摘要
本文介绍了腹板上有两个开口的不规则“Ц”形结构件的研制。通过对模具方案的确定，选择预成形工艺以及对热压罐成形工艺参数进行合理调整，制造出符合设计要求的试验件。
evelopment of carbon fibre composite structural component with two holes on the abdomen in irregular 'Ц' shape is described in the paper. The component has been manufactured successfully after selecting moulds, preforming process and autoclave moulding process based on the requirements of design.
出处
《宇航材料工艺》
CAS
CSCD
北大核心
1996年第4期17-19,共3页
Aerospace Materials & Technology
关键词
碳纤维
复合材料
异型结构件
成形
Carbon fibre composite
Irregular structural component
Forming
