Aircraft engine with means of suspension from the structure...

Aeronautics and astronautics – Aircraft power plants – Mounting

Reexamination Certificate

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Reexamination Certificate

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11116260

ABSTRACT:
An aircraft engine includes a mounting attached to an aircraft structure and transmitting forces between an engine casing and the aircraft structure. The mounting includes a fail safe assembly with a safety clevis with two lugs and a tab arranged between the two lugs. Either the clevis or the tab is fixed to an element of the engine casing and the other tab or clevis is fixed to the structure. A safety hinge pin is perpendicular to the axis of the engine and passes through the tab and the clevis, the two lugs and the tab being parallel to the engine axis.

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patent: 0 997 653 (2000-05-01), None
patent: 2 799 432 (2001-04-01), None

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