文章摘要
固体火箭发动机燃烧室壳体纤维缠绕模具设计
The Design of the Fibre Winding Mold of the Solid Rocket Motor Combustion Chamber Shells
Received:May 13, 2009  Revised:November 10, 2009
DOI：
中文关键词: 固体火箭发动机燃烧室壳体  纤维缠绕  模具设计
英文关键词: solid rocket motor combustion chamber shell  fibre winding  mold design
基金项目:
Author NameAffiliation
HE Xi-ying No.203 Research Institute of China Ordnance Industries， Xi'an 710065， China 
WANG Zhi-gang No.203 Research Institute of China Ordnance Industries， Xi'an 710065， China 
YANG Yue-dong No.203 Research Institute of China Ordnance Industries， Xi'an 710065， China 
ZHAO Hai-e No.203 Research Institute of China Ordnance Industries， Xi'an 710065， China 
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中文摘要:
      介绍一种固体火箭发动机燃烧室壳体纤维缠绕芯模的设计。这项工作的目的在于提供一种可重复使用的纤维缠绕芯模。它采用的方法是钢模分瓣法。这种芯模的关键技术是芯模的组装和脱模。这项工作的意义在于提高纤维缠绕固体火箭发动机燃烧室壳体的比强度,节约生产成本,提高工作效率。
英文摘要:
      This article introduces a designing means of mold of the fibre winding solid rocket motor combustion chamber shell. The purpose of this work lies in providing a mold which can be reused. The mold has valving structure. The key techniques of this mold are assembly and unloading of mold. The intention of this research lies in increasing the specific intensity of the fibre winding solid rocket motor combustion chamber shell，economizing on manufacture cost and promoting work efficiency.
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