1)  lift mechanism
起竖执行机构
1.
The feasible schemes of lift mechanism applied on flatcar are presented,including a four-bar linkage mechanism with a length-alterable component-ball screw shaft,and the calculating methods of structure parameters and force analysis methods of crank rocker mechanism and rotating guide bar mechanism are discussed emphatically.
给出了车载式回转起竖平台起竖执行机构可供选用的机构方案;重点讨论了包含一个可变长度构件且为滚珠丝杆的四连杆机构——摇块机构和转动导杆机构两方案的结构参数计算方法和受力分析方法;通过对比分析,在满足功能要求的前提下,确定了相对较优的摇块机构方案并付之实践,效果理想。
2)  erecting
起竖
1.
Based on the analysis of defects of current erecting process control method,a hybrid control method which combined bang-bang control and single neuron PID adaptive control was proposed to implement quick erecting.
起竖过程是某大型机电设备工作工程中的一个关键环节。
3)  erection mechanism
起竖机构
1.
The computational models of the gravitational moment for the erection mechanism, the wind load with the parallel direction to the erection plane,and the erection force of the cylinder,in erection process were set up according to the prescribed rotational motion and the rotational differential equation of the erection mechanism.
基于导弹起竖过程中起竖机构的转动运动函数和转动微分方程,分别建立了该过程中由于重力所产生的系统重力矩计算模型,风向与起竖平面平行的风载荷计算模型,以及起竖油缸作用力的计算模型。
4)  erecting equipment
起竖设备
1.
Research on synchronous control of large scale erecting equipment;
大型起竖设备的PID同步控制研究
5)  rapid-erection
快速起竖
1.
A new method for designing ballistic missile launch device rapid-erection system is presented to overcome the disadvantage of erection system,which uses fuzzy controller.
文中针对地地导弹的地面发射装置速度慢、时间长的缺陷,在完成起竖装置的非线性建模基础上,提出一种模糊控制设计方法,实现了发射装置的快速起竖控制。
2.
A new method for designing ballistic missile launch device rapid-erection system is presented to overcome the disadvantage of erection system, which uses linear model following method.
针对某导弹的地面发射装置速度慢、时间长的缺陷,在完成起竖装置的非线性建模,并进行反馈线性化的基础上,采用线性模型跟随方法设计,实现了发射装置的快速起竖控制。
6)  erection angle
起竖角
1.
Because of the differences of erection angle during missile launching time,the jet flow in jet pipe which has the properties of high temperature and high velocity,erodes and ablate the antenna of launch vehicle.
在发射过程中,由于导弹发射时,起竖角不同,喷管处的高温高速燃气对发射车天线的冲刷和烧蚀,不同程度地影响地面通信。
参考词条
补充资料：薄膜执行机构
分子式：
CAS号：

性质：利用气压在膜片上所产生的力，通过输出杆驱动阀内件或其他调节机构的一种机构。

说明：补充资料仅用于学习参考，请勿用于其它任何用途。