The invention belongs to the technical field of airplane distributed hybrid electric propulsion system design, and particularly relates to an airplane distributed hybrid electric propulsion system configuration scheme evaluation method and system, and the method comprises the steps: 1, carrying out the assignment of subjective and objective weights of all evaluation indexes; 2, integrating subjective and objective weights of the evaluation indexes, and determining the weight of each evaluation index; and step 3, collecting parameters of each evaluation index, and calculating a score of the aircraft distributed hybrid electric propulsion system configuration scheme based on the weight of each evaluation index.

    本申请属于飞机分布式混电推进系统设计技术领域,具体涉及一种飞机分布式混电推进系统构型方案评价方法及其系统,其中,飞机分布式混电推进系统构型方案评价方法包括:步骤一、对各个评价指标主观、客观权重进行赋值;步骤二、综合评价指标主观、客观权重,确定各个评价指标的权重;步骤三、采集各个评价指标的参数,基于各个评价指标的权重,计算飞机分布式混电推进系统构型方案的评分。


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    Titel :

    Aircraft distributed hybrid electric propulsion system configuration scheme evaluation method and system


    Weitere Titelangaben:

    一种飞机分布式混电推进系统构型方案评价方法及其系统


    Beteiligte:
    WANG XIANGPING (Autor:in) / HE JIAQIAN (Autor:in) / WANG JIANPEI (Autor:in) / SU GUIYING (Autor:in)

    Erscheinungsdatum :

    01.04.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / G06F ELECTRIC DIGITAL DATA PROCESSING , Elektrische digitale Datenverarbeitung



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