Variable vane control system

Patent metadata

Field	Value
Publication number	US-10060285-B2
Application number	US-201414774815-A
Country	US
Kind code	B2
Filing date	Feb 21, 2014
Priority date	Mar 13, 2013
Publication date	Aug 28, 2018
Grant date	Aug 28, 2018

Abstract

A method of controlling a variable vane assembly includes the steps of sensing a first angular deflection of a first array of variable vanes about a first vane axis, and a second angular deflection of a second array of variable vanes about a second vane axis, the first array of variable vanes axially spaced from the second array of variable vanes, and adjusting the angular deflection of one of the first and second arrays of variable vanes, based on the sensed angular deflections from the other of the first and second arrays of variable vanes. A compressor including the variable vane assembly and a method of operating the variable vane assembly for a compressor are also disclosed.

First claim

The invention claimed is:

1. A method of controlling a variable vane assembly, comprising the steps of:
sensing a first angular deflection of a first array of variable vanes about a first vane axis, and a second angular deflection of a second array of variable vanes about a second vane axis, the first array of variable vanes axially spaced from the second array of variable vanes;
calculating whether the first array of variable vanes needs to be adjusted; and
adjusting the angular deflection of one of the first and second arrays of variable vanes, based on the sensed angular deflections from the other of the first and second arrays of variable vanes.

2. The method of claim 1 , wherein the second array of variable vanes comprises inlet guide vanes.

3. The method of claim 1 , further comprising the step of measuring an updated angular deflection of the first array of variable vanes with respect to the first vane axis subsequent to performing the adjusting step.

4. The method of claim 1 , including measuring using rotary variable differential transformers.

5. The method of claim 1 , including calculating and adjusting steps using a full authority digital engine controller.

6. The method of claim 1 , including adjusting with a bellcrank.

7. The method of claim 1 , further comprising the step of inputting a desired angular deflection of the first array of variable vanes.

8. A compressor for a gas turbine engine, comprising:
a plurality of stages, each stage including a plurality of vane arms, wherein the vane arms each include a portion that engages a variable vane and are secured to at least one movable annular ring, wherein at least one movable annular ring includes first and second movable annular rings and the vane arms include first and second ends configured to be secured to the first and second annular rings, respectively;
at least one sensor arranged at each stage, the at least one sensor configured to measure an angular position of the variable vanes; and
a controller configured adjust the at least one movable annular ring based on the angular position measured by the sensor.

9. The compressor of claim 8 , further comprising an actuator arranged at each stage, the actuator configured to move the at least one annular ring, thereby moving the variable vanes.

10. The compressor of claim 9 , wherein the controller controls the actuator of each stage independently.

11. The compressor of claim 8 , further including a plurality of inlet guide vanes arranged upstream from the foremost stage of the plurality of stages.

12. The compressor of claim 11 , wherein at least one of the plurality of inlet guide vanes includes an inlet guide vane sensor configured to determine an angular position of the at least one inlet guide vane.

13. The compressor of claim 12 , wherein the controller is configured to control the actuators based on information from the inlet guide vane sensor.

14. A method of controlling a variable vane assembly for a compressor, comprising:
securing a first plurality of variable vanes to a plurality of vane arms, the vane arms secured to a first movable annular ring at a first end and a second movable annular ring at a second end;
measuring an angular deflection of the first plurality of variable vanes with respect to a vane axis; and
moving the first and second annular rings in response to the measured angular deflection of the first plurality of variable vanes.

15. The method of claim 14 , further comprising the step of measuring an angular deflection of a second plurality of variable vanes.

16. The method of claim 15 , wherein the moving step is in response to the measured angular deflection of the second plurality of variable vanes.

17. The method of claim 16 , wherein the second plurality of variable vanes are inlet guide vanes.

Assignees

• United Technologies Corp

Inventors

• Do Logan H
• Sykes Richard L

Classifications

• F01D9/02

  Nozzles; Nozzle boxes; Stator blades; Guide conduits {, e.g. individual nozzles (nozzle boxes F01D9/047)} · CPC title

• F04D27/0246

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

• F05D2220/3216

  for a special compressor stage · CPC title

• F05D2270/44

  active, predictive, or anticipative · CPC title

• F05D2250/90

  Variable geometry · CPC title