Locking device

Patent metadata

Field	Value
Publication number	US-11267554-B2
Application number	US-202016775873-A
Country	US
Kind code	B2
Filing date	Jan 29, 2020
Priority date	Dec 21, 2016
Publication date	Mar 8, 2022
Grant date	Mar 8, 2022

Abstract

A locking pin associated with one of a fixed wing and a wing tip device, and a bush associated with the other of the fixed wing and wing tip device, the bush configured to receive the locking pin. The bush is located within a bush housing arranged to allow relative movement of the bush in the direction of a longitudinal axis of the locking pin when the locking pin is received within the bush.

First claim

The invention claimed is:

1. A locking mechanism configured for a wing assembly including a fixed wing and a wing tip device, the locking mechanism comprising;
a locking pin mounted to a socket in the fixed wing or the wing tip device of the wing assembly, wherein the locking pin is configured to slide in the socket in a direction of a longitudinal axis of the locking pin and between a retracted position and an extended position;
a bush configured to receive the locking pin while in the extended position and to be disengaged from the locking pin while the locking pin is in the retracted position;
a bush housing fixed to another of the fixed wing and the wing tip device, wherein bush housing includes an aperture configured to receive the bush to allow relative movement of the bush in the direction of the longitudinal axis of the locking pin, and
a Belleville washer in the aperture and between the bush and bush housing.

2. The locking mechanism of claim 1 , wherein a surface of the aperture of the bush housing includes a first ledge extending inward towards the bush, the bush has an outer surface including a second ledge extending outward towards the surface of the aperture of the brush housing, and the Belleville washer is between the first ledge and the second ledge in the direction of the longitudinal axis.

3. The locking mechanism of claim 2 , wherein the aperture of the brush housing includes a third ledge separated from the first ledge in the direction of the longitudinal axis, and the locking mechanism further comprises a second Belleville washer between the bush housing and the bush, and adjacent the third ledge.

4. The locking mechanism of claim 1 , wherein the bush includes an obround aperture configured to receive the locking pin.

5. The locking mechanism of claim 4 , wherein the locking pin includes opposing planar faces configured to face straight sides of the obround aperture in the bush.

6. The locking mechanism of claim 5 , wherein the locking pin includes a first portion which is cylindrical in cross section and a second portion with includes the opposing planar faces, and wherein only the second portion is received by the bush.

7. The locking mechanism of claim 4 , wherein the locking pin includes opposing convex faces and each of the convex faces spans between the opposing planar faces.

8. The locking mechanism of claim 1 , further comprising a detent protruding from an inside surface of the aperture of the bush housing and a recess in an outer surface of the bush, wherein the recess is configured to receive the detent.

Assignees

• Airbus Operations Ltd

Inventors

• Brakes David
• Wildman Eric

Classifications

• B64C3/56 Primary

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

• B64C3/40 Primary

  Varying angle of sweep · CPC title

• B64C23/065

  at the wing tips · CPC title

• F16B21/00

  Means for preventing relative axial movement of a pin, spigot, shaft or the like and a member surrounding it (riveted or deformable spigots F16B19/04; for gudgeon pins F16J1/18); Stud-and-socket releasable fastenings · CPC title

• B64C3/38

  Adjustment of complete wings or parts thereof · CPC title