Retractable landing gear

Patent metadata

Field	Value
Publication number	US-10000279-B2
Application number	US-201615001841-A
Country	US
Kind code	B2
Filing date	Jan 20, 2016
Priority date	Mar 24, 2015
Publication date	Jun 19, 2018
Grant date	Jun 19, 2018

Abstract

The present disclosure describes systems and methods for retractable landing gear. A landing gear arrangement may comprise: a trailing arm; a shock strut; a link rotatably coupled to a first end of the shock strut and rotatably coupled to the trailing arm, the link including a pivot; a rotatable latch rotatably coupled to the link; and an actuator coupled between the rotatable latch and the trailing arm, the rotatable latch configured to rotate about the pivot, the pivot located between a first end and a second end of the rotatable latch, the rotatable latch configured to rotate in a first direction in response to the actuator extending and configured to rotate in a second direction in response to the actuator compressing.

First claim

What is claimed is:

1. A landing gear arrangement comprising:
a trailing arm;
a shock strut;
a link rotatably coupled to a first end of the shock strut and rotatably coupled to the trailing arm, the link including a pivot;
a rotatable latch rotatably coupled to the link; and
an actuator coupled between the rotatable latch and the trailing arm, the rotatable latch configured to rotate about the pivot, the pivot located between a first end and a second end of the rotatable latch, the rotatable latch configured to rotate in a first rotational direction in response to the actuator extending and configured to rotate in a second rotational direction in response to the actuator compressing.

2. The landing gear arrangement of claim 1 , wherein the link is configured to rotate in the first rotational direction in response to the actuator extending and configured to rotate in the second rotational direction in response to the actuator compressing.

3. The landing gear arrangement of claim 2 , wherein the landing gear arrangement is configured to move to an extended position in response to the actuator compressing and is configured to move to a stowed position in response to the actuator extending.

4. The landing gear arrangement of claim 3 , wherein the trailing arm includes a receiving member, the receiving member configured to receive a portion of the link in response to the landing gear arrangement moving to the extended position.

5. The landing gear arrangement of claim 4 , wherein the trailing arm includes a first roller pin and a second roller pin, the rotatable latch configured to be fastened to the first roller pin in response to the actuator compressing and configured to be fastened to the second roller pin in response to the actuator extending.

6. The landing gear arrangement of claim 1 , wherein the trailing arm is configured to be rotatably coupled to a fuselage at a first end of the trailing arm and configured to be coupled to an axle at a second end of the trailing arm.

7. The landing gear arrangement of claim 6 , wherein the actuator is coupled to the trailing arm proximate the first end and the link is coupled to the trailing arm proximate the second end.

8. The landing gear arrangement of claim 1 , wherein a second end of the shock strut is rotably coupled to a fuselage.

9. The landing gear arrangement of claim 1 , wherein the link is connected to the shock strut and the trailing arm via a pin connection at each end.

10. A landing gear arrangement, comprising:
a rotatable latch rotatably coupled to a pivot, the pivot located on a link between a trailing arm and a first end of a shock strut; and
an actuator operatively coupled to the rotatable latch, the actuator configured to actuate in a first linear direction to apply a first moment to the rotatable latch to rotate the rotatable latch in a first rotational direction, wherein the rotatable latch disengages a first roller pin in response to the rotation.

11. The landing gear arrangement of claim 10 , wherein the actuator is configured to actuate in a second linear direction to apply a second moment to the rotatable latch to rotate the rotatable latch in a second rotational direction, wherein the rotatable latch disengages a second roller pin in response to the rotation.

12. The landing gear arrangement of claim 11 , wherein the trailing arm is configured to rotate about a first end of the trailing arm in the first rotational direction in response to the actuator actuating in the second linear direction, and configured to rotate about the first end of the trailing arm in the second rotational direction in response to the actuator actuating in the first linear direction.

13. The landing gear arrangement of claim 12 , wherein a first end of the link is configured to be received by a receiving member in response to the actuator actuating in the second linear direction.

14. The landing gear arrangement of claim 13 , wherein the trailing arm is rotatably coupled to a fuselage at the first end of the trailing arm and coupled to an axle at a second end of the trailing arm.

15. The landing gear arrangement of claim 14 , wherein the shock strut is rotatably coupled to the link at the first end of the shock strut and rotatably coupled to the fuselage at a second end of the shock strut.

16. The landing gear arrangement of claim 15 , wherein the rotatable latch is configured to engage a stopper in response to the rotatable latch rotating in at least one of the first rotational direction and the second rotational direction.

17. The landing gear arrangement of claim 16 , wherein at least one of the trailing arm, the link, or the rotatable latch comprises steel.

Assignees

• Goodrich Corp

Inventors

• Luce William E

Classifications

• B64C25/10 Primary

  retractable, foldable, or the like · CPC title