An assembly for an aircraft that has a wing and an engine pylon having a primary structure with right-side and left-side panels, an upper and a lower spar and a rear rib, two sets of upper or lower shackles, one set fastening the right-side panel to the wing, and a second set fastening the left-side panel to the wing, a fastening element secured to the rear rib or to the lower spar, a rear rod connecting the fastening element to the wing, a transverse shackle connecting the upper spar to the wing, a line connecting two centers of the transverse shackle being oriented transversely relative to a longitudinal axis of the engine pylon, and a reinforcing panel, at each joint between a right-side or left-side panel and an upper or lower shackle, which is fastened along a height against the panel and to which the shackle is also fastened.
ENSEMBLE POUR UN AÉRONEF COMPORTANT UNE AILE ET UN MÂT RÉACTEUR POUR COUPLER UN TURBORÉACTEUR À LADITE AILE
ASSEMBLY FOR AN AIRCRAFT COMPRISING A WING AND A REACTOR MAST FOR COUPLING A JET ENGINE WITH SAID WING
ANORDNUNG FÜR EIN LUFTFAHRZEUG AUS EINEM FLÜGEL UND EINEM TRIEBWERKSTRÄGER ZUR ANKOPPLUNG EINES TURBOTRIEBWERKS AN DIESEN FLÜGEL
2023-04-26
Patent
Electronic Resource
French
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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