Seat for a transport vehicle or craft, in particular an aircraft

Abstract

The invention relates to a seat for a transport vehicle or craft, in particular an aircraft, the seat including a support structure (1) and at least one armrest (2) comprising a rest element (4) mounted on one end of a strut whose other end is hinged to the support structure about a first transverse axis (7) to tilt between an in-use position in which the rest element is substantially horizontal and a forwardly-tilted retracted position in which the rest element is substantially vertical and in front of the seat. Said strut is L-shaped with a first arm (5) hinged at its free end about said first axis and extending substantially rearwards from said first axis when said strut is in its in-use position, and a second arm (6) extending substantially upwards when the strut is in its in-use position, and said rest element is hinged to the free end of said second arm of the strut about a second transverse axis (9).

Description

[0001] The present invention relates to a seat for a transport vehicle or craft, in particular an aircraft, and more particularly to such a seat including a support structure and at least one armrest comprising a rest element mounted on one end of a strut whose other end is hinged to the support structure about a first transverse axis to tilt between an in-use position in which the rest element is substantially horizontal and a forwardly-tilted retracted position in which the rest element is substantially vertical and in front of the seat.

[0002] Such a seat is described in Document FR-A-2 233 821. In that document, the rest element of the armrest is mounted rigidly on the free end of the strut. As a result, even in its retracted position, the armrest takes up a considerable amount of space, in particular the rear portion of the rest element which, in that position, projects forwards and upwards from the front edge of the seat proper.

[0003] An object of the present invention is to mitigate that drawback.

[0004] More particularly, an object of the invention is to make the armrest more compact, in particular when it is in its retracted position.

[0005] Another object of the invention is to provide locking means that are particularly suitable for an armrest of an aircraft cabin seat that can be transformed from an “economy-class” version to a “business-class” version.

[0006] To this end, the invention provides a seat for a transport vehicle or craft, in particular an aircraft, the seat including a support structure and at least one armrest comprising a rest element mounted on one end of a strut whose other end is hinged to the support structure about a first transverse axis to tilt between an in-use position in which the rest element is substantially horizontal and a forwardly-tilted retracted position in which the rest element is substantially vertical and in front of the seat, wherein said strut is L-shaped with a first arm hinged at its free end about said first axis and extending substantially rearwards from said first axis when said strut is in its in-use position, and substantially forwards from said first axis when said strut is in its retracted position and a second arm extending substantially upwards when the strut is in its in-use position, and substantially downwards when the strut is in its retracted position, and wherein said rest element is hinged to the free end of said second arm of the strut about a second transverse axis.

[0007] The term “transverse” is used to mean substantially perpendicular to the plane of symmetry of the seat. The term “forwards” is used to mean the direction in which an occupant of the seat looks, and the term “rearwards” is used to mean the opposite direction.

[0008] The particular shape of the arm and the fact that the rest element is hinged to the arm make it possible to improve significantly the compactness of the armrest in the retracted position.

[0009] In a particular embodiment, said rest element is provided with a recess behind said second axis, which recess is suitable for receiving said second arm when said strut is in its retracted position.

[0010] By enabling that portion of the strut which is connected to the rest element to be received inside said rest element, such a configuration makes it possible to reduce the extent to which the armrest projects forwards when it is in the retracted position.

[0011] Also in a particular embodiment of the invention, first locking means are provided for locking the armrest at least when said strut is in the in-use position.

[0012] More particularly, said first locking means may comprise means for locking the rear portion of the rest element to said support structure.

[0013] Said locking means for locking the rear portion of the rest element to said support structure may comprise a transverse finger mounted on the rear end of said rest element, and organized to co-operate with hook-shaped end of a first lever hinged to said support structure about a third transverse axis.

[0014] It is also possible to provide an unlocking button mounted to move on said support structure so as to move said first lever.

[0015] Also in a particular embodiment of the invention, second locking means are provided for locking the armrest at least when the strut is in the retracted position.

[0016] More particularly, said second locking means may comprise means for locking said rest element to said strut.

[0017] Said securing means may comprise a recess for receiving the front end of said rest element, which recess is integral with said support structure.

[0018] Said second locking means may comprise a second lever hinged to said first arm of said strut about a fourth transverse axis and provided at its free end with a setback organized to co-operate with said transverse finger.

[0019] Said strut may be provided with passageways for at least one cable which may be an electrical cable or a mechanical control cable.

[0020] An abutment may be provided for acting when the rest element is in the in-use position to prevent said rest element from pivoting about said second transverse axis in the direction in which the armrest is put into the in-use position.

[0021] Said abutment may be adjustable.

[0022] A particular embodiment of the invention is described below by way of non-limiting example and with reference to the accompanying drawings, in which:

[0023] FIG. 1 is a perspective view of an armrest of the invention in the in-use position;

[0024] FIG. 2 is a view similar to the FIG. 1 view, with the armrest locked in the retracted position;

[0025] FIG. 3 is a view similar to the FIG. 2 view, with the armrest in the unlocked position;

[0026] FIG. 4 is a longitudinal section view of the armrest as locked in the in-use position;

[0027] FIG. 5 is a longitudinal section view of the armrest as locked in the retracted position;

[0028] FIG. 6 is a cutaway perspective view on a larger scale of the locking means for locking the armrest in the in-use position; and

[0029] FIG. 7 is a view similar to the FIG. 6 view, showing the locking means for locking the armrest in the retracted position.

[0030] The figures show a support structure element 1 for an aircraft seat. In known manner, the structure supports the seat proper and the seat back.

[0031] An armrest 2 mounted on the structure element 1 is essentially made up of a strut 3 and of a rest element 4.

[0032] The strut 3 is substantially L-shaped and it is made up of first and second arms 5 & 6 integral with each other.

[0033] The strut 3 is hinged to the structure element 1 about a transverse axis 7 via that end of the arm 5 which is remote from the arm 6. When the armrest 2 is in its in-use position (shown in FIGS. 1 and 4, the arm 5 is substantially horizontal and extends rearwards from the axis 7. In this position, the arm 6 extends substantially vertically upwards.

[0034] When the armrest 2 is tilted forwards about the axis 7 into the retracted position, the arm 5 extends substantially horizontally forwards from the axis 7 and the arm 6 extends substantially vertically downwards.

[0035] The rest element 4 as provided with its padding 8 is hinged to the free end of the arm 6 about a second transverse axis 9.

[0036] The rest element 4 is made up of two side cheek plates 10 defining a recess 11 between them in the rear of the element.

[0037] When the armrest is in the in-use position, the rest element 4 is substantially horizontal and perpendicular to the arm 6 of the strut 3. When the rest element 4 is in the retracted position, it is substantially vertical and in front of the structure element 1, the arm 6 then being received in the recess 11. In this position, the front portion of the rest element 4 is engaged in a recess 12 integral with the support structure.

[0038] A description follows of the means making it possible to lock the armrest in its in-use position and in its retracted position.

[0039] An adjustable abutment 12′ is mounted on the rest element 4 so as to prevent the rest element from having a degree of freedom through which it can pivot relative to the strut 3 about the axis 9 when the armrest is in the in-use position. The entire armrest is then prevented from having a degree of freedom through which it can pivot about the axis 7 by means described below.

[0040] Since the abutment 12′ is adjustable, it makes it possible to adjust the height of the rest element 4 when said element is in use.

[0041] Between its two cheek plates 10, and behind the recess 11, the rest element 4 is provided with a transverse finger 13.

[0042] A first locking lever 14 is mounted on the structure element 1 and hinged about a third transverse axis 15.

[0043] At its end, the lever 14 is provided with a hook-shaped notch 16 suitable for co-operating with the finger 13. FIG. 6 shows that, when the armrest is in the in-use position, the finger 13 is engaged in the notch 16 and is secured between the walls of said notch and a portion 17 of the structure element 1. Resilient means (not shown) hold the lever 14 in the position shown in FIG. 6.

[0044] An unlocking button 18 is mounted to slide in the structure element 1 facing a projection 19 on the lever 14. The in-use position of the armrest 2 is unlocked by pressing on the button 18 so as to cause the lever 14 to pivot against the drive from the resilient means, and thereby to release the finger 13.

[0045] A description follows of the means for locking the armrest 2 in the retracted position.

[0046] FIG. 7, in particular, shows that a second lever 20 is hinged to the arm 5 of the strut 3 about a fourth transverse axis 21.

[0047] The lever 20 is substantially horizontal both when the armrest is in the in-use position, and when it is in its retracted position. When the armrest is in its retracted position, the lever 20 extends forwards relative to the axis 21.

[0048] At its free end, the lever 20 is provided with a setback 22 into which the finger 13 comes into abutment when the armrest is in its retracted position. Resilient means (not shown) urge the lever 20 into this abutment position. Since, when the armrest is in this position, the front end of the rest element 4 is engaged in the recess 12, the armrest cannot pivot as a whole about the axis 7 and it is thus locked in said position.

[0049] Starting from the retracted position, unlocking takes place by pressing on the lever 20 against the drive from the resilient means so as to release the finger 13 and so as to disunite the strut 3 from the rest element 4.

[0050] Finally, it should be observed that it is optionally possible to omit the lever 20 and then provide merely the recess 12 so as to limit the movement of the armrest when it is in its retracted position.

[0051] In FIGS. 4 and 5, it can also be seen that passageways 23 and 24 are provided in the strut 3. The passageway 23 receives electrical control cables 25 and the passageway 24 receives a mechanical control cable 26.

Claims

1. A seat for a transport vehicle or craft, in particular an aircraft, the seat including a support structure and at least one armrest comprising a rest element mounted on one end of a strut whose other end is hinged to the support structure about a first transverse axis to tilt between an in-use position in which the rest element is substantially horizontal and a forwardly-tilted retracted position in which the rest element is substantially vertical and in front of the seat, wherein said strut is L-shaped with a first arm hinged at its free end about said first axis and extending substantially rearwards from said first axis when said strut is in its in-use position, and substantially forwards from said first axis when said strut is in its retracted position and a second arm extending substantially upwards when the strut is in its in-use position, and substantially downwards when the strut is in its retracted position, and that said rest element is hinged to the free end of said second arm of the strut about a second transverse axis.

2. A seat according to claim 1, in which said rest element is provided with a recess behind said second axis, which recess is suitable for receiving said second arm when said strut is in its retracted position.

3. A seat according to claim 1, provided with first locking means for locking the armrest at least when said strut is in the in-use position.

4. A seat according to claim 3, in which said first locking means comprise means for locking the rear portion of the rest element to said support structure.

5. A seat according to claim 4, in which said locking means for locking the rear portion of the rest element to said support structure comprise a transverse finger mounted on the rear end of said rest element, and organized to co-operate with hook-shaped of a first lever hinged to said support structure about a third transverse axis.

6. A seat according to claim 5, provided with an unlocking button mounted to move on said support structure so as to move said first lever.

7. A seat according to claims 1, including second locking means for locking the armrest at least when the strut is in the retracted position.

8. A seat according to claim 7, in which said second locking means comprise means for locking said rest element to said strut, and securing means for preventing the armrest as locked in this way from pivoting about said first transverse axis.

9. A seat according to claim 8, in which said securing means comprise a recess for receiving the front end of said rest element, which recess is integral with said support structure.

10. A seat according to claim 1, in which said strut is provided with passageways for at least one cable which may be an electrical cable or a mechanical control cable.

11. A seat according to claim 1, in which an abutment is provided for acting when the rest element is in the in-use position to prevent said rest element from pivoting about said second transverse axis in the direction in which the armrest is put into the in-use position.

12. A seat according to claim 11, in which said abutment is adjustable.

13. A seat for a transport vehicle or craft, in particular an aircraft, the seat including a support structure and at least one armrest comprising a rest element mounted on one end of a strut whose other end is hinged to the support structure about a first transverse axis to tilt between an in-use position in which the rest element is substantially horizontal and a forwardly-tilted retracted position in which the rest element is substantially vertical and in front of the seat, wherein said strut is L-shaped with a first arm hinged at its free end about said first axis and extending substantially rearwards from said first axis when said strut is in its in-use position, and substantially forwards from said first axis when said strut is in its retracted position and a second arm extending substantially upwards when the strut is in its in-use position, and substantially downwards when the strut is in its retracted position, and that said rest element is hinged to the free end of said second arm of the strut about a second transverse axis, the seat being provided with first locking means for locking the armrest at least when said strut is in the in-use position, said first locking means comprising means for locking the rear portion of the rest element to said support structure and comprising a transverse finger mounted on the rear end of said rest element, and organized to cooperate with hook-shaped end of a first lever hinged to said support structure about a third transverse axis, the seat including second locking means for locking the armrest at least when the strut is in the retracted position, said second locking means comprising a second lever hinged to said first arm of said strut about a fourth transverse axis and provided at its free end with a setback organized to co-operate with said transverse finger.