飞机环境控制系统

飞机环境控制系统的现状与未来

Present Status and Future of Aircraft Environment Control System

飞机环境控制系统分布式实时仿真

The Real_time Distributed Simulation of Aircraft Environment Control System

基于Matlab的飞机环境控制系统动态仿真

Matlab-based Dynamic Simulation of Aircraft Environmental Control System

介绍了在MATLAB环境下，对飞机环境控制系统的建模方法，开发了飞机环控系统综合仿真的MATLAB工具箱。

MATLAB is applied to the dynamic simulation of the environmental control system ( ECS ) of military aircraft . Modeling method of cooling and controlling parts is introduced respectively based on MATLAB . A toolbox for the simulation of the environment control system is then developed .

飞机环境控制系统的最小熵增分析

Entropy generation minimization analysis for aircraft environmental control system optimal design

综述了飞机环境控制系统研究的发展与前景。

The development and prospect of the aircraft environment control system are summarized .

飞机环境控制系统并行设计

Concurrent design of environmental control systems for aircraft

研究表明，提出的最小熵增分析方法对未来复杂飞机环境控制系统的综合设计具有重要的指导意义。

The method illustrated is applicable to more complex and realistic aircraft environmental control systems .

飞机环境控制系统的模糊控制研究

Fuzzy control of aircraft environmental control system

提出了一种飞机环境控制系统性能参数匹配的焓参数匹配法，该方法尤其适用于有相变换热器的环境控制系统。

For matching the parameters of the environmental control system , an enthalpy-matched method is proposed .

分析结果对飞机环境控制系统的设计具有一定指导作用。

The results obtained in this paper have some guidance function on aircraft environmental control system optimum design .

飞机环境控制系统动态研究是高性能环境控制系统设计的重要内容。

The dynamic research of aircraft environmental control system ( ECS ) is an important step in the advanced ECS design process .

在此基础上，采用分模块建模的思想，利用MATLAB/SIMULINK仿真平台开发了飞机环境控制系统计算机仿真模型库。

Based on it , the computer simulation model library for AECS is established with module structure using software MATLAB / SIMULINK .

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；

Based on concurrent engineering , the development process of the environment control system for aircraft and the structure of system design are analyzed .

利用故障模式分析和故障树的方法，分析了国产某飞机环境控制系统的可靠性数据。

Based on the fault model and fault tree , the data of the environment control system of the airplane made in china were analyzed .

上述研究为飞机环境控制系统的方案选择、参数优化及控制规律的研究等提供了重要依据。

Studies all above provided an important foundation for the selection of the aircraft environmental control system , optimization of parameters and the study of control laws .

以某型飞机环境控制系统为例，利用该模型库构建了环控系统完整的全流量仿真模型，并给出稳态计算结果和动态响应分析。

The example of ACES full simulation model is spliced using the simulation model library and steady simulation result and dynamic process analysis is given in this paper .

一种以热力学第二定律为基础的熵产分析方法，应用于飞机环境控制系统的部件级优化设计。

An entropy generation analysis method based on the second law of thermodynamics was used to component level optimization design of aircraft environmental control system 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。

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 .

该问题的研究对于飞机环境控制系统是十分重要的。它可以用来研究和分析飞行中的生理热应力以及环境控制系统的某些参数对生理热应力的影响。

The investigation of this problem is very important to the environmental centrol system ( ECS ) of a high-performance aircraft , it can be used to research and analyse physio-logical thermal stress and the influence of some parameters of ECS on physiological thermal stress .

提出了一种采用高压空气膜除湿组件的飞机新型环境控制系统（ECS）。

A new type of aircraft environmental control system ( ECS ) using a membrane-based high-pressure air dehumidification package is proposed .

飞机座舱环境控制系统一体化最优设计

The Optimal Integration Design of Aircraft Environmental Control System

国外飞机综合环境控制系统

Aircraft Integrated Environmental Control System

空气循环制冷式飞机地面环境控制系统是沈阳航达机载设备公司立项的重点课题，是为满足新型航空装备的保障需求而研制的。

The airplane ground environmental control system is the important task of ShenYang Hang Da airplane loading equipment company . It is investigated for the demand of new aeronautic equip.

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

分析了国外两种先进的飞机电子吊舱环境控制系统的设计思想和关键技术，在此基础上提出了一种新的环控系统方案，并给出了试验结果。

The analyses of the design concepts and critical techniques of two advanced environmental control systems ( ECS ) for foreign avionics pods are made . A new ECS scheme is raised and the test results of the system are also presented .