Suspension system for a rotary wing aircraft engine

Aeronautics and astronautics – Aircraft power plants – Mounting

Reexamination Certificate

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Details

C244S017270, C248S638000, C248S556000

Reexamination Certificate

active

07461815

ABSTRACT:
The invention relates to a system for suspending an engine of a rotary wing aircraft. The technical field of the invention is that of manufacturing suspension devices for helicopter engines. The invention consists in a device for suspending an engine (21) to a rotary aircraft airframe (26), which device includes a deformable structure (20) interconnecting two attachment zones (13, 17) of the device.

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