机械科学与技术2012，Vol.31Issue(1)：150-158,162,10.
飞机整体壁板时效成形工艺方案研究
Study on the Processing Scheme in Ageing Forming of Integral Panel
甘忠 1邓超 1张旭生 1袁胜2
作者信息
- 1. 西北工业大学现代设计与集成制造技术教育部重点实验室,西安710072
- 2. 成都飞机工业集团有限责任公司,成都610000
- 折叠
摘要
Abstract
The large integral panel is the main structure part of modern advanced civil airplane.The large integral panel forming is an important key technology which must be solved in the airplane developing processes.The ageing forming is an effective method for forming large skin and wall pieces.The principle and characteristics of the ageing forming are analyzed.The processing scheme of the ageing forming for the high-rib complex shaped of panel is discussed and analyzed.Finally,based on the existing research situation and the requirements for developing the large airplane in China,the experimental suggestion and research emphasis on developing ageing forming are pointed out.关键词
时效成形/工艺方案/大型整体壁板Key words
ageing forming/processing scheme/large integral panel分类
矿业与冶金引用本文复制引用
甘忠,邓超,张旭生,袁胜..飞机整体壁板时效成形工艺方案研究[J].机械科学与技术,2012,31(1):150-158,162,10.
