The invention relates to an airborne system architecture and an aircraft comprising the architecture, according to the invention, the airborne system architecture has a regionalized distribution feature and comprises a plurality of regional systems (1), an energy interconnection transmission path (2) and two communication networks (3, 4), the regional systems (1) are uniformly distributed in each region of the aircraft according to regions, and the energy interconnection transmission path (2) is communicated with the two communication networks (3, 4). The internal functions of the regional systems (1) are complete or partially complete, the regional systems (1) communicate with each other through the two communication networks (3, 4), and multiple energy transmission among the regions 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,所述机载系统架构呈区域化分布特征,其包括若干个区域系统(1),能源互联传输通路(2)和两个通信网络(3,4),所述区域系统(1)按区域均布在飞行器的各区域中,各区域系统(1)内部功能完整或部分完整,各区域系统(1)间通过两个通信网络(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:
    FANG YUTONG (Autor:in)

    Erscheinungsdatum :

    2022-04-29


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / H04L TRANSMISSION OF DIGITAL INFORMATION, e.g. TELEGRAPHIC COMMUNICATION , Übertragung digitaler Information, z.B. Telegrafieverkehr



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