An aircraft engine pylon having an upper fitting, an upper panel located below the upper fitting, a shear pin at least partially coupling the upper fitting and the upper panel, and tension fasteners at least partially coupling the upper fitting and the upper panel with the shear pin defining a shear force load path and the tension fasteners defining tension force load paths.
AIRCRAFT ENGINE PYLON
TRIEBWERKSPYLON FÜR LUFTFAHRZEUG
MÂT D'ACCROCHAGE DE MOTEUR POUR AÉRONEF
2022-04-27
Patent
Electronic Resource
English
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |