Active mounts for aircraft engines

Aeronautics and astronautics – Aircraft power plants – Mounting

Patent

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Details

244 1727, 244 1N, 26714015, B64D 2700

Patent

active

055516505

ABSTRACT:
An active mount for fixed wing applications. One aspect of the invention provides decoupling of two tones which are close in frequency by positioning the mount actuators and error sensors in the primary transmission path of the disturbance vibration and by providing adequate spatial separation between the two sets of error sensors to reduce or eliminate cross-coupling of the signals. Another aspect of the invention utilizes orthogonally positioned actuators with corresponding actuators of paired mounts being focalized for each engine.

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