Air tap and engine mount for a turbojet engine

Details Air tap and engine mount for a turbojet engine Air tap and engine mount for a turbojet engine

1989-06-19

1990-05-29

Stout, Donald E.

Power plants

Reaction motor

Interrelated reaction motors

60 3907, 60 3931, 244 54, F02K 304

Patent

active

049284835

ABSTRACT:
The present invention provides an air tapping device for tapping a portion of the air passing through the bypass duct of a fan-type turbojet engine. The device is incorporated into the engine mount and is provided with an anti-vibration mounting to minimize the transmission of engine vibrations to the air tapping device. The device is preferably incorporated into the rear engine mount which attaches the engine to the aircraft structure.

REFERENCES:
patent: 3777489 (1973-12-01), Johnson et al.
patent: 3779006 (1973-12-01), Lewis et al.
patent: 4044973 (1977-08-01), Moorehead
patent: 4155680 (1979-05-01), Linko et al.
patent: 4255083 (1981-03-01), Andre et al.
patent: 4712370 (1987-12-01), MacGee

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