The invention relates to an electric positioning locking device for a tool frame of an aircraft. A locking positioning component is arranged in a base, a positioning flange component is arranged at the external end of the locking positioning component, and a monitor component is arranged at the end face of the positioning flange component. According to the locking device, an assembly tool frame of a large aircraft can be quickly reconstructed under the condition that the assembly tool frame accuracy and reliability of an aircraft are not reduced, so that the assembly tool frame of a large aircraft can be recycled, the novel aircraft development cost can be reduced, the preparation cycle of aircraft development production is greatly shortened, and the requirement for quickly developing novel aircrafts can be met.
Electric positioning locking device for tool frame of aircraft
2016-02-17
Patent
Elektronische Ressource
Englisch
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 |
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