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
04.01.2022
Patent
Elektronische Ressource
Englisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen |
MOUNT ARRANGEMENT FOR TORQUE ROLL VIBRATION ISOLATION
Europäisches Patentamt | 2023
|MOUNT ARRANGEMENT FOR TORQUE ROLL VIBRATION ISOLATION
Europäisches Patentamt | 2020
|MOUNT ARRANGEMENT FOR TORQUE ROLL VIBRATION ISOLATION
Europäisches Patentamt | 2020
|Microgravity Vibration Isolation Mount
British Library Conference Proceedings | 1994
|