Positive displacement compressor and damper bearing system
A positive displacement compressor includes a positive displacement compressor rotor; a shaft operative to support the positive displacement compressor rotor; a bearing operative to support the shaft; a first structure having a first squeeze film compression surface; and a second structure having a second squeeze film compression surface spaced apart radially from the first squeeze film compression surface. The first and second structures are constructed to jointly form a squeeze film damper using the first and second squeeze film compression surfaces. The squeeze film damper is operative to provide squeeze film damping of vibrations. An annular oil discharge groove is disposed adjacent to a first end of the squeeze film damper. A first o-ring gland houses a circumferential-sealing o-ring disposed proximate to the first end of the squeeze film damper. A second o-ring gland houses a second circumferential-sealing o-ring disposed proximate to a second end of the squeeze film damper.
1. A damper bearing system, comprising:
a rolling element bearing;
a first structure having a first squeeze film compression surface;
a second structure having a second squeeze film compression surface spaced apart radially from the first squeeze film compression surface, the first structure and the second structure being constructed to jointly form a squeeze film damper using the first squeeze film compression surface and the second squeeze film compression surface, the squeeze film damper being operative to provide squeeze film damping of vibrations passing through the rolling element bearing upon an orbital motion of the second structure relative to the first structure;
an annular oil discharge groove disposed at a first end of the squeeze film damper, wherein the oil discharge groove is operative to collect oil for discharge from the squeeze film damper;
a first o-ring gland housing a first circumferential-sealing o-ring disposed proximate to the first end of the squeeze film damper; and
a second o-ring gland housing a second circumferential-sealing o-ring disposed proximate to a second end of the squeeze film damper;
wherein the first circumferential-sealing o-ring defines a first o-ring inner diameter, the first o-ring inner diameter sealing against the second squeeze film compression surface of the second structure, and wherein the second circumferential-sealing o-ring defines a second o-ring inner diameter, the second o-ring inner diameter sealing against the second squeeze film compression surface of the second structure.
2. The damper bearing system of claim 1 , wherein the annular oil discharge groove is integral with the first o-ring gland.
3. The damper bearing system of claim 2 , further comprising another annular oil discharge groove integral with the second o-ring gland.
4. The damper bearing system of claim 1 , wherein the second structure is an outer race of the rolling element bearing; and wherein the second compression surface is an outer surface of the outer race.
5. The damper bearing system of claim 1 , wherein the first structure is a static bearing support structure; wherein the first compression surface is an internal surface of the static bearing support structure, and wherein the first o-ring gland, the second o-ring gland and the annular oil discharge groove are disposed in the static bearing support structure.
6. The damper bearing system of claim 1 , wherein the squeeze film damper includes a cylindrical damping cavity defined between the first squeeze film compression surface and the second squeeze film compression surface.
7. The damper bearing system of claim 1 , further comprising an oil feed hole disposed in the first structure between the first end and the second end and operative to supply oil to the squeeze film damper.
8. A positive displacement compressor apparatus, comprising:
a positive displacement compressor or pump rotor;
a shaft operative to support, at least in part, the positive displacement compressor or pump rotor;
a bearing operative to support the shaft;
a first structure having a first squeeze film compression surface;
a second structure having a second squeeze film compression surface spaced apart radially from the first squeeze film compression surface, the first structure and the second structure being constructed to jointly form a squeeze film damper using the first squeeze film compression surface and the second squeeze film compression surface, the squeeze film damper being operative to provide squeeze film damping of vibrations passing through the rolling element bearing upon an orbital motion of the second structure relative to the first structure;
an annular oil discharge groove disposed adjacent to a first end of the squeeze film damper, wherein the oil discharge groove is operative to collect oil for discharge from the squeeze film damper;
a first o-ring gland housing a first circumferential-sealing o-ring disposed proximate to the first end of the squeeze film damper; and
a second o-ring gland housing a second circumferential-sealing o-ring disposed proximate to a second end of the squeeze film damper;
wherein the first circumferential-sealing o-ring defines a first o-ring inner diameter, the first o-ring inner diameter sealing against the second squeeze film compression surface of the second structure, and wherein the second circumferential-sealing o-ring defines a second o-ring inner diameter, the second o-ring inner diameter sealing against the second squeeze film compression surface of the second structure.
9. The positive displacement compressor apparatus of claim 8 , wherein the first structure is a static bearing support structure, and wherein the second structure is a dynamic structure.
10. The positive displacement compressor apparatus of claim 9 , wherein the bearing is a rolling element bearing; wherein the second structure is an outer race of the rolling element bearing; and wherein the second compression surface is an outer surface of the outer race.
11. The positive displacement compressor apparatus of claim 8 , wherein the annular oil discharge groove is integral with the first o-ring gland.
12. The positive displacement compressor apparatus of claim 11 , further comprising another annular oil discharge groove integral with the second o-ring gland.
13. The positive displacement compressor apparatus of claim 8 , wherein the squeeze film damper includes a cylindrical damping cavity.
14. The positive displacement compressor apparatus of claim 8 , further comprising an oil feed hole disposed in the first structure between the first end and the second end and operative to supply oil to the squeeze film damper.
15. A screw compressor, comprising:
a rotating screw compressor rotor operative to compress a gas;
a shaft operative to support, at least in part, the rotating screw compressor rotor;
a rolling element bearing operative to support the shaft;
a first structure having a first squeeze film compression surface;
a second structure having a second squeeze film compression surface spaced apart radially from the first squeeze film compression surface, the first structure and the second structure being constructed to jointly form a squeeze film damper using the first squeeze film compression surface and the second squeeze film compression surface, the squeeze film damper being operative to provide squeeze film damping of vibrations passing through the rolling element bearing upon an orbital motion of the second structure relative to the first structure;
an annular oil discharge groove disposed adjacent to a first end of the squeeze film damper, wherein the oil discharge groove is operative to collect oil for discharge from the squeeze film damper;
a first o-ring gland housing a first circumferential-sealing o-ring disposed proximate to the first end of the squeeze film damper; and
a second o-ring gland housing a second circumferential-sealing o-ring disposed proximate to a second end of the squeeze film damper;
wherein the first circumferential-sealing o-ring defines a first o-ring inner diameter, the first o-ring inner diameter sealing against the second squeeze film compression surface of the second structure, and wherein the second circumferential-sealing o-ring defines a second o-ring inner diameter, the second o-ring inner diameter sealing against the second squeeze film compression surface of the second structure.
16. The screw compressor of claim 15 , wherein the first structure is a static bearing support structure, and wherein the second structure is a dynamic structure.
17. The screw compressor of claim 16 , wherein the bearing is a rolling element bearing; wherein the second structure is an outer race of the rolling element bearing; and wherein the second compression surface is an outer surface of the outer race.
18. The screw compressor of claim 15 , wherein the annular oil discharge groove is integral with the first o-ring gland.
19. The screw compressor of claim 18 , further comprising another annular oil discharge groove integral with the second o-ring gland.
20. The screw compressor of claim 15 , wherein the squeeze film damper includes a cylindrical damping cavity, further comprising an oil feed hole disposed in the first structure and operative to feed oil into the cylindrical damping cavity between the first end and the second end of the squeeze film damper.