A mounting arrangement for mounting a rotary engine to an aircraft structure, wherein the engine has a three orthogonal axes comprising: a roll axis; a pitch axis; and a yaw axis. The mounting arrangement comprises: one-degree-of-freedom links with reaction axes passing through the roll axis. A separate roll constraint has a moment reaction about the roll axis to decouple the torque roll mode from the other one-degree-of-freedom links.
MOUNT ARRANGEMENT FOR TORQUE ROLL VIBRATION ISOLATION
DISPOSITIF DE MONTAGE POUR L`ISOLATION DES VIBRATIONS DU ROULEAU DE COUPLE
2020-11-17
Patent
Electronic Resource
English
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
Microgravity Vibration Isolation Mount
British Library Conference Proceedings | 1994
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