1、
2、

wall temperature response calculation of ablative cooling chamber of lre

液体火箭发动机烧蚀冷却推力室室壁温度响应的计算

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3、

Study of Monitoring Parameter Selection Based on AHP for LRE in Ground Test

基于AHP的液体火箭发动机地面试验监测参数的选取方法研究

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4、

This paper mainly focuses on CAD of LRE design, and present studies on CAD technique of recycled cooling LRE combustion chamber.

本文的主要工作面向液体火箭发动机设计CAD技术,并选择再生冷却式液体火箭发动机推力室设计CAD技术研究作为方向。

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5、

BP ( Back Propagation) neural network used in liquid rocket engine ( LRE) failure simulation and detection was described.

研究了用于液体火箭发动机(LRE)故障仿真与故障检测的神经网络BP(BackPropanation)算法。

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6、

As a conclusion, MATA is suitable for the real time fault detection of LRE turbopump.

因此,MATA适合于液体火箭发动机涡轮泵的实时故障检测。

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7、

Numerical simulation for tank pressurization system of LRE test-bed

液体火箭发动机试验台贮箱增压系统数值仿真

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8、

Based on the damage mitigating control ( DMC), this thesis focuses on the damage analysis and control of the coolant channel ligament which is treated as one of critical components for the liquid-propellant rocket engines ( LRE) during a transiting operating condition.

针对减损控制技术,本文以液体火箭发动机为研究对象,视推力室冷却夹套隔片为易损部件,在发动机的转工况过程中,对其损伤进行分析与控制研究。

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9、

The leak of Liquid Rocket Engine ( LRE ) is very common and dangerous.

液体火箭发动机的泄漏是常见和极其危险的故障.

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10、

The thrust chamber of the LRE works under the condition characterized by pressure and high temperature.

液体火箭发动机推进室里的工质工作在高温高压环境下,可靠的冷却是保证其安全工作的关键技术之一.

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11、

Then, with the help of historical data from LRE test as well as real-time data from rotor test platform, the TP-FDS was validated.

通过转子试验平台实时数据和液体火箭发动机历史试车数据,验证了TP-FDS。

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