Ejector (1) for load (2), including a guide means (4), including: a first top rod (BS1), a first bottom rod (BI1), the first top rod (BS1) being hinged with the aircraft (3) at a first top hinge (AS1), and with the first bottom rod (BI1) at a first median hinge (AM1), the first bottom rod (BI1) being hinged with the load (2) at a first bottom hinge (AI1), the axes of the first three hinges (AS1, AM1, AI1) being parallel, a second top rod (BS2), a second bottom rod (BI2), the second top rod (BS2) being hinged with the aircraft (3) at a second top hinge (AS2), and with the second bottom rod (BI2) at the second median hinge (AM2), the second bottom rod (BI2) being hinged with the load (2) at a second bottom hinge (AI2), the axes of the second three hinges (AS2, AM2, AI2) being parallel, and a synchronization means (5) suitable for copying, by applying a gain thereto, the angle of the first top hinge (AS1) to the angle of the first median hinge (AM1), suitable for copying, by applying a gain thereto, the angle of the second top hinge (AS2) to the angle of the second median hinge (AM2) and suitable for copying, by applying a gain thereto, the angle of the first top hinge (AS1) to the angle of the second top hinge (AS2).
DISPOSITIF DE GUIDAGE POUR EJECTEUR
EJECTOR GUIDE DEVICE
AUSWERFERFÜHRUNGSVORRICHTUNG
01.04.2020
Patent
Elektronische Ressource
Französisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |