Canopy or panel actuation system

Aeronautics and astronautics – Aircraft structure – Fuselage and body construction

Patent

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Details

244122AF, B64C 132

Patent

active

052286428

ABSTRACT:
An aircraft canopy ejection system includes a releasable coupling 22 in the load path between an opening/closing jack 19 and the canopy. The coupling 22 is released immediately before emergency jettison of the canopy.

REFERENCES:
patent: 2327951 (1943-08-01), Zaleske
patent: 2654135 (1953-10-01), Grizzard et al.
patent: 2951274 (1960-09-01), Elsner
patent: 3139721 (1964-07-01), Daubenspeck
patent: 3240520 (1966-03-01), Dailey et al.
patent: 3455248 (1969-07-01), Sutton et al.
patent: 4860838 (1989-08-01), Asak
patent: 4902045 (1990-02-01), McGugan et al.

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