The invention discloses aircraft main landing gear assembling and disassembling equipment. The aircraft main landing gear assembling and disassembling equipment comprises a main support frame, an auxiliary support frame, two lifting sloping plates, two telescopic idler wheels and adjusting screws; the main support frame is an L-shaped steel structure frame formed by a vertical frame and a horizontal frame, the back surface of the vertical frame of the main support frame is connected with a lifting device of a mobile platform through hooks, the two telescopic idler wheels are fixed at the left end and the right end of the upper surface of the vertical frame of the main support frame, and the two lifting sloping plates are respectively connected with the left side and the right side of the horizontal frame of the main support frame through the adjusting screws; the auxiliary frame is arranged in the middle of the horizontal frame of the main support frame. During the operation of the equipment, a landing gear column and an aircraft wheel can be mounted on an aircraft without dismounting, the working load is reduced, and the working procedures are optimized. The equipment can motion on a plane in an omnidirectional way, moves flexibly and is convenient to operate; assembly and disassembly can be finished through adjusting the state of a main landing gear, and the use is convenient.
Aircraft main landing gear assembling and disassembling equipment
2016-01-20
Patent
Electronic Resource
English
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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