IMPELLER FOR A CENTRIFUGAL COMPRESSOR

• US 20070059179A1
• Filed: 09/13/2006
• Published: 03/15/2007
• Est. Priority Date: 09/13/2005
• Status: Active Grant

• Current Assignee: Ingersoll-Rand Industrial U.S., Inc. (Ingersoll Rand, Inc.)
• Original Assignee: Ingersoll-Rand Company (Trane Technologies plc)
• Inventors: Xu, Cheng
• Granted Patent: US 7,563,074 B2
• Time in Patent Office: Days
• US Class Current: 416/182
• CPC Class Codes: F04D 29/162 of a centrifugal flow wheel
• CPC Class Codes: F04D 29/284 for compressors
• CPC Class Codes: F04D 29/30 Vanes

Abstract

An impeller rotatable in a direction of rotation in a centrifugal compressor including an intake ring. The impeller includes a back plate having a shaft portion and a plurality of blades. Each blade extends from the back plate and includes an inducer portion adapted to draw fluid into the impeller and including a leading edge and an exducer portion adapted to discharge the fluid from the impeller and including a trailing edge. A blade pressure side is defined between the leading edge, the trailing edge, the back plate, and a blade tip. The pressure side is convex from the back plate to the blade tip. A blade suction side opposite the pressure side is defined between the leading edge, the trailing edge, the back plate, and the blade tip. The suction side being concave from the back plate to the blade tip.

Claims

1. An impeller rotatable in a direction of rotation in a centrifugal compressor having an intake ring, the impeller comprising:

a back plate including a hub portion; and

a plurality of blades extending from the backplate, each blade including a leading edge that extends radially outward along a non-linear path from adjacent the hub portion.

2. The impeller of claim 1, wherein the non-linear path is backward sweeping.

3. The impeller of claim 2, wherein the plurality of blades define an exducer portion adapted to discharge the fluid, the exducer portion including a trailing edge of each of the blades.

4. The impeller of claim 1, wherein each blade defines a blade tip, and wherein at least a portion of the blade tip leans in a direction opposite the direction of rotation.

5. The impeller of claim 1, wherein each of the plurality of blades defines a blade pressure side that extends from the leading edge to the trailing edge and is convex.

6. The impeller of claim 5, wherein each of the plurality of blades defines a blade suction side opposite the pressure side and extending from the leading edge to the trailing edge, the suction side being concave.

7. The impeller of claim 1, wherein the back plate and the plurality of blades are integrally-formed as a single component from a single contiguous piece of material.

8. The impeller of claim 1, wherein each blade defines a blade tip, and wherein the intake ring and blade tips cooperate to define a non-uniform clearance gap therebetween.

9. The impeller of claim 8, wherein the non-uniform clearance gap is defined by a high-order equation.

10. The impeller of claim 10, wherein each of the blades defines a blade mid-line wrap of between about −

65 degrees to −

90 degrees.

11. An impeller rotatable in a direction of rotation in a centrifugal compressor including an intake ring, the impeller comprising:

a back plate including a hub portion; and

a plurality of blades, each extending from the back plate and including;

an inducer portion adapted to draw fluid into the impeller and including a leading edge,

an exducer portion adapted to discharge the fluid from the impeller and including a trailing edge;

a blade pressure side defined between the leading edge, the trailing edge, the back plate, and a blade tip, the pressure side being convex from the back plate to the blade tip; and

a blade suction side opposite the pressure side and defined between the leading edge, the trailing edge, the back plate, and the blade tip, the suction side being concave from the back plate to the blade tip.

12. The impeller of claim 11, wherein at least a portion of the blade tip leans in a direction opposite the direction of rotation.

13. The impeller of claim 11, wherein the back plate and the plurality of blades are integrally-formed as a single component from a single contiguous piece of material.

14. The impeller of claim 11, wherein the leading edge of each blade extends radially outward from the hub portion along a non-linear path.

15. The impeller of claim 14, wherein the non-linear path is rearward sweeping.

16. The impeller of claim 11, wherein the trailing edge includes a non-linear pressure side edge and a non-linear suction side edge that is not parallel to the pressure side edge.

17. The impeller of claim 11, wherein the blade tip and the intake ring cooperate to define a non-uniform clearance gap therebetween.

18. The impeller of claim 17, wherein the non-uniform clearance gap is defined by a high-order equation.

19. The impeller of claim 11, wherein each of the blades defines a blade mid-line wrap of between about −

65 degrees to −

90 degrees.

20. A centrifugal compressor comprising:

an impeller rotatable in a direction of rotation about an axis and including a plurality of blades that define an inducer portion adapted to draw in fluid during rotation and an exducer portion adapted to discharge the fluid during rotation, each of the blades including a leading edge, a trailing edge, a platform portion, and a blade tip; and

an intake ring having a seal surface disposed adjacent the blade tip to define a clearance gap, the seal surface and the blade tip arranged such that the gap is non-uniform when measured normal to the seal surface.

21. The centrifugal compressor of claim 20, wherein the impeller includes a shaft portion and wherein each leading edge extends radially outward along a non-linear path from the shaft portion.

22. The centrifugal compressor of claim 21, wherein the non-linear path is backward sweeping.

23. The centrifugal compressor of claim 20, wherein each blade includes a blade pressure side defined between the leading edge, the trailing edge, the platform portion, and the blade tip, the pressure surface being convex from the platform portion to the blade tip.

24. The centrifugal compressor of claim 20, wherein each blade includes a blade suction side defined between the leading edge, the trailing edge, the platform portion, and the blade tip, the suction surface being concave from the platform portion to the blade tip.

25. The centrifugal compressor of claim 20, wherein the blade tip leans in a direction opposite the direction of rotation.

26. The centrifugal compressor of claim 20, wherein the trailing edge includes a non-linear pressure side edge and a non-linear suction side edge that is not parallel to the pressure side edge.

27. The centrifugal compressor of claim 20, wherein the clearance gap is larger adjacent the inducer portion than between the inducer portion and the exducer portion and adjacent the exducer portion.

28. The centrifugal compressor of claim 20, wherein the impeller defines a velocity loading parameter during operation, and wherein the clearance gap is inversely related to the velocity loading parameter.

29. The centrifugal compressor of claim 20, wherein each of the blades defines a blade mid-line wrap of between about −

65 degrees to −

90 degrees.