Propeller pitch change actuation system

Patent metadata

Field	Value
Publication number	US-10077103-B2
Application number	US-201615074632-A
Country	US
Kind code	B2
Filing date	Mar 18, 2016
Priority date	Mar 18, 2016
Publication date	Sep 18, 2018
Grant date	Sep 18, 2018

Abstract

A yoke plate arrangement may comprise a yoke plate, a wear plate comprising a wear surface and a contact surface, wherein a post extends from the contact surface, and a yoke plate ear extending from the yoke plate in a radial direction, wherein a first aperture is disposed in the yoke plate ear, the post located at least partially within the first aperture, the contact surface being in contact with the yoke plate ear. The yoke plate arrangement may further comprise a retaining feature for coupling the wear plate to the yoke plate. The wear surface may be for engaging a trunnion bearing.

First claim

What is claimed is:

1. A yoke plate arrangement, comprising:
a yoke plate;
a wear plate comprising a wear surface and a contact surface, wherein a post extends from the contact surface; and
a yoke plate ear extending from the yoke plate and comprising an anti-rotation surface that is normal to a radial direction of the yoke plate ear, wherein a first aperture is disposed in the yoke plate ear, the post is located at least partially within the first aperture, and the contact surface contacts the yoke plate ear via the anti-rotation surface to prevent the wear plate from rotating relative to the yoke plate ear.

2. The yoke plate arrangement of claim 1 , wherein the first aperture extends in a first direction and the yoke plate ear comprises a second aperture extending in a second direction, the second direction being substantially perpendicular to the first direction, wherein the first aperture and the second aperture align.

3. The yoke plate arrangement of claim 2 , further comprising a retaining feature, the retaining feature located at least partially within the second aperture and configured to retain the post inside of the first aperture.

4. The yoke plate arrangement of claim 3 , wherein the post includes a trench extending in the second direction, the retaining feature located at least partially in the trench.

5. The yoke plate arrangement of claim 3 , wherein the post includes a retaining aperture, the retaining feature located at least partially in the retaining aperture.

6. The yoke plate arrangement of claim 3 , wherein the retaining feature comprises a pin.

7. The yoke plate arrangement of claim 6 , wherein the retaining feature further comprises a set-screw, the set-screw threadingly attached to the second aperture.

8. The yoke plate arrangement of claim 2 , wherein the first direction comprises an axial direction and the second direction comprises a circumferential direction.

9. The yoke plate arrangement of claim 2 , wherein the wear surface is configured to contact a trunnion.

10. The yoke plate arrangement of claim 1 , wherein an anti-rotation surface disposed on the yoke plate ear, the anti-rotation surface configured to engage the wear plate to prevent the wear plate from rotating with respect to the yoke plate ear.

11. The yoke plate arrangement of claim 10 , wherein the anti-rotation surface is configured to engage a radially inward surface of the wear plate.

12. A propeller pitch change actuation system, comprising:
a propeller coupled to a trunnion;
a forward yoke plate coupled to a shaft, the forward yoke plate comprising a forward yoke plate ear extending from the forward yoke plate;
an aft yoke plate coupled to the shaft, the aft yoke plate comprising an aft yoke plate ear extending from the aft yoke plate and comprising an anti-rotation surface that is normal to a radial direction of the aft yoke plate ear, wherein a first aperture is disposed in the aft yoke plate ear, the first aperture extending in a first direction, the trunnion located between the forward yoke plate ear and the aft yoke plate ear; and
an aft wear plate coupled to the aft yoke plate ear comprising a wear surface and a contact surface, wherein a post extends from the contact surface, the post located at least partially inside of the first aperture,
wherein the contact surface contacts the aft yoke plate ear via the anti-rotation surface to prevent the aft wear plate from rotating relative to the aft yoke plate ear.

13. The propeller pitch change actuation system of claim 12 , wherein the propeller pitch change actuation system further comprises a forward wear plate coupled to the forward yoke plate ear.

14. The propeller pitch change actuation system of claim 13 , wherein the wear surface is in contact with the trunnion, the trunnion located between the aft wear plate and the forward wear plate.

15. The propeller pitch change actuation system of claim 14 , wherein the contact surface contacts the forward yoke plate ear.

16. The propeller pitch change actuation system of claim 15 , further comprising a retaining feature configured to retain the post within the first aperture.

17. The propeller pitch change actuation system of claim 16 , wherein a second aperture is disposed in the aft yoke plate ear, the second aperture extending in a second direction, the retaining feature located at least partially within the second aperture.

18. A method for installing a wear plate onto a yoke plate, comprising:
inserting a wear plate post into a first aperture disposed in the yoke plate;
pushing the wear plate post into the first aperture until a contact surface of the wear plate contacts a yoke plate ear;
inserting a pin into a second aperture disposed in the yoke plate;
attaching a set-screw to the yoke plate ear to retain the pin; and
preventing the wear plate from rotating relative to the yoke plate via an anti-rotation surface disposed on the yoke plate and in contact with the contact surface, the anti-rotation surface being normal to a radial direction of the yoke plate ear.

19. The method of claim 18 , wherein the pin is inserted into a trench located in the wear plate post in response to the inserting the pin into the second aperture.

20. The method of claim 18 , wherein the pin is inserted into a retaining aperture located in the wear plate post in response to the inserting the pin into the second aperture.

Assignees

• Hamilton Sundstrand Corp

Inventors

• Plickys Mark R

Classifications

• B63H3/00

  Propeller-blade pitch changing {(aircraft propellers B64C11/30; rotors of turbines F01D7/00; axial wind motors F03D7/022; axial-flow pumps F04D29/00)} · CPC title

• B64C11/32 Primary

  mechanical · CPC title

• B64F5/10

  Manufacturing or assembling aircraft, e.g. jigs therefor · CPC title

• B64C11/38

  fluid, e.g. hydraulic · CPC title