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飞机设备吊舱环境控制系统的优化设计
引用本文:余建祖,余雷.飞机设备吊舱环境控制系统的优化设计[J].北京航空航天大学学报,2002,28(1):25-29.
作者姓名:余建祖  余雷
作者单位:北京航空航天大学 飞行器设计与应用力学系
基金项目:航空科研项目;97E51045;
摘    要:介绍了国外机载设备吊舱环境控制系统技术发展的状况,提出了一种新的回冷逆升压式冲压空气循环制冷的吊舱环控系统方案.建立了4种典型吊舱环控系统优化设计的数学模型,并对其优化方法进行了探讨.对系统优化结果的分析表明,优化设计的回冷逆升压式空气循环制冷系统具有最小的载机燃油代偿损失,其性能和效率的综合设计指标达到世界先进水平.

关 键 词:环境控制  系统  设计  优化技术  飞机设备吊舱
文章编号:1001-5965(2002)01-0025-05
收稿时间:2000-05-10
修稿时间:2000年5月10日

Optimized Design of Environmental Control System for Aircraft Avionics Pods
YU Jian-zu,YU Lei.Optimized Design of Environmental Control System for Aircraft Avionics Pods[J].Journal of Beijing University of Aeronautics and Astronautics,2002,28(1):25-29.
Authors:YU Jian-zu  YU Lei
Institution:Beijing University of Aeronautics and Astronautics, Dept. of Flight Vehicle Design and Applied Mechanics
Abstract:The status of development of the technology of environmental control system(ECS) for avionics pods was introduced, a new type re cool reverse boot strap ram air circle cooling scheme of ECS for pods was brought forward. The optimum design mathematical models of typical ECS for pods were created, and the optimum method was discussed. Four types of ECS presently used in military aircraft pods were considered. The sine method combined with simplex method was applied to seek optimal technologic scheme and parameters for these systems. Finally the contrasts and analysis of the results of the system scheme and parameter optimization were made. The results showed that the new pod ECS had less fuel penalty and higher Coefficient of Performance(COP).
Keywords:environmental control  systems  design  optimization technique  aircraft avionics pod
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