摘要
对于企业未来的CIMS,存在一个“CIMS=CAD/CAM+?”的问题。本文针对航空发动机的机匣、盘轴和叶轮这三大类零部件,提出了相应的CIMS结构形式。
“CIMS=CAD/CAM+?”is a problem to the future CIMS of a factory. This paper gives out 3 structures of CIMS, suitable for housings, discs and shafts, integrally bladed rotors as well, and analyses different production organizations relative to the structures of CIMS.
出处
《航空制造工程》
1997年第9期25-26,38,共3页
Aviation Engineering & Maintenance