Electronically actuated mechanical cable release for locking gas spring and method

Abstract

A cable release mechanism for a seat of the type having a seat bottom and a seat back adapted to be moved by a lockable gas spring between upright and reclined positions relative to the seat bottom. An electric motor is operatively attached to the gas spring by a cable movable by the motor to move the seat back between the upright and reclined positions, and a switch is electrically connected to the motor for initiating operation of the motor to move the cable. A related method is also disclosed.

Claims

1. An aircraft passenger seat including a cable release mechanism for actuating an adjustable feature, comprising: a mechanical actuator positioned within the aircraft passenger seat and configured to actuate the adjustable feature; a motor positioned within the aircraft passenger seat proximate the mechanical actuator; a cable interconnecting the motor and the mechanical actuator; a switch positioned within the aircraft passenger seat remote from the motor; and an electrical wire interconnecting the switch and the motor; wherein the switch is configured to actuate the motor to translate the cable to lock or unlock the mechanical actuator to adjust the adjustable feature; and wherein the mechanical actuator is a lockable gas spring, and the motor and the lockable gas spring are positioned proximate each other within a seat bottom portion of the aircraft passenger seat and the switch is positioned in an armrest portion of the aircraft passenger seat.

2. The aircraft passenger seat according to claim 1, wherein the cable is contained within a stationary sheath stationarily fixed to a housing of the motor.

3. The aircraft passenger seat according to claim 1, wherein the switch is an electrically-powered mechanical switch.

4. The aircraft passenger seat according to claim 1, wherein the motor includes a windlass rotatable by the motor to which the cable is connected.

5. The aircraft passenger seat according to claim 1, wherein the switch is an electrically-powered capacitive switch.

6. The aircraft passenger seat according to claim 1, wherein the switch is an electrically-powered mechanical switch mounted on an armrest of the aircraft passenger seat.

7. The aircraft passenger seat according to claim 1, wherein the switch is an electrically-powered capacitive switch mounted on an armrest of the aircraft passenger seat.

Description

BRIEF DESCRIPTION OF THE DRAWING FIGURES

(1) The present invention is best understood when the following detailed description of the invention is read with reference to the accompanying drawings, in which:

(2) FIG. 1 is a schematic perspective view of an aircraft seat cable release mechanism for a locking gas spring that is actuated by an electric motor and triggered by an electronic switch that is adapted for allowing passenger control of a seat back recline mechanism according to an embodiment of the invention; and

(3) FIG. 2 is a simplified schematic side elevation view of the cable release mechanism of FIG. 1.

DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENT

(4) Referring now to FIG. 1, a cable release mechanism is shown at reference numeral 10 and includes a housing 12 in which is contained an electric motor 14. The motor 14 has a windlass 16 fixed to a drive shaft 18 that pulls a sheathed cable 20 that is fixed to the windlass 16. The sheath 22 is fixed in a stationary position, for example to the motor's housing 12. The motor 14 is controlled by control electronics 24 that allow the adjustment and control of the amount of travel imparted to the cable 20. Rotation of the drive shaft 18 by the motor 14 rotates the windlass 16 which in turn drives the cable 20 fore or aft in relation to the stationary sheath 22.

(5) The motor 14 can be actuated by a number of external stimuli, including a mechanical displacement switch, capacitive switch, resistive switch, light switch, and the like. In FIG. 1, a mechanical switch 26 and a capacitive switch 28 are shown as alternative actuation devices, connected to the cable release mechanism 10 by electric wires 30 and 32, respectively. The mechanical cable release components can be located in an optimal position without having to create provisions for routing the mechanical cable 20 and cable sheath 22.

(6) Referring now to FIG. 2, a seat 40 is provided with the mechanical switch 26 that is interconnected by electrically-conductive wire 30 from a seat armrest 42 to the cable release mechanism 10. The seat 40 also includes a seat back 44 and a seat bottom 46 mounted on a frame/leg assembly 48.

(7) The cable 20 is connected to a lockable gas spring 50 which controls the position of the seat back 44 in relation to the seat bottom 46.

(8) The routing of the cable 20 from the actuation point at the motor 14 to the point of interface at the lockable gas spring 50 is very short, and the bend radius typically associated with a sheathed cable is greatly reduced since the wire 30 takes the place of the cable 20 between the mechanical switch 26 to the cable release mechanism 10. Therefore, there is no requirement for physical motion of the cable 20 during actuation. The actuation force at the user input side, for example, the mechanical switch 26, is a constant, while the actuation force required by the sheathed cable 20 can be varied as required by sizing the motor 14 actuating the cable 20 accordingly.

(9) In addition, the cable 20 can be simultaneously actuated by a plurality of inputs, for example, a touch screen, seat-mounted switches, or by a remote controller, for example.

(10) A cable release mechanism for a locking gas spring that is actuated by an electric motor and triggered by an electronic switch according to the invention have been described with reference to specific embodiments and examples. Various details of the invention may be changed without departing from the scope of the invention. Furthermore, the foregoing description of the preferred embodiments of the invention and best mode for practicing the invention are provided for the purpose of illustration only and not for the purpose of limitation, the invention being defined by the claims.