COMPRESSOR HAVING SHELL FITTING

Abstract

A compressor includes a shell, a compression mechanism and a fitting. The shell includes an opening and defines a chamber. The compression mechanism is disposed within the chamber of the shell. The fitting is attached to the shell at the opening. Working fluid flowing through the fitting flows to the compression mechanism. The opening is partially defined by a first edge and a second edge. The first edge includes a first planar surface and the second edge includes a second planar surface that faces the first planar surface. A first portion of the fitting extends at least partially into the opening and a second portion of the fitting abuts against the first and second edges.

Claims

1. A compressor comprising: a shell including an opening and defining a chamber; a compression assembly disposed within the chamber of the shell; and a fitting attached to the shell at the opening, working fluid flowing through the fitting flows to the compression assembly, wherein the opening is partially defined by a first edge and a second edge, the first edge includes a first planar surface and the second edge includes a second planar surface that faces the first planar surface, a first portion of the fitting extends at least partially into the opening and a second portion of the fitting abuts against the first and second edges.

2. The compressor of claim 1, wherein the opening is a non-circular shape.

3. The compressor of claim 1, wherein the opening has opposing arcuate surfaces, and wherein an outer diametrical surface of the fitting abuts against at least one of the opposing arcuate surfaces.

4. The compressor of claim 3, wherein the opposing arcuate surfaces and the first and second edges cooperate to define a circular shape.

5. The compressor of claim 1, wherein the fitting is a suction fitting, and wherein working fluid flowing through the suction fitting flows to the compression assembly.

6. The compressor of claim 1, wherein the first portion of the fitting is a first portion of an axial end surface of the fitting and the second portion of the fitting is a second portion of the axial end surface of the fitting.

7. The compressor of claim 1, wherein the opening has opposing arcuate surfaces, and wherein the opposing arcuate surfaces and the first and second edges cooperate to define a rounded shape.

8. The compressor of claim 1, wherein the opening has opposing arcuate surfaces, and wherein each of the first and second edges are disposed between the opposing arcuate surfaces.

9. The compressor of claim 1, wherein the second portion of the fitting abuts against the first and second edges to prevent an outer diametrical surface of the fitting from contacting the first and second planar surfaces.

10. The compressor of claim 1, wherein the second portion of the fitting abuts against the first and second edges to prevent the second portion of the fitting from extending into the chamber of the shell.

11. The compressor of claim 1, wherein the second portion of the fitting abuts against the first and second edges at a location external to the opening.

12. A compressor comprising: a shell including an opening and defining a chamber; a compression assembly disposed within the chamber of the shell; and a fitting attached to the shell at the opening and at least partially disposed outside of the shell, wherein working fluid flows between the fitting and the compression assembly, wherein the opening is partially defined by a first edge having a first planar surface, a second edge having a second planar surface, and an arcuate surface disposed between the first and second planar surfaces, and wherein the first and second edges prevent the fitting from contacting the first and second planar surfaces and allow the fitting to contact the arcuate surface.

13. The compressor of claim 12, wherein the opening has another arcuate surface that is opposite the arcuate surface, and wherein an outer diametrical surface of the fitting abuts against at least one of the opposing arcuate surfaces.

14. The compressor of claim 12, wherein a first portion of the fitting extends at least partially into the opening and a second portion of the fitting abuts against the first and second edges at a location external to the opening.

15. The compressor of claim 12, wherein the fitting includes a first axial end having a first thickness and a second axial end having a second thickness, the first thickness greater than the second thickness, and wherein the first axial end includes a first portion that extends at least partially into the opening and a second portion that contacts the first and second edges.

16. The compressor of claim 15, wherein the first axial end has a first outer diametrical surface and the second axial end has a second outer diametrical surface, and wherein a first diameter of the first outer diametrical surface is greater than a second diameter of the second outer diametrical surface.

17. The compressor of claim 16, wherein the fitting has a transition portion positioned between the first axial end and the second axial end and having a third outer diametrical surface, and wherein a third diameter of the third outer diametrical surface is smaller than the first and second diameters.

18. The compressor of claim 12, wherein the fitting is made of steel and has a first axial end and a second axial end, and wherein the first axial end is attached to the shell and the second axial end has a copper plating coating.

19. (canceled)

20. (canceled)

Description

DRAWINGS

[0028] The drawings described herein are for illustrative purposes only of selected embodiments and not all possible implementations, and are not intended to limit the scope of the present disclosure.

[0029] FIG. 1 is a cross-sectional view of a compressor having a suction fitting according to the principles of the present disclosure;

[0030] FIG. 2 is a perspective view of a shell of the compressor of FIG. 1 with the suction fitting attached thereto;

[0031] FIG. 3 is a perspective view of the shell of the compressor of FIG. 1 with the suction fitting exploded therefrom;

[0032] FIG. 4 is a cross-sectional view of the shell of the compressor taken along line 4-4 of FIG. 2;

[0033] FIG. 5 is a partial cross-sectional view of the shell of the compressor with the suction fitting exploded therefrom;

[0034] FIG. 6 is a partial cross-sectional view of the shell of the compressor with the suction fitting attached thereto;

[0035] FIG. 7 is a cross-sectional view of the shell of the compressor taken along line 7-7 of FIG. 2;

[0036] FIG. 8 is a partial perspective view of the shell of the compressor with the suction fitting attached thereto; and

[0037] FIG. 9 is another partial perspective view of the shell of the compressor with the suction fitting attached thereto.

[0038] Corresponding reference numerals indicate corresponding parts throughout the several views of the drawings.

DETAILED DESCRIPTION

[0039] Example embodiments will now be described more fully with reference to the accompanying drawings.

[0040] Example embodiments are provided so that this disclosure will be thorough, and will fully convey the scope to those who are skilled in the art. Numerous specific details are set forth such as examples of specific components, devices, and methods, to provide a thorough understanding of embodiments of the present disclosure. It will be apparent to those skilled in the art that specific details need not be employed, that example embodiments may be embodied in many different forms and that neither should be construed to limit the scope of the disclosure. In some example embodiments, well-known processes, well-known device structures, and well-known technologies are not described in detail.

[0041] The terminology used herein is for the purpose of describing particular example embodiments only and is not intended to be limiting. As used herein, the singular forms “a,” “an,” and “the” may be intended to include the plural forms as well, unless the context clearly indicates otherwise. The terms “comprises,” “comprising,” “including,” and “having,” are inclusive and therefore specify the presence of 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, components, and/or groups thereof. The method steps, processes, and operations described herein are not to be construed as necessarily requiring their performance in the particular order discussed or illustrated, unless specifically identified as an order of performance. It is also to be understood that additional or alternative steps may be employed.

[0042] When an element or layer is referred to as being “on,” “engaged to,” “connected to,” or “coupled to” another element or layer, it may be directly on, engaged, connected or coupled to the other element or layer, or intervening elements or layers may be present. In contrast, when an element is referred to as being “directly on,” “directly engaged to,” “directly connected to,” or “directly coupled to” another element or layer, there may be no intervening elements or layers present. Other words used to describe the relationship between elements should be interpreted in a like fashion (e.g., “between” versus “directly between,” “adjacent” versus “directly adjacent,” etc.). As used herein, the term “and/or” includes any and all combinations of one or more of the associated listed items.

[0043] Although the terms first, second, third, etc. may be used herein to describe various elements, components, regions, layers and/or sections, these elements, components, regions, layers and/or sections should not be limited by these terms. These terms may be only used to distinguish one element, component, region, layer or section from another region, layer or section. Terms such as “first,” “second,” and other numerical terms when used herein do not imply a sequence or order unless clearly indicated by the context. Thus, a first element, component, region, layer or section discussed below could be termed a second element, component, region, layer or section without departing from the teachings of the example embodiments.

[0044] Spatially relative terms, such as “inner,” “outer,” “beneath,” “below,” “lower,” “above,” “upper,” and the like, may be used herein for ease of description to describe one element or feature's relationship to another element(s) or feature(s) as illustrated in the figures. Spatially relative terms may be intended to encompass different orientations of the device in use or operation in addition to the orientation depicted in the figures. For example, if the device in the figures is turned over, elements described as “below” or “beneath” other elements or features would then be oriented “above” the other elements or features. Thus, the example term “below” can encompass both an orientation of above and below. The device may be otherwise oriented (rotated 90 degrees or at other orientations) and the spatially relative descriptors used herein interpreted accordingly.

[0045] As shown in FIG. 1, a compressor 10 is provided and may include a hermetic shell assembly 12, first and second bearing housing assemblies 14, 16, a motor assembly 18, a compression mechanism 20, a discharge port or fitting 24 and a suction port or fitting 28.

[0046] As shown in FIG. 1, the shell assembly 12 may form a compressor housing and may include a cylindrical shell 32, an end cap 34 at an upper end thereof, a transversely extending partition 36, and a base 38 at a lower end thereof. The shell 32 and the base 38 may cooperate to define a suction-pressure chamber 39. The end cap 34 and the partition 36 may define a discharge-pressure chamber 40. The partition 36 may separate the discharge-pressure chamber 40 from the suction-pressure chamber 39. A discharge-pressure passage 43 may extend through the partition 36 to provide communication between the compression mechanism 20 and the discharge-pressure chamber 40.

[0047] The first bearing housing assembly 14 may be disposed within the suction-pressure chamber 39 and may be fixed relative to the shell 32. The first bearing housing assembly 14 may include a first main bearing housing 48 and a first bearing 49. The first main bearing housing 48 may house the first bearing 49 therein. The first main bearing housing 48 may fixedly engage the shell 32 and may axially support the compression mechanism 20.

[0048] As shown in FIG. 1, the motor assembly 18 may be disposed within the suction-pressure chamber 39 and may include a stator 60 and a rotor 62. The stator 60 may be press fit into the shell 32. The rotor 62 may be press fit on a drive shaft 64 and may transmit rotational power to the drive shaft 64. The drive shaft 64 may be rotatably supported by the first and second bearing housing assemblies 14, 16. The drive shaft 64 may include an eccentric crank pin 66 having a crank pin flat.

[0049] The compression mechanism 20 may be disposed within the suction-pressure chamber 39 and may include an orbiting scroll 70 and a non-orbiting scroll 72. The first scroll member or orbiting scroll 70 may include an end plate 74 and a spiral wrap 76 extending therefrom. A cylindrical hub 80 may project downwardly from the end plate 74 and may include the first bearing 49 and an unloader bushing 82 disposed therein. The crank pin flat may drivingly engage a flat surface in a portion of the inner bore to provide a radially compliant driving arrangement. An Oldham coupling 84 may be engaged with the orbiting scroll 70 and the bearing housing 48 to prevent relative rotation therebetween.

[0050] As shown in FIG. 1, the second scroll member or non-orbiting scroll 72 may include an end plate 86 and a spiral wrap 88 projecting downwardly from the end plate 86. The spiral wrap 88 may meshingly engage the spiral wrap 76 of the orbiting scroll 70, thereby creating a series of moving fluid pockets. The fluid pockets defined by the spiral wraps 76, 88 may decrease in volume as they move from a radially outer position (at a suction pressure) to a radially intermediate position (at an intermediate pressure) to a radially inner position (at a discharge pressure) throughout a compression cycle of the compression mechanism 20.

[0051] As shown in FIGS. 1-9, the suction fitting 28 may be a single, unitary component. The suction fitting 28 may provide working fluid at a suction-pressure from the suction fitting 28 to a suction inlet 89 of the non-orbiting scroll 72 so that the working fluid can be directed into the radially outermost fluid pocket and subsequently compressed by the compression mechanism 20. The suction fitting 28 may be axially misaligned with the suction inlet 89 of the non-orbiting scroll 72. For example, the suction fitting 28 may be disposed vertically lower than the suction inlet 89. The suction fitting 28 may be generally cylindrical and may be made of a metallic material (e.g., steel), for example. The suction fitting 28 may be attached to the shell 32 at an opening 90 thereof and may also extend at least partially into the opening 90.

[0052] As shown in FIG. 3, the opening 90 may be a non-circular shape and may be defined by a first edge 92, a second edge 94, a first arcuate surface 96 and a second arcuate surface 98. As shown in FIGS. 4 and 7, the first and second edges 92, 94 prevent the suction fitting 28 from extending into the suction-pressure chamber 39. That is, the suction fitting 28 contacts each edge, 92, 94 at a location external to the opening 90 such that the suction fitting 28 is prevented from extending into the suction-pressure chamber 39. The first edge 92 may have a first planar surface 100 and the second edge 94 may oppose the first edge 92 and have a second planar surface 102. The second planar surface 102 may face the first planar surface 100. It should also be understood that the outer surfaces 99, proximate the first and second edges 92, 94, prevent the suction fitting 28 from contacting the first planar surface 100 and the second planar surface 102.

[0053] The first arcuate surface 96 and the second arcuate surface 98 are opposite each other and may cooperate with the first and second edges 92, 94 to define a circular shape. Each of the first and second arcuate surfaces 96, 98 are positioned between the first and second edges 92, 94 (FIGS. 3-5 and 7). As shown in FIG. 4, when the suction fitting 28 is received in the opening 90, the suction fitting 28 abuts against (i.e., contacts) the first and second arcuate surfaces 96, 98. In this way, the suction fitting 28 is prevented from moving in an axial direction (up or down relative to the shell 32) or in a tangential direction (side to side relative to the shell 32). A length of each of the first and second arcuate surfaces 96, 98 is greater than a length of each of the first and second planar surfaces 100, 102.

[0054] The suction fitting 28 may include a shell-attachment section 106, a pipe-attachment section 108 and a transition section 110. The shell-attachment section 106 may have a thickness that is greater than a thickness of the pipe-attachment section 108 and a thickness of the transition section 110. The shell-attachment section 106 has a first outer diametrical surface 112 and a first inner diametrical surface 114. As shown in FIGS. 4 and 6, an axial end 115 of the shell-attachment section 106 is coupled to (i.e., welded) the shell 32 such that the first outer diametrical surface 112 contacts the first and second arcuate surfaces 96, 98 and an axial end surface 116 contacts the first and second edges, 94, 96 (at a location external to the opening 90). Stated differently, a portion of the axial end 115 of the shell-attachment section 106 extends at least partially into the opening 90 such that only a portion of the axial end surface 116 contacts the outer surfaces 99 of the edges 92, 94 and only a portion of the first outer diametrical surface 112 contacts the first and second arcuate surfaces 96, 98. The edges 92, 94 prevent the shell-attachment section 106 from extending through the opening 90 and into the suction-pressure chamber 39.

[0055] The pipe-attachment section 108 may be copper plated and may be attached to an external pipe (not shown) via brazing, for example, so that fluid flowing through the external pipe may flow to the compression pockets (via the suction fitting 28, the suction-pressure chamber 39 and the suction inlet 89). The pipe-attachment section 108 has a second outer diametrical surface 118 and a second inner diametrical surface 120. As shown in FIG. 4, a diameter D1 of the second outer diametrical surface 118 is smaller than a diameter D2 of the first outer diametrical surface 112. A diameter D3 of the second inner diametrical surface 120 is smaller than a diameter D4 of the first inner diametrical surface 114.

[0056] The transition section 110 is positioned between the shell-attachment section 106 and the pipe-attachment section 108 and has a third outer diametrical surface 122 and a third inner diametrical surface 124. A diameter D5 of the third outer diametrical surface 122 is smaller than the diameter D2 of the first outer diametrical surface 112 and the diameter D1 of the second outer diametrical surface 118. A diameter D6 of the third inner diametrical surface 124 is smaller than the diameter D4 of the first inner diametrical surface 114 and the diameter D3 of the second inner diametrical surface 120.

[0057] One of the benefits of the compressor 10 of the present disclosure is the suction fitting 28 having varying thicknesses facilitates attachment to both the shell 32 and the external pipe (not shown). That is, the thickness of the shell-attachment section 106 facilitates welding the suction fitting 28 and the shell 32 and the thickness of the pipe-attachment section 108 facilitates brazing the suction fitting 28 and the external pipe. Stated differently, it is advantageous for the shell-attachment section 106 of the suction fitting 28 to have a large thickness to facilitate welding the suction fitting 28 to the shell 32, and it is advantageous for the pipe-attachment section 108 of the suction fitting 28 to have a small thickness to facilitate brazing the suction fitting 28 to the external pipe. Another benefit of the compressor 10 of the present disclosure is the opening 90 of the shell 32 being defined at least partially by the first and second edges 92, 94 and the arcuate surfaces 96, 98 facilitates positioning of the suction fitting 28 relative to the shell 32 and facilitates attachment (i.e., welding) of the suction fitting 28 to the shell 32.

[0058] It should be understood that other fittings of the compressor 10 may be attached to a respective opening in the shell assembly 12 having similar or identical features or characteristics of the opening 90 that the suction fitting 28 is attached to. For example, the discharge fitting 24 and/or a fluid-injection fitting (a fitting that provides working fluid directly to an intermediate position of the compression pockets) may be attached to the shell assembly 12 at a respective opening partially defined by opposing edges similar or identical to the edges 92, 94 and/or opposing arcuate surfaces similar or identical to the arcuate surfaces 96, 98. In other words, the discharge fitting 24 and/or fluid-injection fitting could have features similar or identical to the suction fitting 28 described above and shown in the figures, and the discharge fitting 24 and/or fluid-injection fitting could be attached to the shell assembly 12 at respective openings similar or identical to the opening 90.

[0059] The foregoing description of the embodiments has been provided for purposes of illustration and description. It is not intended to be exhaustive or to limit the disclosure. Individual elements or features of a particular embodiment are generally not limited to that particular embodiment, but, where applicable, are interchangeable and can be used in a selected embodiment, even if not specifically shown or described. The same may also be varied in many ways. Such variations are not to be regarded as a departure from the disclosure, and all such modifications are intended to be included within the scope of the disclosure.