Aircraft seat for cabin crew

Patent metadata

Field	Value
Publication number	US-10940948-B2
Application number	US-201615774374-A
Country	US
Kind code	B2
Filing date	Nov 7, 2016
Priority date	Nov 10, 2015
Publication date	Mar 9, 2021
Grant date	Mar 9, 2021

Abstract

A seat for cabin crew, intended to be installed in an aircraft, includes a seat structure intended to be fixed to a fixed portion of the aircraft, a seat slide provided with two arms positioned on either side of the seat portion, and a seat portion mounted slidably relative to the seat slide between a retracted position and an extended position. One of the elements among the seat portion and the seat slide includes rollers capable of sliding along corresponding rails provided in the other one of the elements among the seat portion and the seat slide. The rails have a curved shape so that the seat portion forms, in the extended position, an angle of more than 10 degrees, preferably of around 14 degrees, relative to a floor of the aircraft.

First claim

The invention claimed is:

1. A seat for cabin crew, intended to be installed in an aircraft, the seat comprising:
a seat structure configured to be fixed to a fixed portion of the aircraft;
a seat portion;
a seat slide provided with two arms positioned on opposing sides of the seat portion; and
the seat portion being mounted slidably relative to the seat slide between a retracted position and an extended position;
at least one of the seat portion or the seat slide comprises rollers capable of sliding along corresponding rails provided in the other one of the at least one of the seat portion or the seat slide;
the rails having a curved shape so that the seat portion forms, in the extended position, an angle of more than 10 degrees relative to a floor of the aircraft,
wherein the seat further comprises an automatic fold-back system to move the seat automatically from a comfort position to a seating position;
wherein the automatic fold-back system has a resilient cable, wherein a first end of the resilient cable is fixed to the seat structure and a second end is fixed to the seat portion; and
wherein the resilient cable passes over at least one pulley positioned between the first end and the second end of the resilient cable.

2. The seat of claim 1 , further comprising a back rest having a first end mounted rotatably relative to the seat portion and a second end mounted rotatably relative to a head rest of said seat, said head rest being mounted slidably relative to the seat structure such that the head rest moves with of said back rest.

3. The seat of claim 1 , wherein the seat slide is mounted rotatably relative to the seat structure in order to enable the seat to move from a stowed position to a seating position.

4. The seat of claim 1 , wherein the seat portion comprises intermediate positions between the retracted position and the extended position.

5. The seat of claim 1 , wherein a maneuvering means acts to cause the movement between the comfort position and the seating position by unlocking at least one locking pin co-operating with a recess provided in the seat slide, said maneuvering means being connected to the locking pin via a connecting cable.

6. The seat of claim 1 , comprising a leg rest coupled to a shaft mounted rotatably relative to the seat portion and configured to move from a stowed position in which the leg rest is situated under the seat portion to an unfolded position in which the leg rest is situated in an extension of the seat portion.

7. The seat of claim 6 , wherein the leg rest has a synchronization bar comprising a respective roller positioned at ends of the bar, wherein each roller is slidable along a rail provided in an internal face of a side wall of the seat portion.

8. The seat of claim 7 , wherein a first locking system has a locking latch for securing the synchronization bar such that the leg rest is maintained in the unfolded position.

9. The seat of claim 8 , comprising a second locking system for securing the leg rest in the stowed position.

10. The seat of claim 9 , wherein the second locking system has a locking recess installed on a side of a front edge of the leg rest for co-operating with a locking catch disposed on a rear side of the seat portion.

11. The seat of claim 9 , wherein the first and the second locking systems can be actuated via a common maneuvering means.

12. The seat of claim 7 , wherein a damping system can absorb a force exceeding a threshold limit applied to the leg rest.

13. The seat of claim 12 , wherein the damping system has at least one resilient element having a first end mounted rotatably relative to the synchronization bar and a second end mounted rotatably relative to the leg rest.

14. The seat of claim 6 , comprising a foot rest slidably mounted relative to the leg rest and a resilient means that is interposed between the foot rest and the leg rest.

15. The seat of claim 1 , comprising an automatic fold-back system to move said seat automatically from a comfort position to a seating position.

16. The seat of claim 15 , wherein the automatic fold-back system has a resilient cable, wherein a first end of the resilient cable is fixed to the seat structure and a second end is fixed to the seat slide, and wherein the resilient cable passes over at least one pulley positioned between the first end and the second end of the resilient cable.

17. A seat for cabin crew, intended to be installed in an aircraft, the seat comprising:
a seat structure configured to be fixed to a fixed portion of the aircraft;
a seat portion;
a seat slide provided with two arms positioned on opposing sides of the seat portion; and
the seat portion being mounted slidably relative to the seat slide between a retracted position and an extended position;
at least one of the seat portion or the seat slide comprises rollers capable of sliding along corresponding rails provided in the other one of the at least one of the seat portion or the seat slide;
the rails having a curved shape so that the seat portion forms, in the extended position, an angle of more than 10 degrees relative to a floor of the aircraft;
the seat further comprising an automatic fold-back system to move said seat automatically from a comfort position to a seating position,
wherein the automatic fold-back system has a resilient cable, wherein a first end of the resilient cable is fixed to the seat structure and a second end is fixed to the seat slide, and
wherein the resilient cable passes over at least one pulley positioned between the first end and the second end of the resilient cable.

18. A seat for cabin crew, intended to be installed in an aircraft, the seat comprising:
a seat structure configured to be fixed to a fixed portion of the aircraft;
a seat portion;
a seat slide provided with two arms positioned on opposing sides of the seat portion; and
the seat portion being mounted slidably relative to the seat slide between a retracted position and an extended position;
at least one of the seat portion or the seat slide comprises rollers capable of sliding along corresponding rails provided in the other one of the at least one of the seat portion or the seat slide;
the rails having a curved shape so that the seat portion forms, in the extended position, an angle of more than 10 degrees relative to a floor of the aircraft;
comprising a leg rest coupled to a shaft mounted rotatably relative to the seat portion and configured to move from a stowed position in which the leg rest is situated under the seat portion to an unfolded position in which the leg rest is situated in an extension of the seat portion,
wherein the leg rest has a synchronization bar comprising a respective roller positioned at ends of the bar, wherein each roller is slidable along a rail provided in an internal face of a side wall of the seat portion,
wherein a first locking system has a locking latch for securing the synchronization bar such that the leg rest is maintained in the unfolded position,
comprising a second locking system for securing the leg rest in the stowed position,
wherein the second locking system has a locking recess installed on a side of a front edge of the leg rest for co-operating with a locking catch disposed on a rear side of the seat portion.

Assignees

• Safran Seats

Inventors

• Verny Christian
• Lebegue Brice
• Mesaros Alexandre

Classifications

• B64D11/0639

  with features for adjustment or converting of seats · CPC title

• B64D11/0642

  Adjustable headrests · CPC title

• B64D11/0691

  specially adapted for cabin crew · CPC title

• B64D11/064 Primary

  Adjustable inclination or position of seats · CPC title

• B64D11/0643

  Adjustable foot or leg rests · CPC title