The invention relates to a management method for managing at least one aircraft (40) configured to be selectively in a first configuration adapted to a first type of flight that does not require an auxiliary power unit (50) and a second configuration adapted to a second type of flight that requires at least one auxiliary power unit (50). The management method includes selectively mounting in a detachable manner a first light tail cone (46) that does not include an auxiliary power unit or a second tail cone (46 ') that includes at least one auxiliary power unit (50) according to a first type of flight or a second type of flight to be performed by the aircraft. The invention also relates to a management method for managing at least one fleet as well as to an aircraft and to a management device allowing the implementation of the method.

    本发明涉及一种用于管理至少一架飞行器(40)的管理方法,该飞行器被构造为能够选择性地处于适应不需要辅助动力单元(50)的第一类飞行的第一构型以及适应需要至少一个辅助动力单元(50)的第二类飞行的第二构型。管理方法包括根据待由飞行器执行的第一类飞行或第二类飞行而选择性地以可拆卸的方式安装不包括辅助动力单元的第一轻型尾锥(46)或包括至少一个辅助动力单元(50)的第二尾锥(46')。本发明还涉及一种管理至少一个机队的管理方法以及一种飞行器以及一种允许实施该方法的管理装置。


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    Titel :

    Management method for managing configuration of aircraft, aircraft and device allowing implementation of method


    Weitere Titelangaben:

    用于管理飞行器的构型的管理方法及允许实施该方法的飞行器和装置


    Beteiligte:
    DUERR PETER (Autor:in) / CAZAUX BENOIT (Autor:in)

    Erscheinungsdatum :

    21.06.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

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



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