Three-place berthing aircraft divan

Patent metadata

Field	Value
Publication number	US-11059589-B2
Application number	US-201816054036-A
Country	US
Kind code	B2
Filing date	Aug 3, 2018
Priority date	Aug 3, 2018
Publication date	Jul 13, 2021
Grant date	Jul 13, 2021

Abstract

A three-place aircraft divan configured to be installed side-facing in an aircraft and track between an upright sitting position and a berth position. Seat bottom and backrest portions of the divan are movably supported on a static frame and track together. The divan includes inflatable passenger restraints at each seat place and a leg flail prevention device at one end of the frame triggered to actuate in response to an event sensed by a mechanical crash sensor. The inboard leg arrangement of the divan accommodates the installation of two containers for containing high-capacity life rafts under the seat bottom frame, among other equipment.

First claim

What is claimed is:

1. A three-place berthing aircraft divan, comprising:
a fixed frame comprising a seat bottom frame and a backrest frame;
first, second and third inboard legs affixed to the seat bottom frame;
a seat bottom comprising a tracking platform supported by the seat bottom frame and movable relative thereto to track between an upright sitting position and a berth position;
a backrest comprising a back follower supported by the backrest frame and movable relative thereto, the back follower and the tracking platform linked such that the back follower and the tracking platform track together between the upright sitting position and the berth position;
a passenger restraint provided at each seat place, each passenger restraint including a lap belt anchored to the tracking platform and a should harness detachable from the lap belt; and
an automatic leg flail prevention device disposed at one end of the seat bottom frame;
wherein the tracking platform interlocks with the seat bottom frame and each of the lap belts are affixed to an outboard tube of the tracking platform such that each of the lap belts track inboard with the tracking platform and loading on each of the lap belts is transferred to the seat bottom frame through the tracking platform.

2. The aircraft divan of claim 1 , wherein:
the first leg and the third leg are disposed at opposing ends of the seat bottom frame;
the second leg is disposed midway between the first leg and the third leg;
the first leg and the second leg are spaced apart a predetermined distance such that a first container for containing a high-capacity life raft can be installed under the seat bottom frame between the first leg and the second leg; and
the second leg and the third leg are spaced apart a predetermined distance such that a second container for containing a high-capacity life raft can be installed under the seat bottom frame between the second leg and the third leg.

3. The aircraft divan of claim 1 , wherein:
the seat bottom frame comprises lateral frame members at opposing ends thereof each comprising a first track and a second track along which respective first and second guides carried on the tracking platform are guided as the aircraft divan tracks between the upright sitting position and the berth position; and
the backrest frame comprises lateral frame members at opposing ends thereof each comprising a single track along which guides carried on the back follower are guided as the aircraft divan tracks between the upright sitting position and the berth position.

4. The aircraft divan of claim 1 , wherein:
the tracking platform is aligned atop the seat bottom frame when the aircraft divan is in the upright sitting position and the tracking platform tracks inboard in a direction of an adjacent aisle and overhangs the aisle when the aircraft divan is in the berth position; and
the back follower is aligned forward of the backrest frame when the aircraft divan is in the upright sitting position and is positioned atop the seat bottom frame when the aircraft divan is in the berth position.

5. The aircraft divan of claim 1 , further comprising:
a headrest position atop the backrest frame;
cushions affixed to the backrest; and
cushions affixed to the seat bottom.

6. The aircraft divan of claim 1 , wherein the shoulder harness of each passenger restraint is an inflatable shoulder harness detachable from the lap belt, wherein one end of the inflatable shoulder harness is wound on a retractor disposed under the seat bottom frame, and wherein a portion of the inflatable shoulder harness is routed outboard of the backrest frame and stows outside of the retractor such that the retractor provides unceasing tension on the inflatable shoulder harness.

7. The aircraft divan of claim 1 , further comprising a tracking handle disposed at one end of the seat bottom frame coupled to at least one locking pin preventing relative movement between the tracking platform and the seat bottom frame, the tracking handle actuated to disengage the at least one locking pin to allow the aircraft divan to track from the berth position to the upright sitting position.

8. The aircraft divan of claim 1 , further comprising a mechanical crash sensor unit operably connected to the passenger restraints and the automatic leg flail prevention device, the mechanical crash sensor unit including a processor configured to sense a crash event, and in response to the sensed crash event, trigger inflation of a portion of each passenger restraint and deploy the automatic leg flail prevention device.

9. A three-place berthing aircraft divan adapted to be installed side-facing in an aircraft cabin, comprising:
a fixed frame comprising a seat bottom frame and a backrest frame affixed to the seat bottom frame;
a plurality of inboard legs affixed to the seat bottom frame;
a seat bottom supported by the seat bottom frame and comprising a tracking platform movable relative to the seat bottom frame to track between an upright sitting position and a berth position of the aircraft divan;
a backrest supported by the backrest frame and comprising a back follower movable relative to the backrest frame to track the aircraft divan between the upright sitting position and the berth position;
a passenger restraint provided at each seat place comprising a lap belt anchored to the tracking platform and an inflatable should harness detachable from the lap belt;
a leg flail prevention device disposed under one end of the seat bottom frame; and
a mechanical crash sensor unit including a processor configured to sense a crash event, and in response to the sensed crash event, trigger inflation of each inflatable should harness and deploy the leg flail prevention device;
wherein the tracking platform and the back follower are pivotably attached such that the seat bottom and the backrest track together relative to the frame between the upright sitting position and the berth position; and
wherein one end of each inflatable shoulder harness is wound on a retractor affixed under the seat bottom frame, wherein a length of the inflatable shoulder harness remains outside of the retractor such that the retractor provides unceasing tension on the inflatable shoulder harness.

10. The aircraft divan of claim 9 , wherein the plurality of inboard legs includes a first leg, a second leg, and a third leg, wherein the first and second legs are adjacent and the second and third legs are adjacent and are spaced apart such that two containers for each containing a high-capacity life can be installed below the seat bottom frame between the plurality of inboard legs.

11. The aircraft divan of claim 10 , wherein the aircraft divan has a length from about 200 cm to 205 cm, and wherein a distance between the first and second legs, and the second and third legs, is about 100 cm.

12. The aircraft divan of claim 9 , wherein the seat bottom frame and the backrest frame each comprise elongate tracks for guiding tracking of the respective tracking platform and the back follower between the upright sitting position and the berth position, and each of the tracking platform and the back follower comprise vertically-oriented rollers that travel along respective ones of the elongate tracks.

13. The aircraft divan of claim 9 , wherein the tracking platform locks to the seat bottom frame and the lap belts are affixed to an outboard tube of the tracking platform such that the lap belts track inboard with the tracking platform and loading on the lap belts is transferred to the seat bottom frame through the tracking platform.

14. The aircraft divan of claim 9 , further comp

Assignees

• Be Aerospace Inc

Inventors

• Oleson Michael L
• Ho Hau Phuc

Classifications

• B64D11/0641 Primary

  Seats convertible into beds · CPC title

• B64D11/06205

  Arrangements of airbags · CPC title

• B64D2011/0069

  Rest berths, beds or the like · CPC title

• B64D11/0629

  the storage means being specially adapted for emergency equipment · CPC title

• B64D11/0601 Primary

  Arrangement of seats for non-standard seating layouts, e.g. seats staggered horizontally or vertically, arranged in an angled or fishbone layout, or facing in other directions than the direction of flight · CPC title