Convertible structure comprising a plurality of adjacent seats and of variable size along a sliding axis

• US 5,558,309 A
• Filed: 12/16/1994
• Issued: 09/24/1996
• Est. Priority Date: 12/17/1993
• Status: Expired due to Fees

• Current Assignee: Societe Industrielle Et Commerciale De Materiel
• Original Assignee: Societe Industrielle Et Commerciale De Materiel Aeronautique
• Inventors: Marechal, Robert R. L.
• Primary Examiner(s): Ramirez, Ramon O.
• Assistant Examiner(s): TURGEON, MICHAEL
• Application Number:
  US08/358,004
• Time in Patent Office: 648 Days
• Field of Search: 248/188.1, 248/172, 248/670, 248/298.1, 248/424, 297/232, 297/233, 297/234, 297/235, 244/118.5, 244/118.6, 244/122 R, 244/122 AH
• US Class Current: 248/424
• CPC Class Codes: B64D 11/0693 Width modification of seat assemblies, e.g. for class modification

Abstract

A structure comprising a plurality of adjacent seats for a public passenger vehicle, in particular an airliner, the structure being convertible and of variable size along a sliding axis (100), and comprising:

a fixed portion (2) comprising at least two transverse underframes (4) that are spaced apart from each other, fixed to the floor of the passenger cabin, and rigidly connected to one another by longitudinal underframe elements (5) having an axis that is generally parallel to the sliding axis;

at least one moving portion (3) that is movable relative to the fixed portion between two extreme positions, namely a maximum-size first position and a minimum-size second position, the moving portion (3) including an end transverse seat side member (6) rigidly associated with longitudinal support elements (7), and intermediate transverse seat side members (8) parallel to the end transverse seat side member (6) and associated with the longitudinal support elements (6), and serving to mount seat backs and arms; and

locking elements for locking the moving portion (3) to the fixed portion (2) in each of the two extreme positions;

wherein each longitudinal underframe element (5) includes at least two sliding support elements (9) secured to the longitudinal underframe element (5) for sliding along an axis that is parallel to and distinct from the general axis of the associated longitudinal underframe element (5), with a longitudinal support element (7) of the moving portion (3) being slidably received therein and guided in translation along the sliding axis (100).

Claims

1. A structure comprising a plurality of adjacent seats for a public passenger vehicle, in particular an airliner, the structure being convertible and of variable size along a sliding axis (100), and comprising:

a fixed portion (2) comprising at least two transverse underframes (4) that are spaced apart from each other, fixed to the floor of the passenger cabin, and rigidly connected to one another by longitudinal underframe elements (5) having an axis that is generally parallel to the sliding axis;

at least one moving portion (3) that is movable relative to the fixed portion between two extreme positions, namely a maximum-size first position and a minimum-size second position, said moving portion (3) including an end transverse seat side member (6) rigidly associated with longitudinal support elements (7), and intermediate transverse seat side members (8) parallel to the end transverse seat side member (6) and associated with the longitudinal support elements (6), and serving to mount seat backs and arms; and

locking means for locking the moving portion (3) to the fixed portion (2) in each of the two extreme positions;

wherein each longitudinal underframe element (5) includes at least two sliding supports (9) secured to the longitudinal underframe element (5) for sliding along an axis that is parallel to and distinct from the general axis of the associated longitudinal underframe element (5), with a longitudinal support element (7) of the moving portion (3) being slidably received therein and guided in translation along the sliding axis (100).

2. A structure according to claim 1, wherein the intermediate transverse seat side members (8) are slidable relative to the support elements (7) with which they are associated.

3. A structure according to claim 2, wherein the support elements (7) drives said intermediate transverse seat side members (8) in translation along the sliding axis (100) over a previously-chosen distance that is not necessarily the same as the displacement distance of the moving portion (3).

4. A structure according to claim 1, wherein the locking means comprises safety means for locking the moving portion (3) in each of the two extreme positions.

5. A structure according to claim 4, wherein at least one of the longitudinal support elements (7) of each moving portion (3) is hollow, and wherein the safety means comprises a rod (11) coaxially mounted inside the hollow support element (7), free to rotate about the axis of said support element, opening out to one of its ends (16) in an outside face (12) of the end transverse seat side member (6), and having a cam (13) at its other end (15), two grooves (14a, 14b) being provided in the associated underframe element (5) in such a manner that when the cam (13) is in the first position it co-operates with the first groove (14b) to lock the moving portion (3) in translation, and when the cam is in its second position it co-operates with the second groove (14a), changeover between the two positions being achieved firstly by rotating the rod (11) so as to disengage the cam from one of the grooves (14a, 14b);

then by sliding the moving portion (3) towards the other position; and

then by rotating the rod (11) in the opposite direction to engage the cam (13) in the other groove (14a, 14b).

6. A structure according to claim 5, wherein the end (16) opening out in the outside face (12) of the end transverse seat side member (6) has an axial safety lock (17) designed to co-operate with a removable manual actuator device (18) that enables rotary motion to be imparted to the rod (11) in order to pass from one position to the other, which device is prevented from being removed so long as the cam (13) is not correctly positioned in one or other of the grooves (14a, 14b).

7. A structure according to claims 6, wherein the cam (13) is properly positioned in one or other of the grooves (14a, 14b) by means of a system comprising a ball (28) that co-operates with a cavity (19), one of the ball and cavity being disposed in the bottom of the groove and the other at a radial end of the cam.

8. A structure according to claim 7, wherein the sliding supports (9) are fitted with ball-bearing sockets (20).

9. A structure according to claim 8, wherein the rod (11) is urged into a cam position that causes the cam (13) to be engaged in one or other of the grooves (14a, 14b).

10. A structure according to claim 4, wherein the safety means for locking the moving portion (3) in either extreme position comprises a manual actuator device that is made safe by being retained by the structure unless it has been properly locked in position against translation.

11. A structure according to claim 10, wherein at least one of the longitudinal support elements (7) of each moving portion (3) is hollow, and wherein the safety means comprise a rod (11) coaxially mounted inside the hollow support element (7), free to rotate about the axis of said support element, opening out to one its end (16) in the outside face (12) of an end transverse seat side member (6), and having a cam (13) at its other end (15), two grooves (14a, 14b) being provided in the associated underframe element (5) in such a manner that when the cam (13) is in the first position it co-operates with the first groove (14b) to lock the moving portion (3) in translation, and when the cam is in its second position it co-operates with the second groove (14a), changeover between the two positions being achieved firstly by rotating the rod (11) so as to disengage the cam from one of the grooves (14a, 14b);

then by sliding the moving portion (3) towards the other position; and

then by rotating the rod (11) in the opposite direction to engage the cam (13) in the other groove (14a, 14b).

12. A structure according to claim 11, wherein the end (16) opening out in the outside face (12) of the end transverse seat side member (6) has an axial safety lock (17) designed to co-operate with a removable manual actuator device (18) that enables rotary motion to be imparted to the rod (11) in order to pass from one position to the other, which device is prevented from being removed so long as the cam (13) is not correctly positioned in one or other of the grooves (14a, 14b).

13. A structure according to claim 12, wherein the cam (13) is properly positioned in one or other of the grooves (14a, 14b) by means of a system comprising a ball (28) that co-operates with a cavity (19), one of the ball and cavity being disposed in the bottom of the groove and the other at a radial end of the cam.

14. A structure according to claim 13, wherein the sliding supports (9) are fitted with ball-bearing sockets (20).

15. A structure according to claim 14, wherein that rod (11) is urged into a cam position that causes the cam (13) to be engaged in one or other of the grooves (14a, 14b).

16. A structure according to claim 1, wherein one of the end transverse seat side members (10) is rigidly associated with the longitudinal underframe elements (5) so that only one of the seat ends (6) is movable.

17. A structure according to claim 1, wherein each of the end transverse seat side members (6) is rigidly associated with a moving portion (3), each of the two seat ends (10) being movable independently of the other.

18. A structure according to claim 1, wherein the rigid connections between the sliding supports (9) and the longitudinal underframe elements (5) are constituted by links that absorb energy in the event of major acceleration due to an accidental collision of the public passenger vehicle.