Aircraft engine mounting

Power plants – Combustion products used as motive fluid – Having mounting or supporting structure

Reexamination Certificate

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Details

C060S262000

Reexamination Certificate

active

07313920

ABSTRACT:
An aircraft engine mounting assembly comprising a bracket arrangement with two plates located either side of an opening in the structural bypass duct. The bracket arrangement mounts two inclined links which connect to the engine. In normal usage, tension/compression from the links will be passed by the bracket arrangement into the airframe. Upon failure of one of the links the bracket arrangement will engage with the structural bypass duct to transmit engine loads into the airframe via the duct.

REFERENCES:
patent: 3318554 (1967-05-01), Mullins et al.
patent: 3397855 (1968-08-01), Newland
patent: 3398535 (1968-08-01), Hemsworth et al.
patent: 3750983 (1973-08-01), Morris
patent: 3907220 (1975-09-01), Amelio
patent: 4266741 (1981-05-01), Murphy
patent: 4603822 (1986-08-01), Chee
patent: 5076049 (1991-12-01), Von Benken et al.
patent: 5428952 (1995-07-01), Jewess
patent: 5927644 (1999-07-01), Ellis et al.
patent: 7083143 (2006-08-01), Whitmer et al.
patent: 7108224 (2006-09-01), Pasquer et al.
patent: 1 074 068 SP (1967-06-01), None
patent: 849 694 (1996-09-01), None

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