Man-machine hybrid enhanced aircraft structural member design method based on instance reasoning
A technology of aircraft structural parts and case-by-case reasoning, which is applied to computer parts, calculation, image data processing, etc., can solve the time-consuming and labor-intensive pass rate of similar model parts, so as to save modeling time, shorten development cycle, and improve modeling efficiency effect
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[0038] The present invention will be further described in detail below in conjunction with the accompanying drawings. The drawings described here are a part of the present application, and are used to further explain the present invention, but do not constitute a limitation of the present invention.
[0039] (1) Step 1, according to the requirements of the components in the existing design requirements, the designer analyzes its needs in terms of bearing capacity, manufacturing cost, life and its working conditions, from machining parts, sheet metal parts Among the three categories of parts and components, the rudder surface suspension joints in the frame parts are obtained, because the rudder surface suspension joints also include single-head suspension joints, double-head suspension joints, three-head suspension joints and rudder surfaces. Suspension joints, and there are differences in the dimensions of the same type of suspension joints, so further reasoning is required to...
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