A propulsion assembly having a jet engine with a central casing, an attachment pylon having a rigid structure, a front engine attachment and a device for reacting the thrust forces. The front engine attachment has, on either side of a median plane, a front rod articulated via a connection point respectively to the rigid structure and to the central casing, and the reaction device has two central rods, two first fittings as one with the rigid structure and two second fittings as one with the central casing, wherein the two first fittings are independent of one another and wherein each central rod is articulated between a first fitting and a second fitting.
ENSEMBLE PROPULSIF POUR AÉRONEF COMPORTANT UN TURBORÉACTEUR, UN MÂT ET DES MOYENS D ACCROCHAGE DU TURBORÉACTEUR AU MÂT
PROPULSION ASSEMBLY FOR AIRCRAFT COMPRISING A TURBOJET, A MAST AND MEANS FOR ATTACHING THE TURBOJET TO THE MAST
ANTRIEBSBAUGRUPPE FÜR FLUGZEUGE MIT EINEM TURBOJET, EINEM MAST UND MITTELN ZUM BEFESTIGEN DES TURBOJET AN DEM MAST
2024-07-17
Patent
Electronic Resource
French
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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