Escape hatch stay system

Patent metadata

Field	Value
Publication number	US-12264518-B2
Application number	US-202318354239-A
Country	US
Kind code	B2
Filing date	Jul 18, 2023
Priority date	Jul 18, 2022
Publication date	Apr 1, 2025
Grant date	Apr 1, 2025

Abstract

An escape hatch stay system for an aircraft and methods of using the escape hatch stay system. An escape hatch stay system includes a first stop arm, a second stop arm, and a gas strut. The first stop arm is rotatably coupled to the second stop arm, and the second stop arm is pivotably coupled to the gas strut. The first and second stop arms are lockable to preclude relative movement therebetween to lock the escape hatch in an open position. When the escape hatch is in the open position, the escape hatch may not be closed shut without manual intervention. When the escape hatch is in the open position, a load applicable to push the escape hatch open past the open position is damped by the gas strut.

First claim

The invention claimed is:

1. An escape hatch stay system for an escape hatch of an aircraft, comprising:
a first stop arm comprising a first end and a second end, the second end having associated therewith a protruding member and a catch, the protruding member comprising a stop;
a second stop arm comprising a first end and a second end, the second end having associated therewith a connecting member, the connecting member comprising a gap, an end stop surface, and a projection;
a gas strut having a first end and a second end, the second end coupled to the escape hatch; and
a bracket pivotably coupled to the escape hatch, the first end of the second stop arm and the first end of the gas strut each being attached to the bracket;
wherein:
the first end of the first stop arm is coupled to a supporting structure of the aircraft and the second end of the first stop arm is rotatably coupled to the second stop arm;
the first stop arm and the second stop arm are rotatably locked relative to each other to maintain the escape hatch in an open position when the stop abuts the end stop surface and the projection interfaces with the catch; and
the gas strut is configured to dampen a load applicable to push the escape hatch open past the open position.

2. The escape hatch stay system of claim 1 , wherein the gas strut comprises a rate-controlled damping strut.

3. The escape hatch stay system of claim 1 , wherein the first stop arm and the second stop arm are each in an extended position when the first stop arm is rotatably locked relative to the second stop arm.

4. The escape hatch stay system of claim 1 , wherein the first stop arm and the second stop arm are substantially parallel to and laterally displaced from each other when the escape hatch is in a closed position.

5. The escape hatch stay system of claim 1 , wherein a fastener extends through each of the protruding member and the connecting member to rotatably couple the second end of the first stop arm to the second end of the second stop arm.

6. The escape hatch stay system of claim 1 , wherein:
the connecting member has a first wall and a second wall facing the first wall; and
the projection includes a first projection associated with the first wall and a second projection associated with the second wall.

7. The escape hatch stay system of claim 1 , wherein the catch has a lock end and a trigger end.

8. The escape hatch stay system of claim 2 , wherein the trigger end is movable to selectively unlock the first stop arm from the second stop arm.

9. A method of using an escape hatch on an aircraft, comprising:
movably coupling a second end of a first stop arm to a second end of a second stop arm;
attaching a first end of the second stop arm and a first end of a gas strut to a bracket that is movably coupled to the escape hatch;
locking the escape hatch in an open position by locking the first stop arm and the second stop arm such that there is no relative movement therebetween;
damping, using the gas strut, a load applicable to push the escape hatch open past the open position; and
disassociating a catch of the first stop arm from a projecting member of the second stop arm to unlock the escape hatch.

10. The method of claim 9 , wherein the escape hatch moves from a closed position to the open position in a clockwise direction.

11. The method of claim 9 , further comprising attaching a first end of the first stop arm to a support structure of the aircraft.

12. The method of claim 11 , further comprising attaching a second end of the gas strut to the escape hatch.

13. The method of claim 9 , wherein the catch is V-shaped and has a trigger end and a lock end.

14. The method of claim 13 , wherein disassociating the catch from the projecting member comprises disassociating the lock end from the projecting member using the trigger end.

15. The method of claim 14 , wherein the second stop arm, at the second end thereof, includes a connecting member with a hole and a stop.

16. An escape hatch stay system for an escape hatch of an aircraft, comprising:
a first stop arm, a second stop arm, and a gas strut, the second stop arm rotatably coupled to the first stop arm and pivotably coupled to the gas strut via a bracket, the first stop arm rotatably lockable relative to the second stop arm to lock the escape hatch in an open position;
wherein, a load applicable to push the escape hatch open past the open position is damped by the gas strut.

17. The escape hatch stay system of claim 16 , wherein the first stop arm is coupled to a supporting structure that surrounds the escape hatch.

18. The escape hatch stay system of claim 16 , further comprising a catch with a trigger end and a lock end.

19. The escape hatch stay system of claim 18 , wherein the catch is associated with a second end of the first stop arm.

20. The escape hatch stay system of claim 19 , further comprising a projection configured to interface with the catch to lock the first stop arm relative to the second stop arm.

Assignees

• Textron Aviation Inc
• Textron Innovations Inc

Inventors

• Lay Michael Clinton
• Johnson Evan M
• Hoetmer Isaac Anthony
• Pegg Joel Allen
• Harrison Edward Donald

Classifications

• E05C17/32 Primary

  consisting of two or more pivoted rods · CPC title

• E05B41/00 Primary

  Locks with visible indication as to whether the lock is locked or unlocked {(indicator lights E05B17/10)} · CPC title

• E05B85/10

  Handles · CPC title

• E05F1/1091

  with a gas spring (E05F1/1292 takes precedence) · CPC title

• B64C1/1423 Primary

  Passenger doors · CPC title