The mathematical model for aircraft engine, heat exchanger, duct, venturi, valve and other components in aircraft environment control system (AECS) is described in this paper.
介绍了飞机环境控制系统中发动机引气、热交换器、管道、文氏管以及阀门等部件的数学模型。
Based on concurrent engineering, the development process of the environment control system for aircraft and the structure of system design are analyzed.
基于并行工程方法，分析了飞机环境控制系统的研制流程和系统设计的结构层次；
On the basis of the theory of Man-Machine-Environment system, physiological requirements for temperature control in military aircraft cabins were identified.
根据人-机-环境系统理论，论证了军用飞机座舱温度控制的生理学要求。
In order to improve environment adaptability, control precise and efficiency of aircraft antiskid brake system.
为了提高刹车系统的环境适应性、控制精度和刹车效率。
In order to improve environment adaptability, control precise and efficiency of aircraft antiskid brake system.
为了提高刹车系统的环境适应性、控制精度和刹车效率。
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