System for securing an aircraft door

Patent metadata

Field	Value
Publication number	US-9868505-B2
Application number	US-201715444762-A
Country	US
Kind code	B2
Filing date	Feb 28, 2017
Priority date	Nov 19, 2015
Publication date	Jan 16, 2018
Grant date	Jan 16, 2018

Abstract

Systems and methods for securing an emergency exit door on an armrest of a seat are provided. A system includes a latch connected to an armrest of a seat of a vehicle. The latch is moveable relative to the armrest between a stowed position and a deployed position. The latch is structured and arranged to engage an edge of a door that is associated with an exit of the vehicle to hold the door on the armrest.

First claim

What is claimed is:

1. A method, comprising:
detecting an action at a door associated with an overwing exit at an exit row of an aircraft; and
modifying a seat in the exit row based on the detecting the action at the door, wherein the modifying the seat comprises at least one of:
automatically deploying a latch in an armrest of the seat;
automatically rotating a distal end of the armrest downward; and
automatically moving the seat to increase a size of an egress path of the exit row.

2. The method of claim 1 , wherein a sensor performs the detecting.

3. The method of claim 1 , wherein an actuation system performs the modifying.

4. The method of claim 1 , wherein the detected action at the door comprises one of:
movement of a handle of the door beyond a threshold position; and
movement of the door out of the exit.

5. The method of claim 1 , wherein the modifying the seat comprises both of:
the automatically deploying the latch in the armrest of the seat; and
the automatically rotating the distal end of the armrest downward.

6. The method of claim 5 , further comprising locking the latch in a deployed position after the automatically deploying the latch.

7. The method of claim 1 , wherein the modifying the seat comprises both of:
the automatically deploying the latch in the armrest of the seat; and
the automatically moving the seat to increase the size of the egress path of the exit row.

8. The method of claim 7 , wherein the moving the seat comprises moving the seat in an aft direction along a floor of the aircraft.

9. The method of claim 8 , further comprising, based on the detecting the action at the door, moving another seat in a forward direction along the floor of the aircraft.

10. The method of claim 7 , further comprising locking the latch in a deployed position after the automatically deploying the latch.

Assignees

• IBM

Inventors

• Childress Rhonda L
• Eckert Kim A
• Kuang Jente B
• Kumhyr David B
• Mcnair Ryan D

Classifications

• B60N2/4279

  electric or electronic triggering · CPC title

• E05C19/02

  Automatic catches, i.e. released by pull or pressure on the wing (E05C19/06 takes precedence {; with locking means E05B63/22}) · CPC title

• B64C1/1423 Primary

  Passenger doors · CPC title

• E06B7/00

  Special arrangements or measures in connection with doors or windows ({arrangements against burglary at the edges of the wings E06B5/113} ; screening or similar protective devices E06B9/00) · CPC title

• B64D11/064

  Adjustable inclination or position of seats · CPC title