An assembly of an engine with a pylon, including a force reacting assembly having a connection device and two rods, the connection device including a shoe. A spreader extends between first and second ends and has a central part connected to the shoe by a main connection including a main rotation pin and axis in a plane of symmetry of the connection device. Two fittings are on either side of the plane of symmetry each having two arms between which the spreader is positioned. A first, respectively second, rod includes a front end fastened to the engine and a rear end fastened to the first, respectively second, end of the spreader and to the first, respectively second, fitting by a secondary connection. Two extensions of the spreader are each associated with a pair of elastic stops. For the first, respectively second, end of the spreader, each stop is between an arm of the first, respectively second, fitting and the extension.
ASSEMBLAGE D'UN MOTEUR AVEC UN MÂT D'AÉRONEF
ASSEMBLY OF AN ENGINE WITH AN AIRCRAFT MAST
ZUSAMMENBAU EINES MOTORS MIT EINEM LUFTFAHRZEUGMAST
05.04.2023
Patent
Elektronische Ressource
Französisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
ASSEMBLAGE D'UN MÂT D'ACCROCHAGE AVEC UN MOTEUR D'AÉRONEF
Europäisches Patentamt | 2025
|