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Research And Implementation Of Rapid Design Technology For The Aircraft Assembly Fixtures Frame

Posted on:2008-09-03Degree:MasterType:Thesis
Country:ChinaCandidate:H Y JiangFull Text:PDF
GTID:2132360215497767Subject:Mechanical engineering
Abstract/Summary:PDF Full Text Request
The frame is the base of the aircraft tooling, the quality and the development time of an aircraft assembly fixture are significantly affected by it. At present, there are some disadvantages in the process of frame design, such as: poor quality of the models and little reuse of the design. In order to solve these problems, rapid design for aircraft assembly fixtures frame technology is studied. A sub-system of frame rapid design is developed according to the requirement of a large aeronautics corporation. The main jobs of this paper are as followed:1) The reuse of the frame design technology for aircraft assembly fixtures is researched. a frame line part library is built with the templet driven technology, the reuse of the frame line part come true by the tools for instantiation and instance modification. The design resources are effectively used, some repeating work is cut.2) Two methods to obtain the assembly feature are proposed: the straight way by the Enumeration method and the indirect way by project features to the assembly plane. All of the assembly features of the frame and the adjustable bearings are obtained by these two methods which makes the frame automatic assembly technology for aircraft assembly fixtures come true.3) The frame automatic assembly technology aircraft assembly fixtures based on assembly features is researched. A binary tree assembly model is used to express the assembly information of the frame for aircraft assembly fixtures, the automatic assembly between the frame, the aircraft and the adjustable bearing is completed within the three steps: distribute, obtain and evaluate assembly feature. Finally, the efficiency of the frame assembly design is proved.4)The frame interpart modeling technology for aircraft assembly fixtures is researched, the intersection methods are concluded and the arithmetic of the single-cut, double-cut and inter-cut intersection is proposed, the interpart fast modeling of the frame design for aircraft assembly fixture come true. 5)Based on the researches mentioned before, a sub-system of frame fast design for aircraft assembly fixture is developed on CATIA. The sub-system is used to design the aircraft assembly fixtures in a large aeronautics corporation and make a good- effect.
Keywords/Search Tags:CAD, Tooling, Assembly Fixture, Frame, Rapid Design
PDF Full Text Request
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