Rear hanging structure for a turbojet engine

Details Rear hanging structure for a turbojet engine Rear hanging structure for a turbojet engine

1992-08-14

1993-08-24

Peters, Jr., Joseph F.

Aeronautics and astronautics

Aircraft power plants

Mounting

248554, 248555, 60 3931, B64D 2700

Patent

active

052382060

ABSTRACT:
The rear hanging structure by which a turbojet engine is suspended from a mast under the wing of an aircraft includes a brace which is fixed to the mast and to which the engine is attached by at least three suspension links, the brace includes two parts which are fitted one within the other and are dimensioned in such a way as to ensure that each is able to take all of the suspension stresses independently of the other, the pins by which the brace is connected to the mast and to the suspension links passing through both parts of the brace. The redundancy thus achieved increases considerably the reliability of the suspension.

REFERENCES:
patent: 2818225 (1957-12-01), Kent
patent: 4634081 (1987-01-01), Chee
patent: 4725019 (1988-02-01), White
patent: 5078342 (1992-01-01), Langley et al.

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