Method for detecting finish machining clamping deformation of aircraft component
作者： Zeng Liusheng , Zhou Chong , Huang Jinjin , Cao Qingxia , Yang Huan
DOI:
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摘要: A method for detecting finish machining clamping deformation of an aircraft component comprises the steps that according to a requirement component, position installing device paired structure is selected, with be carried out arranged on frame, installed determined position, and then appearance adjusted in state required by technology through adjusting device; support used fixing dial indicator frame or at close structure, detection contact around 50 mm away from meanwhile pointer zero point; again so can firmly clamped, detected indicator, slightly adjusted, finally technological docking mode. Operation easy convenient, zero, application range wide, production cost low.
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