1) aerify component
充气构件
1.
Put forward software airplane navigation mould design basic way of thinking, for aerify component form principle, material option and gasbag body design with analyse and test by force calculation and software airplane wing model design, have verified action preliminarily "gasing component" reasonability and feasibility.
提出软体飞机航模设计的基本思路,对充气构件的形成原理、材料选择、气囊形体设计和受力计算、软体飞机机翼模型设计进行分析和实验,初步验证了作为“充气构件”的合理性与可行性。
3) inflatable structure
充气结构
1.
The results indicated that inner pressure can recuperate the geometric imperfection of material,enhance the buckling load of tube obviously,and provide the application basis for the inflatable structure in space.
该结论为充气结构在空间的应用提供依据。
4) inflatable module
可充气组件
5) air-supported membrane structures
充气膜结构
1.
The air-supported membrane structures were compared with the tension one in this paper.
以测地线为裁剪线进行裁剪设计,得到充气膜结构的施工下料尺寸。
6) air-supported membrane structure
充气膜结构
1.
Considering advantages of large geometric deformation and small distortion of air-supported membrane structure,constrain conditions and mechanics characteristics to the different air-supported membrane structures are analyzed based on the construction mechanics and modeling technology.
考虑充气膜结构的几何大变形和小应变的特点,以建筑力学和造型技术为基础,对不同造型充气结构的约束条件、力学性能等方面进行分析,总结不同造型充气结构的优缺点并对其进行造型分类,突出其不同功用。
补充资料：Al-Li合金构件——歼7-II飞机舱口盖及副翼扰流片
Al-Li合金构件——歼7-II飞机舱口盖及副翼扰流片
Al—Ll合金构件——歼7一I 1机舱口盖及副翼扰流片 张自供稿
说明：补充资料仅用于学习参考，请勿用于其它任何用途。
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