Title of article
Abnormal Shape Mould Winding
Author/Authors
Hongya، نويسنده , , Fu and Xianfeng، نويسنده , , Wang and Zhenyu، نويسنده , , Han and Yunzhong، نويسنده , , Fu، نويسنده ,
Issue Information
روزنامه با شماره پیاپی سال 2007
Pages
7
From page
552
To page
558
Abstract
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.
Keywords
Filament Winding , Fiber technology , Vane , composite material , airplane inlet
Journal title
Chinese Journal of Aeronautics
Serial Year
2007
Journal title
Chinese Journal of Aeronautics
Record number
2264687
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