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液氧煤油发动机稳态故障仿真分析
引用本文:党锋刚,马红宇,李春红,宋春.液氧煤油发动机稳态故障仿真分析[J].火箭推进,2012(2):27-31.
作者姓名:党锋刚  马红宇  李春红  宋春
作者单位:西安航天动力研究所,陕西西安710100
基金项目:国家高技术项目(2008AA705040)
摘    要:根据液氧煤油补燃循环发动机的特点,建立了稳态工作过程故障仿真数学模型,并针对比较典型的几种故障模式,进行了仿真计算与效应分析,最后进行了故障参数特征的初步提取。结果表明,选定的10个缓变热力参数,可对泄漏、堵塞及涡轮泵等典型故障模式进行有效识别和分离。

关 键 词:补燃循环  稳态故障  仿真计算  特征提取

Steady-state fault simulation and effect analysis of LOX/kerosene rocket engine
DANG Feng-gang,MA Hong-yu,LI Chun-hong,SONG Chun.Steady-state fault simulation and effect analysis of LOX/kerosene rocket engine[J].Journal of Rocket Propulsion,2012(2):27-31.
Authors:DANG Feng-gang  MA Hong-yu  LI Chun-hong  SONG Chun
Institution:(Xi'an Aerospace Propulsion Institute,Xi'an 710100,China)
Abstract:The simulation mathematical model of fault occurring in the steady-state working process is built and simulation software is designed according to the characteristics of LOX/kerosene staged combustion cycled rocket engine.Several typical failure modes are simulatively calculated.The effect of the fault is analyzed and characteristics of the fault modes are extracted.Ten slow variable thermal parameters were selected on the basis of the anaysis result to identify the faut modes of leakage and jamming in the fuel pipe of engine.
Keywords:staged combustion cycle  steady-state fault  simulation calculation  characteristic extraction
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