Clearance control

Patent metadata

Field	Value
Publication number	US-9719365-B2
Application number	US-201314031695-A
Country	US
Kind code	B2
Filing date	Sep 19, 2013
Priority date	Oct 22, 2012
Publication date	Aug 1, 2017
Grant date	Aug 1, 2017

Abstract

A clearance control device including a segment having a passage to deliver fluid towards a component rotating past the segment. Also a fluid flow device having a first fluid path coupled to the passage and a second fluid path that is decoupled from the passage. A first plasma generator is located in the fluid flow device that directs fluid towards the first fluid path; a second plasma generator is located in the fluid flow device that directs fluid towards the second fluid path; and a control arrangement is configured to alternately energize the first and second plasma generators at an energizing frequency to deliver fluid to the passage at a frequency coincident with the passing frequency of the component.

First claim

The invention claimed is:

1. A clearance control device comprising:
a segment having a passage to deliver fluid towards a component rotating past the segment;
a fluid flow device having a first fluid path coupled to the passage and a second fluid path that is decoupled from the passage;
a first plasma generator located in the fluid flow device that directs fluid towards the first fluid path;
a second plasma generator located in the fluid flow device that directs fluid towards the second fluid path; and
a control arrangement configured to alternately energise the first and second plasma generators at an energising frequency, to deliver fluid to the passage at a frequency coincident with the passing frequency of the component.

2. The clearance control device as claimed in claim 1 wherein the fluid flow device comprises a switched vortex valve.

3. The clearance control device as claimed in claim 2 wherein the second fluid path closes the valve.

4. The clearance control device as claimed in claim 1 wherein the fluid flow device comprises a bifurcated fluid passage.

5. The clearance control device as claimed in claim 1 wherein the first and second plasma generators are located at an inlet to the fluid flow device.

6. The clearance control device as claimed in claim 5 wherein the first and second plasma generators are spaced apart across a fluid path into the fluid flow device.

7. The clearance control device as claimed in claim 1 wherein the first and second plasma generators each comprise a pair of electrical terminals separated by a gap across which a spark may travel to generate plasma.

8. The clearance control device as claimed in claim 1 wherein the first and second plasma generators each comprise a dielectric barrier discharge actuator.

9. The clearance control device as claimed in claim 1 wherein the passage is angled to deliver the fluid in the opposite direction to fluid passing between the component and the segment.

10. The clearance control device as claimed in claim 9 wherein the passage forms an angle (α) of 1° to 90° to the plane of the segment facing the component.

11. The clearance control device as claimed in claim 1 further comprising a sensor coupled to the control arrangement, the sensor arranged to sense the passing frequency of the component.

12. The clearance control device as claimed in claim 1 wherein the energising frequency is coincident with the passing frequency of the component.

13. The clearance control device as claimed in claim 1 further comprising a Hartmann oscillator coupled between the first fluid path and the passage, wherein the Hartmann oscillator is arranged to receive inlet flow from the first fluid path and deliver output flow to the passage.

14. The clearance control device as claimed in claim 13 wherein the energising frequency modulates amplitude of the inlet flow to the Hartmann oscillator such that the output flow from the Hartmann oscillator includes a frequency coincident with the passing frequency of the component.

15. The clearance control device as claimed in claim 13 further comprising a fluid filter arranged to receive the output flow from the Hartmann oscillator and to deliver filtered fluid to the passage.

16. The clearance control device as claimed in claim 1 wherein the control arrangement is arranged to energise the first and second plasma generators for unequal periods.

17. The clearance control device as claimed in claim 1 , wherein the segment comprises at least two passages.

18. A rotor sub-assembly comprising a rotor having an array of blades, a casing segment surrounding the rotor blades and the clearance control device as claimed in claim 1 wherein the component comprises a blade of the array of blades.

19. A seal arrangement comprising the clearance control device as claimed in claim 1 wherein the segment comprises a seal segment (and the component comprises a rotating component against which the seal acts.

20. A gas turbine engine comprising the clearance control device as claimed in claim 1 .

Assignees

• Rolls Royce Plc

Inventors

• Bacic Marko
• Scanlon Timothy John
• Daniel Ronald William

Classifications

• F01D11/24

  by selectively cooling-heating stator or rotor components · CPC title

• F01D11/20

  Actively adjusting tip-clearance · CPC title

• F05D2270/62

  Electrical actuators · CPC title

• F05D2260/16

  Fluid modulation at a certain frequency · CPC title

• F05D2270/172

  by a plasma generator, e.g. control of ignition · CPC title