Emergency exit system

Details Emergency exit system Emergency exit system

B - Operations, Transporting

60

J

B60J 9/02 (2006.01) B61D 17/00 (2006.01) B64C 1/14 (2006.01) B64C 1/32 (2006.01) B64D 25/08 (2006.01) B64G 1/52 (2006.01)

Patent

CA 2307384

An emergency exit system for use primarily in a helicopter or other aircraft includes a panel closing an opening in the fuselage of the aircraft, a plurality of latches for releasably securing the panel in the opening; a release mechanism including slides on each side of the opening for retracting the latches to release the panel; a drive for operating the slides, a drive latch for releasably locking the drive in a cocked condition; and a plurality of principal grab bars strategically located in recesses adjacent to the opening and connected to the drive by cables, whereby actuation of any one of the grab bars causes simultaneous release of all of the latches so that the panel can be jettisoned.

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