Airline door retractable wave fence with steps for evacuation

Patent metadata

Field	Value
Publication number	US-9902485-B2
Application number	US-201414311105-A
Country	US
Kind code	B2
Filing date	Jun 20, 2014
Priority date	Jun 20, 2014
Publication date	Feb 27, 2018
Grant date	Feb 27, 2018

Abstract

Systems, methods, and apparatus for permitting evacuation of an aircraft following a water landing are disclosed. In one or more embodiments, the disclosed method involves deploying, an evacuation unit, from inside a storage housing located proximate a door of the aircraft. In one or more embodiments, the evacuation unit comprises at least one step and a wave fence. In at least one embodiment, when the evacuation unit is fully deployed, at least a portion of the wave fence is in water-tight contact with at least a portion of a frame of the door such that water flow into the aircraft is prevented and/or inhibited.

First claim

We claim:

1. A method for permitting evacuation of an aircraft following a water landing, the method comprising:
deploying an evacuation unit of the aircraft from inside a storage housing located proximate a door of the aircraft,
wherein the evacuation unit comprises at least two step, a wave fence, and an infrastructure comprising a plurality of bars, and
wherein when the evacuation unit is fully deployed, at least a portion of the wave fence is in water-tight contact with at least a portion of a frame of the door such that water flow into the aircraft is at least one of prevented and inhibited.

2. The method of claim 1 , wherein a top step of the at least two steps comprises an upper surface of the wave fence upon which an occupant evacuating the aircraft can step.

3. The method of claim 1 , wherein the storage housing is one of located under at least one floor panel, located on a portion of an inflatable slide, located on an interior wall of the aircraft, and located on an exterior wall of the aircraft.

4. The method of claim 1 , wherein the method further comprises opening the storage housing to expose the evacuation unit for deployment.

5. The method of claim 1 , wherein after deployment of the evacuation unit, the wave fence is located at least one of interior to the aircraft and exterior to the aircraft.

6. The method of claim 1 , wherein the infrastructure is foldable.

7. The method of claim 6 , wherein the deploying of the evacuation unit comprises unfolding the infrastructure by at least one of compressed gas, hydraulics, electrical power, pneumatics, at least one spring, and at least one manual pump.

8. The method of claim 6 , wherein the method further comprises:
attaching, to a first location proximate a first side of the frame of the door, a first side of the wave fence; and
attaching, to a second location proximate a second side of the frame of the door, a second side of the wave fence.

9. The method of claim 8 , wherein the attaching of the first side of the wave fence to the first location and the attaching of the second side of the wave fence to the second location are via at least one of at least one rail, at least one fastener, and at least one zipper.

10. An apparatus for permitting evacuation of an aircraft following a water landing, the apparatus comprising:
at least two steps;
a wave fence;
an infrastructure comprising a plurality of bars; and
a storage housing located at least partially within a floor of the aircraft and located proximate a door of the aircraft,
wherein the apparatus of the aircraft is to be deployed from inside the storage housing, and
wherein when the apparatus is fully deployed, at least a portion of the wave fence is in water-tight contact with at least a portion of a frame of the door such that water flow into the aircraft is at least one of prevented and inhibited.

11. The apparatus of claim 10 , wherein a top step of the at least two steps comprises an upper surface of the wave fence upon which an occupant evacuating the aircraft can step.

12. The apparatus of claim 10 , wherein the infrastructure is foldable.

13. The apparatus of claim 12 , wherein the apparatus is configured to deploy by unfolding the infrastructure by at least one of compressed gas, hydraulics, electrical power, pneumatics, at least one spring, and at least one manual pump.

14. A system for permitting evacuation of an aircraft following a water landing, the system comprising:
an evacuation unit of the aircraft to be deployed from inside a storage housing,
wherein the evacuation unit comprises at least two step, a wave fence, and an infrastructure comprising a plurality of bars; and
the storage housing located at least partially within a floor of the aircraft and located proximate a door of the aircraft; and
wherein when the evacuation unit is fully deployed, at least a portion of the wave fence is in water-tight contact with at least a portion of a frame of the door such that water flow into the aircraft is at least one of prevented and inhibited.

15. The system of claim 14 , wherein a top step of the at least two steps comprises an upper surface of the wave fence upon which an occupant evacuating the aircraft can step.

16. The system of claim 14 , wherein the infrastructure is foldable.

17. The system of claim 16 , wherein the evacuation unit is configured to deploy by unfolding the infrastructure by at least one of compressed gas, hydraulics, electrical power, pneumatics, at least one spring, and at least one manual pump.

Assignees

• Boeing Co

Inventors

• Barmichev Sergey
• Sankrithi Mithra
• Eckert David

Classifications

• B64D25/18

  Flotation gear · CPC title

• B64D25/14

  Inflatable escape chutes · CPC title

• B64D25/08

  Ejecting or escaping means · CPC title

• B64C1/24 Primary

  Steps mounted on, and retractable within, fuselages · CPC title

• Y10S244/905

  Cross-Sectional Technologies · mapped topic