Turbo compressor and turbo refrigerator

Patent metadata

Field	Value
Publication number	US-9822789-B2
Application number	US-201514627399-A
Country	US
Kind code	B2
Filing date	Feb 20, 2015
Priority date	Aug 28, 2012
Publication date	Nov 21, 2017
Grant date	Nov 21, 2017

Abstract

A turbo compressor that has a pressure equalizing tube that circulates a gas from a gear unit accommodation space toward an IGV accommodation space, and an oil separation device that is provided in the gear unit accommodation space to separate lubricating oil that is contained in the gas, in which the oil separating device has a suction duct that communicates with the pressure equalizing tube, and the suction duct has a centrifugal separation portion provided with a first demister, a second demister provided on the downstream side of the first demister in relation to the suction direction, and a curved passage provided between the first demister and the second demister.

First claim

The invention claimed is:

1. A turbo compressor comprising:
a compression stage that is provided with an impeller that rotates;
a housing provided with a first space that in addition to housing lubricating oil houses a gear member that transmits rotating force to the impeller, and a second space in which the ambient pressure becomes lower than the first space;
a pressure equalizing tube that circulates a gas from the first space toward the second space; and
an oil separating device that is provided in the first space and that separates the lubricating oil contained in the gas,
wherein the oil separating device has a suction passage that communicates with the pressure equalizing tube; and
the suction passage has:
a suction port which opens to the first space and from which the suction passage suctions the gas of the first space,
an interconnecting opening which communicates with the pressure equalizing tube and from which the suction passage discharges the gas to the pressure equalizing tube, and
a centrifugal separation portion that is provided with a first demister, a second demister that, in relation to a flow direction of the gas from the suction port to the interconnecting opening in the suction passage, is provided on the downstream side of the first demister, and a curved passage that is provided between the first demister and the second demister.

2. The turbo compressor according to claim 1 , wherein the centrifugal separation portion, in relation to the rotation direction of the gear member, is provided on the upstream side of the pressure equalizing tube.

3. The turbo compressor according to claim 1 , wherein the curved passage has an oil catching portion on the curved outer side of the curved passage.

4. The turbo compressor according to claim 2 , wherein the curved passage has an oil catching portion on the curved outer side of the curved passage.

5. The turbo compressor according to claim 3 , wherein the oil catching portion has a concavo-convex shape.

6. The turbo compressor according to claim 4 , wherein the oil catching portion has a concavo-convex shape.

7. The turbo compressor according to claim 1 , wherein
the centrifugal separation portion comprises a first centrifugal separation portion that, in relation to the rotation direction of the gear member, is provided on the upstream side of the pressure equalizing tube, and a second centrifugal separation portion that is provided on the downstream side of the pressure equalizing tube.

8. The turbo compressor according to claim 2 , wherein
the centrifugal separation portion comprises a first centrifugal separation portion that, in relation to the rotation direction of the gear member, is provided on the upstream side of the pressure equalizing tube, and a second centrifugal separation portion that is provided on the downstream side of the pressure equalizing tube.

9. The turbo compressor according to claim 3 , wherein
the centrifugal separation portion comprises a first centrifugal separation portion that, in relation to the rotation direction of the gear member, is provided on the upstream side of the pressure equalizing tube, and a second centrifugal separation portion that is provided on the downstream side of the pressure equalizing tube.

10. The turbo compressor according to claim 4 , wherein
the centrifugal separation portion comprises a first centrifugal separation portion that, in relation to the rotation direction of the gear member, is provided on the upstream side of the pressure equalizing tube, and a second centrifugal separation portion that is provided on the downstream side of the pressure equalizing tube.

11. The turbo compressor according to claim 5 , wherein
the centrifugal separation portion comprises a first centrifugal separation portion that, in relation to the rotation direction of the gear member, is provided on the upstream side of the pressure equalizing tube, and a second centrifugal separation portion that is provided on the downstream side of the pressure equalizing tube.

12. The turbo compressor according to claim 6 , wherein
the centrifugal separation portion comprises a first centrifugal separation portion that, in relation to the rotation direction of the gear member, is provided on the upstream side of the pressure equalizing tube, and a second centrifugal separation portion that is provided on the downstream side of the pressure equalizing tube.

13. The turbo compressor according to claim 7 , wherein the curved passage comprises a first curved passage of the first centrifugal separation portion and a second curved passage of the second centrifugal separation portion and the first curved passage of the first centrifugal separation portion is longer than the second curved passage of the second centrifugal separation portion.

14. The turbo compressor according to claim 8 , wherein the curved passage comprises a first curved passage of the first centrifugal separation portion and a second curved passage of the second centrifugal separation portion and the first curved passage of the first centrifugal separation portion is longer than the second curved passage of the second centrifugal separation portion.

15. The turbo compressor according to claim 9 , wherein the curved passage comprises a first curved passage of the first centrifugal separation portion and a second curved passage of the second centrifugal separation portion and the first curved passage of the first centrifugal separation portion is longer than the second curved passage of the second centrifugal separation portion.

16. The turbo compressor according to claim 10 , wherein the curved passage comprises a first curved passage of the first centrifugal separation portion and a second curved passage of the second centrifugal separation portion and the first curved passage of the first centrifugal separation portion is longer than the second curved passage of the second centrifugal separation portion.

17. The turbo compressor according to claim 11 , wherein the curved passage comprises a first curved passage of the first centrifugal separation portion and a second curved passage of the second centrifugal separation portion and the first curved passage of the first centrifugal separation portion is longer than the second curved passage of the second centrifugal separation portion.

18. The turbo compressor according to claim 12 , wherein the curved passage comprises a first curved passage of the first centrifugal separation portion and a second curved passage of the second centrifugal separation portion and the first curved passage of the first centrifugal separation portion is longer than the second curved passage of the second centrifugal separation portion.

19. The turbo compressor according to claim 7 , wherein the first centrifugal separation portion and the second centrifugal separation portion are integrally connected.

20. A turbo refrigerator comprising:
a condenser that liquefies a compressed refrigerant;
an evaporator that by evaporating the refrigerant that is liquefied by the condenser cools a cooling object; and
a turbo compressor that compresses the refrigerant that is evaporated by the evaporator and supplies it to the condenser,
wherein the turbo refrigerator is provided with the turbo compressor according to claim 1 as the turbo compressor.

Assignees

• Ihi Corp
• Daikin Ind Ltd

Inventors

• Oda Kentarou
• Yoshinaga Seiichiro
• Sakuma Nobuyoshi

Classifications

• F04D17/12 Primary

  Multi-stage pumps · CPC title

• F25B2600/027

  by controlling pressure · CPC title

• F25B2500/16

  Lubrication · CPC title

• F25B31/002

  Lubrication · CPC title

• F25B1/10

  with multi-stage compression (with cascade operation F25B7/00) · CPC title