摘要
针对T型翼片的技术指标,依据应力分析结果,介绍了缠绕和铺层两种成型工艺,静力试验的结果表明:两种成型工艺均满足规定的均布载荷下、挠度小于200mm的主要技术指标,通过对比两种工艺的优缺点,认为铺层工艺更适合该翼片的生产。
This study aims at the technology need of some missile wings. According to the result of strain analysis, two kinds of processing methods of filament winding and moulding is introduced. The static test results show that two kinds of processing methods satisfy the need of general flexibility less than 200 mm, under the uniform load of XX kg. By comparison of the two kinds of processing methods, moulding is regarded as more suitable method for processing of T-type missile wings.
出处
《宇航材料工艺》
CAS
CSCD
北大核心
2009年第1期70-72,共3页
Aerospace Materials & Technology
关键词
缠绕
铺层
工艺
静力试验
翼片
Filament winding, Moulding, Processing, Statics test, Missile wings
