Concentric shafts for remote independent variable vane actuation

Patent metadata

Field	Value
Publication number	US-10107130-B2
Application number	US-201615079417-A
Country	US
Kind code	B2
Filing date	Mar 24, 2016
Priority date	Mar 24, 2016
Publication date	Oct 23, 2018
Grant date	Oct 23, 2018

Abstract

An actuator system including a harmonic drive operable to drive a variable vane system of a gas turbine engine.

First claim

What is claimed is:

1. A gas turbine engine defined about a central longitudinal axis, comprising:
a first actuator;
a first harmonic drive driven by the first actuator, the harmonic drive comprising a strain wave gearing mechanism;
a first drive shaft driven by the first harmonic drive;
a first variable vane stage;
a first unison ring operable to drive the first variable vane stage, the first unison ring driven by the first drive shaft;
a second actuator;
a second harmonic drive driven by the second actuator, the harmonic drive comprising a strain wave gearing mechanism;
a second drive shaft driven by the second harmonic drive, the first drive shaft coaxial with the second drive shaft, the first and second drive shaft extend through a firewall;
a second variable vane stage; and
a second unison ring operable to drive the second variable vane stage, the second unison ring driven by the second drive shaft, wherein the strain wave gearing mechanism include a fixed circular spline, a flex spline attached to an output shaft, and a wave generator attached to an input shaft, the flex spline driven by the wave generator with respect to the circular spline.

2. A gas turbine engine defined about a central longitudinal axis, comprising:
a first actuator;
a first harmonic drive driven by the first actuator, the harmonic drive comprising a strain wave gearing mechanism;
a first drive shaft driven by the first harmonic drive;
a first variable vane stage;
a first unison ring operable to drive the first variable vane stage, the first unison ring driven by the first drive shaft;
a second actuator;
a second harmonic drive driven by the second actuator, the harmonic drive comprising a strain wave gearing mechanism;
a second drive shaft driven by the second harmonic drive, the first drive shaft coaxial with the second drive shaft, the first and second drive shaft extend through a firewall;
a second variable vane stage; and
a second unison ring operable to drive the second variable vane stage, the second unison ring driven by the second drive shaft, wherein the first drive shaft is parallel with the central longitudinal axis.

3. A gas turbine engine defined about a central longitudinal axis, comprising:
a first actuator;
a first harmonic drive driven by the first actuator, the harmonic drive comprising a strain wave gearing mechanism;
a first drive shaft driven by the first harmonic drive;
a first variable vane stage;
a first unison ring operable to drive the first variable vane stage, the first unison ring driven by the first drive shaft;
a second actuator;
a second harmonic drive driven by the second actuator, the harmonic drive comprising a strain wave gearing mechanism;
a second drive shaft driven by the second harmonic drive, the first drive shaft coaxial with the second drive shaft, the first and second drive shaft extend through a firewall;
a second variable vane stage; and
a second unison ring operable to drive the second variable vane stage, the second unison ring driven by the second drive shaft, wherein the first drive shaft and the second drive shaft include a respective first drive gear and a second drive gear operable to drive the respective first unison ring and the second unison ring, wherein the respective gear segment is meshed with the respective first drive gear and the second drive gear in a sliding relationship.

4. The gas turbine engine as recited in claim 3 , wherein the first unison ring and the second unison ring include a respective gear segment meshed with the respective first drive gear and the second drive gear.

5. A gas turbine engine defined about a central longitudinal axis, comprising:
a first actuator;
a first harmonic drive driven by the first actuator, the harmonic drive comprising a strain wave gearing mechanism;
a first drive shaft driven by the first harmonic drive;
a first variable vane stage;
a first unison ring operable to drive the first variable vane stage, the first unison ring driven by the first drive shaft;
a second actuator;
a second harmonic drive driven by the second actuator, the harmonic drive comprising a strain wave gearing mechanism;
a second drive shaft driven by the second harmonic drive, the first drive shaft coaxial with the second drive shaft, the first and second drive shaft extend through a firewall;
a second variable vane stage; and
a second unison ring operable to drive the second variable vane stage, the second unison ring driven by the second drive shaft, wherein the first and second actuators, and the first and second harmonic drives, are located on a side of the firewall that provides a thermally controlled environment, wherein the thermally controlled environment is about 160 F and a side opposite the thermally controlled environment is 200 F-600 F.

Assignees

• United Technologies Corp

Inventors

• Suciu Gabriel L
• Zimmitti Jonathan F
• Chandler Jesse M

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

• F05D2220/32

  in gas turbines · CPC title

• F05D2240/12

  Fluid guiding means, e.g. vanes · CPC title

• F05D2260/57

  using servos, independent actuators, etc. · CPC title

• F16H19/001

  for conveying reciprocating or limited rotary motion · CPC title