Compressor and turbo chiller

Patent metadata

Field	Value
Publication number	US-9897092-B2
Application number	US-201314655030-A
Country	US
Kind code	B2
Filing date	Jul 26, 2013
Priority date	Dec 28, 2012
Publication date	Feb 20, 2018
Grant date	Feb 20, 2018

Abstract

A compressor ( 2 ) characterized by being equipped with: a rotary shaft ( 12 ); multiple impellers attached to the rotary shaft; a main flow path that guides a fluid from the prior-stage impeller to the latter-stage impeller; a chamber ( 31 ) that forms a circle centered around the axial line and connects to the main flow path; a suction nozzle ( 32 ) that guides the fluid from the outer circumferential side toward the inner circumferential side in the chamber; multiple movable vanes provided in the main flow path at intervals in the circumferential direction of the axial line and capable of moving and thereby adjusting the flow volume of the fluid passing through the main flow path; and a drive mechanism ( 42 ) that is provided at one side in the circumferential direction of the suction nozzle ( 32 ) within the chamber ( 31 ), and that changes the angle of the multiple movable vanes. In addition, of the one side and the other side in the circumferential direction within the chamber ( 31 ), the suction nozzle ( 32 ) is inclined toward the other side so as to increase the flow volume of the fluid toward the other side.

First claim

The invention claimed is:

1. A compressor comprising:
a rotary shaft which rotates around an axis line;
a plurality of impellers mounted on the rotary shaft;
a main flow path which guides a fluid from the impeller of a preceding stage to the impeller of a subsequent stage;
a chamber which has a ring shape comprising a first semi-circumferential side and a second semi-circumferential side, is centered on the axis line, and is in fluid communication with the main flow path;
a suction nozzle which introduces the fluid into the chamber toward an inner periphery side from an outer periphery side;
a plurality of movable vanes which are provided in the main flow path at intervals in a circumferential direction with respect to the axis line and are movable, thereby adjusting a flow rate of the fluid flowing through the main flow path; and
a drive mechanism which changes angles of the plurality of movable vanes,
wherein the drive mechanism is provided in the first semi-circumferential side of the chamber with respect to the suction nozzle, and the suction nozzle is inclined toward the second semi-circumferential side of the chamber such that the flow rate of the fluid to the second semi-circumferential side increases.

2. The compressor according to claim 1 , wherein a guide blade which guides the fluid such that the flow rate of the fluid to the second semi-circumferential side other side out of one side and the other side in the circumferential direction in the chamber increases is provided on an outlet side of the suction nozzle.

3. The compressor according to claim 2 , wherein the guide blade is formed of a plurality of blades, where the length of each successive blade is greater than the previous blade, moving in a direction from the first semi-circumferential side to the second semi-circumferential side.

4. The compressor according to claim 3 , wherein a flow path guide formed so as to make a flow path of the chamber narrower as it goes toward the drive mechanism is provided in the chamber.

5. The compressor according to claim 4 , wherein the drive mechanism is provided at a position spaced apart by 90° in the circumferential direction with respect to the suction nozzle.

6. The compressor according to claim 3 , wherein the drive mechanism is provided at a position spaced apart by 90° in the circumferential direction with respect to the suction nozzle.

7. The compressor according to claim 2 , wherein a flow path guide formed so as to make a flow path of the chamber narrower as it goes toward the drive mechanism is provided in the chamber.

8. The compressor according to claim 7 , wherein the drive mechanism is provided at a position spaced apart by 90° in the circumferential direction with respect to the suction nozzle.

9. The compressor according to claim 2 , wherein the drive mechanism is provided at a position spaced apart by 90° in the circumferential direction with respect to the suction nozzle.

10. The compressor according to claim 1 , wherein a flow path guide formed so as to make a flow path of the chamber narrower as it goes toward the drive mechanism is provided in the chamber.

11. The compressor according to claim 10 , wherein the drive mechanism is provided at a position spaced apart by 90° in the circumferential direction with respect to the suction nozzle.

12. The compressor according to claim 1 , wherein the drive mechanism is provided at a position spaced apart by 90° in the circumferential direction with respect to the suction nozzle.

13. A turbo chiller comprising: the compressor according to claim 1 .

Assignees

• Mitsubishi Heavy Ind Ltd

Inventors

• Koga Jun
• Omura Shintaro

Classifications

• F05B2210/403

  Radial inlet and axial outlet · CPC title

• F04D29/4213

  suction ports · CPC title

• F04D29/4206

  especially adapted for elastic fluid pumps · CPC title

• F05B2250/501

  Inlet · CPC title

• F04D17/122 Primary

  the individual rotor discs being, one for each stage, on a common shaft and axially spaced, e.g. conventional centrifugal multi- stage compressors · CPC title