Variable vane actuation system for a turbo machine

Patent metadata

Field	Value
Publication number	US-10704411-B2
Application number	US-201816054248-A
Country	US
Kind code	B2
Filing date	Aug 3, 2018
Priority date	Aug 3, 2018
Publication date	Jul 7, 2020
Grant date	Jul 7, 2020

Abstract

A system for operating a turbo machine is generally provided, the system including a variable vane assembly including a first plurality of vanes coupled together by a first unison member and a second plurality of vanes coupled together by a second unison member. An actuation system is coupled to each of the first unison member and the second unison member and a solenoid actuator is coupled to the variable vane assembly and the actuation system.

First claim

What is claimed is:

1. A system for operating a turbo machine, the system comprising:
a variable vane assembly comprising a first plurality of vanes coupled together by a first unison member and a second plurality of vanes coupled together by a second unison member;
an actuation system coupled to each of the first unison member and the second unison member; and
a solenoid actuator coupled to the variable vane assembly and the actuation system.

2. The system of claim 1 , wherein the solenoid actuator is coupled to one or more of the unison members of the variable vane assembly.

3. The system of claim 1 , wherein the actuation system comprises a coupling member, wherein the coupling member is coupled to each of the unison members.

4. The system of claim 3 , wherein the solenoid actuator is coupled to the coupling member of the actuation system.

5. The system of claim 1 , wherein the solenoid actuator is coupled to the first unison member of the variable vane assembly.

6. The system of claim 1 , wherein the first plurality of vanes comprises an inlet guide vane.

7. The system of claim 1 , wherein the solenoid actuator defines a two-position solenoid actuator.

8. The system of claim 1 , wherein the solenoid actuator defines a proportional solenoid actuator.

9. The system of claim 1 , the system further comprising:
a controller configured to perform operations, the operations comprising:
displacing the first plurality of vanes from a first rotational angle corresponding to a first position of the solenoid actuator to a second rotational angle corresponding to a second position of the solenoid actuator independent of movement from the actuation system.

10. The system of claim 9 , the operations further comprising:
offsetting a change in rotational angle at the first plurality of vanes from the actuation system via displacing the solenoid actuator.

11. The system of claim 9 , the operations further comprising:
displacing the first plurality of vanes and the second plurality of vanes via the actuation system.

12. The system of claim 9 , the operations further comprising:
adjusting the rotational angle of the plurality of vanes via the solenoid actuator at one or more operating conditions of the turbo machine between zero revolutions per minute and maximum steady state operating condition.

13. A turbo machine engine, the engine comprising:
a compressor section;
a turbine section;
a variable vane assembly comprising a first plurality of vanes coupled together by a first unison member and a second plurality of vanes coupled together by a second unison member;
an actuation system coupled to each of the first unison member and the second unison member; and
a solenoid actuator coupled to the variable vane assembly and the actuation system.

14. The engine of claim 13 , wherein the solenoid actuator is coupled to one or more of the unison members of the variable vane assembly.

15. The engine of claim 13 , wherein the actuation system comprises a coupling member, wherein the coupling member is coupled to each of the unison members.

16. The engine of claim 15 , wherein the solenoid actuator is coupled to the coupling member of the actuation system.

17. The engine of claim 13 , wherein the solenoid actuator is coupled to the first unison member of the variable vane assembly.

18. The engine of claim 13 , wherein the first plurality of vanes comprises an upstream-most stage of the compressor section.

19. The engine of claim 13 , wherein the first plurality of vanes comprises an inlet guide vane of a high pressure compressor of the compressor section.

20. The engine of claim 13 , wherein the variable vane assembly, the actuation system, and the solenoid actuator are coupled to the turbine section.

Assignees

• Gen Electric

Inventors

• Mielke Mark Joseph

Classifications

• F01D17/162 Primary

  for axial flow, i.e. the vanes turning around axes which are essentially perpendicular to the rotor centre line (F01D17/167 takes precedence) · CPC title

• F05D2270/701

  proportional · CPC title

• F04D29/563

  specially adapted for elastic fluid pumps · CPC title

• F05D2240/128

  Nozzles · CPC title

• F05D2260/57

  using servos, independent actuators, etc. · CPC title