Advanced composite aircraft cowl

Details Advanced composite aircraft cowl Advanced composite aircraft cowl

1987-02-18

1989-05-02

Barefoot, Galen

Aeronautics and astronautics

Aircraft structure

181214, 181222, 181292, 244 1N, 244 53R, B64D 3300, F01N 124

Patent

active

048261068

ABSTRACT:
An aircraft cowl, and in particular a translating cowl, used as a component of a thrust reverser, formed of at least one one-piece bondment cured in a single operation. Preferably, a one-piece inner bondment and a one-piece outer bondment fastened together at a joining region. The bondments have constant density cores and tapered closures. Acoustically absorbing materials are part of the lay up for one of the bondments and are integrally cured therein.

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patent: 4313524 (1982-02-01), Rose
patent: 4344995 (1982-08-01), Hammer
patent: 4533098 (1985-08-01), Bonini et al.
patent: 4585189 (1986-04-01), Buxton

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