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1)  wing pole
连翼杆
1.
In developing course the rocket engine of certain flight-assisted equipment’s empennage wing pole whorl root part splits leads to the shell body fly not steadily occurs many times.
分析了某型助飞发动机的喷管与尾翼连翼杆组件的温度与应力场,找到了多次发生火箭发动机尾翼连翼杆螺纹根部处断裂的问题所在,给出了解决方案。
2)  flap lever
副翼拱杆
3)  joined wing
连翼布局
1.
On the basis of collecting,trimming,and analyzing the overseas research information about joined wing aircraft,this paper presents the research history and design characteristics of joined wing aircraft.
在收集、整理、分析国外连翼布局飞机研究资料的基础上,介绍了国外连翼布局飞机的研究历程和设计特点;特别是基于近年来对未来战场信息情报、监视、侦察任务的需求,介绍了连翼布局探测无人机这一新的作战概念和装备技术的研究进展情况。
2.
In the design of joined wing, the complex and the interaction between each specialities and subjects are unknown from previous design experience.
连翼布局飞机设计中,各专业学科之间的相互影响和复杂性是以前的设计中所未知的。
4)  joined-wing
连接翼
1.
The aerodynamics investigation of the joined-wing configuration;
连接翼布局气动特性研究
5)  wing-body revolved mechanism
翼身连动
1.
The design of wing-body revolved mechanism,as a key technique,must be hard enough to suffer the lift and moment during varying wing,moreover,the fuselage can not be overweight.
针对变前掠翼无人机设计了一种翼身连动机构,使无人机能够根据任务需求,在直机翼、前掠翼、三角翼之间进行气动布局转换,从而在整个任务飞行过程都能达到性能最佳。
6)  Connecting rod
连杆
1.
Vibratory mechanism connecting rod fuzzy reliability analysis of QTJ type block molding machine;
卷绕机四杆机构连杆模糊可靠性分析与改造
2.
Design and calculation of wedge rolling die for aluminum alloy connecting rod pretreated blank;
铝合金连杆预制件楔形横轧模具的设计计算
3.
Influence of starting notch geometry parameters of connecting rod on its fracture splitting force;
连杆预制裂纹槽几何参数对胀裂力的影响
补充资料:连动杆
1.指连杆。
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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