This paper also provides processing methods for the aircraft SMCs specific geometric features, such as symmetry, pilot hole, bend relief and so on, in this foundation, the corresponding post processing subsystems is designed.

 
  • 對于航空鈑金零件上特有的幾何特征,如對稱(chēng)性、導孔、止裂孔等,本文提出了相關(guān)處理方法,并在此基礎上設計了相應的后置處理子系統。
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