A device for fixing a lifting tooling on an aircraft component includes a threaded screw, a hollow body, an orientation and positioning system, and a retraction system. The threaded screw has a longitudinal axis and includes a distal end having a screw head. The threaded screw further includes a threaded proximal end and an intermediate part. The hollow body houses the threaded screw while allowing the rotation of the threaded screw along its longitudinal axis. The orientation and positioning system is configured to allow rotation of the threaded screw about axes transverse to the longitudinal axis of the threaded screw, and translation of the threaded screw parallel to its longitudinal axis. The retraction system is configured to retract the threaded proximal end of the threaded screw in the hollow body.
DISPOSITIF POUR LA FIXATION D'UN OUTILLAGE DE LEVAGE SUR PORTE D'INVERSEUR DE POUSSÉE DE NACELLE D'AÉRONEF
DEVICE FOR ATTACHING A LIFTING TOOL TO AN AIRCRAFT NACELLE THRUST REVERSER DOOR
VORRICHTUNG ZUR BEFESTIGUNG EINES HEBEWERKZEUGS AN EINER SCHUBUMKEHRKLAPPE EINER FLUGZEUGGONDEL
2024-04-24
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 |
European Patent Office | 2020
|European Patent Office | 2021
|PORTE D'INVERSEUR DE POUSSEE POUR NACELLE DE TURBOREACTEUR
European Patent Office | 2017
|European Patent Office | 2019
|European Patent Office | 2016
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