Impeller shroud with pneumatic piston for clearance control in a centrifugal compressor

Patent metadata

Field	Value
Publication number	US-10309409-B2
Application number	US-201615165468-A
Country	US
Kind code	B2
Filing date	May 26, 2016
Priority date	May 26, 2016
Publication date	Jun 4, 2019
Grant date	Jun 4, 2019

Abstract

A system for controlling the clearance distance between an impeller blade tip of a centrifugal compressor and a radially inner surface of an impeller shroud in a turbine engine. The system comprises a high pressure air source, an air piston mounted between an engine casing and the shroud and adapted to receive high pressure air from the high pressure air source, a mounting arm coupling the shroud and air piston, and a slidable coupling adapted to allow axial movement of the shroud and joining the shroud to an axial member.

First claim

What is claimed is:

1. A compressor shroud assembly in a turbine engine, the compressor shroud assembly comprising:
a static compressor casing;
an air piston mounted to said casing, said air piston comprising a chamber adapted to receive actuating air;
an aft extending mounting arm coupled to said air piston, wherein said aft extending mounting arm moves axially while maintaining a radial alignment when said air piston is actuated; and
an impeller shroud for encasing a rotatable centrifugal compressor, the impeller shroud coupled at a forward end to said casing by a slidable coupling that maintains an air boundary during the full range of axial movement of said impeller shroud, the impeller shroud mounted proximate an aft end to said aft extending mounting arm, said impeller shroud moving relative to the rotatable centrifugal compressor in an axial direction while maintaining a radial alignment when said air piston is actuated.

2. The compressor shroud assembly of claim 1 wherein said air piston chamber is adapted to receive air from the discharge of the rotatable centrifugal compressor.

3. The compressor shroud assembly of claim 1 wherein said air piston comprises a forward rigid member mounted at a forward end to said casing, an aft rigid member coupled at an aft end to said mounting arm, and a flexible member coupling said forward and aft rigid members to thereby form said air piston chamber.

4. The compressor shroud assembly of claim 3 wherein said flexible member comprises a hoop having a U-shaped cross section.

5. The compressor shroud assembly of claim 3 wherein said flexible member comprises a bellows forming a hoop.

6. The compressor shroud assembly of claim 1 further comprising a chamber bounded in part by said casing and at least a portion of the impeller shroud proximate the aft end thereof, said chamber being pressurized by exducer air.

7. The compressor shroud assembly of claim 1 further comprising a chamber bounded in part by said casing and at least a portion of said impeller shroud proximate the forward end thereof, said chamber being pressurized by inducer air.

8. The compressor shroud assembly of claim 1 further comprising one or more sensors for measuring the air pressure in said air piston chamber, said air piston being actuated or vented in response to the measured pressure in said air piston chamber.

9. The compressor shroud assembly of claim 1 further comprising one or more sensors for measuring the clearance gap between said impeller shroud and the rotatable centrifugal compressor, said air piston being actuated or vented in response to the clearance gap measure by the one or more sensors.

10. A compressor shroud assembly in a turbine engine, the compressor shroud assembly comprising:
a static compressor casing;
an air piston mounted to said casing, said air piston comprising a chamber adapted to receive actuating air;
an aft extending mounting arm coupled to said air piston, wherein said aft extending mounting arm moves axially while maintaining a radial alignment when said air piston is actuated;
an impeller shroud for encasing a centrifugal compressor, the impeller shroud mounted at a forward end to said casing and mounted proximate an aft end to said aft extending mounting arm, said impeller shroud moving relative to the rotatable centrifugal compressor in a cantilevered manner from said forward end thereof when said air piston is actuated, said impeller shroud moving radially inward and axially aft at a central portion of the impeller shroud; and
a chamber bounded in part by said casing and at least a portion of said impeller shroud, wherein said air piston and said aft extending mounting arm are disposed within said chamber.

11. The compressor shroud assembly of claim 10 wherein said air piston chamber is adapted to receive air from the discharge of the rotatable centrifugal compressor.

12. The compressor shroud assembly of claim 10 wherein said air piston comprises a forward rigid member mounted at a forward end to said casing, an aft rigid member coupled at an aft end to said mounting arm, and a flexible member coupling said forward and aft rigid members to thereby form said air piston chamber.

13. The compressor shroud assembly of claim 12 wherein said flexible member comprises a hoop having a U-shaped cross section.

14. The compressor shroud assembly of claim 12 wherein said flexible member comprises a bellows forming a hoop.

15. A method of dynamically changing a clearance gap between a rotatable centrifugal compressor and an impeller shroud encasing the rotatable centrifugal compressor, said method comprising:
mounting a pressure-actuated piston to a static casing;
mounting the impeller shroud to the piston, the impeller shroud slidably coupled to the casing; and
actuating the piston to thereby move the impeller shroud relative to a rotatable centrifugal compressor, wherein the slidable coupling between said impeller shroud and said casing maintains an air boundary during the full range of axial movement of said impeller shroud.

16. The method of claim 15 further comprising providing air from the discharge of the rotatable centrifugal compressor to actuate the piston.

17. The method of claim 16 further comprising slidably coupling the forward end of the impeller shroud to the casing, wherein the impeller shroud moves relative to the rotatable centrifugal compressor in an axial direction while maintaining a radial alignment when the piston is actuated.

18. The method of claim 15 further comprising sensing the fluid pressure in an actuating chamber of the piston and actuating the piston in response to the sensed fluid pressure.

19. The method of claim 15 further comprising sensing the clearance gap between the rotatable centrifugal compressor and the impeller shroud and actuating the piston in response to the sensed clearance gap.

Assignees

• Rolls Royce Corp

Inventors

• Nesteroff Michael
• Acker Jonathan
• Crutchfield Jeffrey
• Ottow Nathan

Classifications

• F01D11/08

  for sealing space between rotor blade tips and stator (specially-shaped blade tips therefor F01D5/20) · CPC title

• F05D2220/32

  in gas turbines · CPC title

• F04D29/284

  for compressors · CPC title

• F01D11/22

  by mechanically actuating the stator or rotor components, e.g. moving shroud sections relative to the rotor · CPC title

• F05D2260/50

  Kinematic linkage, i.e. transmission of position · CPC title