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在某飞机结构中存在一系列相似的结构件,通过运用参数化的方法,使这些相似的零件仅通过修改某些参数值来实现,取代了以往通过重新根据飞机理论基准和理论曲面,依次建立新模型,依次运行该相似结构设计的全过程的方法。
A series of similar structural elements exist in an airplane structure. By using a parametric method, these similar parts are only realized by modifying certain parameter values, instead of relying on re-establishing theoretical planes and theoretical surfaces based on the aircraft and sequentially establishing The new model, in turn, runs the entire process of designing similar structures.