1) expanding mechanism of missile wing
弹翼展开机构
2) launching installment of missile wing
弹翼展开装置
1.
,simulate and acquire aerodynamic coefficients while launching installment of missile wing in ground,finally opti- mize actuator coefficients and ensure launching missile wing.
介绍了弹翼展开装置的计算模型、载荷条件、研制方案、测试电路、试验结果等,在地面模拟确定弹翼展开过程中所需的气动力参数,从而优化了作动筒参数,保证了弹翼的顺利展开。
3) deployment mechanism
展开机构
1.
Techniques of dampers for spacecraft deployment mechanism;
航天器展开机构阻尼器技术概述
2.
Reliability analysis of the deployment mechanism of a large satellite antenna based on the non-probabilistic model;
基于非概率模型的星载天线展开机构可靠性分析
3.
For the shortage of the system reliability data in the initial stages of the design of spaceborne antenna deployment mechanism,a unascertained method for the system reliability allocation is proposed.
针对星载天线展开机构系统设计初期可靠性数据缺乏的情况,提出了系统可靠性分配的未确知方法。
4) unfolding mechanism
展开机构
1.
A surface inspection system composed of optical microscope,digital imaging system and unfolding mechanism has been developed to provide image data for detecting natural defects on the surface of polished Si_3N_4 balls.
为保证表面不漏检,应用螺旋面展开法设计球面展开机构,推导球面展开运动方程,计算转速控制曲线,分析了控制参数对检测系统精度和检测效率的影响,为陶瓷球表面缺陷自动分类和识别提供了可靠方法。
2.
The operation principle of meridian unfolding mechanism of Aviko K type bearing ball out surface inspection machine is introduced in this paper.
对ＡｖｉｋｏＫ型钢球外观检验机中独特的钢球子午线展开机构进行理论分析，将单驱动轮展开机构与双驱动轮展开机构进行了比较。
5) Deployable mechanism
展开机构
1.
Research on the system of a large space deployable mechanism;
一种大型空间展开机构的系统研究
2.
Precision analysis model is set up by analyzing deployable mechanism of folding wing of a missile.
通过分析导弹折叠弹翼展开机构 ,建立了精度分析模型 。
6) mechanism deploying
机构展开
补充资料：半硬壳式弹体(见弹道导弹弹体)
半硬壳式弹体(见弹道导弹弹体)
semi-hard-shelled missile body
bQn yingkeshi dan桩半硬壳式弹体(semi一hard一shelled、ssilebody)见弹道导弹弹体。
说明：补充资料仅用于学习参考，请勿用于其它任何用途。
参考词条