飞机设备吊舱环境控制系统的优化设计  

Optimized Design of Environmental Control System for Aircraft Avionics Pods

作　　者：余建祖[1] 余雷[1] 

机构地区：[1]北京航空航天大学飞行器设计与应用力学系

出　　处：《北京航空航天大学学报》2002年第1期25-29,共5页Journal of Beijing University of Aeronautics and Astronautics

基　　金：航空科学基金资助项目 (97E5 10 45 )

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 .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. 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).

关 键 词：环境控制系统 优化设计 飞机设备吊舱 军用飞机 

分 类 号：V223[航空宇航科学与技术—飞行器设计] V271.4