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C/ E 复合材料网格缠绕结构一体化设计
引用本文:提亚峰,张铎,董波.C/ E 复合材料网格缠绕结构一体化设计[J].宇航材料工艺,2010,40(6).
作者姓名:提亚峰  张铎  董波
作者单位:西北工业大学航天学院,西安
摘    要:根据多年的设计生产实践,总结了复合材料网格缠绕结构的优缺点。在发挥其优点的基础上,针对复合材料网格缠绕结构的缺点,提出了一体化设计设想,给出了一体化研制流程,并对流程中的各个环节进行了探讨。分析表明,对复合材料网格缠绕结构进行一体化设计可缩短研制周期,降低研制成本,从而可以使复合材料网格缠绕结构得到进一步推广使用。

关 键 词:C/E复合材料  网格缠绕结构  一体化设计

Integration Design for C/ E Composites Trellis Wound Structure
Ti Yafeng,Zhang Duo,Dong Bo.Integration Design for C/ E Composites Trellis Wound Structure[J].Aerospace Materials & Technology,2010,40(6).
Authors:Ti Yafeng  Zhang Duo  Dong Bo
Institution:College of Astronautics,Northwestern Polytechnical University
Abstract:This paper summarizes the advantages and the disadvantages of the carbon/ epoxy composites trellis
wound structure based on multiple experiences of design and production of the structure. In order to exert the advantage and overcome the disadvantage of the structure,the views and the flows of integration design are given. The details
of the flows are discussed. The analysis indicates that it can reduce the development cycle and the development cost so
that the carbon/ epoxy composites trellis wound structure can be widely applied in project.
Keywords:Carbon/ epoxy composite  Trellis wound structure  Integration design
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