民用飞机发动机灭火系统性能计算分析
作者:
作者单位:

上海飞机设计研究院,上海 201210

作者简介:

李一德男,硕士,工程师。主要研究方向:民用飞机防火系统设计。E-mail:liyide@comac.cc

通讯作者:

李一德E-mail:liyide@comac.cc

中图分类号:

V233.7+47

基金项目:


Performance calculation and analysis of civil aircraft engine fire extinguishing system
Author:
Affiliation:

Shanghai Aircraft Design and Research Institute, Shanghai 201210 , China

Fund Project:

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    摘要:

    选取填充Halon1301灭火剂的某飞机右发动机灭火系统为仿真模型准确性验证对象,采用Amesim软件开展仿真建模与计算,通过计算结果与试验数据的对比确定仿真模型的准确性。选取填充HFC-125灭火剂的某型发动机灭火系统为仿真对象进行建模与计算,分析氮气在灭火瓶中的充装压力、灭火管内径等参数灭火喷嘴流量、灭火剂浓度的影响。结果表明:发动机灭火喷嘴的流量与发动机核心舱内的灭火剂浓度随着灭火瓶氮气填充压力的升高而升高,但升高幅度较小;在一定范围内选取内径较大的灭火导管可以显著提高发动机灭火喷嘴流量,同时,灭火剂喷射时间显著降低,但超出一定范围时,选取更大内径的灭火导管,灭火喷嘴流量提高幅度较小,灭火剂喷射时间降低的幅度也较小。

    Abstract:

    Using Amesim software and based on the multiphase flow theory formula, a certain type of engine fire suppression system using Halon1301 fire extinguishing agent was modeled, and the accuracy of the model was verified by comparing it with its experimental data. Model and calculate the fire extinguishing system of a certain type of engine using HFC-125 fire extinguishing agent, and analyze the influence of parameters such as fire extinguishing agent filling pressure and fire extinguishing pipeline diameter on the spray flow rate and concentration of fire extinguishing agent. The results show that the flow rate of the engine fire extinguishing nozzle and the concentration of fire extinguishing agent in the engine core compartment increase with the increase of nitrogen filling pressure in the fire extinguishing bottle, but the increase is relatively small; selecting a fire extinguishing duct with a larger inner diameter within a certain range can significantly increase the flow rate of the engine fire extinguishing nozzle. At the same time, the spraying time of the fire extinguishing agent is significantly reduced. However, when the range is exceeded, selecting a larger inner diameter fire extinguishing duct will result in a smaller increase in the flow rate of the fire extinguishing nozzle and a smaller decrease in the spraying time of the fire extinguishing agent.

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引用本文

李一德.民用飞机发动机灭火系统性能计算分析[J].民用飞机设计与研究,2024(4):57-63. ( in Chinese)

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  • 在线发布日期: 2025-01-10
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