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The Validation of the Feasibility of Abnormal Form Patch Winding

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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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Periodical:

Materials Science Forum (Volumes 532-533)

Pages:

129-132

DOI:

https://doi.org/10.4028/www.scientific.net/MSF.532-533.129

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Online since:

December 2006

Authors:

Xian Feng Wang, Hong Ya Fu, Zhen Yu Han

Keywords:

Airplane Inlet, Composite Material, Patch Winding

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© 2006 Trans Tech Publications Ltd. All Rights Reserved

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References

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