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The Validation of the Feasibility of Abnormal Form Patch Winding

Journal Materials Science Forum (Volumes 532 - 533)
Volume Advances in Materials Manufacturing Science and Technology II
Edited by Chengyu Jiang, Geng Liu, Dinghua Zhang and Xipeng Xu
Pages 129-132
DOI 10.4028/www.scientific.net/MSF.532-533.129
Citation Xian Feng Wang et al., 2006, Materials Science Forum, 532-533, 129
Online since December, 2006
Authors Xian Feng Wang, Hong Ya Fu, Zhen Yu Han
Keywords Airplane Inlet, Composite Material, Patch Winding
Abstract

The theory of composite material patch winding is proposed to determine the winding trajectory by a meshed data model. The bridge condition on the concave surface is considered in this work. This paper puts forward the judgmental principles and corresponsive solutions by applying differential geometry theory and space geometry theory. To validate the feasibility of the patch winding method, the winding control code is programmed. Furthermore, the airplane inlet winding experiments are carried out.

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