1) liquid oxygen/kerosene space propulsion system

液氧/煤油空间推进系统
1.
This paper studies the dynamic characteristics in the startup processes of liquid oxygen/kerosene space propulsion system.
以液氧/煤油空间推进系统为研究对象,对该系统的动态特性进行了分析和研究,建立了整个推进系统的动态过程的数学模型,并采用Matlab软件中的simulink工具仿真了液氧/煤油发动机动态过程中各参数的变化情况,并对仿真结果进行了具体的分析。
2) space propulsion system

空间推进系统
1.
This paper established dynamic mathematical models of simulation modules of the space propulsion system in the whole operation process,which include liquid pipeline module,triple link module,filling-in pipeline module,thrust chamber module and so on.
建立空间推进系统仿真模块(包括液体管道模块、三通模块、充填模块、推力室模块等)的数学模型。
2.
This paper introduces basic theory of the bond graph,and by using the theory,fault diagnosis for space propulsion system is studied.
介绍了键合图基本理论,并利用其理论对空间推进系统进行了故障诊断研究。
3.
An approach of cloud neural network was proposed and used for fault detection and diagnosis of the space propulsion system.
本文提出并研究了用于空间推进系统故障检测与诊断的云神经网络方法,并以某空间推进系统推力器为研究对象进行了验证。
3) liquid propulsion system

液体推进系统
1.
The burning rate of energetic liquid is one of the key parameters to affect the combustion property of liquid propulsion system.
结果表明,它满足指数燃速定律,并从试验数据拟合出燃速系数和燃速指数,其结果可为液体推进系统内弹道设计提供基础数据。
4) thrust hydraulic system

推进液压系统
1.
Pressure and flow compound control analysis of thrust hydraulic system for shield tunnelling machine;
盾构掘进机推进液压系统压力流量复合控制分析
2.
Simulation of pressure flow hybrid control of thrust hydraulic system of shield tunneling machines;
盾构机推进液压系统比例压力流量复合控制仿真
3.
The principle of the thrust hydraulic system was expounded,and simulation was carried out with the AMESim tool.
阐述了盾构机推进液压系统的原理,利用AMESim仿真工具对该系统进行了仿真分析。
5) hydraulic propulsion system

液压推进系统
1.
The function, pump package control,partition design and hydraulic control mode for single partition of hydraulic propulsion system are introduced in terms ofΦ14.
87 m超大直径泥水气平衡盾构,介绍了其液压推进系统的功能、泵组控制、分区设计、单个分区的液压控制方式。
6) space propulsion

空间推进
1.
The fault diagnostic expert system for space propulsion system was established.

采用人工智能的方法,对空间推进系统进行了有效的分区,并利用文中介绍的组合红线算法进行故障判定,建立了空间推进系统故障诊断的专家系统。
补充资料:固液混合火箭推进剂(见火箭推进剂)
固液混合火箭推进剂(见火箭推进剂)
solid-liguid hybrid rocket propellant
guye hunhe huoiian tui)in)i固液混合火箭推进剂(s olid一Iiguid hy-brid rocket proPellant)见火箭推讲齐,}_
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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