1) reusable liquid propellant rocket engine
可重复使用液体火箭发动机
1.
This paper studies the problem of tradeoff optimization between damage of reusable liquid propellant rocket engine\'s turbine blade and control input sequences during the start-up process.
针对可重复使用液体火箭发动机起动过程,研究了系统控制输入序列的变化对以涡轮叶片为代表的关键部件累积损伤的影响。
2) liquid rocket engine
液体火箭发动机
1.
SVM implemented in fault diagnosis of liquid rocket engine;
支持向量机用于液体火箭发动机的故障诊断
2.
Improvement on simulation software for static characteristics of liquid rocket engine;
液体火箭发动机稳态特性仿真软件的改进
3.
Evaluation of human reliability in liquid rocket engine testing;
液体火箭发动机试验过程中人的可靠性评价研究
3) liquid propellant rocket engine
液体火箭发动机
1.
Steady state fault detection and diagnosis of liquid propellant rocket engines based on decision tree method;
基于决策树方法的液体火箭发动机稳态段故障诊断
2.
The stability analysis technique based on nonlinear theory for liquid propellant rocket engine;
液体火箭发动机基于非线性理论的稳定性分析方法
3.
Stochastic simulation method of performance reliability estimation on liquid propellant rocket engine;
液体火箭发动机性能可靠性的随机仿真方法
4) Liquid-propellant rocket engine
液体火箭发动机
1.
Research ofdamage mitigating and life extending method for liquid-propellant rocket engines based on main object;
液体火箭发动机基于主要目标的减损与延寿控制方法
2.
Based on the back propagation and radial basis function neural network,and using the tool of Matlab and Lab Windows/CVI,the real-time fault detection algorithms for the start-up and main-stage process of a certain liquid-propellant rocket engine in ground tests are developed in this paper.
以某大型液体火箭发动机为研究对象,针对其启动和稳态工作过程,利用Matlab和Lab Windows/CVI等编程工具,基于神经网络技术,开发实现了其地面试车过程实时故障检测的BP(Back Propagation)和RBF(Radial Basis Function)算法。
3.
The ATA algorithm was improved for the platform for liquid-propellant rocket engines and the applicability of the algorithm was improved.
以平台液体火箭发动机为研究对象,改进和完善了用于发动机实时故障检测的自适应阈值门限算法(ATA算法),提高了算法检测的适用性。
5) cup
[英][kʌp] [美][kʌp]
(液体火箭发动机)前室[火]
6) liquid motor,liquid propulsor,liquid propellant rocket,liquid-rocket unit
液体火箭发动机<火>
补充资料：液体火箭发动机
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