PRESSURE EXCHANGER WITH FLOW DIVIDER IN ROTOR DUCT

Abstract

A pressure exchanger includes a rotor including rotor ducts that extend parallel to each other. The pressure exchanger further includes a flow divider that has a substantially flat shape and is located in the rotor ducts, where the flow divider partitions an inner space of one of the rotor ducts into flow paths configured to communicate fluid. The flow divider defines an aspect ratio of each of the plurality of flow paths, where the aspect ratio is a ratio of a width of one of the flow paths in a radial direction with respect to an axial length of one of the flow paths in the axial direction.

Claims

1. A pressure exchanger comprising: a rotor configured to rotate about an axis, the rotor defining a plurality of rotor ducts extending parallel to the axis, each rotor duct extending between a first side surface and a second side surface of the rotor that are spaced apart from each other in an axial direction, wherein the rotor is configured to communicate a first fluid through the first side surface of the rotor and to communicate a second fluid through the second side surface of the rotor; and a flow divider that has a substantially flat shape and that is located in one or more of the plurality of rotor ducts, the flow divider partitioning an inner space of one of the plurality of rotor ducts into a plurality of flow paths that are configured to communicate at least one of the first fluid or the second fluid, wherein the flow divider defines an aspect ratio of each of the plurality of flow paths, the aspect ratio being a ratio of a width of one of the plurality of flow paths in a radial direction with respect to an axial length of the one of the plurality of flow paths in the axial direction.

2. The pressure exchanger of claim 1, wherein each of the plurality of flow paths has an equal aspect ratio.

3. The pressure exchanger of claim 2, wherein each of the plurality of flow paths has an equal cross-sectional area.

4. The pressure exchanger of claim 3, wherein each of the plurality of flow paths has the same width and the same axial length.

5. The pressure exchanger of claim 1, wherein an axial length of the flow divider is less than a rotor length of the rotor in the axial direction.

6. The pressure exchanger of claim 5, wherein the rotor length is greater than the axial length of each of the plurality of flow paths in the axial direction, and wherein the flow divider comprises: a first axial end surface that is spaced apart from and recessed relative to the first side surface of the rotor in the axial direction; and a second axial end surface that is spaced apart from and recessed relative to the second side surface of the rotor in the axial direction.

7. The pressure exchanger of claim 1, further comprising a plurality of flow dividers including the flow divider, the plurality of flow dividers being located inside the plurality of rotor ducts, respectively.

8. The pressure exchanger of claim 7, wherein the plurality of flow dividers comprise a first and second flow dividers that are located inside the one of the plurality of rotor ducts and that define three or more flow paths in the one of the plurality of rotor ducts.

9. The pressure exchanger of claim 8, wherein the first flow divider comprises a first plate, and the second flow divider comprises a second plate that intersects the first plate.

10. The pressure exchanger of claim 9, wherein a radial width of each of the first plate and the second plate is less than or equal to a diameter of the one of the plurality of rotor ducts, and wherein an axial length of each of the first plate and the second plate is equal to the axial length of the plurality of flow paths in the axial direction.

11. The pressure exchanger of claim 10, wherein the plurality of flow dividers further comprise a third flow divider located inside the one of the plurality of rotor ducts, the third flow divider including a third plate that intersects the first flow divider and the second flow divider, and wherein a radial width of the third plate and the radial width of each of the first plate and the second plate are equal to a radius of the one of the plurality of rotor ducts.

12. The pressure exchanger of claim 1, wherein the one of the plurality of rotor ducts comprises: a step portion defined in the one of the plurality of rotor ducts; a first rotor portion that extends from the first side surface of the rotor to the step portion; and a second rotor portion that extends from the second side surface of the rotor to the step portion, and wherein the flow divider is one of a plurality of flow dividers that are located in the first rotor portion and the second rotor portion.

13. The pressure exchanger of claim 12, wherein the plurality of flow dividers comprise: a first flow divider that is located in and extends along the first rotor portion, the first flow divider having a first inner end that faces the step portion; and a second flow divider that is located in and extends along the second rotor portion, the second flow divider having a second inner end that faces the first inner end and the step portion.

14. The pressure exchanger of claim 13, wherein the aspect ratio is defined by a width of the first flow divider or the second flow divider in the radial direction with respect to a sum of axial lengths of the first flow divider and the second flow divider.

15. The pressure exchanger of claim 14, wherein the width of the first flow divider is different from the width of the second flow divider, and the axial length of the first flow divider is different from the axial length of the second flow divider.

16. The pressure exchanger of claim 1, wherein the rotor is made of ceramic, and wherein the flow divider is made of a plastic material and in contact with the one of the plurality of rotor ducts.

17. The pressure exchanger of claim 16, wherein the flow divider is coupled to an inner surface of the one of the plurality of rotor ducts by friction without an adhesive.

18. The pressure exchanger of claim 16, wherein the flow divider is coupled to an inner surface of the one of the plurality of rotor ducts by friction and with an adhesive.

19. The pressure exchanger of claim 1, further comprising: a first end cover located at the first side surface of the rotor, the first end cover defining a first pair of apertures configured to communicate the first fluid; and a second end cover located at the second side surface of the rotor, the second end cover defining a second pair of apertures configured to communicate the second fluid having, wherein the flow divider comprises: a first end that faces the first end cover and is spaced apart from the first end cover in the axial direction, and a second end that faces the second end cover and is spaced apart from the second end cover in the axial direction.

20. The pressure exchanger of claim 1, wherein a duct length of each of the plurality of rotor ducts in the axial direction is greater than the axial length of the plurality of flow paths.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

[0024] FIG. 1 is a circular cross-sectional view showing an example of a pressure exchanger in related art.

[0025] FIG. 2 is a perspective view showing an example of a pressure exchanger according to the present disclosure.

[0026] FIG. 3 is a perspective view showing an example of a rotor of the pressure exchanger and examples of flow dividers according to the present disclosure.

[0027] FIGS. 4A to 4C are views showing examples of flow divider structures.

[0028] FIG. 5 is a cross-sectional view showing an example of a rotor duct including split flow dividers that accommodate duct manufacturing offsets.

[0029] Like reference symbols in the various drawings indicate like elements.

DETAILED DESCRIPTION

[0030] One or more implementations of the present disclosure will be described below. These described implementations are only exemplary of the present disclosure. As discussed in detail below, the described implementations relate generally to a rotary pressure exchanger including a plurality of rotor ducts defined in a rotor.

[0031] The present disclosure describes one or more examples of flow dividers that are located inside the rotor duct to reduce a dead volume in the rotor of the pressure exchanger and to increase flow capacity of the pressure exchanger.

[0032] FIG. 1 is a circular cross-sectional view showing an example of operation of a pressure exchanger in related art.

[0033] For instance, the pressure exchanger includes a rotor 5 located between a pair of end covers 14 and 15 that face high-pressure streams and low-pressure streams. The end covers 14 and 15 include sealing areas 8 and 9 that are disposed at central areas of the end covers, respectively. The rotor 5 may include multiple rotor ducts that extend through an inside of the rotor 5. The rotor 5 may be located between the high-pressure and low-pressure streams and configured to rotate about an axis passing through the sealing areas 8 and 9.

[0034] The end cover 14 may define a plurality of apertures connected to an inlet duct 12 and an outlet duct 13. For example, the end cover 14 includes a first aperture connected to the inlet duct 12 and configured to receive a low pressure seawater feed 1 having C.sub.1 salinity (i.e., concentration of salt), and a second aperture connected to the outlet duct 13 and configured to discharge a high pressure seawater output 3 having C.sub.1 salinity.

[0035] The end cover 15 may define a plurality of apertures connected to an inlet duct 10 and an outlet duct 11. For example, the end cover 15 includes a first aperture connected to the inlet duct 10 and configured to receive a high pressure brine feed 4 having C.sub.0 salinity, and a second aperture connected to the outlet duct 11 and configured to discharge a low pressure brine water output 2 having C.sub.0 salinity. The salinity (C.sub.0) of the brine water feed 4 may be greater than the salinity (C.sub.1) of the seawater feed 1.

[0036] The seawater feed 1 may, while moving in a direction from the sealing area 9 toward the end cover 15, gradually move a dead volume 6 in the rotor 5 toward the end cover 15. For example, the dead volume 6 may constitute about 40% of an overall duct volume of the rotor 5 and remain in the rotor 5. Based on rotation of the rotor 5, the dead volume 6 may, while moving toward the end cover 15, displace the brine volume 7 in the rotor 5 through the low pressure outlet duct 11. The displacement volume may constitute about 60% of the overall duct volume.

[0037] As shown in FIG. 1, the dead volume 6 may separate the different streams and remain in the rotor ducts, while oscillating back and forth along the axis of the rotor 5 for each revolution of the rotor 5. For example, the dead volume may separate the seawater feed 1 and the brine water output 2, and separate the brine water feed 4 and seawater output 3. The dead volume 6 may define a salinity gradient having salinity C.sub.0 at the brine interface of the dead volume and salinity C.sub.1 at the seawater interface of the dead volume. For example, FIG. 1 illustrates a plurality of portions of the dead volume 6 in the rotor ducts in gray scale. The dead volume 6 may secure a low mixing transfer between brine water and seawater.

[0038] FIG. 2 is a perspective view showing an example of a pressure exchanger according to the present disclosure.

[0039] In some implementations, a pressure exchanger 200 can include a rotor 210, a first end cover 220, and a second end cover 230. The first end cover 220 comprises at least one high pressure inlet 240 configured to receive a first stream of high pressure liquid. The first stream can have a first concentration. The first end cover 220 can further include at least one low pressure outlet 250 through which the first stream flows out of the pressure exchanger 200. In some cases, the pressure exchanger 200 can include a rod 270 that holds the rotor 210 and end covers 220 and 230 together. The rod 270 may include or serve as a shaft that defines an axis 201 of rotation of the rotor 210. For instance, the rotor 210 can rotate about the axis 201 in one or both of a clockwise direction and a counterclockwise direction. The rotor 210 and the end covers 220 and 230 can communicate first fluid and second fluid, which is similar to the operation of the rotor 5 and the end covers 14 and 15 described above with FIG. 1.

[0040] The rotor 210 can rotate relative to the end covers 220 and 230 by various driving mechanisms. For example, the rotor 210 may mechanically rotate about a shaft (e.g., rod 270) that extends along the axis 201. The shaft may be rotated by a driving device such as a motor. In some implementations, the rotor 210 (or the shaft of the rotor 210) can be configured to rotate by a flow entering to the rotor 210. For instance, the pressure exchanger 200 can further include a ramp structure that includes an inclined surface with respect to the axis 201. The inclined surface of the ramp structure can be configured to face and contact incoming flow streams. Based on pressure of the incoming flow streams applied to the inclined surface of the ramp structure, the rotor 210 can rotate about the shaft relative to the end covers 220 and 230.

[0041] In some implementations, a rotation speed of the rotor 210 can be determined based on the arrangement of the incline surface of the ramp structure. For example, the rotation speed of the rotor 210 may be determined based on increasing or decreasing an inclined angle of the incline surface with respect to the axis 201. In some examples, the rotation speed of the rotor 210 may be determined based on increasing or decreasing an area or a number of the incline surfaces arranged in the ramp structure. In some examples, the rotation speed of the rotor 210 may vary based on a pattern of the inclined surface of the ramp structure.

[0042] Alternatively or in addition, the rotation speed of the rotor 210 can be controlled by adjusting a flow rate or pressure of the incoming streams. For example, the rotation speed of the rotor 210 can be increased based on an increase of the flow rate of the incoming stream to the end cover 220. The rotation speed of the rotor 210 can be decreased based on a decrease of the flow rate of the incoming stream to the end cover 220. In this example, the rotation speed of the rotor 210 depends on the flow rate of the incoming stream to the end cover 220.

[0043] In some implementations, the rotation speed of the rotor 210 can be controlled independent of the flow rate of the incoming stream. For example, the rotor 210 can be rotated by a separate driving device such as a motor. In another example, one or more components of the pressure exchanger 200 may be replaced to adjust the rotation speed of the rotor 210 while keeping the same flow rate of the incoming stream. In particular, the end cover 220, the end cover 230, rotor 210, or the ramp structure having the inclined surface can be replaced to adjust the rotation speed of the rotor 210. In some examples, the end cover 220 and the end cover 230 may include the ramp structure having the inclined surface.

[0044] In some implementations, the rotor 210, the end covers 220 and 230, and the rod 270 or another axle may be made of a corrosion resistant material, such as ceramic. For example, the end covers, rotor, and/or axle may be made of Alumina ceramic (aluminum oxide ceramic), including 92% to 99.8% aluminum oxide ceramic, for example. In some cases, the end covers, rotor, and/or axle may be made of Alumina ceramic including 99.8% aluminum oxide ceramic.

[0045] FIG. 3 is a perspective view showing an example of a rotor of the pressure exchanger and examples of flow dividers.

[0046] For example, the rotor 210 can includes multiple rotor ducts 202 that extend parallel to the axis 201, where each rotor duct 202 extends between a first side surface 211 and a second side surface 212 of the rotor 210. The first side surface 211 and the second side surface 212 are spaced apart from each other in an axial direction of the axis 201. As explained above, the rotor 210 can be configured to rotate about the axis 201 and communicate a first fluid through the first side surface 211 of the rotor 210 and a second fluid through the second side surface 212 of the rotor 210.

[0047] The pressure exchanger 200 can include a plurality of flow dividers having a non-tubular shape. For example, the flow dividers can have a substantially flat shape (e.g., a plate shape). FIG. 3 illustrates three flow dividers or plates 203, 204, and 205, for example, but the pressure exchanger 200 can include more or less flow dividers in other implementations. In some implementations, each of the rotor ducts 202 can include one or more flow dividers therein that extend through each rotor ducts 202.

[0048] The flow divider 203 represents a first insertion position in which the flow divider 203 is partially inserted into one of the rotor ducts 202. The flow divider 204 represents a second insertion position in which the flow divider 204 is further pushed into one of the rotor ducts 202 and makes surface alignment or flush with the first side surface 211. In some cases, the second insertion position may be a final position of the flow divider 204. In some implementations, the second insertion position is not a final position of the flow divider 204.

[0049] For example, the flow divider 205 represents a third insertion position in which the flow divider 205 is further pushed into one of the rotor ducts 202 and its end positioned slightly below or recessed relative to the first side surface 211. That is, the flow divider 205 has a first axial end surface that is spaced apart from and recessed relative to the first side surface 211 in the axial direction. The flow divider 205 can further include a second axial end surface that is spaced apart from and recessed relative to the second side surface 212 of the rotor 210 in the axial direction.

[0050] In some examples, the third insertion position of the flow divider 205 can be the final position of each of the flow dividers to avoid any mechanical contact or interference with the opposing end cover 220 or 230 (see FIG. 2). Thus, the rotor 210 can rotate relative to the end covers 220 and 230 without interference with the flow dividers in their final positions inside the rotor ducts 202. For instance, an axial length of the flow divider 205 can be less than a rotor length (“L”) of the rotor 210 in the axial direction such that the axial ends of the flow divider 205 are recessed relative to the first side surface 211 and the second side surface 212, respectively.

[0051] In some implementations, where the rotor 210 is made of ceramic as described above, the flow dividers can be made of plastic or composite materials. The flow dividers can be held in place by friction force against inner surfaces of the rotor ducts 202, and, in some examples, aided with an adhesive or glue.

[0052] The flow divider can partition each rotor duct 202 into multiple equal resistance flow elements or paths without any sealing or structural support function. The flow dividers 203, 204, and 205 can reduce an aspect ratio of the flow elements to thereby reduce mixing of the fluid streams inside the rotor duct 202 and increase a utilization of the rotor space without increasing a rotation speed of the rotor 210.

[0053] For example, the flow divider 205 can define an aspect ratio of two flow paths defined in the rotor duct 202. Specifically, the aspect ratio can be a ratio of a width of one flow path in a radial direction with respect to an axial length of the flow path in the axial direction. The width can be less than or equal to a diameter of one rotor duct 202, and the length can be less than or equal to the rotor length L. In some examples, each of the plurality of flow paths can have an equal width or define an equal cross-sectional area. In addition, each of the plurality of flow paths can have an equal axial length to thereby define an equal aspect ratio for the plurality of flow paths.

[0054] FIGS. 4A to 4C are views showing various examples of flow divider structures disposed in a rotor duct.

[0055] FIG. 4A illustrates an example of a flow divider including a single wall or plate 41 that divides the rotor duct 202 into two equal resistance flow paths 42. In this example, each flow path 42 can have an equal cross-section area, for example, a half of a circle area defined by the rotor duct 202. A radial width of each flow path 42 can be between a radius and a diameter of the circle area defined by the rotor duct 202. In some cases, the aspect ratio can be determined based on an effective diameter of a virtual circle that has the same area as the cross-section area of one flow path. For example, referring to FIG. 4A, the effective diameter of the virtual circle can be 1/√{square root over (2)} of the diameter of the circle area defined by the rotor duct 202. In some implementations, each of flow path 42 can apply an equal flow resistance to the fluid streams such that the fluid streams flow with an equal flow velocity when an equal pressure difference is applied to axial ends of each flow path 42. This is one of important conditions to maximize flow capacity without increasing mixing between the fluid streams in the rotor duct 202.

[0056] FIG. 4B illustrates an example of a flow divider having a hub structure including three plates or walls 43 that define three equal resistance flow paths 44. In some examples, the flow divider structure can be symmetrical with respect to a diameter of the circle area defined by the rotor duct 202. In the example shown in FIG. 4B, the effective diameter of the virtual circle can be 1/√{square root over (3)} of the diameter of the circle area defined by the rotor duct 202 because each of the pie-shaped areas has ⅓ of the circle area defined by the rotor duct 202. The effective diameter of the virtual circle can be used to determine the aspect ratio of the flow paths 44. In some implementations, each of flow path 44 can apply an equal flow resistance to the fluid streams such that the flow streams flow with an equal flow velocity when an equal pressure difference is applied to axial ends of each flow path 44.

[0057] In some examples, the flow divider structure may not be symmetrical but rather be adapted to the actual shape of the rotor duct 202. For instance, the rotor duct 202 can have a non-circular shape, and the flow dividers can be arranged to define a plurality of flow paths that have an equal cross-sectional area regardless of the shape or symmetricity of each of the plurality of flow paths. In some implementations, the flow divider structure can include an increased number of flow dividers. For example, one rotor duct 202 can include a flow divider that includes three or more flow divider portions or walls therein (e.g., FIGS. 4B and 4C).

[0058] FIG. 4C illustrates an example of a flow divider including four plates or walls 45 that define four equal resistance flow paths 46. In the example shown in FIG. 4C, the effective diameter can be ½ of the diameter of the circle area defined by the rotor duct 202 because each of the pie-shaped area has ¼ of the circle area defined by the rotor duct 202. The effective diameter of the virtual circle can be used to determine the aspect ratio of the flow paths 46. In some implementations, each flow path 46 can apply an equal flow resistance to the fluid streams such that the fluid streams flow with an equal flow velocity when an equal pressure difference is applied to axial ends of each flow path 46.

[0059] FIG. 5 is a cross-sectional view showing an example of a rotor duct including split flow dividers that accommodate duct manufacturing offsets. For examples, FIG. 5 illustrates a cross-section area of a rotor duct 213 including a step portion 214 that can be generated from machining of the rotor duct 213. For example, the step portion 214 can be generated at a position halfway from both ends of the rotor duct 213.

[0060] In some examples, a misalignment of a boring process of the rotor duct 213 may result in the step portion 214. In particular, the boring process can be performed from the first side surface 211 toward the second side surface 212 and then performed from the second side surface 212 toward the first side surface 211. In some cases, the boring process can be simultaneously performed from the first side surface 211 and the second side surface 212 toward the opposing side surfaces. The step portion 214 can be generated if the boring process from the side surfaces are performed along two axes that are slightly offset from each other.

[0061] In some examples, the misalignment of the boring process can vary from one rotor duct to another. For example, a location of the step portion 214 relative to the side surface 211 and 212 can vary from one rotor duct to another. In some cases, a step depth of the step portion 214 can vary, as well, from one rotor duct to another.

[0062] In some implementations, the flow divider can include two or more separate flow dividers 52 and 54 inserted from each end of the rotor duct 213 to accommodate the misalignment or variation of the boring process. For example, the rotor duct 213 includes the step portion 214, a first rotor portion that extends from the first side surface 211 to the step portion 214, and a second rotor portion that extends from the second side surface 212 to the step portion 214. The first flow divider 52 can be located in and extend along the first rotor portion (e.g., the right part of the step portion 214 in FIG. 5), and the first flow divider 52 has a first inner end that faces the step portion 214. The second flow divider 54 can be located in and extend along the second rotor portion (e.g., the left part of the step portion 214 in FIG. 5), and the second flow divider 54 has a second inner end that faces the first inner end and the step portion 214.

[0063] In some implementations, an outer end of at least one of the first flow divider 52 or the second flow divider 54 may be spaced apart from the corresponding side surface 211 or 212. For example, the outer end of each of the first flow divider 52 and the second flow divider 54 can be recessed relative to the corresponding side surfaces 211 and 212 by a distance “d.” In some cases, the aspect ratio can be defined as D/k(L−2d), where D denotes an inner diameter of the rotor duct 213, and k denotes an adjustment coefficient according to an effect diameter. The effective diameter can be determined by a number of flow paths defined by the flow divider (e.g., k=√{square root over (N)}, where N is a number of flow paths in one rotor duct).

[0064] Referring to FIG. 5, the aspect ratio can be proportional to a width (“W”) of the first flow divider 52 or the second flow divider 54 in the radial direction, and the aspect ratio can be inversely proportional to a sum of axial lengths of the first flow divider and the second flow divider. For example, the sum of axial lengths of the first flow divider 52 and the second flow divider 54 may be less than or equal to the distance L between the first side surface 211 and the second side surface 212. The distance L can be defined as the rotor length L (see FIG. 3).

[0065] In some cases, the width W of the first flow divider 52 can be equal to the width of the second flow divider 54, and the axial length of the first flow divider 52 can be equal to the axial length of the second flow divider 54. For example, the axial length of the first flow divider 52 and the second flow divider 54 can be a half of (L−2d).

[0066] In some implementations, the width (W1) of the first flow divider 52 can be different from the width (W2) of the second flow divider 54, and the axial length (L1) of the first flow divider 52 can different from the axial length (L2) of the second flow divider 54 to accommodate variation in the boring process of each rotor duct. In some examples, the first flow divider 52 can be recessed by dl from the side surface 211, and the second flow divider 54 can be recessed by d2 from the side surface 212. That is, the separate flow dividers 52 and 54 can have structure for accommodating manufacturing offsets to thereby provide strong friction force to keep the structure from moving, and wearing of the flow dividers 52 and 54 and the rotor duct 213 can be reduced.

[0067] All examples described herein are merely to describe the present disclosure in greater detail. Therefore, it should be understood that the scope of the present disclosure is not limited to the example implementations described above or by the use of such terms unless limited by the appended claims. Also, it should be apparent to those skilled in the art that various alterations, substitutions, and modifications may be made within the scope of the appended claims or equivalents thereof.