The device has a rigid structure (8) and a front aerodynamic structure (24) that is mounted on the structure (8) via a mounting unit. The mounting unit comprises two connecting rods (32) placed in a symmetric manner with respect to a vertical median plane of the device, parallel to a longitudinal direction (X) of the device. A lower end of each rod is connected to an upper spar of the structure (8) and an upper end of each rod is connected in an articulated manner to a lower spar of the structure (24). The rods are designed such that their lengths are adjustable.
DISPOSITIF D'ACCROCHAGE D'UN MOTEUR INTERPOSE ENTRE UNE VOILURE D'AERONEF ET LEDIT MOTEUR
ENGINE MOUNTING STRUCTURE INTERPOSED BETWEEN AN AIRCRAFT WING SYSTEM AND SAID ENGINE
MOTORMONTAGESTRUKTUR ZWISCHEN EINEM FLUGZEUGFLÜGELSYSTEM UND DEM MOTOR
2017-06-07
Patent
Elektronische Ressource
Französisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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