A mounting arrangement for mounting a rotary engine (2) to an aircraft structure, wherein the engine has a three orthogonal axes comprising: a roll axis (5); a pitch axis (14); and a yaw axis (15). The mounting arrangement comprises: one-degree-of-freedom links with reaction axes passing through the roll axis (5). A separate roll constraint has a moment reaction about the roll axis (5) to decouple the torque roll mode from the other one-degree-of-freedom links.
MOUNT ARRANGEMENT FOR TORQUE ROLL VIBRATION ISOLATION
LAGERANORDNUNG ZUR PENDELSCHWINGUNGSISOLIERUNG
AGENCEMENT DE MONTAGE POUR ISOLER LES VIBRATIONS D'UN ROULEAU DE COUPLE
2023-11-15
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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