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液氧煤油发动机稳态故障仿真分析

党锋刚 马红宇 李春红 宋春

火箭推进2012,Vol.38Issue(2):27-31,5.
火箭推进2012,Vol.38Issue(2):27-31,5.

液氧煤油发动机稳态故障仿真分析

Steady-state fault simulation and effect analysis of LOX/kerosene rocket engine

党锋刚 1马红宇 1李春红 1宋春1

作者信息

  • 1. 西安航天动力研究所,陕西西安710100
  • 折叠

摘要

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.

关键词

补燃循环/稳态故障/仿真计算/特征提取

Key words

staged combustion cycle/steady-state fault/simulation calculation/characteristic extraction

分类

航空航天

引用本文复制引用

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,2012,38(2):27-31,5.

基金项目

国家高技术项目 ()

火箭推进

OACSTPCD

1672-9374

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