Supersonic centrifugal compressor

• US 5,123,811 A
• Filed: 11/29/1989
• Issued: 06/23/1992
• Est. Priority Date: 12/05/1988
• Status: Expired due to Fees

• Current Assignee: Kazuo Kuroiwa
• Original Assignee: Kazuo Kuroiwa
• Inventors: Kuroiwa, Kazuo
• Primary Examiner(s): Look, Edward K.
• Assistant Examiner(s): NGUYEN, HOANG M
• Application Number:
  US07/442,718
• Time in Patent Office: 937 Days
• Field of Search: 415/206, 415/207, 415/212.1, 415/170.1, 415/172.1, 415/173.1, 415/173.5, 415/174.5, 415/177, 415/146, 415/211.2, 415/148, 415/126, 415/150, 415/156 , 415/10, 415/178, 417/279
• US Class Current: 415/207
• CPC Class Codes: F04D 17/10 for compressing or evacuating
• CPC Class Codes: F04D 21/00 Pump involving supersonic speed of pumped fluids
• CPC Class Codes: F04D 29/083 especially adapted for elastic fluid pumps
• CPC Class Codes: F04D 29/162 of a centrifugal flow wheel
• CPC Class Codes: F04D 29/441 especially adapted for elastic fluid pumps

Abstract

A supersonic centrifugal compressor comprising an impeller (2), a plurality of vanes (13) radially extending in the impeller to form a plurality of radially extending flow channels therebetween, and a diffuser (3) circumferentially surrounding the impeller and having a circumferential flow channel communicating with the flow channels of the impeller. In the impeller (2), at least one nozzle (18) is provided at the outlet of the flow channel and a contraction (20) is provided at the inlet of the flow channel, so that the flow channel is a low speed flow channel (21). Thus the speed of the fluid is low in the low speed flow channel (21) and high at the outlet of the nozzle (18). Also, in the diffuser (3), backflow preventing and friction reducing projections (33) are provided concentrically in the inner surface of the casing (11). Also, leakage preventing and pressure reducing vanes (37) are provided between the side disk (14, 15) of the impeller (2) and the casing (11), rotatably with the rotatable drive shaft (6). Also, the diffuser (3) comprises a concentric annular contraction (41) and an annular divergent channel (42) on the downstream side thereof. A cross-sectional area of the flow channel at the outlet of the annular divergent channel (42) is greater than that of the flow channel at the largest cross-sectional region (44) on the upstream side of the annular contraction (41), to allow control of the shock wave.

Claims

1. A centrifugal compressor comprising a casing (11) with an inner surface, an impeller (2) rotatably inserted in said casing about an axis and comprising a pair of side discs (14, 15) with outer surfaces facing the inner surface of said casing and a plurality of vanes (13) radially extending in said side discs to form a plurality of radially extending flow channels between two adjacent vanes, a difuser (3) circumferential flow channel communicating with said flow channels of said impeller, wherein backflow preventing and friction reducing projections (33) are provided concentrically in the inner surface of said casing (11) about said axis, wherein each of said projections (33) has a spoon-shaped cross-section with a sharpened end tip which faces said side disk (14 or 15).

2. A centrifugal compressor according to claim 1, wherein a wall between said backflow preventing and friction reducing projections (33) has a rounded shape.

3. A centrifugal compressor according to claim 1, wherein a clearance adjusting means (34) is provided for adjusting a clearance between at least one of said backflow preventing and friction reducing projections (33) and said side disk (14, 15).

4. A centrifugal compressor according to claim 1, wherein an electrically insulating member (35) is provided in a mechanically interposed member between said backflow preventing and friction reducing projection (33) and a portion of said side disks (14, 15) facing said backflow preventing and friction reducing projection.

5. A centrifugal compressor according to claim 1, wherein a pressure detecting device (17) is provided in said casing (11).

6. A centrifugal compressor comprising a casing (11) with an inner surafce, an impeller (2) rotatably inserted in said casing about an axis and comprising a pair of side discs (14, 15) with outer surfaces facing the inner surface of said casing and a plurality of vanes (13) radially extending in said side discs to form a plurality of radially extending in said side discs to form a plurality of radially extending flow channels between two adjacent vanes, a diffuser (3) circumferentially surrounding said impeller and having a circumferential flow channel communicating with said flow channels of said impeller, and a rotatable shaft (6) for securing said impeller for rotation therewith, wherein leakage preventing and pressure reducing vanes (37) are provided between said side disk (14, 15) and said casing (11), said leakage preventing and pressure reducing vanes (37) being rotatable with said rotatable shaft (6), wherein said vanes (37) are in part provided along the radial length of side disk (14, 15) at the inner circumferential surface (31) of the central opening of the side disk (14) and at the outer circumferential surface 39 of side disk (14).

7. A centrifugal compressor according to claim 6, wherein each of said leakage preventing and pressure reducing vanes (37) have a sharpened edge in a cross-section of fluid flow.

8. A centrifugal compressor according to claim 6, wherein each of said leakage preventing and pressure reducing vanes (37) has a spoon-shaped cross-section in a cross-section along which the fluid flows.

9. A centrifugal compressor according to claim 6, wherein said leakage preventing and pressure reducing vanes (37) are cantilevered vanes.

10. A centrifugal compressor according to claim 6, wherein backflow returning projection (38) are provided at the fluid inlets of said leakage preventing and pressure reducing vanes (37), said backflow returning projections (38) being fixed to said casing concentrically and consecutively about said axis.

11. A centrifugal compressor according to claim 10, wherein each of said backflow returning projections (38) has a spoon-shaped cross-section with a sharpened end tip.

12. A centrifugal compressor according to claim 10, wherein a wall between said backflow returning projections (38) has a rounded shape.

13. A centrifugal compressor according to claim 10, wherein a clearance adjusting means is provided.

14. A centrifugal compressor according to claim 10, wherein an electrically insulating member is provided in a mechanically interposed member between said backflow returning projection (38) and a portion of said side disks (14, 15) facing said backflow returning projection.

15. A centrifugal compressor according to claim 6, wherein a pressure averaging chamber (40) is provided at the outlet of said leakage preventing and pressure reducing vanes (37).

16. A centrifugal compressor comprising a casing (11), an impeller (2) inserted in said casing and rotatable about an axis, a plurality of vanes (13) radially extending in said impeller about said axis to form a plurality of radially extending flow channels between two adjacent vanes, and a diffuser (3) circumferentially surrounding said impeller and having a circumferential flow channel communicating with said flow channels of said impeller, each of said flow channels of said impeller having an inlet on the radially inner side of said impeller and an outlet on the radially outer side of said impeller, wherein at least one nozzle (18) is provided at said outlet of each of said flow channels of said impeller, and a contraction (20) is provided at said inlet of each of said flow channels of said impeller, so that each of said flow channels of said impeller is a low speed flow channel (21), wherein said impeller further includes a pair of side discs (14, 15), one of said side discs (14) having an inner circumferential surface (31) forming a central opening to which an outer correspondingly circumferential surface (39) of an inner ring-shaped portion of said casing (11) is sealingly faced, a shaft (6) extending through said inner ring-shaped portion of said casing with the other side disc (15) secured thereon for rotation therewith, an inlet flow passage (108) being formed between said inner circumferential surface of said inner ring-shaped portion of said casing and the outer surface of said shaft, and wherein the distance from the axis of said shaft (6) to said inlet (19) of said flow channel of said impeller (2) is greater than that from the axis of said shaft (6) to said inner circumferential surface (31) of said one side disc (14).

17. A centrifugal compressor comprising a casing (11), an impeller (2) inserted in said casing and rotatable about an axis, a plurality of vanes (13) radially extending in said impeller about said axis to form a plurality of radially extending flow channels between two adjacent vanes, and a diffuser (3) circumferentially surrounding said impeller and having a circumferential flow channel communicating with said flow channels of said impeller, each of said flow channels of said impeller having an inlet on the radially inner side of said impeller and an outlet on the radially outer side of said impeller, wherein at least one nozzle (18) is provided at said outlet of each of said flow channels of said impeller, and a contraction (20) is provided at said inlet of each of said flow channels of said impeller, so that each of said flow channels of said impeller is a low speed flow channel (21), wherein said impeller includes a pair of side discs (14, 15), one of said side discs (14) having an inner circumferential surface (31) forming a central opening to which an outer correspondingly circumferential surface (39) of an inner ring-shaped portion of said casing (11) is sealingly faced, a shaft (6) extending through said inner ring-shaped portion of said casing with the other side disc (15) secured thereon for rotation therewith, an inlet flow passage (108) being formed between said inner circumferential surface of said inner ring-shaped portion of said casing and the outer surface of said shaft, and wherein a circumferential pressure increasing projection (32) is provided concentrically and consecutively on said inner circumferential surface (31) of said side disc (14).

18. A centrifugal compressor comprising a casing (11), an impeller (2) inserted in said casing and rotatable about an axis, a plurality of vanes (13) radially extending in said impeller about said axis to form a plurality of radially extending flow channels between two adjacent vanes, and a diffuser (3) circumferentially surrounding said impeller and having a circumferential flow channel communicating with said flow channels of said impeller, each of said flow channels of said impeller having an inlet on the radially inner side of said impeller and an outlet on the radially outer side of said impeller, wherein at least one nozzle (18) is provided at said outlet of each of said flow channels of said impeller, and a contraction (20) is provided at said inlet of each of said flow channels of said impeller, so that each of said flow channels of said impeller is a low speed flow channel (21), wherein said impeller includes a pair of side discs (14, 15), one of said side discs (14) having an inner circumferential surface (31) forming a central opening to which an outer correspondingly circumferential surface (39) of an inner ring-shaped portion of said casing (11) is sealingly faced, a shaft (6) extending through said inner ring-shaped portion of said casing with the other side disc (15) secured thereon for rotation therewith, an inlet flow passage (108) being formed between said inner circumferential surface of said inner ring-shaped portion of said casing and the outer surface of said shaft, and wherein a circumferential pressure increasing projection (32) is provided concentrically and consecutively on said inner circumferential surface (31) of said side disc (14), and wherein said circumferential pressure increasing projection (32) has a spoon-shaped cross-section with a sharpened end tip projecting inward of the flow channel.

19. A centrifugal compression comprising a casing (11), an impeller (2) rotatably inserted in said casing about an axis and comprising a plurality of vanes (13) radially extending in said impeller to form a plurality of radially extending flow channels between two adjacent vanes, a diffuser (3) circumferentially surrounding said impeller and having a circumferential flow channel communicating with said flow channels of said impeller, and a rotatable shaft (6) for securing said impeller for rotation therewith, wherein an annular contraction (41), which has a variable cross-section, and an annular divergent channel (42) on the downstream side of said annular contraction are concentrically provided in said circumferential flow channel of said diffuser (3), and a circumferential fluid collecting means (4) is connected at an outer end of said circumferential flow channel of said diffuser (3), a cross-sectional area of the flow channel at the outlet of said annular divergent channel (42) being greater than that of the flow channel at the largest cross-sectional region (44) on he upstream side of said annular contraction (41), and wherein a position detecting means is provided for detecting a position of a variable portion of said circumferential flow channel of said diffusers (3).

20. A centrifugal compressor comprising a casing (11), an impeller (2) rotatably inserted in said casing about an axis and comprising a plurality of vanes (13) radially extending in said impeller to form a plurality of radially extending flow channels between two adjacent vanes, a diffuser (3) circumferentially surrounding said impeller and having a circumferential flow channel communicating with said flow channels of said impeller, and a rotatable shaft (6) for securing said impeller for rotation therewith, wherein an annular contraction (41) and an annular divergent channel (42) on the downstream side of said annular contraction are concentrically provided in said circumferential flow channel of said diffuser (3), and a circumferential fluid collecting means (4) is connected at an outer end of said circumferential flow channel of said diffuser (3), a cross-sectional area of the flow channel at the outlet of said annular divergent channel (42) being greater than that of the flow channel at the largest cross-sectional region (44) on the upstream side of said annular contraction (41), wherein a position adjusting device (61) is provided for adjusting the position of said casing (11) relative to another main casing.