IP Library Granted Patent US 7,444,921
Granted Patent B2
US 7,444,921 · App. 11/497,116 · Granted Nov 4, 2008

Swash ring compressor

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Quick Facts
Patent No.
US 7,444,921
App. No.
11/497,116
Granted
Nov 4, 2008
Kind
B2
Abstract

A variable displacement compressor is disclosed. The compressor includes a crankcase for receiving a fluid. The crankcase has a plurality of compression chambers in which the fluid is compressed. A plurality of pistons disposed within the crankcase and are configured for reciprocal movement within the plurality of chambers to compress and pump the fluid. Further, a rotor assembly having a drive shaft and a rotor, wherein the rotor has a first pivot arm support member extending from a first surface of the rotor. A sleeve is slidably engaged with the drive shaft and configured for axial movement along a longitudinal axis of the drive shaft. A swash ring is coupled to the plurality of pistons and to the rotor by means of a pivot arm. Rotary motion of the swash ring and rotor causes reciprocal motion of the plurality of pistons within the plurality of chambers.

Claims (57)

1. A variable displacement compressor, the compressor comprising:

a crankcase for receiving a fluid, wherein the crankcase has a plurality of compression chambers in which the fluid is compressed;

a plurality of pistons disposed within the crankcase and configured for reciprocal movement within the plurality of chambers to compress and pump the fluid;

a rotor assembly having a drive shaft and a rotor;

a first pivot pin support member extending from a first surface of the rotor;

a sleeve slidably engaged to the drive shaft and configured for axial movement along a longitudinal axis of the drive shaft;

a swash ring coupled to the plurality of pistons and through rotary motion of the swash ring causes reciprocal motion of the plurality of pistons within the plurality of chambers, and wherein the swash ring is pivotally mounted to the sleeve, whereby axial movement of the sleeve along the longitudinal axis of the drive shaft causes the swash ring to be inclined relative to the rotor;

a bushing disposed within an aperture in the swash ring and configured for movement within the aperture; and

a first pivot pin connected to the bushing at a first end and to the first pivot pin support member at a second end.

2. The compressor of claim 1 wherein the swash ring is made of a soft material.

3. The compressor of claim 1 wherein the soft material is selected from the group consisting of: aluminum, copper alloys and powder metals.

4. The compressor of claim 1 further comprising a spring disposed around the drive shaft for biasing the swash ring away from the rotor.

5. The compressor of claim 1 further comprising a second pivot pin for connecting the swash ring to the drive shaft.

6. The compressor of claim 5 further comprising a second pivot pin support member fixed to the drive shaft for supporting the second pivot pin.

7. The compressor of claim 1 further comprising a counterweight member extending from the first surface of the rotor to counter balance the centrifugal forces created by the rotation of the swash ring.

8. The compressor of claim 7 wherein the counterweight member extending from the first surface of the rotor is disposed opposite the pivot pin support member.

9. The compressor of claim 7 wherein the counterweight member extending from the first surface of the rotor and is disposed inward of the swash ring.

10. The compressor of claim 1 further comprising a thrust bearing to provide axial movement of the swash ring along the drive shaft toward the rotor.

11. The compressor of claim 1 further comprising a swash ring stop member extending from the first surface of the rotor to prevent angular rotation of the swash ring past a predefined angle.

12. The compressor of claim 1 wherein the first end of the first pivot pin is spherically shaped.

13. The compressor of claim 12 wherein the bushing has a spherical surface that cooperates with the spherical shape of the first end of the first pivot pin.

14. The compressor of claim 12 wherein the bushing has a cylindrical outer surface configured for sliding movement with in the aperture of the swash ring.

15. The compressor of claim 1 wherein the second end of the first pivot pin is cylindrically shaped.

16. The compressor of claim 1 wherein the first end of the first pivot pin has a substantially cylindrical shape.

17. The compressor of claim 16 wherein the bushing is an elongated tubular member having an aperture for receiving the first end of the first pivot pin.

18. The compressor of claim 16 wherein the first end of the first pivot pin has an annular groove for receiving a retaining member to secure the bushing to the pivot pin.

19. A variable displacement compressor, the compressor comprising:

a crankcase for receiving a fluid, wherein the crankcase has a plurality of compression chambers in which the fluid is compressed;

a plurality of pistons disposed within the crankcase and configured for reciprocal movement within the plurality of chambers to compress and pump the fluid;

a rotor assembly having a drive shaft and a rotor, wherein the rotor has a pivot arm support member extending from a first surface of the rotor;

a sleeve slidably engaged to the drive shaft and configured for axial movement along a longitudinal axis of the drive shaft;

a swash ring coupled to the plurality of pistons and through rotary motion of the swash ring causes reciprocal motion of the plurality of pistons within the plurality of chambers, and wherein the swash ring is pivotally mounted to the sleeve, whereby axial movement of the sleeve along the longitudinal axis of the drive shaft causes the swash ring to be inclined relative to the rotor;

a first bushing disposed within an aperture in the swash ring and configured for movement within the aperture; and

a pair of pivot pins pivotally connected to the bushing at a first end and fixed to the pivot arm support member at a second end.

20. The compressor of claim 19 further comprising a spring disposed around the drive shaft for biasing the swash ring away from the rotor.

21. The compressor of claim 19 further comprising a counterweight member extending from the first surface of the rotor to counter balance the centrifugal forces created by the rotation of the swash ring.

22. The compressor of claim 21 wherein the counterweight member extending from the first surface of the rotor is disposed opposite the pivot pin support member.

23. The compressor of claim 21 wherein the counterweight member extending from the first surface of the rotor and is disposed inward of the swash ring.

24. The compressor of claim 19 further comprising a thrust bearing to provide axial movement of the swash ring along the drive shaft toward the rotor.

25. The compressor of claim 19 further comprising a swash ring stop member extending from the first surface of the rotor to prevent angular rotation of the swash ring past a predefined angle.

26. The compressor of claim 19 wherein the first end of each of the pair of pivot pins is spherically shaped.

27. The compressor of claim 26 wherein the second end of each of the pivot pins is cylindrically shaped.

28. The compressor of claim 19 wherein the first bushing has a spherical surface that cooperates with the spherical shape of each of the first ends of the pair of pivot pins.

29. The compressor of claim 28 wherein the first bushing has a cylindrical outer surface configured for sliding movement with in the aperture of the swash ring.

30. The compressor of claim 19 further comprising a second bushing having a spherical surface that cooperates with the spherical shape of each of the first ends of the pair of pivot pins and having a cylindrical outer surface configured for sliding movement within a second aperture of the swash ring.

31. The compressor of claim 19 wherein the first bushing is an elongated tubular member having apertures for receiving the each of first ends of the pair of pivot pins.

32. The compressor of claim 31 wherein each of the first ends of the pair of pivot pins has an annular groove for receiving a retaining member to secure the first bushing to the pair of pivot pins.

33. A variable displacement compressor, the compressor comprising:

a crankcase for receiving a fluid, wherein the crankcase has a plurality of compression chambers in which the fluid is compressed;

a plurality of pistons disposed within the crankcase and configured for reciprocal movement within the plurality of chambers to compress and pump the fluid;

a rotor assembly having a drive shaft and a rotor;

a first sleeve slidably engaged to the drive shaft and configured for axial movement along a longitudinal axis of the drive shaft;

a swash ring coupled to the plurality of pistons and through rotary motion of the swash ring causes reciprocal motion of the plurality of pistons within the plurality of chambers, and wherein the swash ring is pivotally mounted to the first sleeve, whereby axial movement of the first sleeve along the longitudinal axis of the drive shaft causes the swash ring to be inclined relative to the rotor;

a second sleeve disposed within a bore in the swash ring; and

a pivot pin fixed at a first end to the drive shaft and in contact with the second sleeve at a second end.

34. The compressor of claim 33 wherein the second sleeve is secured to the bore in the swash ring and the second end of the pivot pin is in sliding contact with the second sleeve.

35. The compressor of claim 33 wherein the second sleeve is in slidable contact with the bore in the swash ring and the second end of the pivot pin is rotatable within the second sleeve.

Assignments (6)
CHANGE OF NAME Recorded Oct 30, 2015
From: HALLA VISTEON CLIMATE CONTROL CORPORATION
To: HANON SYSTEMS
Reel/Frame 037007/0103 →
RELEASE OF SECURITY INTEREST IN INTELLECTUAL PROPERTY Recorded Jun 9, 2014
From: MORGAN STANLEY SENIOR FUNDING, INC.
To: VISTEON CORPORATION; VC AVIATION SERVICES, LLC; VISTEON ELECTRONICS CORPORATION; VISTEON GLOBAL TECHNOLOGIES, INC.; VISTEON INTERNATIONAL HOLDINGS, INC.; VISTEON GLOBAL TREASURY, INC.; VISTEON EUROPEAN HOLDINGS, INC.; VISTEON SYSTEMS, LLC; VISTEON INTERNATIONAL BUSINESS DEVELOPMENT, INC.
Reel/Frame 033107/0717 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Aug 2, 2013
From: VISTEON GLOBAL TECHNOLOGIES, INC.
To: HALLA VISTEON CLIMATE CONTROL CORPORATION
Reel/Frame 030935/0958 →
RELEASE BY SECURED PARTY AGAINST SECURITY INTEREST IN PATENTS ON REEL 025241 FRAME 0317 Recorded Apr 26, 2011
From: MORGAN STANLEY SENIOR FUNDING, INC.
To: VISTEON CORPORATION; VC AVIATION SERVICES, LLC; VISTEON ELECTRONICS CORPORATION; VISTEON GLOBAL TECHNOLOGIES, INC.; VISTEON INTERNATIONAL HOLDINGS, INC.; VISTEON GLOBAL TREASURY, INC.; VISTEON EUROPEAN HOLDING, INC.; VISTEON SYSTEMS, LLC; VISTEON INTERNATIONAL BUSINESS DEVELOPMENT, INC.
Reel/Frame 026178/0412 →
SECURITY AGREEMENT (REVOLVER) Recorded Oct 19, 2010
From: VISTEON CORPORATION; VC AVIATION SERVICES, LLC; VISTEON ELECTRONICS CORPORATION; VISTEON GLOBAL TECHNOLOGIES, INC.; VISTEON INTERNATIONAL HOLDINGS, INC.; VISTEON GLOBAL TREASURY, INC.; VISTEON EUROPEAN HOLDINGS, INC.; VISTEON SYSTEMS, LLC; VISTEON INTERNATIONAL BUSINESS DEVELOPMENT, INC.
To: MORGAN STANLEY SENIOR FUNDING, INC., AS AGENT
Reel/Frame 025238/0298 →
SECURITY AGREEMENT Recorded Oct 19, 2010
From: VISTEON CORPORATION; VC AVIATION SERVICES, LLC; VISTEON ELECTRONICS CORPORATION; VISTEON GLOBAL TECHNOLOGIES, INC.; VISTEON INTERNATIONAL HOLDINGS, INC.; VISTEON GLOBAL TREASURY, INC.; VISTEON EUROPEAN HOLDING, INC.; VISTEON SYSTEMS, LLC; VISTEON INTERNATIONAL BUSINESS DEVELOPMENT, INC.
To: MORGAN STANLEY SENIOR FUNDING, INC., AS AGENT
Reel/Frame 025241/0317 →