Attachment for rotary actuator to wing

Patent metadata

Field	Value
Publication number	US-12313148-B2
Application number	US-202217979881-A
Country	US
Kind code	B2
Filing date	Nov 3, 2022
Priority date	Nov 4, 2021
Publication date	May 27, 2025
Grant date	May 27, 2025

Abstract

A rotary actuator mounting system configured to attach a rotary actuator to and between two relatively moveable parts, the rotary actuator being attached to a first of the two relatively moveable parts and to a second of the relatively moveable parts such that operation of the actuator causes one of the first and second relatively movable parts to rotate relative to the other of the first and second relatively movable parts about an axis of the rotary actuator. The system includes a compliant attachment component connecting the actuator to the first relatively moveable part, the compliant attachment component having a first end attached to the first movable part and a second end attached to the actuator, and wherein at least one of the first and the second end is in the form of a ball bearing arranged to be received in a complementary socket on the actuator and/or the first movable part.

First claim

The invention claimed is:

1. A rotary actuator mounting system configured to:
attach a rotary actuator to and between two relatively moveable parts, the rotary actuator including a stator configured to attach to a first of the two relatively moveable parts and a rotor part rotatable relative to the stator part, configured to be attached to a second of the two relatively moveable parts such that operation of the actuator causes one of the first and second relatively movable parts to rotate relative to the other of the first and second relatively movable parts about an axis of the rotary actuator, the mounting system further comprising:
a compliant attachment component for connecting the stator part to the first relatively moveable part, the compliant attachment component having a first end configured to be attached to the first movable part and the stator part of the actuator,
wherein at least one of the first end and the second end is in the form of a ball bearing arranged to be received in a complementary socket on the actuator and/or the first movable part;
wherein one or both the first end and the second end is a ball bearing.

2. The rotary actuator mounting system of claim 1 , wherein the rotary actuator comprises one or more earth members and wherein the first end of the attachment component is attached to an earth member.

3. The rotary actuation mounting system of claim 1 , wherein the rotary actuator comprises an output rotor attached to the second relatively moveable part.

4. The rotary actuation mounting system of claim 1 , wherein the rotary actuator is a rotary geared actuator.

5. The rotary actuator mounting system of claim 1 , wherein the compliant attachment component comprises two compliant attachment components, wherein a first compliant attachment component is attached between a first location of the actuator and a first side of the first relatively movable part and a second compliant attachment component is attached between a second location of the actuator and a second side of the first relatively movable structure.

6. The rotary actuator mounting system of claim 5 , wherein the actuator comprises a first earth member at the first location, to which the first compliant attachment component is attached, and a second earth member at the second location, to which the second compliant attachment component is attached.

7. An aircraft wing comprising:
a main wing body part;
a second wing part movable relative to the main wing body part; and
a rotary actuator mounting system as claimed in claim 1 arranged to mount the rotary actuator to one of the main wing body part and the second wing part to cause rotation of the second wing part relative to the main wing body part.

8. The aircraft wing as claimed in claim 7 , wherein the actuator is mounted to the main wing body part.

9. The aircraft wing as claimed in claim 7 , wherein the second wing part is a wing tip.

Assignees

• Goodrich Actuation Systems Ltd

Inventors

• Darby Jonathan

Classifications

• B64C13/28 Primary

  mechanical · CPC title

• B64C23/072

  the wing tip airfoil devices being moveable in their entirety · CPC title

• B64C9/02

  Mounting or supporting thereof · CPC title

• B64C3/56

  Folding or collapsing to reduce overall dimensions of aircraft · CPC title

• F16H19/08 Primary

  for interconverting rotary motion and oscillating motion · CPC title