Aircraft passenger accommodation unit

Patent metadata

Field	Value
Publication number	US-12134474-B2
Application number	US-202017766878-A
Country	US
Kind code	B2
Filing date	Oct 7, 2020
Priority date	Oct 8, 2019
Publication date	Nov 5, 2024
Grant date	Nov 5, 2024

Abstract

The invention provides an aircraft passenger accommodation unit comprising a seat, a shell defining an opening that allows a passenger to egress between an aisle and the seat and a door, comprising a base portion, translatable in a first direction across the opening of the shell, between a retracted position and an extended position, and a second portion, translatable relative to the base portion in a second direction that is transverse to the first direction, between a stowed position and a deployed position. When the second portion is in the deployed position, the base portion is able to translate between the extended position and the retracted position. The invention also provides a method of opening and a method of closing a door.

First claim

The invention claimed is:

1. An aircraft passenger accommodation unit for location in an aircraft cabin adjacent to an aisle, comprising:
(i) a seat;
(ii) a shell at least partially surrounding the seat, wherein the shell defines an opening that allows a passenger to egress between the aisle and the seat; and
(iii) a door for providing variable access through the opening between the aisle and the seat, wherein the door comprises:
a base portion, translatable in a first direction across the opening of the shell, between a retracted position, which allows passenger egress between the seat and the aisle through the opening, and an extended position in which passenger egress between the aisle and the seat through the opening is at least partially blocked by the base portion; and
a second portion, translatable relative to the base portion in a second direction that is transverse to the first direction, the second portion being translatable between a stowed position in which the second portion at least partially overlaps the base portion to define a first overlap area of the base portion and a deployed position in which a second overlap area of the base portion is defined, the second overlap area being smaller than the first overlap area;
wherein, when the second portion is in the deployed position, the base portion is able to translate between the extended position and the retracted position,
the aircraft passenger accommodation unit further comprising a support mechanism, wherein the support mechanism is arranged to support the second portion when the second portion is in the deployed position, wherein the support mechanism comprises a guide mechanism arranged to guide translation of the second portion when the second portion is in the deployed position and the base portion is translated between the extended and retracted positions, and wherein the guide mechanism comprises a guide track and a corresponding guide member, wherein the second portion is provided with one of the guide track and the guide member, and the shell is provided with the other of the guide track and the guide member, and wherein the guide member and guide track are arranged so that the guide member is engageable with and translatable relative to the guide track, so as to guide translation of the second portion when the second portion is in the deployed position and the base portion is translated between the extended and retracted positions; and
wherein the guide member comprises at least two guide jaws, and a biasing member that biases the jaws towards each other to retain the guide track in between the jaws when the second portion is in the deployed position.

2. The aircraft passenger accommodation unit of claim 1 , wherein the guide track is provided on and extends across the second portion of the door in a direction substantially parallel to the first direction, and wherein the guide member is provided on the shell.

3. The aircraft passenger accommodation unit of claim 1 , wherein the guide member comprises a release latch, and wherein, when the release latch is activated, the release latch acts against the biasing member, and causes the guide jaws to move apart from each other and enables the guide track to be released.

4. The aircraft passenger accommodation unit of claim 3 , wherein the shell is provided with the guide member, and wherein at least a portion of the release latch protrudes from the shell.

5. The aircraft passenger accommodation unit of claim 3 , wherein, when the second portion is in the deployed position, activation of the release latch allows the second portion to move to the stowed position.

6. The aircraft passenger accommodation unit of claim 5 , wherein the guide member comprises a first guide member abutment surface and the guide track comprises a corresponding first guide track abutment surface, wherein the first guide member abutment surface and first guide track abutment surface are arranged such that the first guide member abutment surface abuts the first guide track abutment surface when the second portion is in the deployed position, thereby preventing one of:
a. movement of the second portion from the deployed position towards the stowed position, and
b. movement of the second portion from the deployed position further away from the stowed position.

7. The aircraft passenger accommodation unit of claim 6 , wherein the guide member comprises a second guide member abutment surface, facing in an opposite direction to the first guide member abutment surface, and the guide track comprises a second guide track abutment surface, facing in an opposite direction to the second guide track abutment surface, wherein the second guide member abutment surface and second guide track abutment surface are arranged such that the second guide member abutment surface abuts the second guide track abutment surface when the second portion is in the deployed position, thereby preventing the other of:
a. movement of the second portion from the deployed position towards the stowed position, and
b. movement from the deployed position further away from the stowed position.

8. The aircraft passenger accommodation unit of claim 1 , further comprising a deployment guide mechanism, wherein the deployment guide mechanism is arranged to guide translation of the second portion between the stowed position and the deployed position.

9. The aircraft passenger accommodation unit of claim 8 , wherein the deployment guide mechanism comprises a deployment guide track and a deployment guide member, wherein the base portion is provided with one of the deployment guide track and the deployment guide member, and the second portion is provided with the other of the deployment guide track and the deployment guide member, so as to guide translation of the second portion between the stowed position and the deployed position.

10. The aircraft passenger accommodation unit of claim 1 , further comprising a retraction guide mechanism, wherein the retraction guide mechanism is arranged to guide translation of the base portion between the retracted position and the extended position.

11. The aircraft passenger accommodation unit of claim 10 , wherein the retraction guide mechanism comprises a retraction guide track and a retraction guide member, wherein the base portion is provided with at least one of the retraction guide track and the retraction guide member, and wherein the shell is provided with the other of the retraction guide track and the retraction guide member, so as to guide translation of the base portion between the extended position and the retracted position.

12. The aircraft passenger accommodation unit of claim 1 , further comprising a securement mechanism, wherein the securement mechanism is arranged to secure the base portion in the extended position.

13. The aircraft passenger accommodation unit of claim 12 , wherein the securement mechanism comprises a magnetic latch, wherein the shell is provided with a first part of the latch, and the base portion is provided with a second part of the latch, the first and second parts being magnetically attracted to each other.

14. The aircraft passenger accommodation unit of claim 1 , wherein the shell comprises a cavity for housing the door when the base portion is in the retracted position.

15. The aircraft passenger accommodation unit of claim 14 , wherein the cavity provides space for the base portion and the second portion when the base portion is in the retracted position, and when the second portion is in the deployed position.

16. A method of opening or closing a door of an aircraft passe

Assignees

• Safran Seats Gb Ltd

Inventors

• Woodington James B
• Leung Heather Ck
• Riley Michael

Classifications

• E05Y2900/502

  for aircraft or spacecraft · CPC title

• E05D15/48

  allowing alternative movements ({E05D15/0604 takes precedence } ; for vertically-sliding wings E05D15/22) · CPC title

• E05D15/165

  Details, e.g. sliding or rolling guides (E05D15/18 - E05D15/24 take precedence) · CPC title

• E05C19/16

  Devices holding the wing by magnetic or electromagnetic attraction {(E05C17/56 takes precedence)} · CPC title

• B64D11/0606 Primary

  with privacy shells, screens, separators or the like (class dividers B64D11/0023) · CPC title