The invention provides an aircraft repairing maneuvering device, comprising a chassis frame. A cabin is arranged on the chassis frame. The cabin is internally provided with an electric cabinet, a power module, a welding module, a riveting module, a paint spraying module, a fitter module, an external cable, a flaw detection module, a duct processing module, a sheet metal processing module, an accessory module, an engraving module and a marking module. The cabin comprises a front wall, a rear wall, a left wall, a right wall, a bottom part and a top part. The electric cabinet is installed on an upper interlayer in the front part of the cabin through a supporting rack; the power module is fixedly installed at the lower end of the electric cabinet; the external cable is fixedly installed at the lower end of the power module; the fitter module and the marking module are arranged on the upper interlayer in the front part of the cabin; the duct processing module is arranged on a lower interlayer in the front part of the cabin; the engraving module and the flaw detection module are arranged on the upper interlayer in the middle part of the cabin; the welding module and the paint spraying module are arranged on the lower interlayer in the middle part of the cabin; the riveting module and the sheet metal processing module are arranged on the lower interlayer in the rear part of the cabin; the accessory module is arranged in the available space in the front part, middle part and rear part of the cabin. The device is small in size, complete in function, high in maneuverability and convenient in carrying.
Aircraft repairing maneuvering device
2015-08-26
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 |
Flutter of Maneuvering Aircraft
ASCE | 2014
|Flutter of Maneuvering Aircraft
Online Contents | 2015
|Structural dynamics of maneuvering aircraft
Tema Archiv | 1987
|