Mounting devices for multiple flow turbojet engines

Details Mounting devices for multiple flow turbojet engines Mounting devices for multiple flow turbojet engines

1980-11-06

1984-04-10

Croyle, Carlton R.

Power plants

Reaction motor

Air passage bypasses combustion chamber

60 3932, 74520, 74106, 138 37, 138113, 138114, 248555, 248556, F02K 140, F02K 302

Patent

active

044413130

ABSTRACT:
A mounting device for mounting the exhaust casing of a turbojet engine on a rigid support structure connected with an aircraft, there being at least two flows, i.e., a primary flow in the exhaust casing and a secondary flow in a shroud which surrounds the casing and which is fastened to the support structure by a rigid ring. The device consists of a plurality of arms each having means to control its orientation.

REFERENCES:
patent: 2936978 (1960-05-01), Lauck
patent: 2936999 (1960-05-01), Coar et al.
patent: 3412560 (1968-11-01), Gaubatz
patent: 3886737 (1975-06-01), Grieb

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