Displacement mechanism of a tray table mounted on an armrest of a seat, in particular an airplane seat

Abstract

A displacement mechanism of a tray table mounted on an armrest of a seat, said mechanism allowing to correct the lie angle of said tray table keeping it substantially horizontal, said seat being provided with a displacement mechanism, said displacement mechanism of a tray table providing a lever, hinged in the front-upper zone of the armrest where said tray table is arranged, said lever allowing said tray table to rotate in a longitudinal vertical plane, a hinge, arranged at the end of said lever opposite to the one hinged to the armrest, allowing said tray table to rotate according to an arc of a circle lying in a substantially vertical transversal plane, coupling means, provided under said tray table, and downward facing, when said tray table is in a use position, in proximity of said hinge, said lever being hinged on the armrest.

Claims

1. An airplane seat displacement mechanism, comprising: a displacement mechanism of a tray table mounted on an armrest of a seat, said mechanism allowing to automatically correct the lie angle of said tray table keeping it substantially horizontal, said seat being provided with a cradle type displacement mechanism; said displacement mechanism of a tray table providing a lever, hinged in the front-upper zone of the armrest where said tray table is arranged, said lever allowing said tray table to rotate in a longitudinal vertical plane; a hinge, arranged at the end of said lever opposite to the one hinged to the armrest, the hinge allowing said tray table to rotate according to an arc of a circle lying in a substantially vertical transversal plane; coupling means, provided under said tray table, and downward facing, when said tray table is in a use position by the passenger, in proximity of said hinge; said lever being hinged on the armrest on the same axis of an adjusting element; said adjusting element being shaped in order to allow engagement and disengagement by said coupling means, to a connection element with the displacement mechanism of the seat.

2. Mechanism according to claim 1, wherein said coupling means is a tooth, provided under said tray table, and downward facing, when said tray table is in a use position by the passenger, and in that said adjusting element is shaped so as to comprise a cavity in its upper peripheral profile, said cavity having an identical and complementary profile to that of said tooth in order to allow engagement and disengagement by means of said tooth to a connection element with the displacement mechanism of the seat.

3. Mechanism according to claim 1, wherein said coupling means is a cavity, provided under said tray table, and downward facing, when said tray table is in a use position by the passenger, and in that said adjusting element is shaped so as to comprise a tooth in its upper peripheral profile, said tooth having an identical and complementary profile to that of said cavity in order to allow engagement and disengagement by means of said cavity to a connection element with the displacement mechanism of the seat.

4. Mechanism according to claim 2, wherein said cavity of said adjusting element or of said coupling means has a trapezoidal shape.

5. Mechanism according to claim 1, wherein said adjusting element is connected to said connection element by means of a suitable kinematic chain.

6. Mechanism according to claim 1, wherein said connection element is made of a finger shaped element.

7. Mechanism according to claim 1, wherein said seat is an airplane seat.

Description

(1) The present invention will be described in the following for illustrative, but not limitative purposes, according to its preferred embodiments, with particular reference to the figures of the enclosed drawings, wherein:

(2) FIG. 1 is a first schematic view of a sidearmrest with tray table extracted;

(3) FIG. 2 is a second schematic view of a sidearmrest with tray table extracted and partial view of the main structure or seat during its displacement;

(4) FIG. 3 schematically shows a first view of the mechanism according to the invention;

(5) FIG. 4 schematically shows a second view of the mechanism according to the invention;

(6) FIG. 5 schematically shows the initial step of deployment of the tray table after its extraction from a sidearmrest provided with the mechanism according to the invention;

(7) FIG. 6 shows an intermediate step of deployment of tray table and shows a particular of mechanism of FIG. 5; and

(8) FIG. 7 shows the final step of deployment of tray table provided with mechanism of FIG. 5.

(9) Observing the figures of the enclosed drawings, it is described an embodiment of the mechanism according to the invention. Particularly, sidearmrest 1, with tray table 2 extracted, are schematically shown in FIG. 1.

(10) By reference number 3 it is generically indicated mechanism of the seat (not shown), that can be every type of seat permitting cradle movement.

(11) The solution according to the present invention claimed and shown in the figures does not require any control system assisted by electronic systems suitably programmed, but it is only based on mechanisms operated by movements of the main movable part 3 of the seat.

(12) Observing now FIGS. 3-7, it is noted that joint mechanism according to the invention for tray table 2 comprises a lever 4, hinged to the frontupper zone of side 1 on which tray table 2 is provided.

(13) Said lever 4 permits rotations of tray table 2 about a longitudinal vertical plane.

(14) A hinge 5 is provided at the end of the lever 4 opposed with respect to the hinged end, permitting to the tray table 2 to rotate along an arc lying along a plane that is an essentially verticaltransverse plane.

(15) Further, table 2 has a tooth 6 in its lower part (see FIG. 7) (when in the passenger use position) close to said hinge 5. When table 2 is in the passenger use position, said tooth 6 is thus faced downward.

(16) Lever 4 on which tray table 2 is hinged, is hinged on sidearmrest 1 on the same axis of an adjustment axis 7, having a cavity in its upper peripheral profile. Said cavity can have a profile equal and complementary with respect to the profile of the tooth 6, e.g. a trapezoidal shape, to promote engagement and disengagement of tooth 6 from said cavity.

(17) As an alternative, in further embodiments not shown, having the same effects, cavity can be provided in the tray table and the tooth in the adjustment element, thus obtaining the same result described with reference to the solution providing the tooth on the tray table and the cavity on the adjustment element.

(18) When the tray table 2 extracted from the sidearmrest 1 is rotated to be brought in the use position, said tooth 6 engages within the cavity of the abovementioned adjustment element 7.

(19) Thus, attitude (and thus lying of the tray table 2 surface plane) is due to the adjustment element 7 with which it is engaged, in a set longitudinal angular position, tooth 6 of tray table 2.

(20) The above adjustment element 7 is connected through a suitable kinematic chain (as for example illustrated, for illustrative, but not limitative, purposes in FIGS. 3 and 4 and generically indicated by reference number 8, since the same result can be obtained by a different kinematic chain) with finger 9, varying its angulation with respect to sidearmrest 1, if the latter is in the standard transition arrangement (FIG. 1) or in the cradle arrangement (FIG. 2).

(21) Kinematic chain 8 mentioned in the above permits to the adjustment element 7 rotating in such a way to maintain tray table 2 attitude constantly close to the horizontal plane.

(22) The present invention has been described for illustrative, but not limitative, purposes, according to its preferred embodiments, but it is to be understood that variations and/or modifications can be introduced by one skilled in the art, without departing from the relevant scope as defined in the enclosed claims.