The invention relates to an on-board system architecture and an aircraft comprising the architecture, according to the invention, the on-board system architecture has a location functionalization feature that performs differentiated system functions due to a location layout, mainly comprising a number of functionalized regional systems (1), an energy interconnection transmission path (2) and two communication networks (3, 4), the functional area systems (1) are distributed in all areas of the aircraft according to needs, main functions in all the functional area systems (1) are kept relatively independent and complete, communication is carried out through the two communication networks (3 and 4), and multiple kinds of energy transmission among the areas is carried out through the energy interconnection transmission path (2).

    本发明涉及一种机载系统架构及包含架构的飞行器,根据本发明,所述机载系统架构具有区位功能化特征,其因区位布局执行差异化系统功能,主要包括若干个功能化区域系统(1)、能源互联传输通路(2)和两个通信网络(3,4),所述功能化区域系统(1)按需分布在飞行器的各区域中,各功能化区域系统(1)中主要功能保持相对独立完整,并通过2个通信网络(3,4)进行通信,通过能源互联传输通路(2)进行区域间多种能量传输。


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    Titel :

    Airborne system architecture and aircraft


    Weitere Titelangaben:

    一种机载系统架构及飞行器


    Beteiligte:
    DENG YIXUAN (Autor:in)

    Erscheinungsdatum :

    2022-04-01


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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