摘要
用内旋压、无模摩擦收颈旋压方法,试制出整体旋压油箱壳体,减轻质量30%,减少焊缝70%。叙述了旋压工艺和旋压过程中出现的问题及解决办法。
By integral spinning, a tank shell was produced which showed deductions in weight and weld seam by30% and 70% respectively. The spinning process and its limitations are discussed in this paper.
出处
《宇航材料工艺》
CAS
CSCD
北大核心
1998年第4期57-59,共3页
Aerospace Materials & Technology