An engine attachment configured to link an engine and an aircraft pylon comprising a first end fitting having two mutually parallel wings, a joining piece positioned between the first end fitting wings and linked to the first end fitting by a link system, fixing elements, linking the first end fitting and the pylon, including first and second fixing elements positioned between the first end fitting wings which are inclined by an angle of between 10 and 45° to be able to be put in place and removed in the presence of the joining piece linked to the first end fitting by the link system. The inclined fixing elements absorb lateral loads. The joining piece and the first end fitting are linked by the link system before the engine is fixed to the pylon. The engine is fixed to the pylon by putting the fixing elements in place.
AIRCRAFT ENGINE ATTACHMENT COMPRISING INCLINED FIXING ELEMENTS, AIRCRAFT COMPRISING SAID ENGINE ATTACHMENT AND METHOD FOR FIXING AN ENGINE TO AN AIRCRAFT PYLON USING SAID ENGINE ATTACHMENT
2019-10-17
Patent
Electronic Resource
English
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
Propulsion system for aircraft comprising turbojet engine, pylon and engine attachment
European Patent Office | 2025
|Propulsion system for aircraft comprising turbojet engine, pylon and engine attachment
European Patent Office | 2025
|Propulsion system for aircraft comprising turbojet engine, pylon and engine attachment
European Patent Office | 2025
|