A unit for handling an aircraft turbojet engine includes a frame, a front cradle and a rear cradle designed for supporting the turbojet engine, and a plurality of electric actuators. The cradles include devices for securing the turbojet engine. The plurality of electric actuators includes three electric actuators, where a first one and second one are arranged opposite each other, on either side of a longitudinal axis of the frame, connected to the front cradle and arranged for moving same in vertical translation, and where a third actuator is connected to the rear cradle and arranged for moving the same in vertical translation. The handling unit further includes a device for rotary driving of the front cradle about a longitudinal axis of the turbojet engine.
ENSEMBLE DE MANUTENTION D'UN TURBORÉACTEUR D'AÉRONEF
MAINTENANCE ASSEMBLY FOR AN AIRCRAFT TURBINE ENGINE
WARTUNGSVORRICHTUNG FÜR EIN FLUGZEUGTURBINENTRIEBWERK
2022-01-26
Patent
Electronic Resource
French
IPC: | B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen |
Ensemble de manutention d’un cône d’éjection pour turboréacteur d’aéronef
European Patent Office | 2024
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