Failure tolerant engine mounting

Aeronautics and astronautics – Aircraft power plants – Mounting

Patent

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Details

60 3931, 248554, B64D 2716

Patent

active

050783424

ABSTRACT:
A failure tolerant engine mounting is formed by three links between the engine and its support structure, one of the links being arranged so that in the event of failure of either of the other links it will form a connection between three points on the engine and supporting structure which are symmetrically arranged about a vertical axis through the engines center of gravity.

REFERENCES:
patent: 3907220 (1975-09-01), Amelio
patent: 4044973 (1977-08-01), Moorehead
patent: 4065077 (1977-12-01), Brooks
patent: 4560122 (1985-12-01), Parkinson et al.
patent: 4997145 (1991-03-01), Hodgkinson

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