Manufacturing method for large-scale thin-wall skin with inner ribs and complex mold cavities
A manufacturing method and skinning technology, applied in the field of mechanical processing, can solve the problems of high difficulty in CNC machining, low pass rate, large skin deformation, etc., and achieve the goals of simplifying the difficulty of CNC machining, accurately ensuring wall thickness, and improving surface accuracy Effect
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[0019] The test part is a skin part in a certain type of missile. The material of the part is 7A04 aluminum alloy. The product structure is a thin-walled part with inner ribs and complex inner cavity. The wall thickness of the large skin is 4mm, see attached figure 1 .
[0020] (1) Collect the original skin geometric parameters, simulate and flatten the skin, collect the corresponding data after flattening, program rough machining and finishing machining, and calculate the required minimum blank:
[0021] According to the specific structure of the required skin, collect its geometric parameters, and then use UG sheet metal modeling software to simulate and expand it into a flat state, see the attached figure 2 , get the corresponding geometric parameters after flattening, and program roughing and finishing according to these parameters.
[0022] Principle: According to the specific structure and size of the skin parts and the characteristics of flat plate bending and circle...
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