Mounting bypass gas turbines engines on aircraft

Aeronautics and astronautics – Aircraft power plants – Mounting

Patent

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248 5, B64D 2716

Patent

active

040132463

ABSTRACT:
A bypass gas turbine engine is mounted from an aircraft pylon by a mounting arrangement in which the engine outer casing and the core gas generator are mounted independently to the pylon and in which all the connections between the outer casing and the pylon and between the core gas generator and the pylon lie in substantially the same two planes.

REFERENCES:
patent: 3042349 (1962-07-01), Pirtle et al.
patent: 3352114 (1967-11-01), Wilde et al.
patent: 3397855 (1968-08-01), Newland
patent: 3675418 (1972-07-01), Lenkeit et al.
patent: 3750983 (1973-08-01), Morris
patent: 3837602 (1974-09-01), Mullins
patent: 3848832 (1974-11-01), Stanley et al.

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