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1)  cryogenic liquid rocket engine
低温液体火箭发动机
1.
One set of one-dimensional unsteady homogenous mathematic models for flow and heat process of natural circulation precooling loop of cryogenic liquid rocket engine was established,whilst both inverted annular model and dispersed model were introduced for the prediction of filming boiling region.
针对低温液体火箭发动机预冷自然循环回路的流动与传热过程,建立了一维非稳态均相流数学模型,采用反环状流和弥散流两种流型描述膜态沸腾流型及传热特性。
2)  cryogenic rocket engine
低温火箭发动机
3)  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
4)  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
5)  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。
6)  Cryogenic propellant rocket engine
低温推进剂火箭发动机
补充资料:低温


低温
hypothermia

  低温状态下脑组织对缺氧的耐受性明显增加。体温低于37℃时,每减低1℃,脑组织代谢率减少6.7%,颅内压减低5.5%,在人工呼吸、心脏按压的同时或稍后应给予降温处理,可采用正规冬眠疗法使体温降至肛温35℃左右,目前尤为重视头部局部降温,戴冰帽,头温降至32℃左右,重症要降温3~5天。
  
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