首页 | 本学科首页   官方微博 | 高级检索  
     检索      

复杂形体面片缠绕成型方法的分析与实现
引用本文:王显峰%富宏亚%韩振宇%王永章.复杂形体面片缠绕成型方法的分析与实现[J].宇航材料工艺,2006,36(6):39-41.
作者姓名:王显峰%富宏亚%韩振宇%王永章
作者单位:哈尔滨工业大学机电学院,哈尔滨,150001
基金项目:国家自然科学基金;哈尔滨工业大学校科研和教改项目
摘    要:通过对复杂形体缠绕成型方法的分析,提出了面片缠绕的思想;同时针对缠绕过程中可能存在的架空问题提出了一套可行的判定准则和解决方案。以面片缠绕理论为基础,针对飞机发动机进气道缠绕成型,编制缠绕控制程序并进行相应的实验,验证了面片缠绕方法的实用性,为航空航天高性能构件的缠绕成型探索了一条新的途径。

关 键 词:纤维缠绕  飞机进气道  缠绕成型
收稿时间:2005-10-08
修稿时间:2005-10-082006-03-30

Analysis and Realization of Patch Winding Method for Complex Form
Wang Xianfeng,Fu Hongya,Han Zhenyu,Wang Yongzhang.Analysis and Realization of Patch Winding Method for Complex Form[J].Aerospace Materials & Technology,2006,36(6):39-41.
Authors:Wang Xianfeng  Fu Hongya  Han Zhenyu  Wang Yongzhang
Institution:College of Mechanical Engineering, Harbin Institute of Technology, Harbin 150001
Abstract:By analyzing the method of complex form winding,the idea of patch winding is proposed. A series of feasible judging principles and schemes is put forword to deal with the bridge condition that maybe present during the patch winding. Based on the patch winding theory, the controlling program of patch winding is programed. The practicability of patch winding method is validated by the experiments carried out on airplane inlet. A new way for the winding of components with high performance is explored for avigation and astronavigation industry.
Keywords:Filament winding  Airplane inlet  Winding
本文献已被 CNKI 维普 万方数据 等数据库收录!
点击此处可从《宇航材料工艺》浏览原始摘要信息
点击此处可从《宇航材料工艺》下载免费的PDF全文
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号