A propulsion assembly having a pylon, a turbomachine comprising an engine and a fan that is enclosed by a fan casing, a nacelle surrounding the engine and the fan casing and having a load support disposed in the top part of the nacelle, a front engine attachment between the pylon and a front part of the engine, a rear engine attachment between the pylon and a rear part of the engine, a front fan attachment between the fan casing and the load support, and a rear pylon attachment between the pylon and the load support. Such a propulsion assembly allows a reduction in bulk since the load of the turbojet engine is distributed between the load support and the pylon, and the pylon is attached to the engine.
ENSEMBLE DE MOTORISATION POUR UN AÉRONEF COMPRENANT UN SUPPORT DE CHARGE
MOTOR ASSEMBLY FOR AN AIRCRAFT COMPRISING A LOAD SUPPORT
MOTORISIERUNGSEINHEIT FÜR EIN LUFTFAHRZEUG, DIE EINEN LASTTRÄGER UMFASST
2021-12-01
Patent
Elektronische Ressource
Französisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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