Ejection launch mechanism

Details Ejection launch mechanism Ejection launch mechanism

1974-10-07

1976-06-01

Brown, David H.

Ordnance

Rocket launching

Method of making

89 15R, 89 1812, F41F 306, F41F 502

Patent

active

039600513

ABSTRACT:
A breech and latch mechanism is described herein for use in an aircraft mile ejection launching system. The described mechanism is characterized by a fluid actuated piston that rotates a bell crank and link from a hook locking over-center position to a hook retracting position. The piston acts also as a sequencing valve to pass fluid to pressure actuated ejection rams. A pressure fluid distributing orifice structure and a pyrotechnic cartridge igniting firing pin structure are described also.

REFERENCES:
patent: 2774282 (1956-12-01), Ballash et al.
patent: 3057652 (1962-10-01), Geffner et al.
patent: 3186301 (1965-06-01), Buschers
patent: 3524381 (1970-08-01), Miller
patent: 3722944 (1973-03-01), Dand
patent: 3771412 (1973-11-01), Lebovitz

Affiliated with

Also associated with

Rating

Ejection launch mechanism does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Ejection launch mechanism, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Ejection launch mechanism will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFUS-PAI-O-2398528