Vane arm having a claw

Patent metadata

Field	Value
Publication number	US-10208618-B2
Application number	US-201414167382-A
Country	US
Kind code	B2
Filing date	Jan 29, 2014
Priority date	Feb 4, 2013
Publication date	Feb 19, 2019
Grant date	Feb 19, 2019

Abstract

An exemplary variable vane actuation system for a gas turbine engine includes a vane arm attachable to a vane stem and configured to rotate the vane stem about a radially extending axis. The vane arm includes a claw feature to be press-fit onto the vane stem.

First claim

We claim:

1. A variable vane actuation system for a gas turbine engine comprising:
a vane arm attachable to a vane stem of a vane and configured to rotate the vane stem about a radially extending axis, wherein the vane arm includes a claw feature to be press-fit onto the vane stem, wherein the claw feature includes opposing fingers extending away from a top surface toward the vane, the top surface including a surface opening extending completely through the top surface from a radially inward facing side of the top surface to a radially outward facing side of the top surface, the top surface having a flat side that is configured to interface with a flat area of the vane stem when the claw feature is press fit onto the vane stem.

2. The variable vane actuation system of claim 1 , wherein the claw feature is to be press-fit radially onto the vane stem.

3. The variable vane actuation system of claim 1 , wherein the surface opening in the surface comprises a D-shaped opening corresponding with a D-shaped portion of the vane stem.

4. The variable vane actuation system of claim 3 , further comprising a tab washer assembled onto the D-shaped portion of the vane stem and configured to bend over an end of the vane arm.

5. The variable vane actuation system of claim 4 , further comprising a threaded lock nut attached to the D-shaped portion of the vane stem to hold the vane arm to the vane stem.

6. The variable vane actuation system of claim 3 , wherein the D-shaped portion is threaded.

7. The variable vane actuation system of claim 1 , wherein the claw feature has an interference fit to the vane stem that is from 0.002 inches to 0.006 inches.

8. The variable vane actuation system of claim 1 , wherein the opposing fingers each terminate at respective faces spaced from each other to define a claw opening that receives the vane stem, the faces configured to interface directly with opposing sides of the vane stem, wherein the claw opening is radially spaced from the surface opening.

9. The variable vane actuation system of claim 8 , wherein a distance between the faces prior to receiving the vane stem is less than a distance between the faces after receiving the vane stem.

10. The variable vane actuation system of claim 1 , wherein a portion of the vane stem extends radially though the surface opening.

11. The variable vane actuation system of claim 1 , further comprising a pin to couple an end of the vane arm to an actuation ring, the end opposite the claw feature, wherein the pin is assembled radially to the actuation ring.

12. The variable vane actuation system of claim 11 , wherein attachment of the claw feature to the vane stem limits radially outward movement of the pin.

13. A method of assembling a variable vane actuation system, comprising:
press-fitting a claw feature of a vane arm onto a vane stem extending radially from a vane of a vane assembly while a portion of the vane stem extends through a surface opening in the vane arm, the surface opening radially spaced from the claw feature such that the claw feature extends radially closer to the vane than the surface opening does, wherein the vane assembly is a continuous structure having both the vane stem and the vane, wherein the claw feature includes fingers terminating at faces spaced from each other to define a claw opening that receives the vane stem after the press-fitting.

14. The method of claim 13 , further comprising press-fitting the claw feature radially on the vane stem by moving the claw feature in a radial direction from a position radially outside a flat area of the vane arm to a position radially aligned with the flat area, wherein the surface opening extends completely through the vane arm from a radially inward facing side of the vane arm to a radially outward facing side of the vane arm.

15. The method of claim 13 , wherein a distance between the faces prior to the press-fitting is less than a distance between the faces after the press-fitting, wherein the claw opening is radially spaced from the surface opening.

16. The method of claim 13 , further comprising moving an end of the vane arm radially to move the end between an uncoupled position with an actuation ring and a coupled position with the actuation ring, the end opposite the claw feature.

17. The method of claim 16 , further comprising limiting radial outward movement of the end from the coupled position to the uncoupled position using, exclusively, attachment of the claw feature to the vane stem.

18. The method of claim 13 , wherein the surface opening in the surface is a D-shaped opening corresponding with a D-shaped portion of the vane stem.

19. A method of coupling a vane arm within a gas turbine engine, comprising:
moving a vane arm radially from an uninstalled position to an installed position within a gas turbine engine;
receiving a portion of a vane stem within an aperture of the vane arm during the moving, the aperture extending through the vane arm and opening to both a radially inward facing surface and a radially outward facing surface of the vane arm, the vane stem extending radially from a vane of a vane assembly prior to the receiving, the vane assembly a continuous structure having both the vane and the vane stem, the aperture of the vane arm radially spaced from an opening between opposing fingers of a claw portion of the vane arm such that the aperture is radially outside the opening between the opposing fingers; and
press-fitting the claw portion of the vane arm over the vane stem during the moving.

Assignees

• United Technologies Corp

Inventors

• Gasmen Eugene C
• Pudvah Bernard W
• Wiecko Stanley

Classifications

• F01D17/14 Primary

  varying effective cross-sectional area of nozzles or guide conduits · CPC title

• Y10T29/49316

  Impeller making · CPC title

• F04D29/563

  specially adapted for elastic fluid pumps · CPC title

• Y10T29/49321

  Assembling individual fluid flow interacting members, e.g., blades, vanes, buckets, on rotary support member · CPC title

• 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