A propulsion assembly for an aircraft, having a turbomachine, a pylon, and a device for reacting thrust forces having a main fitting, a spreader pivoting on the main fitting and having an opening, two rods articulated to the turbomachine and to the spreader, a secondary fitting fastened beneath the pylon and having a secondary female clevis constituted of two secondary arms passed through by holes of oblong shape and aligned along a secondary axis (R2), wherein the spreader is housed in the secondary female clevis of the secondary fitting, wherein the opening is coaxial with the secondary axis (R2), and a backup connection pin inserted with a tight fit into the opening and with clearance into the holes. Also an aircraft with such a propulsion assembly.
ENSEMBLE DE MOTORISATION D'AÉRONEF COMPORTANT UN DISPOSITIF DE REPRISE D'EFFORTS DE POUSSÉE
AIRCRAFT ENGINE ASSEMBLY COMPRISING A THRUST FORCE RECEIVING DEVICE
MOTORISIERUNGSEINHEIT FÜR EIN FLUGZEUG MIT EINER VORRICHTUNG ZUR AUFNAHME VON SCHUBKRÄFTEN
2025-05-07
Patent
Electronic Resource
French
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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