摘要
多预埋件覆铝箔碳面板/铝蜂窝夹层结构件具有预埋件多、孔位精度要求高、工艺难度大等特点,本文从工艺、工装的角度介绍了其研制过程。
This paper describes the developing process of a Aluminiumhoneycomb sandwich structure with carbon fiber reinforced composite face-sheet bonded with Aluminium-foil from the view of technical process andtechnical devices. This structure had many pre-inlaid joints, required rigo-rous hole position, and was difficult to process.
出处
《宇航材料工艺》
CAS
CSCD
北大核心
1993年第4期66-68,共3页
Aerospace Materials & Technology