Pod for suspending a turbojet engine unit of the bypass type und

Details Pod for suspending a turbojet engine unit of the bypass type und Pod for suspending a turbojet engine unit of the bypass type und

1992-05-22

1993-01-26

Peters, Jr., Joseph F.

Aeronautics and astronautics

Aircraft power plants

Mounting

248554, 248555, B64D 2700

Patent

active

051816750

ABSTRACT:
A pod for suspending a turbojet engine unit below the wing of an aircraft includes a suspension assembly with two laterally spaced front beams connecting the turbojet fan casing to the wing, and two rear links disposed in a common vertical plane and pivotally connected at one end to the wing and at the other end to a connection link which is connected at least to the exhaust casing of the engine, the front beams being interconnected by cross-bracing and being connected at the level of the downstream edge of the cross-bracing to at least one fixed part of the engine.

REFERENCES:
patent: 3201069 (1965-08-01), Haskin
patent: 3517897 (1970-06-01), Wells
patent: 4013246 (1977-03-01), Nightingale
patent: 4055041 (1977-10-01), Adamson et al.
patent: 4147029 (1979-04-01), Sargisson
patent: 4458863 (1984-07-01), Smith
patent: 4506850 (1985-03-01), McConnell
patent: 4555078 (1995-11-01), Groguard
patent: 4717094 (1988-01-01), Chee
patent: 4725019 (1988-02-01), White
patent: 4917331 (1990-04-01), Hager et al.

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