Inlet guide vane mechanism

Patent metadata

Field	Value
Publication number	US-10364826-B2
Application number	US-201414768708-A
Country	US
Kind code	B2
Filing date	Feb 20, 2014
Priority date	Feb 20, 2013
Publication date	Jul 30, 2019
Grant date	Jul 30, 2019

Abstract

An inlet guide vane assembly ( 60 ) is provided including a plurality of vane subassemblies ( 62 ) configured to rotate relative to a blade ring housing ( 64 ) to control a volume of air flowing there through. The inlet guide vane assembly ( 60 ) also includes a plurality of drive mechanisms ( 80 ). Each drive mechanism ( 80 ) is operably coupled to one of the plurality of vane subassemblies ( 62 ). The vane subassemblies ( 62 ) may be rotated independently.

First claim

What is claimed is:

1. An inlet guide vane assembly, comprising:
a plurality of vane subassemblies configured to rotate relative to a blade ring housing to control a volume of air flowing there through; and
a plurality of independently operable drive mechanisms, each of the plurality of drive mechanisms being operably coupled to one of the plurality of vane subassemblies such that each of the vane subassemblies is rotatable about a respective axis independently.

2. The inlet guide vane assembly according to claim 1 , wherein the drive mechanisms are selected from one of an actuator, stepper motor, and servo motor.

3. The inlet guide vane assembly according to claim 1 , wherein each vane subassembly includes a flat air foil vane connected to a vane shaft.

4. The inlet guide vane assembly according to claim 3 , wherein a coupling directly couples each vane shaft to a shaft of one of the plurality of drive mechanisms.

5. The inlet guide vane assembly according to claim 1 , wherein the plurality of drive mechanisms are arranged adjacent the blade ring housing within a cavity of a suction housing.

6. The inlet guide vane assembly according to claim 5 , wherein the suction housing includes a cover connected to a back plate to form the cavity.

7. The inlet guide vane assembly according to claim 1 , wherein the inlet guide vane assembly is arranged within a cavity of a suction housing and the plurality of drive mechanisms is located adjacent an exterior surface of the suction housing.

8. The inlet guide vane assembly according to claim 1 , wherein the inlet guide vane assembly is arranged within a cavity of a suction housing and a portion of each of the plurality of drive mechanisms extends through a wall of the suction housing into the cavity.

9. A compressor assembly of a chiller refrigeration system, comprising:
a compressor; and
an inlet guide vane assembly arranged generally within a suction housing positioned adjacent an inlet of the compressor, the inlet guide vane assembly including a plurality of vane subassemblies configured to rotate relative to the suction housing to control a volume of air flowing into the compressor, and a plurality of independently operable drive mechanisms, each of the plurality of drive mechanisms being operably coupled to one of the plurality of vane subassemblies such that each of the vane subassemblies is rotatable about a respective axis independently.

10. The compressor assembly according to claim 9 , wherein the drive mechanisms are selected from one of an actuator, stepper motor, and servo motor.

11. The compressor assembly according to claim 10 , wherein each vane subassembly includes a flat air foil vane connected to a vane shaft.

12. The compressor assembly according to claim 11 , wherein a coupling directly couples each vane shaft to a shaft of one of the plurality of drive mechanisms.

13. The inlet guide vane assembly according to claim 9 , wherein the plurality of drive mechanisms are arranged adjacent the blade ring housing within a cavity of a suction housing.

14. The inlet guide vane assembly according to claim 13 , wherein the suction housing includes a cover connected to a back plate to form the cavity.

15. A method of positioning an inlet guide vane assembly of a compressor in a chiller refrigeration system, the method comprising:
determining, using a controller, an allowable position of each vane subassembly of a plurality of vane subassemblies in response to a current position of each vane subassembly in the inlet guide vane assembly and load conditions of the chiller refrigeration system;
providing power from a power source to at least one of a plurality of drive mechanisms, each drive mechanism being coupled to a single vane subassembly, wherein a first output signal provided to the power source by the controller indicates to which of the plurality of drive mechanisms the power source should supply power; and

moving the at least one vane subassembly independently from another vane subassembly to the predetermined position.

16. The method according to claim 15 , wherein a second output signal provided by the controller indicates a direction and an amount that each of the vane subassemblies should be rotated.

17. The method according to claim 15 , wherein a position signal provided to the controller by each of the plurality of vane subassemblies is used to verify that each of the vane subassemblies was moved to the determined position.

Assignees

• Carrier Corp

Inventors

• Sishtla Vishnu M

Classifications

• F04D17/10

  for compressing or evacuating · CPC title

• F25B31/026

  with compressor of rotary type · CPC title

• F25B49/022

  Compressor control arrangements · CPC title

• F05D2250/51

  Inlet · CPC title

• F04D27/0246 Primary

  by varying geometry within the pumps, e.g. by adjusting vanes · CPC title