IP Library Granted Patent US 7,628,357
Granted Patent B2
US 7,628,357 · App. 11/415,285 · Granted Dec 8, 2009

Aircraft safety seat

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Quick Facts
Patent No.
US 7,628,357
App. No.
11/415,285
Granted
Dec 8, 2009
Kind
B2
Abstract

An aircraft safety seat that has a supporting structure and a bucket seat supported by the structure, the bucket seat has a seat and a back which are lined together, the back being installed on the structure so as to slide generally downwards, wherein at least one connection rod connected by its first end to the support and by its other end to the seat, the connecting rod being generally horizontal when in normal use, and being suited for pivoting downwards by its first end under the effect of a force exerted downwards on the seat, against the action of a shock absorber.

Claims (10)

1. An aircraft safety seat comprising a supporting structure and a bucket seat supported by said supporting structure, said supporting structure comprises a fixed part and a mobile part, said mobile part being installed in an adjustable fashion so as to slide generally vertically on said fixed part, said bucket seat comprising a seat and a back linked together, said back being installed on said supporting structure so as to slide generally downwards, wherein at least one connecting rod being connected at a first end to said mobile part of said supporting structure and at a second end to said seat, and a shock absorber being coupled to said connecting rod at a connection point on said connecting rod, wherein said connection point is not at either of said first and second ends of said connecting rod, said connecting rod being generally horizontal when in normal use, and being suited for pivoting downwards by its first end under the effect of a force exerted downwards on said seat, against the action of said shock absorber.

2. An aircraft safety seat according to claim 1 , in which said shock absorber is a linear absorber in which a first end is fixed to said supporting structure and a second end is fixed to said connecting rod.

3. An aircraft seat according to claim 2 , in which said first end of the linear absorber is fixed to said supporting structure above said connection point of said connecting rod.

4. An aircraft safety seat according to claim 1 , in which said back is installed so as to slide on said supporting structure by at least one annular linear element.

5. An aircraft safety seat according to claim 1 , in which said bucket seat and said mobile part are assembled so as to slide on said fixed part in substantially the same direction.

6. An aircraft safety seat according to claim 1 , comprising two lateral connecting rods, each of which is connected to one of the sides of said seat.

7. An aircraft safety seat according to claim 6 , comprising an attachment point for a seatbelt on the connection between at least one of said lateral connecting rods and the supporting structure.

8. An aircraft safety seat according to claim 7 , further comprising a lap, sash or crotch-strap seatbelt.

9. An aircraft safety seat according to claim 6 , comprising an attachment point for a seatbelt on said bucket seat, said attachment point being connected by another connecting rod to the connection between the supporting structure and at least one of said lateral connecting rods, said other connecting rod being designed to deform in the event of a crash.

10. An aircraft safety seat according to claim 1 , wherein said connection point is about in the middle of said connecting rod.

Assignments (2)
CHANGE OF NAME Recorded Nov 23, 2015
From: SOCIETE INDUSTRIELLE ET COMMERCIALE DE MATERIEL AERONAUTIQUE
To: ZODIAC SEATS FRANCE
Reel/Frame 037151/0893 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded May 2, 2006
From: MERCIER, BERTRAND; LUNEAU, ETIENNE
To: SOCIETE INDUSTRIELLE ET COMMERCIALE DE MATERIEL AERONAUTIQUE
Reel/Frame 017848/0347 →