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GRAPH-THEORY-BASED AUXILIARY COOLING SYSTEM SIMULATION MODELING METHOD FOR LARGE PASSENGER AIRPLANE

机译:基于图形理论的辅助冷却系统模拟大型乘客飞机的仿真建模方法

摘要

Disclosed is a graph-theory-based auxiliary cooling system simulation modeling method for a large passenger airplane. An auxiliary cooling system is based on a vapor compression refrigeration cycle. The method comprises: 1) firstly, according to a set encoding rule, encoding a subsystem of the auxiliary cooling system and subunits of the subsystem; 2) generating, on the basis of the encoded auxiliary cooling system, an edge set and a point set of a directed graph, and constructing the directed graph; 3) the directed graph being expressed as an adjacent matrix; 4) decoding the adjacent matrix, and acquiring the type of the subsystem of the auxiliary cooling system, a connecting manner for each subunit, and the flow direction of a refrigerating medium; and 5) according to a decoding result, performing calculation to obtain a refrigerating medium inlet state and a refrigerating medium outlet state of each subunit. By means of the modeling method, a universal auxiliary cooling system simulation model for a large passenger airplane can be established quickly and accurately, and the modeling method is applicable to the configuration of different auxiliary cooling systems and has versatility.
机译:公开了一种基于图形 - 理论的辅助冷却系统模拟建模型建模方法,用于大型乘客飞机。辅助冷却系统基于蒸汽压缩制冷循环。该方法包括:1)首先,根据集合编码规则,编码辅助冷却系统的子系统和子系统的亚基; 2)基于编码的辅助冷却系统,边缘组和定向图的点组和构造定向图; 3)所指示的图表被表示为相邻矩阵; 4)解码相邻矩阵,并获取辅助冷却系统的子系统的类型,每个亚单元的连接方式,以及制冷介质的流动方向; 5)根据解码结果,执行计算以获得每个子单元的制冷介质入口状态和制冷介质出口状态。借助于建模方法,可以快速准确地建立用于大型客机的通用辅助冷却系统仿真模型,并且建模方法适用于不同辅助冷却系统的配置并具有多功能性。

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