Flexible suspension for turbine engine

Details Flexible suspension for turbine engine Flexible suspension for turbine engine

2011-03-22

2011-03-22

Dinh, Tien (Department: 3644)

Aeronautics and astronautics

Aircraft power plants

Mounting

C248S557000

Reexamination Certificate

active

07909285

ABSTRACT:
A suspension for suspending a turbine engine from the structure of an aircraft is disclosed. The suspension includes a beam with a first element including a first attachment unit which attaches the beam to the structure and a second element including a second attachment unit which attaches to the beam to the turbine engine. The beam further includes a first plate and a second plate. The plates are positioned transversely to the axis of the engine and joined together by a layer of elastomer. The first plate being secured to the first element and the second plate to the second element. This arrangement allows vibration damping between the engine and the structure of the aircraft.

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