Movement butt joint device for large body part of airplane general assembly
A docking device and general assembly technology, applied in aircraft assembly, aircraft parts, ground installations, etc., can solve the problems of low docking accuracy, long stagnation time of large parts, hidden safety and quality hazards, etc., to eliminate assembly stress and meet the requirements of automatic docking Effect
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Applications(China)
- Current Assignee / Owner
- Publication Date
- 2011-11-23
- Estimated Expiration
- Not applicable · inactive patent
Smart Images
Figure 1 Figure 2 Figure 3
Abstract
Description
Technical field
[0001] The invention relates to the field of automatic docking of large parts of aircraft general assembly, in particular to a mobile docking device for large parts of a fuselage. Background technique
[0002] Aircraft assembly automation docking technology is the beginning of the final assembly of the aircraft, and it is also one of the most important links in the aircraft manufacturing process. Its assembly quality and efficiency directly affect the subsequent assembly production process. The docking of large parts of the aircraft fuselage still adopts the traditional manual hoisting and docking mode. The docking accuracy is low, the work efficiency is low, the labor intensity is high, and the large components stand for a long time, and there are certain safety and quality risks in the docking. In order to improve and ensure the fuselage docking assembly technology and assembly quality, it is imperative to change the docking mode of traditional hoisting aircraft...
Examples
Embodiment Construction
[0013] With reference to the drawings, the frame body 16 of the mobile docking device for large parts of the aircraft assembly fuselage is welded by rigid structural parts. On both sides of the frame body 16, there are two symmetrical upper docking working platforms 3, The inner side of the main body 16 is provided with a lower docking work platform 5, and a telescopic work platform 7 is also provided on the rear side of the frame body 16. The telescopic work platform 7 is connected to the rear side of the frame body 16 through a sliding rod 8 and a positioning pin 9. Operators can stand on the above-mentioned working platform to measure the posture of the docking surface of the fuselage and do the docking work; there are rollers 6 and anchor bolts 4 at the bottom of the frame body. During transportation, the anchor bolts are raised and the device and the device are connected with the rollers. The large part of the fuselage is moved to the docking platform of the aircraft, and t...