| 复合材料机体结构选用树脂体系的探讨 |
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| 引用本文： | 黄承恭,吴启荣.复合材料机体结构选用树脂体系的探讨[J].直升机技术,2000(2):16-20. |
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| 作者姓名： | 黄承恭 吴启荣 |
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| 作者单位： | 中国直升机设计研究所,景德镇 |
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| 摘 要： | 由于复合材料的优点如此之多，复合材料的应用日益广泛，但在具体设计时应选用何种固化温度的树脂体系人们有不同的见解，本文将结合工程设计体会作些探讨。
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| 关 键 词： | 直升机 树脂体系 复合材料 主体结构 高温固化 |
SOME DISCUSSION OF THE COMPOSITE FUSELAGE FRAME IN CHOICING RESIN CURING TEMPERATURE |
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| Authors: | Huang Chenggong Wu Qirong |
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| Institution: | Chinese Helicopter Research and Development Institute..Jingdezhen. 333001 |
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| Abstract: | Because composites has so many advantages that it has achieved a wide number of applications . there are still many different opinion in choicing resin curing temperature. This paper presents some discussions with some actual design pratices. |
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| Keywords: | composite moistured temperlure affect primary structure high temperature curing |
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