Emergency exit system for aircraft or other vehicle
AssigneeHer Majesty the Queen in right of Canada, as represented by the Minister of National Defence
InventorsChristopher J. Brooks, Albert P. Bohemier, Lee R. Miller
Life of this patent
Estimating the term…
Abstract
An emergency exit system for use on a helicopter or other aircraft includes a frame (4) defining an opening (6) for receiving a panel (8) to close the opening (6); a plurality of latches (10, 117) for releasably securing the panel (8) in the opening (6); a plurality of release mechanisms (12); a cable (45, 118) extending around at least a major portion of the frame (4) for releasing the panel (8); and a plurality of actuators (14) strategically located around the opening and connected to the cable (45, 118), whereby actuation of any one of the actuators (14) causes simultaneous release of all of the latches (10, 117) so that the panel (8) can be jettisoned.
Claims11
An emergency exit system comprising a frame for mounting in a vehicle;
- an opening in said frame through which the vehicle can be entered or exited;
- a panel for closing said opening;
- a plurality of plungers slidable in said frame for movement between panel latching and panel release positions, said plurality of plunger releasably retaining the panel in the frame;
- a plurality of release mechanisms for moving said plungers from said panel latching position in which said panel is retained in the frame to said panel release position in which said panel is removable from said frame;
- a plurality of principal actuators located at several, spaced apart locations around a periphery of the frame, said principal actuators including a plurality of bars rotatably mounted to frame and connected to said plungers, each bar being adapted to individually move said plungers to the panel release position when said bar is actuated;
- and a cable extending around a substantial portion of said frame connecting said principal actuator bars to said release mechanisms, said release mechanisms including first racks and pinions connecting said bars to said cable for moving said cable when one of said bars is rotated;
- and second racks and pinions connecting said cable to said plungers for moving the plungers from the panel latching position to the panel release position, whereby, when any one of the bars is rotated, all of the plungers are simultaneously moved to the panel release position, permiting ejection of the panel from the frame.
Dependencies are inferred from the claim text.