Aircraft latch assembly with lock

Patent metadata

Field	Value
Publication number	US-12480342-B2
Application number	US-202318388656-A
Country	US
Kind code	B2
Filing date	Nov 10, 2023
Priority date	Nov 10, 2022
Publication date	Nov 25, 2025
Grant date	Nov 25, 2025

Abstract

An aircraft assembly includes a keeper, a latch and a lock. The latch includes a handle and a hook structure operatively coupled to the handle. The hook structure is engaged with the keeper when the handle is in a closed position. The hook structure is disengaged from the keeper when the handle is in an open position. The lock includes a catch, a lever and a spring. The lever is configured to rotate about an axis between a locked position and an unlocked position. The lever is aligned with the catch locking the handle in the closed position when the lever is in the locked position. The lever is misaligned from the catch unlocking the handle from the closed position when the lever is in the unlocked position. The spring biases the lever axially along the axis in a direction towards the handle.

First claim

What is claimed is:

1 . An assembly for an aircraft, comprising:
a keeper; a latch including a handle and a hook structure operatively coupled to the handle, the handle configured to move between a closed position and an open position, the hook structure engaged with the keeper when the handle is in the closed position, and the hook structure disengaged from the keeper when the handle is in the open position; a handle release device comprising a push button, the handle release device configured to lock the handle in the closed position when the push button is in a first position, the handle release device configured to unlock the handle from the closed position when the push button is in a second position, and the push button forming a catch; and a lock including the catch, a lever and a spring, the lever configured to rotate about an axis between a locked position and an unlocked position, the lever aligned with the catch locking the handle in the closed position when the lever is in the locked position, the lever misaligned from the catch unlocking the handle from the closed position when the lever is in the unlocked position, and the spring biasing the lever axially along the axis in a direction towards the handle.

2 . The assembly of claim 1 , wherein the spring comprises a coil spring.

3 . The assembly of claim 1 , wherein the spring is axially adjacent and contacts the lever.

4 . The assembly of claim 1 , wherein
the lock further includes a bolt rotatably mounted to the handle; the lever is rotationally fixed to the bolt; and the spring is mounted on and circumscribes the bolt.

5 . The assembly of claim 4 , wherein the lever is configured to axially translate along the bolt.

6 . The assembly of claim 4 , wherein the bolt projects axially away from the handle and sequentially through the lever and the coil spring to an interior distal end of the bolt.

7 . The assembly of claim 6 , wherein
the lock further includes a retainer mounted to the bolt at the interior distal end; and the spring is arranged axially between the lever and the retainer.

8 . The assembly of claim 4 , wherein
the lock further includes a mount and a retainer; the mount rotatably mounts the bolt to the handle; the retainer is mounted to the bolt; and the spring is arranged axially between the lever and the retainer, and the spring presses the lever axially against the mount.

9 . The assembly of claim 4 , wherein
the bolt projects axially into an aperture in the handle and to an exterior distal end of the bolt; and the bolt has a wrenching feature at the exterior distal end.

10 . The assembly of claim 1 , wherein the push button is nested in an aperture in the handle.

11 . The assembly of claim 1 , wherein the handle release device is pivotally mounted to the handle.

12 . The assembly of claim 1 , wherein
the handle extends longitudinally between a first end and a second end; and the lock is arranged at an intermediate location between the first end and the second end.

13 . The assembly of claim 1 , wherein the lever overlaps a side of the catch when the lever is in the locked position.

14 . The assembly of claim 1 , wherein the lever projects into a slot in the catch when the lever is in the locked position.

15 . The assembly of claim 1 , further comprising:
a fixed structure; a first aircraft component pivotally attached to the fixed structure, the latch mounted to the first aircraft component; and a second aircraft component pivotally attached to the fixed structure, the keeper mounted to the second aircraft component.

16 . An assembly for an aircraft, comprising:
a latch including a handle and a hook structure operatively coupled to the handle, the handle configured to move between a closed position and an open position; a handle release device mounted to the handle and comprising a push button, the handle release device configured to lock the handle in the closed position when the push button is in an undepressed position, and the handle release device configured to unlock the handle from the closed position when the push button is in a depressed position; and a lock including a lever and a spring, the lever mounted to the handle and configured to rotate about an axis between a locked position and an unlocked position, the lever aligned with the push button locking the push button in the undepressed position when the lever is in the locked position, the lever misaligned from the push button unlocking the push button from the undepressed position when the lever is in the unlocked position, and the spring biasing the lever axially along the axis in a direction towards the handle.

17 . The assembly of claim 16 , wherein the handle release device locks the handle to the hook structure when the push button is in the undepressed position.

18 . An assembly for an aircraft, comprising:
a latch including a handle and a hook structure operatively coupled to the handle, the handle configured to move between a closed position and an open position; a handle release device comprising a catch, the handle release device configured to lock the handle in the closed position when the catch is in a first position, the handle release device configured to unlock the handle from the closed position when the catch is in a second position; and a lock including the catch, a mount, a bolt, a lever, a spring and a retainer, the mount rotatably attaching the bolt to the handle, the bolt projecting axially along an axis out of an aperture in the handle and sequentially through the mount, the lever, the spring and the retainer, the lever rotationally fixed to the bolt and configured to rotate about the axis between a locked position and an unlocked position, the lever aligned with the catch locking the handle in the closed position when the lever is in the locked position, the lever misaligned from the catch unlocking the handle from the closed position when the lever is in the unlocked position, and the spring axially compressed between the lever and the retainer.

19 . The assembly of claim 18 , wherein
a push button forms the catch; and the push button is nested in an aperture in the handle.

Assignees

• Rohr Inc

Inventors

• Shivarudrappa Shashidhar
• Challamreddy Sangareddy

Classifications

• B64D29/06 Primary

  Attaching of nacelles, fairings or cowlings · CPC title

• E05B13/10

  formed by a lock arranged in the handle · CPC title

• E05C19/145

  flush · CPC title

• E05C3/08 Primary

  the handle or member moving essentially towards or away from the plane of the wing or frame · CPC title