1) aircraft component
飞机构件
1.
Aircrafts will be dangerous if burned aircraft components can not be detected accurately.
电导率法是检测烧伤飞机构件的重要手段。
2) aircraft structure
飞机构件
1.
In view of the practical test demand for some burned battle aircraft,the burned aircraft structure has been tested with hardness testing.
结果发现,硬度测试不能完全代替强度测试;单独使用硬度测试法对火烧飞机构件进行检测存在很大的隐患。
2.
In order to make clear the accuracy and reliability of testing result when replacing strength testing with hardness testing in burned aircraft structure examination, burn simulation experiments are carried out by taking aluminum alloys LY12cz and LC4cs as test materials.
试验结果表明,热处理强化后的铝合金受热损伤之后,硬度值达到规定要求时,强度值不一定能满足使用要求;硬度测试不能完全代替强度测试;单独使用硬度测试法对火烧飞机构件进行检测存在很大的隐患。
3) aircraft structural part
飞机结构件
1.
In order to decrease the weight of aircraft structural part effectively,face to the skeleton of aircraft,the author regards the conceptual design of structural part(such as strengthen frame,general frame and canard beam) as research content.
由此可以得出3点结论:(1)采用CAD/CAE和拓扑优化相结合用于飞机结构件的初始方案设计是可行的;(2)作者提出的"改进的敏度阈值"拓扑优化算法是有效的;(3)构建一种具有良好操作性的、有别于经验设计的飞机结构件概念设计新方法。
4) aircraft primary structure application
飞机主受力构件
5) typical components of plane
飞机典型构件
6) aircraft structure part
飞机结构零件
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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