Emergency oxygen system for aircraft

Claim 2

In an emergency oxygen system for an aircraft of the type having a plurality of oxygen masks normally stored in a mask compartment located behind a normally locked door in an upper rear portion of the back of one seat position of a multi-passenger seating unit, said seating unit having a chassis for supporting seat cushion means for each seat position of said seating unit and at least said back of said one seat position, the improvement wherein a generator compartment for containing an oxygen generating canister is attached to said chassis at a remote location relative to said mask compartment, said generator compartment being positioned at least substantially under the plane of said seat cushion means, said generator compartment housing both an oxygen generator canister positioned therein and a first release mechanism for activating said canister to produce oxygen, a plurality of oxygen flow tubes being joined at their opposite ends to said canister and to said plurality of oxygen masks, and a control cable assembly including a longitudinally movable control wire extending between said mask compartment and said generator compartment, said control wire being attached to said first release mechanism at its lower end and to a second release mechanism at its upper end, said control wire being operable at its said lower end to activate said first release mechanism so as to cause oxygen to be generated by said generator and to flow to said oxygen masks when its said upper end is moved longitudinally by a force applies to it by said second release mechanism in response to a pulling force applied to a mask by a passenger, said masks including a tether member which actuates said second release mechanism when pulled.

Claim 3

The oxygen system of claim 1 wherein said oxygen tubes and said control cable assembly are supported by the front surface of said back of said one seat position and are isolated and protected by cover means from direct contact with seat cushion means which are adapted to overlie said back.

Claim 4

The oxygen system of claim 2 wherein said cover means includes an elongated channel member mounted to a side edge portion of said back.

Claim 5

The oxygen system of claim 3 wherein said channel member is hinged to said back for access to said oxygen flow tubes and control cable assembly, said channel member and back further including complementary fastening means.

Claim 6

The oxygen system of claim 3 wherein said cover means includes a thick-walled flexible tubular sheath which surrounds said flow tubes and cable assembly and extends from at least the lower end portion of the channel member to the generator compartment, said tubular sheath serving to permit flexure of said flow tubes and cable assembly in the region of the seat located between the back and seat cushions when the back is reclined relative to the chassis.

Claim 7

The oxygen system of claim 1 wherein said control cable assembly includes a tubular outer shroud portion which surrounds and protects said movable control wire, said tubular outer shroud portion being threaded at at least one end of said cable assembly for a sufficient portion of its length to permit a complementary adjustment nut to be located at various positions thereon.

Claim 8

The oxygen system of claim 1 wherein said generator compartment has a first guide bracket member fixedly mounted adjacent one end thereof for guiding the generally vertically positioned canister activating pin end of an activating cord assembly which forms a portion of said first release mechanism so that a generally horizontal pulling force applied to the other end of the cord assembly, in the generally longitudinal direction of the axis of the canister, will cause the activating pin to be separated from said canister, thereby activating said canister.

Claim 9

The oxygen system of claim 7 wherein a second bracket member is mounted for pivotal movement adjacent the opposite end of the generator compartment, said second bracket member having one portion engaged with one end of said control wire and another portion engaged with the end of said cord assembly which is opposite to the end with the canister activating pin.

Claim 10

The oxygen system of claim 6 wherein said second release mechanism includes a bracket fixedly mounted in said mask compartment and having a support portion for fixedly mounting the upper end of said tubular shroud, said support portion supporting said control cable assembly in alignment with a guide sleeve element which is also fixedly mounted on said last named bracket at a predetermined distance from said support portion, said guide sleeve element having an aperture through its side wall near its end which is remote from said support portion, said aperture being adapted to support a release pin element attached to the end of said tether member and retain it in a position normal to the axis of said guide sleeve element, a release element mounted on the upper outer end of the control wire, said release element having an outer side surface which is complementary to the inner surface of said guide sleeve element, a compression spring mounted in surrounding relation to said control wire and positioned so as to be retained at one of its ends by said support portion attached to said tubular shroud and at its other end by the inner end surface of said release element, said spring being compressed to at least substantially its maximum extent when said release element is sufficiently retracted within said guide sleeve element that said release pin element can be located in said aperture in said guide sleeve element and have an end portion positioned sufficiently across an outer end portion of said release element that it will prevent outward movement of said release element, said spring having sufficient force and sufficient length that, when said release pin element is released, it will cause said control wire to move a sufficient distance relative to said tubular shroud that its lower end portion will activate said first release mechanism.