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复合材料结构件固化变形的控制,无论从原理上,还是从空客公司、波音公司已经取得的成果上来看,都证明是可行的,而且也达到了最初的目标:缩短研制周期,降低生产成本,实现复合材料结构的整体化和设计/制造一体化。
The control of the solidification and deformation of the composite structural members proved to be feasible both in principle and from the achievements already made by Airbus and Boeing and also achieved the initial goal of shortening the development cycle and lowering the production cost , To achieve the overall structure of the composite material and design / manufacturing integration.