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- Application of Aircraft Structural Part Conceptual Design Based on Topology Optimization Method 拓扑优化方法在飞机结构件概念设计中的应用
- aircraft structural part 飞机结构件
- FA-CAPP: A Knowledge-based CAPP system for Aircraft Structural Parts in CIMS Envionment CIMS环境下一种飞机结构件知识基CAPP系统FA－CAPP
- FA-CAD/CAPP/CAM SYSTEM FOR THE COMPLICATED AIRCRAFT STRUCTURE PARTS 复杂飞机结构零件FA-CAD/CAPP/CAM系统
- A machine or structural part that supports another part. 支持物机器或建筑起支撑作用的结构部分
- Study on Feature Definition of Aircraft Structure Parts in CIMS Environment CIMS环境下飞机结构件的特征定义研究
- The structural part of cloth. 纹理布匹的构造部分
- Composite material repair for various structural parts of aircraft, such as Radome, flight control surface, etc. 雷达罩、操作舵面等飞机部件日常复合材料修理工作。
- A device, such as a wedge or pin, inserted to lock together mechanical or structural parts. 楔、栓象楔、栓一样的一种装置，插入以使机械或结构部件锁在一起
- Introduce the application of the check of structure part and mould. 简要介绍了结构件及模具检测实际使用情况。
- However, when the outside wall is a structural part of the building, the wall must be made before the roof. 然而，如果外墙是建筑物的结构部分，那么就必须先筑墙，才能再建屋顶。
- It is very effective to use the scanning electron beam (EB) heating to braze the stainless steel structural part with capillary-to-plate joints. 用电子束扫描加热的方法对具有毛细管板接头的不锈钢结构件进行钎焊是非常有效的。
- Linking Riveting Process Parameters to the Fatigue Performance of Riveted Aircraft Structure. 铆接过程参数与铆接飞机结构的疲劳性能的联系。
- This part of the language is referred to as a data manipulation language (DML). Creating tables falls under DDL, the structural part. 这一部分的语言被称之为DML。创建数据表被归在DDL类，即结构部分。
- I-DEAS.Through this detailed stress analysis, we may justify the designand repair of aircraft structures. 及经由不同修补方法修补的应力分布 .;以作为读者的参考
- Through simulation and analysis,design optimization to a strength structural part made of mica microcrystal glass ceramics had been studied. 以云母微晶玻璃陶瓷为研究对象,通过模拟和分析,设计了一种金属热防护系统承力结构件,对可加工陶瓷的结构件进行了优化设计;
- A formula in terms of DFR value to describe the relationship between the fatigue properties of aircraft structure and the corrosion time was presented. 提出了一种用DFR值描述飞机结构的疲劳性能随腐蚀时间变化的关系式。
- Her seat is in the fore part of the aircraft. 她的座位在飞机前部。
- Structural parts requiring high strength; machine parts,truck chassis parts. 用于需要高温强度的结构部分，接写零件及货车底盘。
- The results indicated that the anticorrosive properties of the heavy-duty coating SEBF/SLF are much better than the ordinary coating on the active service aircraft structures. 结果表明，与现役飞机典型涂层相比，SEBF/SLF重腐蚀防护涂层的抗环境腐蚀性有明显改进。
