Vane pumping machine utilizing invar-class alloys for maximizing operating performance and reducing pollution emissions

• US 6,162,034 A
• Filed: 03/01/1999
• Issued: 12/19/2000
• Est. Priority Date: 03/01/1999
• Status: Expired due to Term

• Current Assignee: Mallen Research Limited Partnership
• Original Assignee: Mallen Research Limited Partnership
• Inventors: Mallen, Brian D.
• Primary Examiner(s): Vrablik, John J.
• Application Number:
  US09/258,791
• Time in Patent Office: 659 Days
• Field of Search: 418/178, 418/179, 418/235, 418/259, 418/265, 418/260
• US Class Current: 418/178
• CPC Class Codes: F01C 1/3442 the surfaces of the inner and outer member, forming the working space, being surfaces of revolution
• CPC Class Codes: F01C 21/0836 comprising guiding means, e.g. cams, rollers
• CPC Class Codes: F04C 2230/602 Gap; Clearance
• CPC Class Codes: F04C 2240/50 Bearings
• CPC Class Codes: F05C 2201/0466 Nickel
• CPC Class Codes: F05C 2203/0813 Carbides
• CPC Class Codes: F05C 2251/042 Expansivity

Abstract

A rotary vane pumping machine have a core structure and peripheral components interfacing with the core structure. The core structure includes a stator assembly defining a contoured surface of a stator cavity, a rotor spinning around a rotor shaft axis that is fixed relative to the stator cavity, and end plates disposed on either side of the rotor. The rotor has a plurality of radial vanes slots for housing a corresponding plurality of vanes that slide within the radial vane slot of the rotor. The plurality of vanes, stator cavity and rotor define a plurality of chamber cells. The core structure is substantially made of low coefficient of thermal expansion Invar materials to achieve precise non-contact sealing clearances between components of the machine.

Claims

1. A rotary vane pumping machine having a core structure and peripheral components interfacing with the core structure, the core structure comprising:

a stator assembly comprising an annular ring, the inner circumferential surface of the annular ring defining a contoured surface of a stator cavity;

a rotor spinning around a rotor shaft axis, the rotor shaft axis being a fixed rotational axis relative to the stator cavity, the rotor having a plurality of radial vane slots and the rotor and stator being in relative rotation;

a plurality of vanes, each of the plurality of vanes sliding with at least one of a radial and axial component of vane motion within a corresponding radial vane slot of the rotor, and each of the plurality of vanes having a tip portion and a base portion, the base portion having at least one protruding tab extending from at least one axial end therefrom;

a guidance device engaging the tabs to control radial movement of the vanes; and

a first end plate and a second end plate, each being adjacent an axial side of the rotor located therebetween, with the rotor shaft extending through at least one of the first end plate and the second end plate, wherein an outer circumferential surface of the rotor comprises an annular sealing lip extending axially toward respective of the first end plate and the second end plate,

wherein the plurality of vanes, the stator cavity, and the rotor define a plurality of chamber cells,

wherein the vane tip portion and the contour of the stator cavity are spaced apart by a radial clearance,

wherein the stator assembly, rotor, guidance device, first end plates and second end plate together define a first combined core structure, and

wherein the first combined core structure is substantially comprised of an invar-class alloy.

2. The rotary machine of claim 1, the guidance device further comprising:

a translation ring disposed at one axial end of the rotary vane pumping machine corresponding to the end of the protruding tabs, the translation ring rotating around a fixed hub located within one of the first and second end plates, the fixed hub being eccentric to the rotor shaft axis; and

a plurality of linear channels formed in the translation ring, wherein the at least one protruding tab extending from the base portion of each of the plurality of vanes communicates with a respective linear channel in the translation ring, whereby the rotor rotation causes rotation of the vanes and a corresponding rotation of the translation ring.

3. The rotary machine of claim 2, wherein the plurality of vanes, stator assembly, rotor, first end plate, second end plate and translation ring, together define a second combined core structure, and

wherein the second combined core structure is substantially comprised of an invar-class alloy.

4. The rotary machine of claim 2, further comprising bearing pad inserts fixed to linear segments of a modified linear translation ring, the inserts being in contact with roller bearings disposed between the linear segments and the vane tabs.

5. The rotary machine of claim 2, further comprising bearing pad inserts fixed to the linear channels, the inserts being in contact with roller bearings disposed between the vane tabs and the linear channels.

6. The rotary machine of claim 5, further comprising bearing pad inserts fixed to the vane tabs, the inserts being in contact with roller bearings disposed between the vane tabs and the linear channels.

7. The rotary machine of claim 1, further comprising thrust bearings surrounding the rotor shaft and disposed between the rotor and respective of the first end plate and second end plate, thereby preventing contact between the annular sealing lip and each of the first end plate and the second end plate.

8. The rotary machine of claim 7, further comprising bearing pad inserts fixed to the radial vane slots in the rotor, the inserts being in contact with roller bearings disposed between the vanes and the radial vane slots.

9. The rotary machine of claim 8, further comprising bearing pad inserts fixed to azimuthal faces of the vanes, the inserts being in contact with roller bearings disposed between the vanes and the radial vane slots.

10. The rotary machine of claim 8, wherein the bearing pad inserts are comprised of hardened-steel.

11. The rotary machine of claim 8, wherein the bearing pad inserts are comprised of carbide.

12. The rotary machine of claim 1, wherein the stator assembly comprises a near-zero expansion ceramic liner.

13. The rotary machine of claim 12, wherein the ceramic liner is one selected from a group consisting of NZP class ceramics.

14. The rotary machine of claim 1, wherein the radial clearance between the vane tip portion and the contour of the stator cavity is less than 0.001" per 1" of maximum chamber height (Ch_max), wherein (Ch_max) is the difference in extension of a vane between its maximum extension from the rotor and its maximum retraction into the rotor.

15. The rotary machine of claim 14, wherein the radial clearance between the vane tip portion and the contour of the stator cavity is less than 0.0005" per 1" of maximum chamber height (Ch_max).

16. The rotary machine of claim 1, wherein an axial clearance between a respective side of each vane and the confronting one of the first and second end plates is less than 0.001" per 1" of maximum chamber height (Ch_max), wherein (Ch_max) is the difference in extension of a vane between its maximum extension from the rotor and its maximum retraction into the rotor.

17. The rotary machine of claim 16, wherein the axial clearance between the respective side of each vane and the confronting one of the first and second end plates is less than 0.0005" per 1" of maximum chamber height (Ch_max).

18. The rotary machine of claim 1, wherein an axial clearance between the rotor annular sealing lip and the confronting one of the first and second end plates is less than 0.0005" per 1" of maximum chamber height (Ch_max), wherein (Ch_max) is the difference in extension of a vane between its maximum extension from the rotor and its maximum retraction into the rotor.

19. The rotary machine of claim 18, wherein the axial clearance between the rotor annular sealing lip and the confronting one of the first and second end plates is less than 0.0002" per 1" of maximum chamber height (Ch_max).

20. The rotary machine of claim 1, wherein an azimuthal clearance between an azimuthal face of the vane and a confronting vane slot seal, extending from a radial vine slot wall, is less than 0.0005" per 1" of maximum chamber height (Ch_max), wherein (Ch_max) is the difference in extension of a vane between its maximum extension from the rotor and its maximum retraction into the rotor.

21. The rotary machine of claim 20, wherein the azimuthal clearance between the azimuthal face of the vane and the confronting radial vane slot wall is less than 0.0002" per 1" of maximum chamber height (Ch_max).