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液体火箭发动机稳态故障仿真及分析
引用本文:吴建军,张育林,陈启智. 液体火箭发动机稳态故障仿真及分析[J]. 推进技术, 1994, 15(3): 6-13
作者姓名:吴建军  张育林  陈启智
作者单位:国防科技大学航天技术系
摘    要:建立了液体火箭发动机稳态故障数学模型,编制了实用计算程序。调整方程组中的有关系数的参数,该模型既可用于在正常工况下评定性能参数随干扰因素的随机变化,进行发动机静态特性仿真。又可用于在故障状态下发动机性能参数衰减退化的计算,进行发动机稳态故障效应的仿真。

关 键 词:液体推进剂 火箭发动机 发动机

STEADY FAULT SIMULATION AND ANALYSIS OF LIQUID ROCKET ENGINE
Wu Jianjun,Zhang Yulin and Chen Qizhi. STEADY FAULT SIMULATION AND ANALYSIS OF LIQUID ROCKET ENGINE[J]. Journal of Propulsion Technology, 1994, 15(3): 6-13
Authors:Wu Jianjun  Zhang Yulin  Chen Qizhi
Affiliation:Department of Aerospace Technology, National University of Defense Technology, Changsha, 410073;Department of Aerospace Technology, National University of Defense Technology, Changsha, 410073;Department of Aerospace Technology, National University of Defense Technology, Changsha, 410073
Abstract:This paper presents a steady fault analysis model of a liquid rocket engine, which involves various disturbing factors and fault statuses affecting main performances of liquid rocket engine. By adjusting some coefficients or parameters in the model equation, the model can be used for engine steady fault simulation under a normal engine condition. The paper presents main simulation calculation method and results of fault simulation.
Keywords:Liquid propellant rocket engine  Engine failure  Steady  Failure mode  Fault simulation  Fault analysis
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