Bidirectional hatch for passenger rest compartment

Patent metadata

Field	Value
Publication number	US-11235852-B2
Application number	US-201816127088-A
Country	US
Kind code	B2
Filing date	Sep 10, 2018
Priority date	Sep 10, 2018
Publication date	Feb 1, 2022
Grant date	Feb 1, 2022

Abstract

A bi-directional egress hatch for a passenger aircraft may allow passengers to rapidly and safely exit an overhead cabin of the aircraft onto the main deck, while allowing cabin crew to safely ascend into the overhead cabin if need be. Hatch panels may blend in with overhead bin doors and ceiling panels of the main cabin; the inner portions of the hatch panels (facing the overhead cabin) may include anti-skid portions and graspable handles for descending passengers. The hatch may be easily activated by a passenger with a single motion (or remotely activated, or autodeployed). Once activated, the hatch panels may swing open and a telescoping ladder may deploy from the inner portion to the main deck, remaining rigid once reaching the floor. Similarly, any barriers protecting the ladder from passengers in the overhead cabin may be released, granting access to the telescoping ladder.

First claim

We claim:

1. A bidirectional hatch for a passenger aircraft, comprising:
at least one hatch panel disposed in an overhead area of an aircraft and capable of transitioning from a closed state to an open state when the hatch is activated, the hatch panel having an inner portion and an outer portion;
and
at least one ascent/descent device coupled to the inner portion, the ascent/descent device including a telescoping ladder comprising at least two telescoping vertical rails connected by a plurality of rungs, the rails and the rungs fashioned of a rigid material, the telescoping ladder configured to:
deploy toward a deck located beneath the overhead area when the hatch is activated;
and
remain in a rigid state when the telescoping ladder has deployed toward the deck;

the ascent/descent device configured to, in its deployed state, allow at least one individual to 1 ) descend from the overhead area to the deck and 2 ) ascend from the deck to the overhead area.

2. The bidirectional hatch of claim 1 , further comprising:
at least one rail fixed to the inner portion on either side of the ascent/descent device, the rail configured to be grasped by the individual.

3. The bidirectional hatch of claim 1 , wherein:
the deck includes at least one passenger cabin including at least one of a ceiling panel and an overhead bin usable by a passenger, the overhead bin accessible via a bin door;
and
the outer portion is configured to appear substantially identical to at least one of the bin door and the ceiling panel.

4. The bidirectional hatch of claim 3 , wherein the ascent/descent device is configured to deploy into an aisle within the passenger cabin.

5. The bidirectional hatch of claim 4 , wherein the aisle includes one or more of:
a longitudinal aisle substantially parallel to a longitudinal or roll axis of the aircraft;
and
a cross aisle substantially parallel to a lateral or pitch axis of the aircraft.

6. The bidirectional hatch of claim 1 , wherein the at least one hatch panel is a primary hatch, further comprising:
at least one second hatch configured to pivot toward an adjacent ceiling panel of the aircraft when transitioning from the closed state to the open state.

7. The bidirectional hatch of claim 1 , wherein the overhead area includes an overhead passenger cabin comprising one or more passenger compartments accessible via a corridor.

8. The bidirectional hatch of claim 7 , wherein the inner portion is accessible from the overhead passenger cabin via a removable panel disposed within the corridor.

9. The bidirectional hatch of claim 7 , wherein:
at least one of the one or more passenger compartments includes a bunk capable of accommodating at least one passenger;
and
the inner portion is accessible from the passenger compartment via the bunk.

10. The bidirectional hatch of claim 1 , wherein the ascent/descent device includes at least one damper device configured to regulate a rate of deployment of the ascent/descent device.

11. The bidirectional hatch of claim 1 , wherein the hatch is capable of activation by the individual via an activation device disposed within the overhead area.

12. The bidirectional hatch of claim 1 , wherein the hatch is automatically deployable.

13. The bidirectional hatch of claim 1 , wherein the hatch is remotely deployable.

14. The bidirectional hatch of claim 1 , wherein the ascent/descent device is stored behind a safety barrier when not in its deployed state, the safety barrier releasable when the hatch is activated.

15. The bidirectional hatch of claim 14 , wherein the safety barrier includes a safety net.

16. The bidirectional hatch of claim 1 , wherein the inner portion is at least partially covered by an anti-skid surface.

17. The bidirectional hatch of claim 1 , wherein the bidirectional hatch is disposed within a monument.

18. The bidirectional hatch of claim 1 , wherein the bidirectional hatch is disposed within an entry vestibule connecting the overhead area and the deck.

Assignees

• Rockwell Collins Inc
• Be Aerospace Inc

Inventors

• Behr Nicolas
• Moe Daniel N
• Barrett David

Classifications

• B64C1/32

  Severable or jettisonable parts of fuselage facilitating emergency escape · CPC title

• B64D11/00 Primary

  Passenger or crew accommodation; Flight-deck installations not otherwise provided for · CPC title

• B64D2011/0084

  Bed units for passengers attached to the ceiling of the fuselage · CPC title

• B64D2011/0076

  for crew members, e.g. for sleeping during flight · CPC title

• B64C1/14

  Windows; Doors; Hatch covers or access panels; Surrounding frame structures; Canopies; Windscreens {accessories therefor, e.g. pressure sensors, water deflectors, hinges, seals, handles, latches, windscreen wipers}(fairings movable in conjunction with undercarriage elements B64C25/16; bomb doors B64D1/06) · CPC title