The present disclosure provides a tooling for handling a nacelle of an aircraft turbojet engine. The tooling includes a gantry having at least one upper support bar which is hinged about at least a first upper axis of rotation (A) by a first upper hinge. The upper support bar is hinged between at least a first support position in which the upper bar has a first attachment which is adapted to be fastened on a first type of nacelle, and at least a second support position in which the upper support bar has a second attachment which is adapted to be fastened on a second type of nacelle.
OUTILLAGE POUR LA MANUTENTION D'UNE NACELLE DE TURBORÉACTEUR D'AÉRONEF
TOOL FOR HANDLING AN AIRCRAFT ENGINE NACELLE
WERKZEUG ZUR HANDHABUNG EINER LUFTFAHRZEUGTRIEBWERKGONDEL
20.03.2019
Patent
Elektronische Ressource
Französisch
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 |
OUTILLAGE POUR LA MANUTENTION D'UNE NACELLE DE TURBOREACTEUR D'AERONEF
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