| 液氢液氧火箭发动机稳态数值仿真与故障分析 |
| |
| 引用本文： | 刘冰,张育林. 液氢液氧火箭发动机稳态数值仿真与故障分析[J]. 国防科技大学学报, 1997, 19(6): 15-19 |
| |
| 作者姓名： | 刘冰 张育林 |
| |
| 作者单位： | 国防科技大学航天技术系!长沙，410073，国防科技大学航天技术系!长沙，410073 |
| |
| 摘 要： | 根据发动机工作的物理过程建立了大型液氢液氧火箭发动机稳态故障的数学模型，数学模型包含了70个工作参数和45个干扰因素，采用了布罗伊登法求解。确立了各种故障的正确仿真机制，对计算结果进行了分析，并与试车结果相比较，吻合良好。
|
| 关 键 词： | 液氢液氧推进剂 液体火箭发动机 故障仿真 故障分析 |
| 收稿时间： | 1996-11-10 |
LH2/O2 Rocket Engine Steady Number Simulation and Fault Analysis |
| |
| Liu Bing and Zhang Yulin. LH2/O2 Rocket Engine Steady Number Simulation and Fault Analysis[J]. Journal of National University of Defense Technology, 1997, 19(6): 15-19 |
| |
| Authors: | Liu Bing and Zhang Yulin |
| |
| Abstract: | The steady fault mathematical mode of large LH and LO rocket engine is built according to the process of engine. This mathematical mode contains seventy capable parameters and forty five disturbing parameters, in whide the Broyden method is adopted to find the solution. It has established the right way to simulate the fault. Finally we analyse the result of the simulation, at the same time, we compare it with the hot-test. They coincide well. |
| |
| Keywords: | LH_2/O_2 propellant Liquid rocket engine fault simulation fault analysis |
| 本文献已被 CNKI 等数据库收录！ |
| 点击此处可从《国防科技大学学报》浏览原始摘要信息 |
|
点击此处可从《国防科技大学学报》下载免费的PDF全文 |
