Variable vane scheduling

Patent metadata

Field	Value
Publication number	US-10267326-B2
Application number	US-201213669510-A
Country	US
Kind code	B2
Filing date	Nov 6, 2012
Priority date	Sep 27, 2012
Publication date	Apr 23, 2019
Grant date	Apr 23, 2019

Abstract

An example variable vane scheduling method includes adjusting variable vanes from a position based on a first schedule to a position based on a different, second schedule in response to a control feature. An example method of controlling flow through a compressor of a turbomachine includes moving variable vanes to positions that allow more flow into the compressor in response to bleed air being communicated away from the compressor.

First claim

We claim:

1. A variable vane scheduling method, comprising:
adjusting variable vanes from a position based on a first schedule to a position based on a different, second schedule in response to a control feature that includes at least an amount of bleed air,
wherein the variable vanes control flow through a compressor of a turbomachine, and the first and the second schedules determine the position based on a variable that includes at least a rotational speed of a rotor of the compressor and a temperature of the compressor.

2. The variable vane scheduling method of claim 1 , wherein the first schedule includes positions that permit a first amount of flow into the compressor, and the second schedule includes positions that permit a second amount of flow into the compressor, the first amount less than the second amount.

3. The variable vane scheduling method of claim 1 , wherein the variable vanes are adjusted according to the first schedule when the amount of bleed air is relatively low, and the variable vanes are adjusted according to the second schedule when the amount of bleed air is relatively high.

4. The variable vane scheduling method of claim 3 , wherein the variable vanes are adjusted based on the first schedule when the amount of bleed air is zero.

5. The variable vane scheduling method of claim 1 , wherein the variable includes the rotational speed divided by the temperature.

6. The variable vane scheduling method of claim 1 , wherein temperature is a compressor inlet temperature.

7. The variable vane scheduling method of claim 1 , including using a position of a bleed valve to determine the amount of bleed air.

8. The variable vane scheduling method of claim 1 , further comprising adjusting the variable vanes according to the first schedule when a bleed valve is closed, the second schedule when the bleed valve is partially open, and a third schedule when the bleed valve is fully open.

9. The variable vane scheduling method of claim 1 , wherein the turbomachine is a propulsion engine comprising a fan.

10. A turbomachine controller assembly, comprising:
a controller configured to adjust an array of variable vanes within a compressor, wherein the controller adjusts the array according to a first schedule when a first amount of bleed air is communicated from the compressor, and adjusts the array according to a second schedule when a different, second amount of bleed air is communicated from the compressor,
wherein the first and the second schedules determine the position based on a variable that includes at least a rotational speed of a rotor of the compressor and a temperature of the compressor.

11. The turbomachine controller assembly of claim 10 , wherein the first schedule includes positions that permit less flow through the compressor than the positions of the second schedule.

12. The turbomachine controller assembly of claim 11 , wherein the second amount of bleed air comprises no bleed air communicated from the compressor.

13. The turbomachine controller assembly of claim 10 , wherein the controller monitors a bleed valve position to determine whether the first amount or the second amount of bleed air is communicated from the compressor.

14. The turbomachine controller assembly of claim 10 , wherein the first and the second schedules are determined based at least on a compressor rotor speed and an inlet temperature.

15. The turbomachine controller assembly of claim 10 , wherein the controller adjusts the array of variable vanes according to the first schedule when a bleed valve is closed, the second schedule when the bleed valve is partially open, and a third schedule when the bleed valve is fully open.

16. The turbomachine controller assembly of claim 10 , wherein the array and the compressor are part of a propulsion engine that includes a fan.

17. A method of controlling flow through a compressor of a turbomachine, comprising:
moving variable vanes according to a first schedule or a second schedule in response to bleed air being communicated away from the compressor,
wherein the variable vanes control flow through the compressor, and the first and the second schedules determine the position based on a variable that includes at least a rotational speed of a rotor of the compressor and a temperature of the compressor.

18. The method of claim 17 , further comprising moving the variable vanes according to the first schedule when a bleed valve is closed, the second schedule when the bleed valve is partially open, and a third schedule when the bleed valve is fully open.

19. The method of claim 17 , wherein the variable vanes and the compressor are part of a propulsion engine that includes a fan.

Assignees

• United Technologies Corp

Inventors

• Teicholz Matthew D
• Spiesman Paul H
• Wojcik Kerri A
• Gendron John R
• Bartkowski Glenn D
• Blake Sean D J
• Tempelman William G

Classifications

• F02C6/08 Primary

  the gas being bled from the gas-turbine compressor · CPC title

• F04D27/009

  by bleeding, by passing or recycling fluid · CPC title

• F04D27/0246 Primary

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

• F04D27/0215

  Arrangements therefor, e.g. bleed or by-pass valves · CPC title

• F02C9/20

  by throttling; by adjusting vanes · CPC title