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- aeroengine nacelle 航空发动机消声短舱
- Would you like to prepare the nacelle? 你能去准备机舱吗?
- This method was applied to design the aeroengine control system. 将该方法应用于航空发动机控制+系统设计中。
- Different nacelle with deeper ross-section and intake over propeller shaft. 发动机舱、螺旋桨轴处的进气口有一些不同。
- Dense smoke coming out of No4 engine cowling( engine nacelle), fire suspected. 第四号发动机整流罩冒浓烟,可能着火。
- The sensor shall be located at nacelle height, eccentric to the tower axis. 传感器必须处于机舱高度,并偏离塔架轴线。
- We want to lift the top section and the nacelle of no.X is there any problems? 我们想要吊X号的上段和机舱有什么问题吗?
- This research can accumulate experiences and properties data for manufacturing aeroengine components with EBW. 研究旨在为航空发动机构件的电子束焊接加工制造积累经验和性能数据。
- A dynamic strain gage is developed for dynamic stress test at900℃ of turbine rotor blades of an aeroengine. 为了对某型航空发动机涡轮转子叶片在900℃温下进行动应力测试,研制了900℃态应变计。
- Comfortable at dish box container, nacelle, tracery wall, window box and balcony help advance somebody's career. 适于盘盒容器,吊篮,花墙,窗盒和阳台栽培。
- DC torque motor under the reaction flywheel control mode was used in nacelle azimuth control in this paper. 摘要实现了用直流力矩电机在反作用飞轮控制方式下对气球吊篮的方位控制。
- Abstract: The foundation and simulation of aeroengine starter for flight simulator is discussed in this paper. 文摘:在飞行模拟训练器的研制中,发动机的起动过程是需要重点研究和模拟的过程之一。
- If the nacelle movement is not transmitted to the tower, a suitable relative movement may be sensed as a substitute. 如果机舱的运动没有传递到塔架,作为替代,则必须测量适当的相对运动。
- The wall thickness of the hollow aeroengine turbine blade is a critical parameter for ensuring its strength. 航空发动机空心涡轮叶片的壁厚是保证叶片强度的一个关键参数。
- An O-ring located in nacelle flange is applied between the grease channels in nacelle and bearing. 在机舱润滑油脂通道和轴承之间有O形圈,O形圈位于机舱法兰上。
- The establishment and existing problems of metallurgy model standard for an aeroengine are introduced. 介绍了某型航空发动机冶金型号标准的编制情况及其尚存在的问题。
- The system mainly includes subsystems of tower base control and nacelle control. 主控系统包括塔基控制和机舱控制子系统。
- The applications of nonlinear backstepping control strategy's design method in aeroengine control were analyzed. 摘要主要研究了非线性反演控制规律设计方法在航空发动机控制中的应用。
- A full digital control system with PC/104 in nacelle decoupling mechanism is introduced. 介绍用PC/104实现高空气球吊篮反捻机构的全数字控制系统。
- A diagnostic expert system for oil system of aeroengine--DIAG has been developed. 本文介绍了一个用于航空发动机润滑系统故障诊断的专家系统 --DIAG系统。