| 无纵向温度变形的复合材料管的铺层设计 |
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| 引用本文： | 陈烈民.无纵向温度变形的复合材料管的铺层设计[J].宇航材料工艺,1999,29(5):20-22,29. |
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| 作者姓名： | 陈烈民 |
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| 作者单位： | 北京空间飞行器总体设计部,北京,100086 |
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| 摘 要： | 提出了无纵向温度变形的复合材料管子铺层设计的一种方法。通过对三类碳纤维／环氧复合材料的管子的实例计算表明：高模碳纤维，而不是极高模量碳纤维，更适合于航天结构的应用。
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| 关 键 词： | 温度变形 复合材料 铺层设计 管结构 航天 |
Lay-up Design for Composite Material Tube Having no Longitudinal Thermal Deformation |
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| Chen Liemin.Lay-up Design for Composite Material Tube Having no Longitudinal Thermal Deformation[J].Aerospace Materials & Technology,1999,29(5):20-22,29. |
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| Authors: | Chen Liemin |
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| Institution: | Beijing Institute of Spacecraft System Engineering Beijing 100086 |
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| Abstract: | This paper presents a method for lay up design of composite material tube having no longitudinal thermal deformation. It is shown that the high modulus carbon fiber , not the extra-high modulus carbon fiber, is more suitable for application in spacecraft structures,according to calculating results for three types of carbon fiber /epoxy composite materials. |
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| Keywords: | Thermal deformation Composite material Lay up design |
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