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Abnormal Shape Mould Winding
A theory of composite material patch winding is proposed to determine the winding trajectory with a meshed data model. Two different conditions are considered in this study. One is Bridge condition on the concave surface and the other is Slip line condition in the process of patch winding. This paper presents the judgment principles and corresponding solutions by applying differential geometry theory and space geometry theory. To verify the feasibility of the patch winding method, the winding control code is programmed. Furthermore, the winding experiments on an airplane inlet and a vane are performed. From the experiments, it shows that the patch winding theory has the advantages of flexibility, easy design and application.
作 者： Fu Hongya Wang Xianfeng Han Zhenyu Fu Yunzhong 作者單位： School of Mechatronics Engineering, Harbin Institute of Technology, Harbin 150001, China 刊 名： 中國(guó)航空學(xué)報(bào)(英文版) ISTIC 英文刊名： CHINESE JOURNAL OF AERONAUTICS 年，卷(期)： 2007 20(6) 分類(lèi)號(hào)： V2 關(guān)鍵詞： filament winding fiber technology composite material airplane inlet vane【Abnormal Shape Mould Winding】相關(guān)文章：