the compressor 100 as indicated in FIG. 4. FIG. 6 is a partial front perspective view of the compressor 100, with the upper portion 108A of the housing 102 omitted.

[0121] As shown in FIG. 5, the intermediate injection chamber 144 surrounds the non-orbiting scroll 112. For example, the intermediate injection chamber 144 has an annular shape. The annular shape may be circular (e.g., see FIG. 5), oval, rectangular, etc. In the illustrated embodiment, the intermediate injection inlet 104C is radially aligned with the intermediate injection port 150. In an embodiment, the intermediate injection inlet 104C may be radially offset from the intermediate injection port 150. For example, the inlet opening for the intermediate injection inlet 104C and the outlet opening for the intermediate injection port 150 may partially overlap in the radial direction or may not overlap in the radial direction. In one such embodiment, the non-orbiting scroll 112 may include multiple intermediate injection ports 150, and the intermediate injection chamber 144 can fluidly connect the intermediate injection inlet 104C to the multiple intermediate injection ports 150.

[0122] As shown in FIGS. 5 and 6, each of the bands 180, 182 encircles the non-orbiting scroll 112. Each of the bands 180, 182 can have an annular shape (e.g., a ring shape). The first band 180 and the second band 182 are spaced apart from each other forming the intermediate injection chamber 144 therebetween. The intermediate injection chamber 144 encircles the non-orbiting scroll 112. The intermediate injection chamber 144 has an annular shape.

[0123] The bands 180, 182 may each be included in the non-orbiting scroll 112, in the housing 102, or as a separate component. In the illustrated embodiment, the bands 180, 182 are portions of the non-orbiting scroll 112. For example, the bands 180, 182 are provided as extensions from the baseplate 113 of the non-orbiting scroll 112 (e.g., extend from the baseplate 113 of the non-orbiting scroll 112, the baseplate 113 of the non-orbiting scroll 112 is formed to include the bands 180, 182). The bands 180, 182 may be provided on/extend from an outer circumferential surface 126 of the non-orbiting scroll 112 (e.g., an outer circumferential surface 126 of the baseplate 113 of the non-orbiting scroll 112).

[0124] The bands 180, 182 can be made of any suitable material (e.g., able to be pressed to form the interference fit, able to withstand the temperatures used in shrink fitting, able to withstand the pressure and/or temperatures that occur during operation of the compressor, and the like). For example, a band 180, 182 may be a metal ring (e.g., a copper ring, or the like) that is fit onto the outer circumference of the non-orbiting scroll 112 (e.g., onto the outer circumference of the baseplate 113 of the non-orbiting scroll 112). For example, a band 180, 182 may be a metal ring that is fit on the inner surface/circumference of the upper portion 108A of the compressor housing 102. For example, a band may be a crush ring (e.g., metal crush ring) that is provided between the upper portion 108A of the compressor housing 102 and the non-orbiting scroll 112 and is crush fit into place. For example, a band may be made of a polymer material (e.g., modified polymer) that is capable of withstanding the fitting conditions/temperatures.

[0125] In an embodiment, one or both of the bands 180, 182 may be provided on an inner surface 110 of the housing 102 (see FIG. 4), an outer surface of the non-orbiting scroll 112 (e.g., outer circumferential surface 126), and/or as a separate component from the non-orbiting scroll 112 and the housing 102. In an embodiment, the bands 180, 182 may be included in both of the non-orbiting scroll 112 and the housing 102 (e.g., one band 180, 182 included in the non-orbiting scroll 112 and the other band 180, 182 included in the housing 102).

[0126] FIG. 7 is a cross-sectional view of an embodiment of a scroll compressor 200. The view in FIG. 7 is a vertical cross-sectional view of the scroll compressor 200, similar to the view in FIG. 3. Dashed arrows are provided in FIGS. 7 and 8 to indicate the flow of working fluid within the scroll compressor 200.

[0127] The compressor 200 can have similar features as described for scroll compressor 100 in FIGS. 3-6, except as described below. For example, the compressor 200 includes a compressor housing 202 (e.g., compressor housing 202 including an upper portion 208A and a lower portion 208B), a suction inlet 204A, a discharge outlet 204B, a pair of intermeshed scroll members 212, 214 (e.g., non-orbiting scroll member 212 with baseplate 213 and spiral wrap 218, orbiting scroll member 214 with baseplate 215 and spiral wrap 220), a bearing support 234, a suction chamber 240, a discharge chamber 242, a crankshaft 260, and an electric motor 262, similar to the compressor 100 in FIGS. 3-6. It should be appreciated that features of the compressor 200 may be similar to similar features as discussed herein with respect to compressor 100 in FIGS. 3-6. In an embodiment, the compressor 200 may have features and/or modifications as similarly discussed for the compressor 100. In one non-limiting example, the compressor 200 may have an external electric/combustion motor for rotating the crankshaft 260 such that the electric motor 262 would be omitted, as similarly discussed for the electric motor 162 in the compressor 100.

[0128] In an embodiment, the scroll compressor 200 may be the compressor 10 in the refrigerant circuit 1 FIG. 1A, the compressor 10 in the refrigerant circuit 1 of FIG. 1B, the compressor 10 in the refrigerant circuit 1 of FIG. 1C, the compressor 10 in the refrigerant circuit 1 of FIG. 1D. The compressor 200 includes intermediate injection inlets 204C, 204D that receive flows f.sub.i*-1, f.sub.i*-2 of intermediate working fluid. For example, the intermediate injection inlets 204C, 204D of the compressor 200 may correspond with the intermediate injection inlets 16A, 16B of the compressor 10 in FIGS. 1A-1D that receive respective flows of intermediate working fluid.

[0129] Referring to FIG. 7, applying known aspects of scroll compressor compression, the scroll compressor 200 utilizes the intermeshing of the two scroll members 212, 214 to form the plurality of compression pockets 216 in which gas is trapped and then compressed. The spiral wrap 218 of the non-orbiting scroll 212 is intermeshed with the spiral wrap 220 of the orbiting scroll member 214 forming the compression pockets 216 there between. The compression pockets 216 include intermediate compression pockets 217 that is partially through the compression process (e.g., similar to the intermediate compression pockets 117 in the compressor 100).

[0130] The compressor housing 202 of the scroll compressor 200 includes upper portion 208A and lower portion 208B. As shown in FIG. 7, the suction inlet 204A extends through the lower portion 208B of the compressor housing 202 (e.g., suction inlet 204A is disposed in the compressor housing 202, suction inlet 204A is disposed in the lower portion 208B of the compressor housing 202). The compressor 200 includes the intermediate injection inlets 204C, 204D that each extend through the compressor housing 202 (e.g., intermediate injection inlets 204C, 204D each disposed in the compressor housing 202, intermediate injection inlets 204C, 204D each disposed in the upper portion 208A of the compressor housing 202). As shown in FIG. 7, the compressor 200 includes a first intermediate injection inlet 204C and a second intermediate injection inlet 204D. The intermediate injection inlets 204C, 204D each extend through the upper portion 208B of the compressor housing 202.

[0131] The compressor housing 202 contains an internal volume that includes the suction chamber 240, the discharge chamber 242, a plurality of intermediate injection chambers (e.g., a first intermediate injection chamber 244A, a second intermediate injection chamber 244B) of the compressor 200. The discharge chamber 242, the suction chamber 240, and the intermediate injection chambers 244A, 244B are at different pressures. For example, the suction chamber 240 is at a suction pressure (e.g., the first pressure P.sub.1*), the discharge chamber 242 is at the discharge pressure (e.g., the second pressure P.sub.2*), the first intermediate injection chamber 244A is at the discharge pressure or an intermediate pressure (e.g., the third pressure P.sub.3*), and the second intermediate injection chamber 244B is at the discharge pressure or an intermediate pressure (e.g., the fourth pressure P.sub.4*).

[0132] In an embodiment, the intermediate injection chambers 244A, 244B may be at different pressures (e.g., pressure P.sub.3* is different from pressure P.sub.4*). In an embodiment, the intermediate injection chambers 244A, 244B may each be at the same pressure (e.g., third pressure P.sub.3*=fourth pressure P.sub.4*) For example, the working fluid in the first intermediate injection chamber 244A and working fluid in the second intermediate injection chamber 244B can be at the same pressure while being at different temperatures, contain different phases (e.g., be gaseous, be liquid, be in a mixed gas/liquid phase) and/or having different compositions (e.g., being lubricant rich, being refrigerant rich, or the like). The intermediate injection chambers 244A, 244B are discussed in more detail below with respect to FIG. 8.

[0133] The discharge chamber 242 is disposed between the compressor housing 202 and the non-orbiting scroll member 212 (e.g., between the upper portion 208A of the compressor housing 202 and the non-orbiting scroll member 212). As shown in FIG. 7, the discharge chamber 242 is a volume defined by the compressor housing 202 and the non-orbiting scroll member 212 (e.g., defined by the upper portion 208A of the compressor housing 202 and the non-orbiting scroll member 212). The discharge chamber 242 may also be referred to as an upper volume of the compressor 200.

[0134] The suction chamber 240 is disposed between the compressor housing 202 and the non-orbiting scroll member 212 (e.g., between the lower portion 208B of the compressor housing 202 and the non-orbiting scroll member 212). The suction chamber 240 is disposed opposite to the discharge chamber 242 with respect to the non-orbiting scroll 212. For example, the suction chamber 240 and the discharge chamber 242 can be disposed on opposite sides of the non-orbiting scroll 212. As shown in the illustrated embodiment, the discharge chamber 242 and the suction chamber 240 are fluidly separated by the non-orbiting scroll 212. As shown in FIG. 7, the suction chamber 240 is a volume defined by the compressor housing 202 and the non-orbiting scroll member 212 (e.g., defined by the lower portion 208A of the compressor housing 202 and the non-orbiting scroll member 212). The suction chamber 240 may also be referred to as a lower volume of the compressor 200.

[0135] As shown in FIG. 7, the intermeshed scrolls 212, 214 have an inlet 224 through which gas flows into the intermeshed scrolls 212, 214 and an outlet 222 through which the compressed is discharged. For example, the inlet 224 can have a similar configuration as discussed for the inlet 124 in FIG. 3, and the outlet 222 can have a similar configuration as discussed for the outlet 122 in FIG. 3.

[0136] The compressor 200 includes intermediate injection ports 250A, 250B formed in the non-orbiting scroll 212 for injecting intermediate working fluid into the intermeshed scrolls 212, 214. The intermediate injection ports 250A, 250B fluidly connect the intermediate injection chambers 244A, 244B to one or more intermediate compression pockets 217 of the intermeshed scrolls 212, 214. Each of the intermediate injection ports 250A, 250B is a separate passageway extending through the non-orbiting scroll member 212 (e.g., separate passageways extending through the baseplate 213 of the non-orbiting scroll member 212). The intermediate injection ports 250A, 250B are configured to receive/supply flows of intermediate working fluid (i.e., in flow f.sub.i*-1 and in flow f.sub.i*-2) into the intermeshed scrolls 212, 214. The intermediate injection inlets 204C, 204D may be configured to supply stream(s) of liquid intermediate working fluid, stream(s) of gaseous intermediate working fluid, or a combination thereof.

[0137] The intermediate working fluid supplied via the intermediate injection inlets 204C, 204D may be stream(s) of intermediate refrigerant (e.g., intermediate working fluid containing a majority of refrigerant), stream(s) of intermediate lubricant (e.g., intermediate working fluid containing a majority of lubricant), or a combination thereof. The intermediate injection inlets 204C, 204D may be configured to supply intermediate lubricant (e.g., lubricant rich working fluid, working fluid that contains a majority of liquid lubricant, working fluid that is mostly or entirely liquid lubricant), to supply intermediate refrigerant (e.g., intermediate working fluid containing a majority of refrigerant), or to supply both a stream of intermediate lubricant and a stream of intermediate refrigerant. In an embodiment, intermediate refrigerant supplied by one or more of the intermediate injection inlets 204C, 204D may be in a gaseous state (e.g., mostly or entirely gaseous), liquid state (e.g., mostly or entirely liquid), or in a mixed state.

[0138] In an embodiment, the first intermediate injection inlet 204C can be a gaseous intermediate inlet configured to receive/supply gaseous intermediate working fluid (e.g., the working fluid/refrigerant in the flow f.sub.i*-1 is mostly gaseous, the working fluid/refrigerant in the flow f.sub.i*-1 is at or about entirely gaseous), and the second intermediate injection inlet 204D can be a liquid intermediate inlet configured to receive/supply liquid intermediate working fluid (e.g., the working fluid/refrigerant in the flow f.sub.i*-2 is in a mixed state, the working fluid/refrigerant in the flow f.sub.i*-2 is mostly liquid, the working fluid/refrigerant in the flow f.sub.i*-2 is at or about entirely liquid).

[0139] In an embodiment, one of the intermediate injection inlets 204D, 204C may be a liquid intermediate inlet configured to receive/supply lubricant (e.g., the working fluid in the flow f.sub.i*-2 contains liquid lubricant, a majority of the working fluid in the flow f.sub.i*-2 is lubricant). For example, injected lubricant may help provide sealing between tips of the wraps 218, 220 of the scrolls 212, 214 and/or provide cooling. In an embodiment, a first intermediate injection inlet 204C can be configured to receive/supply intermediate refrigerant and the second intermediate injection inlet 204D can be configured to receive/supply intermediate lubricant (e.g., lubricant at a pressure above suction pressure, lubricant at the discharge pressure).

[0140] An intermediate compression pocket 217 is one of the compression pockets 216 that is partially through the compression process (e.g., at a pressure between the inlet pressure P.sub.1* and the discharge pressure P.sub.2*, has travelled part way and is disposed at an intermediate position between the inlet 224 and the outlet 222). The gaseous and/or liquid intermediate working fluid is added to the working fluid already within the intermediate compression pocket 217, which is then further compressed (e.g., to the discharge pressure P.sub.2*). When the injected working fluid contains liquid working fluid, the liquid working can undergo a pressure drop while flowing into the intermediate compression pocket 217 (e.g., as it flows to the intermediate compression pocket 217, within the intermediate compression pocket 217 that is at relatively lower pressure). The pressure drop can cause evaporation of the working fluid, which provides cooling. The location of each of the outlets of the intermediate inlet ports 250A, 250B with respect to the compression process may vary, as similarly discussed herein with respect to the intermediate inlet port(s) 150 in the compressor 100 of FIGS. 2-6. The location for the outlets of each intermediate inlet port 250A, 250B may be selected as similarly discussed herein with respect to the intermediate inlet port(s) 150 in the compressor 100 of FIGS. 2-6.

[0141] The working fluid is compressed by the intermeshed scrolls 212, 214 as the working fluid travels between the intermeshed scrolls 212, 214. The compressed working fluid flows out of the scroll compressor 200 by flowing from the outlet 222 of the intermeshed scrolls 212, 214 to and through the discharge outlet 204B. The working fluid enters the intermeshed scrolls 212, 214 at the relatively lower pressure (e.g., at suction pressure, at the first pressure P.sub.1*), and is discharged from intermeshed scrolls 212, 214 at a relative higher pressure (e.g., at discharge pressure, at the second pressure P.sub.2*). The intermediate working fluid is at the relatively higher pressure(s) or at the intermediate pressure(s) (e.g., at pressure(s) between the suction pressure and the discharge pressure, at or about the discharge pressure, at the third pressure P.sub.3*, at the fourth pressure P.sub.4*) also flows into the intermeshed scrolls 212, 214.

[0142] The suction inlet 204A is fluidly connected to the inlet 224 of the intermeshed scrolls 212, 214 (e.g., the suction chamber 240 fluidly connects the suction inlet 204A to the inlet 224 of the intermeshed scrolls 212, 214). The suction flow f.sub.S* of the working fluid flows from the suction inlet 204A into the inlet 224 of the intermeshed scrolls 212, 214 (e.g., through the suction chamber 240, the intermeshed scrolls 212, 214 suctioning working fluid from the suction chamber 240). In the illustrated embodiment, suction chamber 240 is at the suction/inlet pressure of the suction flow f.sub.S* (e.g., the working fluid within the is at the suction/inlet pressure of the suction flow f.sub.S*).

[0143] The discharge outlet 204B is fluidly connected to the outlet 222 of the intermeshed scrolls 212, 214 (e.g., the discharge chamber 242 fluidly connects the outlet 222 of the intermeshed scrolls 212, 214 to the discharge outlet 204B). The discharge flow f.sub.D* of the compressed working fluid flows from outlet 222 of the intermeshed scrolls 212, 214 to and through the discharge outlet 204B of the compressor 200 (e.g., through the discharge volume 242). The discharge chamber 242 is at the discharge pressure (e.g., the working fluid within the discharge chamber 242 is at the discharge pressure of the discharge flow f.sub.D*).

[0144] FIG. 8 is a partial cross-sectional view of the compressor 200, according to an embodiment. For example, FIG. 8 is an enlarged portion of the view in FIG. 7. Dashed lines indicate a cutoff of the compressor 200 in the view of FIG. 8.

[0145] As shown in FIG. 8, the plurality of intermediate injection chambers of the compressor 200 include the first intermediate injection chamber 244A and the second intermediate injection chamber 244B. Each of the intermediate injection chambers 244A, 244B respectively supply intermediate working fluid from a respective intermediate injection inlet 204C, 204D to one or more respective intermediate injection ports 250A, 250B. In the compressor 200, at least two streams of intermediate working fluid is supplied into the compression pockets 216 (e.g., into the intermediate compression pockets 217).

[0146] The first intermediate injection inlet 204C fluidly connects to the first intermediate injection chamber 244A. A first injection flow f.sub.i*-1 (of intermediate working fluid) is directed from the first intermediate injection inlet 204C to and through the first intermediate injection port 250A into an intermediate compression pocket 217. The intermediate working fluid in first injection flow f.sub.i*-1 may be referred to as first intermediate working fluid.

[0147] As shown in FIG. 8, the first intermediate injection chamber 244A fluidly connects the first intermediate injection inlet 204C of the compressor 200 to the first intermediate injection port 250A in the non-orbiting scroll 212. For example, the first intermediate injection inlet 204C fluidly connects to the first intermediate injection chamber 244A, and the first intermediate injection chamber 244A fluidly connects to the first intermediate injection port 250A in the non-orbiting scroll 212. The first intermediate injection chamber 244A directs the intermediate working fluid from the intermediate injection inlet 204C into the first intermediate injection port 250A in the non-orbiting scroll 212. The intermediate injection chamber 244 is at the pressure of the first intermediate working fluid (e.g., the working fluid within the first intermediate injection chamber 244A is of the first intermediate injection flow f.sub.i*-1).

[0148] The second intermediate injection inlet 204D fluidly connects to the second intermediate injection chamber 244B. A second intermediate injection flow f.sub.i*-2 (of intermediate working fluid) is directed from the second intermediate injection inlet 204D to and through the second intermediate injection port 250B into an intermediate compression pocket 217. The intermediate working fluid in the second intermediate injection flow f.sub.i*-2 may be referred to as second intermediate working fluid. It should be appreciated that first intermediate working fluid and second intermediate working fluid does not refer to different types of working fluid (e.g., can refer to the same working fluid in the refrigerant circuit, having different properties, as discussed above).

[0149] As shown in FIG. 8, the second intermediate injection chamber 244B fluidly connects the second intermediate injection inlet 204D of the compressor 200 to the second intermediate injection port 250B in the non-orbiting scroll 212. For example, the second intermediate injection inlet 204D fluidly connects to the second intermediate injection chamber 244B, and the second intermediate injection chamber 244B fluidly connects to the second intermediate injection port 250B in the non-orbiting scroll 212. The second intermediate injection chamber 244B directs the intermediate working fluid from the second intermediate injection inlet 204D into the second intermediate injection port 250B in the non-orbiting scroll 212. The second intermediate injection chamber 244B is at the pressure of the second intermediate working fluid (e.g., the working fluid within the second intermediate injection chamber 244B is of the second intermediate injection flow f.sub.i*-2). It should be appreciated that first intermediate working fluid and second intermediate working fluid does not refer to different types of working fluid (e.g., can refer to the same working fluid in the refrigerant circuit, having at different pressures and/or temperatures, as discussed above).

[0150] The first intermediate injection port 250A extends through the non-orbiting scroll member 212 to a location at which one or more intermediate compression pocket(s) 217 are formed. The first intermediate injection port 250A is a passageway that extends all the way through the non-orbiting scroll 212. The second intermediate injection port 250A extends through the non-orbiting scroll member 212 to a location at which intermediate compression pocket(s) 217 are formed. The second intermediate injection port 250B is a passageway that extends all the way through the non-orbiting scroll 212. The first and second intermediate injection ports 250A, 250B are different (i.e., fluidly separate) passageways in the non-orbiting scroll 212.

[0151] The first intermediate injection port 250A and the second intermediate injection port 250B may be configured to inject into different intermediate pockets 217 (e.g., do not simultaneously inject into the same intermediate pocket 217). In an embodiment, the first intermediate injection port 250A may be configured to inject into the same intermediate pocket 217 at different times. For example, the first intermediate injection port 250A injects into an intermediate pocket 217, and later in the compression cycle (e.g., after the intermediate pocket 217 is moved closer to the discharge 222), the second intermediate injection port 250B injects into the same intermediate pocket 217.

[0152] As shown in FIG. 8, the compressor 200 includes a plurality of bands 280, 282, 284 disposed within the housing 202 of the compressor 200. The bands 280, 282, 284 include a first band 282, a second band 282, and a third band 284. The first band 280 may also be referred to as a lower band, the second band 282 may also be referred to as a middle band, and the third band 284 may also be referred to an upper band. The bands 280, 282, 284 each extend between the non-orbiting scroll 212 and the compressor housing 202. Each band 280, 282, 284 forms a respective seal between the compressor housing 208 and the non-orbiting scroll member 212 (e.g., each forms a respective seal between the upper portion 208A of the compressor housing 202 and the non-orbiting scroll 212).

[0153] Each of the bands 280, 282, 284 can have a similar location/configuration as discussed for the bands 180, 182 of the compressor 100 in FIGS. 4-6. For example, each of the bands 280, 282, 284 extends around a circumference of the non-orbiting scroll 212, as shown and discussed for each of the bands 180, 182 of the compressor 100 in FIGS. 4-6. As shown in FIG. 8, the bands 280, 282, 284 are spaced apart from each other in the axial direction (e.g., in axial direction D.sub.1* of the compressor 200, vertically spaced apart). For example, the second band 282 is disposed between the first band 282 and the third band 284 in the axial direction, and the second band 282 is spaced apart in the axial direction from each of the first band 280 and the third band 284 in the axial direction. Each of the intermediate injection chambers 244A, 244B is respectfully formed by the gap between a respective pair of the bands 280, 282, 284.

[0154] The first intermediate injection chamber 244A is formed by the gap between a first pair of the bands 280, 282. In the illustrated embodiment, the first intermediate injection chamber 244A is formed by the gap between the first band 280 and the second band 282. Said gap is also between the compressor housing 202 and the non-orbiting scroll 212 (e.g., the first intermediate injection chamber 244A is formed between the first and second bands 280, 282 and between the compressor housing 202 and the non-orbiting scroll 212). The first intermediate injection chamber 244A is a volume defined by the compressor housing 202, the non-orbiting scroll member 212, and the first pair of bands 280, 282 (e.g., the first band 280 and the second band 282). The first intermediate injection chamber 244A is defined by the first pair of bands 280, 282 (e.g., the first band 280 and the second band 282), the compressor housing 202 (e.g., the upper portion 208A of the compressor housing 202), and the non-orbiting scroll 212.

[0155] The second intermediate injection chamber 244B is formed by the gap between a second pair of the bands 282, 284 (i.e., different from the first pair of bands 280, 282). In the illustrated embodiment, the second intermediate injection chamber 244B is formed by the gap between the second band 282 and the third band 284. Said gap is also between the compressor housing 202 and the non-orbiting scroll 212 (e.g., the second intermediate injection chamber 244B is formed between the second and second third 282, 284 and between the compressor housing 202 and the non-orbiting scroll 212). The second intermediate injection chamber 244B is a volume defined by the compressor housing 202, the non-orbiting scroll member 212, and the second pair of bands 282, 284 (e.g., the second band 282 and the third band 284). The second intermediate injection chamber 244B is defined by the second pair of bands 282, 284 (e.g., the second band 282 and the third band 284), the compressor housing 202 (e.g., the upper portion 208A of the compressor housing 202), and the non-orbiting scroll 212.

[0156] The first intermediate injection chamber 244A connects to the first intermediate injection port 250A that extends through the non-orbiting scroll member 212 (e.g., the first intermediate injection port 250A extends from the first intermediate injection chamber 244A). The second intermediate injection chamber 244B connects to the second intermediate injection port 250B that extends through the non-orbiting scroll member 212 (e.g., second intermediate injection port 250B extends from the second intermediate injection chamber 244B).

[0157] The bands 280, 282, 284 can each form a seal between a respective pair of the suction chamber 240, the discharge chamber 242, the first intermediate injection chamber 244A, and the second intermediate injection chamber 244B. The first band 280 can form a seal between the first intermediate injection chamber 244A and the suction chamber 240. For example, the first band 280 prevents working fluid from flowing between the intermediate injection chamber 244 and the suction chamber 240 (e.g., prevents working fluid from flowing directly between the first intermediate injection chamber 244A and the suction chamber 240, and prevents working fluid from flowing directly from the first intermediate injection chamber 244A into the suction chamber 240). In the illustrated embodiment, the first band 280 also in part defines the suction chamber 240.

[0158] The second band 282 can form a seal between the first intermediate injection chamber 244A and the second intermediate chamber 244B. For example, the second band 282 prevents working fluid from flowing between the first and second intermediate injection chambers 244A, 244B (e.g., prevents working fluid from flowing directly between the first and second intermediate injection chambers 244A, 244B, prevents working fluid from flowing directly from the first intermediate injection chamber 244A into the second intermediate injection chambers 244B, and prevents working fluid from flowing directly from the second intermediate injection chamber 244B into the first intermediate injection chamber 244A). The second band 282 partially defines at least one of the first intermediate chamber 244A, 244B. In the illustrated embodiment, the second band 282 partially defines both the first intermediate chamber 244A and the second intermediate chamber 244B.

[0159] The third band 284 can form a seal between the second intermediate injection chamber 244B and the discharge chamber 242. For example, the third band 284 prevents the working fluid from flowing between the second intermediate injection chamber 244B and the discharge chamber 242 (e.g., prevents working fluid from flowing directly between the second intermediate injection chamber 244B and discharge chamber 242, and prevents the working fluid from flowing directly from the discharge chamber 242 into the second intermediate injection chamber 244B). In the illustrated embodiment, the third band 284 also defines the discharge chamber 242.

[0160] In the illustrated embodiment, the three bands 280, 282, 284 are used to form the two intermediate injection chambers 244A, 244B. It should be appreciated that in other embodiments a different number of bands 280, 282, 284 may be used to form a different number of intermediate injection chambers 244A, 244B. For example, compressor 200 in other embodiments may have four or more of the bands 280, 282, 284 that form two or more intermediate injection chambers 244A, 244B. In an embodiment, four bands may be used to form the two intermediate injection chambers (e.g., a first intermediate injection chamber formed by a first band and a second band, a second intermediate injection chamber formed by a third band and a fourth band, where none of the bands defining both intermediate injection chambers). In such an embodiment, an open or unused volume/chamber may be formed between the two intermediate injection chambers (e.g., by the gap between the second and third bands). It should also be appreciated that in some embodiments, one or more additional bands may be provided between the intermediate injection chambers 244A, 244B, between the intermediate injection chambers 244A, 244B and the suction chamber 240, and/or between the intermediate injection chambers 244A, 244B and the discharge chamber 242. For example, the additional band(s) may provide additional sealing between the chambers 240, 242, 244A, 244B.

[0161] The upper portion 208A of the compressor housing 202 is interference fit onto the non-orbiting scroll 212 via the bands 280, 282, 248. This interference fit of the upper portion 208A of the compressor housing 202 in the compressor 200 can be similar to the interference fit as discussed for the upper portion 108A of the compressor housing 102 in the compressor 100 in FIGS. 2-6 (e.g., similar except for with a different bands configuration). For example, in an embodiment, the interference fit of the upper portion 208A is a press fit of the upper portion 208A onto the non-orbiting scroll 212. For example, in an embodiment, the interference fit of the upper portion 208A onto the non-orbiting scroll 212 is a shrink fit (e.g., formed by shrink fitting).

[0162] Each intermediate injection chamber 244A, 244B in the compressor 200 may have a similar shape/configuration as discussed for the intermediate injection chamber 144 in the compressor 100 of FIGS. 2-6. For example, one or more of the intermediate injection chambers 244A, 244B can encircle the non-orbiting scroll 212 and can have an annular shape (e.g., each the intermediate injection chambers 244A, 244B encircles the non-orbiting scroll, each the intermediate injection chambers 244A, 244B has an annular shape).

[0163] In the illustrated embodiment, each of the intermediate injection inlets 204C, 204D is radially aligned with its respective intermediate injection port 250A, 250B (e.g., first intermediate injection inlet 204C aligned with first intermediate injection port 250A, second intermediate injection inlet 204D aligned with second intermediate injection port 250B). In an embodiment, an intermediate injection inlet 204D, 204D may be radially offset from the intermediate injection port 250A, 250B to which it is fluidly connected.

[0164] In an embodiment, one or more of the intermediate injection chambers 244A, 244B may supply working fluid to a plurality of intermediate injection ports. For example, the non-orbiting scroll 212 may include multiple intermediate injection ports 250A fluidly connected to the first intermediate injection chamber 244A (e.g., a plurality of the first intermediate injection ports 250A fluidly connected to/extending from the first intermediate injection chamber 244A) and/or multiple intermediate injection ports 250B fluidly connected to the second intermediate injection chamber 244B (e.g., a plurality of the second intermediate injection ports 250B fluidly connected to/extending from the second intermediate injection chamber 144B). The first intermediate injection chamber 244A can fluidly connect the first injection inlet 204C to multiple (first) intermediate injection ports 250A and/or the second intermediate injection chamber 244B can fluidly connect the second injection inlet 204D to multiple (second) intermediate injection ports 250B.

[0165] The bands 280, 282, 284 in the compressor 200 may each have a similar shape/configuration as discussed for the bands 180, 182 in the compressor 100 of FIGS. 2-6. For example, one or more of the bands 280, 282, 284 can encircle the non-orbiting scroll 212 and can have an annular shape (e.g., a ring shape) (e.g., each of the bands 280, 282, 284 encircles the non-orbiting scroll 212, each of the bands 280, 282, 284 has an annular shape).

[0166] The bands 280, 282, 284 may be included in the non-orbiting scroll 212, in the housing 202, and/or as a separate component, as similarly discussed for the bands 180, 182 of the compressor 100 in FIGS. 2-6. For example, in an embodiment, each band 280, 282, 284 may be provided on the housing 202 (e.g., on an inner surface of the housing 202), on the non-orbiting scroll 212 (e.g., on an outer circumferential surface of the non-orbiting scroll 212), or as a separate component from the non-orbiting scroll 212 and the housing 202.

[0167] As shown in FIG. 8, the bands 280, 282, 284 can be portions of the non-orbiting scroll 212. In an embodiment, a band 280, 282, 284 may be a separate component (e.g., a crush ring, a metal ring, a copper ring, a polymer material ring, or the like). In an embodiment, a band 280, 282, 284 may be a portion of the housing 202 (e.g., a portion of the upper portion 208A of the housing 202). In an embodiment, the bands 280, 282, 284 may be included in both of the non-orbiting scroll 212 and the housing 202 (e.g., at least one of the bands 280, 282, 284 included in the non-orbiting scroll 212 and at least one of more of the other bands 280, 282, 284 included in the housing 202).

[0168] FIG. 9 is a block flow diagram for a method 1000 of making a scroll compressor. For example, the method 1000 may be employed to make the scroll compressor 100 in FIGS. 2-6. For example, the method 1000 may be employed to make the scroll compressor 200 in FIGS. 7-8. The method 1000 can start at 1010 or 1020.

[0169] At 1010, an upper portion (e.g., upper portion 108A, upper portion 208A) of a compressor housing (e.g., compressor housing 102, compressor housing 202) is heated. The upper portion is heated at 1010 to a temperature above ambient temperature (e.g., above 70? F.). The heating 1010 causes the upper portion to expand. In particular, the heating 1010 causes an inner diameter of the upper portion to increase. The increased inner diameter of the upper portion is at least equal to a diameter of a non-orbiting scroll (e.g., non-orbiting scroll 112, non-orbiting scroll 212) and bands (e.g., bands 180, 182, bands 280, 282, 284) of the compressor. In an embodiment, the increased inner diameter of the upper portion is greater than the diameter of the non-orbiting scroll and the bands. The method 1000 then proceeds to 1020.

[0170] At 1020, the upper portion of the compressor housing is placed over the non-orbiting scroll, with the bands each being disposed between the upper portion of the compressor housing and the non-orbiting scroll. The upper portion of the compressor housing is placed over the non-orbiting scroll such that the upper portion of the compressor housing surrounds the non-orbiting scroll. For example, the non-orbiting scroll and the bands being disposed within the upper portion of the compressor housing. The method 1000 then proceeds to 1030.

[0171] At 1030, the upper portion of the compressor housing is interference fit onto the non-orbiting scroll member via the bands. The interference fitting at 1030 forms one or more intermediate injection chambers (e.g., intermediate injection chamber 144, first intermediate chamber 244A, second intermediate chamber 244B) within the compressor housing. The bands define the intermediate injection chamber(s). The interference fitting at 1030 can also form a discharge chamber (e.g., discharge chamber 142, discharge chamber 242) within the compressor housing. In an embodiment, the interference fitting also forms a suction chamber (e.g., suction chamber 140, suction chamber 240) within the compressor housing. For example, the bands also define the discharge chamber and/or the suction chamber within the compressor.

[0172] In an embodiment, the interference fitting at 1030 is shrink fitting 1032 of the upper portion of the compressor housing onto the non-orbiting scroll member 1032. In such an embodiment, the method 1000 can start at 1010. At 1032, the upper portion of the compressor housing is cooled to shrink fit the upper portion onto the non-orbiting scroll member 1032. The upper portion is cooled while containing the non-orbiting scroll and bands (e.g., while placed around/surrounding the non-orbiting scroll and bands). The cooling at 1030 results in the shrink fitting of the upper portion of the compressor housing onto the non-orbiting scroll via the bands. For example, the cooling of the relatively hot/heated upper portion at 1030 causes the upper portion to shrink, and said shrinking fits/affixes the upper portion onto non-orbiting scroll via the bands. Said shrinking results in an interference fit between the upper portion of the compressor housing and the non-orbiting scroll via each of the shrink bands.

[0173] In an embodiment, the interference fitting at 1030 is press fitting 1034 of the upper portion of the compressor housing onto the non-orbiting scroll member 1032. In such an embodiment, the method 1000 can start at 1020. At 1034, the upper portion of the compressor housing is pressed onto the upper portion onto the non-orbiting scroll member. For example, the upper portion of the compressor housing is molded/deformed onto the bands and the non-orbiting scroll member. For example, fasteners (e.g., bolts, screws, or the like) may be used to help with maintaining the upper portion of compressor housing affixed in place on the non-orbiting scroll member.

[0174] It should be appreciated that the method 1000 in an embodiment may be modified to include features as shown and/or as described above for the compressor 100 in FIGS. 2-6 and/or to include features as shown and/or as described above for the compressor 200 in FIGS. 7-8.

Aspects

[0175] Any of Aspects 1-10 may be combined with any of Aspects 11-43, any of Aspects 11-16 maybe combined with any of Aspects 17-43, any of Aspects 20-31 may be combined with any of Aspects 32-43, any of Aspects 32-38 may be combined with any of Aspects 39-42, and any of Aspects 39-40 may be combined with any of Aspects 40-42. [0176] Aspect 1. A scroll compressor, comprising: a compressor housing containing a suction chamber, a discharge chamber, and an intermediate injection chamber; an orbiting scroll member and a non-orbiting scroll member intermeshed to form compression pockets within the compressor housing, the compression pockets configured to suction from the suction chamber and discharge into the discharge chamber, the non-orbiting scroll member including an intermediate injection port fluidly connecting the intermediate injection chamber to at least one of the compression pockets; and a first band and a second band disposed within the compressor housing and each extending between the non-orbiting scroll member and the compressor housing, the intermediate injection chamber being defined by the first band and the second band. [0177] Aspect 2. The scroll compressor of Aspect 1, wherein the first band forms a seal between the intermediate injection chamber and the discharge chamber, and the second band forms a seal between the intermediate injection chamber and the suction chamber. [0178] Aspect 3. The scroll compressor of any one of Aspects 1 and 2, wherein a first band and a second band each extend from the non-orbiting scroll member to the compressor housing. [0179] Aspect 4. The scroll compressor of any one of Aspects 1-3, further comprising: a suction inlet in the compression housing, the suction chamber fluidly connecting the suction inlet to an inlet of the compression pockets, a discharge outlet in the compression housing, the discharge chamber fluidly connecting an outlet of the compression pockets to the discharge outlet, and an intermediate injection inlet in the compression housing, the intermediate injection chamber fluidly connecting the intermediate injection inlet to intermediate injection port in the non-orbiting scroll member. [0180] Aspect 5. The scroll compressor of any one of Aspects 1-4, wherein the intermediate injection chamber encircles the non-orbiting scroll member. [0181] Aspect 6. The scroll compressor of any one of Aspects 1-5, wherein the first band and the second band each encircle the non-orbiting scroll member. [0182] Aspect 7. The scroll compressor of any one of Aspects 1-6, wherein the intermediate injection chamber has an annular shape. [0183] Aspect 8. The scroll compressor of any one of Aspects 1-7, wherein the compressor housing includes an upper portion and a lower portion, the first band extending from the non-orbiting scroll member to the upper portion of the compressor housing, the intermediate injection chamber being defined by the upper portion of the compressor housing. [0184] Aspect 9. The scroll compressor of Aspect 8, wherein the upper portion of the compressor housing is shrink fitted onto the non-orbiting scroll member via the first band and the second band. [0185] Aspect 10. The scroll compressor of any one of Aspects 1-9, wherein the first band contacts the compressor housing and the non-orbiting scroll member. [0186] Aspect 11. A heating, ventilation, air conditioning, and refrigeration (HVACR) system, comprising: a refrigerant circuit including a condenser, a plurality of expanders, an evaporator, and a scroll compressor fluidly connected, a working fluid flowing through the refrigerant circuit, wherein the scroll compressor includes: a compressor housing containing a suction chamber, a discharge chamber, and an intermediate injection chamber, an orbiting scroll member and a non-orbiting scroll member intermeshed to form compression pockets within the compressor housing, the compression pockets configured to suction from the suction chamber and discharge into the discharge chamber, the non-orbiting scroll member including an intermediate injection port fluidly connecting the intermediate injection chamber to at least one of the compression pockets, and a first band and a second band each extending between the non-orbiting scroll member and the compressor housing, the intermediate injection chamber being defined by the first band and the second band. [0187] Aspect 12. The HVACR of Aspect 11, wherein the first band forms a seal between the intermediate injection chamber and the discharge chamber, and the second band forms a seal between the intermediate injection chamber and the suction chamber. [0188] Aspect 13. The HVACR of any one of Aspects 11 and 12, wherein the first band and the second band each extend from the non-orbiting scroll member to the compressor housing. [0189] Aspect 14. The HVACR of any one of Aspects 11-13, wherein the scroll compressor includes: a suction inlet in the compression housing, the suction chamber fluidly connecting the suction inlet to an inlet of the compression pockets, a discharge outlet in the compression housing, the discharge chamber fluidly connecting an outlet of the compression pockets to the discharge outlet, and an intermediate injection inlet in the compression housing, the intermediate injection chamber fluidly connecting the intermediate injection inlet to intermediate injection port in the non-orbiting scroll member. [0190] Aspect 15. The HVACR of any one of Aspects 11-14, wherein the intermediate injection chamber encircles the non-orbiting scroll member. [0191] Aspect 16. The HVACR of any one of Aspects 11-15, wherein the first band and the second band each encircle the non-orbiting scroll member. [0192] Aspect 17. A method of making a scroll compressor, comprising: placing an upper portion of a compressor housing over a non-orbiting scroll member, the upper portion of the compressor housing surrounding the non-orbiting scroll member, and a first band and a shrink band each being disposed between the upper portion of the compressor housing and the non-orbiting scroll member; and interference fitting the upper portion of the compressor housing onto the non-orbiting scroll member via the first band and the second band, wherein the interference fitting forms an intermediate injection chamber defined by the first band, the second band, the upper portion of the compressor housing, and the non-orbiting scroll member, the intermediate injection chamber fluidly connecting an intermediate injection inlet in the compressor housing to an intermediate injection port in the non-orbiting scroll member. [0193] Aspect 18. The method of claim 17, further comprising: heating of the upper portion of the compressor housing, prior to placing the upper portion of the compressor housing onto the non-orbiting scroll member, wherein the interference fitting is a shrinking fitting that includes cooling of the upper portion of the compressor housing, which results in the upper portion of the compressor housing being shrink fit onto the non-orbiting scroll member via the first band the second band, the first band and the second band being shrink bands. [0194] Aspect 19. The method of any one of Aspects 17 and 18, wherein the scroll compressor includes a non-orbiting scroll member intermeshed with the non-orbiting scroll member to form compression pockets, and the interference fitting forms a discharge chamber that fluidly connects an outlet of the compression pockets to the discharge outlet. [0195] Aspect 20. A scroll compressor, comprising: a compressor housing containing a suction chamber, a discharge chamber, and intermediate injection chambers; an orbiting scroll member and a non-orbiting scroll member intermeshed to form compression pockets within the compressor housing, the compression pockets configured to suction from the suction chamber and discharge into the discharge chamber, the non-orbiting scroll member including intermediate injection ports fluidly connecting the intermediate injection chambers to the compression pockets; and at least three bands disposed within the compressor housing, each of the at least three bands extending between the non-orbiting scroll member and the compressor housing, and the intermediate injection chambers being defined by pairs of the three or more bands. [0196] Aspect 21. The scroll compressor of Aspect 20, wherein the intermediate injection chambers include a first intermediate injection chamber and a second intermediate injection chamber, and the intermediate injection ports include: a first intermediate injection port fluidly connecting the first intermediate injection chamber to at least one of the compression pockets, and a second intermediate injection port fluidly connecting the second intermediate injection chamber to at least one of the compression pockets. [0197] Aspect 22. The scroll compressor of Aspect 21, wherein the pairs of the three or more bands include: [0198] a first pair of the bands, the first intermediate injection chamber defined by the first pair of bands, and [0199] a second pair of the bands, the second intermediate injection chamber defined by the second pair of bands. [0200] Aspect 23. The scroll compressor of Aspect 22, wherein the at least three bands include a first band, the first pair of the bands and the second pair of the bands each include the first band. [0201] Aspect 24. The scroll compressor of Aspect 23, wherein the at least three bands include a second band and a third band, the first pair of the bands including the second band, and the second pair of the bands including the third band. [0202] Aspect 25. The scroll compressor of any one of Aspects 21-24, further comprising: a suction inlet in the compression housing, the suction chamber fluidly connecting the suction inlet to an inlet of the compression pockets, a discharge outlet in the compression housing, the discharge chamber fluidly connecting an outlet of the compression pockets to the discharge outlet, a first intermediate injection inlet in the compression housing, the first intermediate injection chamber fluidly connecting the first intermediate injection inlet to the first intermediate injection port in the non-orbiting scroll member, and a second intermediate injection inlet in the compression housing, the second intermediate injection chamber fluidly connecting the second intermediate injection inlet to the second intermediate injection port in the non-orbiting scroll member. [0203] Aspect 26. The scroll compressor of any one of Aspects 20-25, wherein the at least three bands include: a first band that forms a seal between the intermediate injection chambers and the discharge chamber, and a second band that forms a seal between the intermediate injection chambers and the suction chamber. [0204] Aspect 27. The scroll compressor of any one of Aspects 20-26, wherein each of the at least three bands extends from the non-orbiting scroll member to the compressor housing. [0205] Aspect 28. The scroll compressor of any one of Aspects 20-27, wherein each of the at least three bands contacts the non-orbiting scroll member and the compressor housing. [0206] Aspect 29. The scroll compressor of any one of Aspects 20-28, wherein one or more of the at least three bands encircles the non-orbiting scroll member, and one or more of the intermediate injection chambers encircles the non-orbiting scroll member and has an annular shape. [0207] Aspect 30. The scroll compressor of any one of Aspects 20-29, wherein the compressor housing includes an upper portion and a lower portion, the three or more bands including a first band extending from the non-orbiting scroll member to the upper portion of the compressor housing, and the intermediate injection chambers including a first intermediate injection chamber defined by the first band, the upper portion of the compressor housing, and the non-orbiting scroll member. [0208] Aspect 31. The scroll compressor of Aspect 30, wherein the upper portion of the compressor housing is shrink fitted onto the non-orbiting scroll member via the three or more bands. [0209] Aspect 32. A heating, ventilation, air conditioning, and refrigeration (HVACR) system, comprising: a refrigerant circuit including a condenser, an expander, an evaporator, and a scroll compressor fluidly connected, a working fluid flowing through the refrigerant circuit, wherein the scroll compressor includes: a compressor housing containing a suction chamber, a discharge chamber, and intermediate injection chambers, an orbiting scroll member and a non-orbiting scroll member intermeshed to form compression pockets within the compressor housing, the compression pockets configured to suction from the suction chamber and discharge into the discharge chamber, the non-orbiting scroll member including intermediate injection ports fluidly connecting the intermediate injection chambers to the compression pockets, and at least three bands disposed within the compressor housing, each of the at least three bands extending between the non-orbiting scroll member and the compressor housing, and the intermediate injection chambers being defined by pairs of the three or more bands. [0210] Aspect 33. The HVACR system of Aspect 32, wherein the pairs of the three or more bands include: a first pair of the bands, the intermediate injection chambers including a first intermediate injection chamber defined by the first pair of bands, and a second pair of the bands, the intermediate injection chambers including a second intermediate injection chamber defined by the second pair of bands. [0211] Aspect 34. The HVACR system of any one of Aspects 32 and 33, wherein the intermediate injection chambers include a first intermediate injection chamber and a second intermediate injection chamber, and the intermediate injection ports include: a first intermediate injection port fluidly connecting the first intermediate injection chamber to at least one of the compression pockets, and a second intermediate injection port fluidly connecting the second intermediate injection chamber to at least one of the compression pockets. [0212] Aspect 35. The HVACR system of any one of Aspects 32-34, wherein the suction chamber is configured to receive a suction flow of the working fluid, the discharge chamber is configured to receive a discharge flow of the working fluid from compression pockets, and the intermediate injection chambers including a first intermediate injection chamber configured to receive a first intermediate injection flow of the working fluid and a second intermediate injection chamber configured to receive a second intermediate injection flow of the working fluid. [0213] Aspect 36. The HVACR system of Aspect 35, further comprising: a first intermediate injection inlet in the compression housing configured to direct the first intermediate injection flow of the working fluid into the first intermediate injection chamber, the first intermediate injection chamber fluidly connecting the first intermediate injection inlet to the first intermediate injection port in the non-orbiting scroll member, and a second intermediate injection inlet in the compression housing configured to direct the second intermediate injection flow of the working fluid into the second intermediate injection chamber, the second intermediate injection chamber fluidly connecting the second intermediate injection inlet to the second intermediate injection port in the non-orbiting scroll member. [0214] Aspect 37. The HVACR system of any one of Aspects 32-36, further comprising: a suction inlet in the compression housing configured to direct the suction flow of the working fluid into the suction chamber, the suction chamber fluidly connecting the suction inlet to an inlet of the compression pockets, a discharge outlet in the compression housing configured to direct the discharge flow of the working fluid from the discharge chamber out of the compressor, the discharge chamber fluidly connecting an outlet of the compression pockets to the discharge outlet, [0215] Aspect 38. The HVACR system of any one of Aspects 32-37, wherein the suction chamber is configured to receive a suction flow of the working fluid, the discharge chamber is configured to receive a discharge flow of the working fluid from compression pockets, and the intermediate injection chambers including a first intermediate injection chamber configured to receive a first intermediate injection flow of the working fluid and a second intermediate injection chamber configured to receive a second intermediate injection flow of the working fluid. [0216] Aspect 39. A method of making a scroll compressor, comprising: placing an upper portion of a compressor housing over a non-orbiting scroll member, the upper portion of the compressor housing surrounding the non-orbiting scroll member, and at least three bands being disposed between the upper portion of the compressor housing and the non-orbiting scroll member; and interference fitting the upper portion of the compressor housing onto the non-orbiting scroll member via the at least three bands, wherein the interference fitting forms intermediate injection chambers defined by pairs of the at least three bands, the upper portion of the compressor housing, and the non-orbiting scroll member, the intermediate injection chambers fluidly connecting intermediate injection inlets in the compressor housing to intermediate injection ports in the non-orbiting scroll member. [0217] Aspect 40. The method of Aspect 39, further comprising: heating of the upper portion of the compressor housing, prior to placing the upper portion of the compressor housing onto the non-orbiting scroll member, wherein the interference fitting is a shrinking fitting that includes cooling of the upper portion of the compressor housing, which results in the upper portion of the compressor housing being shrink fit onto the non-orbiting scroll member via the at least three bands, the at least three bands being shrink bands. [0218] Aspect 41. A scroll compressor, comprising: a compressor housing containing a suction chamber, a discharge chamber, and one or more intermediate injection chambers; an orbiting scroll member and a non-orbiting scroll member intermeshed to form compression pockets within the compressor housing, the compression pockets configured to suction from the suction chamber and discharge into the discharge chamber, the non-orbiting scroll member including one or more intermediate injection ports fluidly connecting the one or more intermediate injection chambers to at least one of the compression pockets; and bands disposed within the compressor housing, each of the bands extending between the non-orbiting scroll member and the compressor housing, the one or more intermediate injection chambers being defined by the bands. [0219] Aspect 42. A heating, ventilation, air conditioning, and refrigeration (HVACR) system, comprising: a refrigerant circuit including a condenser, an expander, an evaporator, and a scroll compressor fluidly connected, a working fluid flowing through the refrigerant circuit, wherein the scroll compressor includes: a compressor housing containing a suction chamber, a discharge chamber, and one or more intermediate injection chambers, an orbiting scroll member and a non-orbiting scroll member intermeshed to form compression pockets within the compressor housing, the compression pockets configured to suction from the suction chamber and discharge into the discharge chamber, the non-orbiting scroll member including one or more intermediate injection ports fluidly connecting the one or more intermediate injection chambers to at least one of the compression pockets, and bands disposed within the compressor housing, each of the bands extending between the non-orbiting scroll member and the compressor housing, the one or more intermediate injection chambers being defined by the bands. [0220] Aspect 43. A method of making a scroll compressor, comprising: placing an upper portion of a compressor housing over a non-orbiting scroll member, the upper portion of the compressor housing surrounding the non-orbiting scroll member, and bands being disposed between the upper portion of the compressor housing and the non-orbiting scroll member; and interference fitting the upper portion of the compressor housing onto the non-orbiting scroll member via the bands, wherein the interference fitting forms one or more intermediate injection chamber each defined the bands, the upper portion of the compressor housing, and the non-orbiting scroll member, the one or more intermediate injection chambers fluidly connecting one or more intermediate injection inlets in the compressor housing to one or more intermediate injection ports in the non-orbiting scroll member.

[0221] The terminology used herein is intended to describe particular embodiments and is not intended to be limiting. The terms a, an, and the include the plural forms as well, unless clearly indicated otherwise. The terms comprises and/or comprising, when used in this Specification, specify the presence of the stated features, integers, steps, operations, elements, and/or components, but do not preclude the presence or addition of one or more other features, integers, steps, operations, elements, and/or components. In an embodiment, connected and connecting as described herein can refer to being directly connected and directly connecting, and/or contacts and contacting as described herein can refer to directly contacts and directly contacting.

[0222] With regard to the preceding description, it is to be understood that changes may be made in detail, especially in matters of the construction materials employed and the shape, size, and arrangement of parts without departing from the scope of the present disclosure. This Specification and the embodiments described are exemplary only, with the true scope and spirit of the disclosure being indicated by the claims that follow.