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Aircraft environmental control systems modeling for configuration selection

机译:飞机环境控制系统建模,用于配置选择

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摘要

According to the statistics about civil transportation aircraft EnvironmentalControl system (ECS), the three-wheel high pressure water separation system(HPWS) and low pressure water separation system (LPWS) are the mostcommon choices for the 150-seat airliners. Although the former has become themainstream configuration for air conditioning pack, the latter is still used onBoeing 737-600/700. In order to compare the two configurations and choose thebetter one for a specific aircraft, simulation and analysis are done.The cabin heat load is calculated at first in order to calculate required enginebleed air mass flow. Then a specific aircraft is defined so that required structuraldimensions and cabin comfort indexes can be obtained based on Airbus 320.Thirdly, the component models are built by Matlab/Simulink according to thefundamental knowledge of heat transfer and aerodynamics, the workingprinciples and mechanical dimensions of the components, the ambientenvironmental parameters and some data from Airbus 320. Consequently, thecomplete system model can be assembled. After confirming the validity of themodel by checking the required ram air mass flow and temperature deviation ofthe state points referred to Airbus 320, the simulation model is used to doanalyze the specific aircraft. Finally, through comparing the different values ofram air mass flow and turbine expansion ratio, as well as the system mass,economic cost and reliability, the better configuration is selected.It can be summarized that the three-wheel LPWS requires less ram air massflow (0.012kg/s) and a little lower expansion ratio (0.02) than the HPWS, and italso has lower weight (63% of HPWS), lower (83% of HPWS) cost and higherreliability (140% of HPWS), thus it is the suitable configuration for the specificaircraft.
机译:根据民用飞机环境控制系统(ECS)的统计数据,三轮高压水分离系统(HPWS)和低压水分离系统(LPWS)是150座客机的最常见选择。尽管前者已成为空调系统的主流配置,但后者仍在波音737-600 / 700上使用。为了比较这两种配置并针对特定飞机选择更好的配置,进行了仿真和分析。首先计算机舱热负荷,以计算所需的发动机引气质量流量。然后定义一架特定的飞机,以便可以根据空中客车320获得所需的结构尺寸和机舱舒适性指标。第三,由Matlab / Simulink根据传热和空气动力学的基本知识,飞机的工作原理和机械尺寸来建立组件模型。组件,周围环境参数和来自空客320的一些数据。因此,可以组装完整的系统模型。在通过检查所需的冲压空气质量流量和参考空客320的状态点的温度偏差确认了模型的有效性之后,使用仿真模型对特定飞机进行重新分析。最后,通过比较冲压空气质量流量和涡轮膨胀比的不同值,以及系统质量,经济成本和可靠性,选择了更好的配置。可以得出结论,三轮LPWS需要较少的冲压空气质量流量( 0.012kg / s)和比HPWS稍低的膨胀率(0.02),而且重量更轻(HPWS的63%),成本更低(HPWS的83%)和可靠性更高(HPWS的140%),因此适用于特定飞机的配置。

著录项

  • 作者

    Peng Xiong;

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  • 年度 2013
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  • 原文格式 PDF
  • 正文语种 {"code":"en","name":"English","id":9}
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