To reduce flexural deformations of an engine, an engine assembly comprises a device for attaching the engine onto a structure of an aircraft, the attachment device including a primary structure, an attachment device for attaching the engine onto the primary structure of the attachment pylon, and a nacelle including thrust reversal cowls, each equipped with an inner structure arranged around a case portion of the engine. The assembly includes flexible devices for transmitting forces, arranged between the case portion and the inner structures of the cowls, each device including an elastically deformable device configured so that in the closed position of the cowl, with the engine at a standstill, it adopts a partial elastic deformation state allowing the device to apply a prestress force on the case portion.
ENSEMBLE MOTEUR POUR AERONEF, COMPRENANT DES DISPOSITIFS SOUPLES DE TRANSMISSION D'EFFORTS AGENCES ENTRE LES CAPOTS D'INVERSION DE POUSSEE ET LE MOTEUR
2018-03-09
Patent
Electronic Resource
French
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
European Patent Office | 2018
|ENSEMBLE MOTEUR POUR AERONEF COMPRENANT UN MOTEUR AINSI QU'UN MAT D'ACCROCHAGE D'UN TEL MOTEUR
European Patent Office | 2017
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