Mounting system for coupled turboshaft gas turbine engines

Details Mounting system for coupled turboshaft gas turbine engines Mounting system for coupled turboshaft gas turbine engines

1983-10-06

1985-02-19

Barefoot, Galen L.

Aeronautics and astronautics

Aircraft power plants

Mounting

244 1727, 248554, 248639, 60 3931, 180 696, B64D 2700, B64D 2716

Patent

active

045000549

ABSTRACT:
A mounting system for two turboshaft gas turbine engines which are connected by a coupling gearbox. The mounting system comprises a front mounting attached to the gearbox which permits pivotal movement of the engine/gearbox assembly but restrains longitudinal movement and two strut members which support the engines vertically but provide no lateral or longitudinal support. The engines are interconnected by link members and an intermediate member rotatably attached to the vehicle which permit relative lateral movement between the engines but constrain any lateral movements of the engines which are in unison relative to the vehicle.

REFERENCES:
patent: 1664129 (1928-03-01), Pallenberg
patent: 2324542 (1943-07-01), Schan
patent: 2539960 (1951-01-01), Marchant et al.
patent: 2718756 (1955-09-01), McDowall
patent: 2828607 (1958-04-01), Johnson
patent: 3180426 (1965-04-01), Crim
patent: 3288404 (1966-11-01), Schmidt et al.
patent: 3592421 (1971-07-01), Kopp
patent: 3907220 (1975-09-01), Amelio

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