A fastening system (1) and an aircraft comprising such a fastening system. The fastening system comprises a longitudinal box (4), a plurality of upper shaped bodies (7) fastened to an upper end of the longitudinal box (4), and a plurality of lower shaped bodies (10) fastened to a lower end of the longitudinal box (4), at least two upper shaped bodies (7) comprising two fastening means (8) such that each fastening means connects a fastening point (9) of the can (2) to the upper shaped bodies (7), the at least one lower forming body (10) comprises two second fastening means (11) such that each second fastening means connects a second fastening point (12) of the can (2) to the lower forming body (10). The fastening system (1) allows an operator to access a canister that can be fastened by the fastening system (1).

    紧固系统(1)和包括这种紧固系统的飞行器。紧固系统包括纵向箱(4)、被紧固到纵向箱(4)的上端部的多个上成形体(7)和被紧固到纵向箱(4)的下端部的多个下成形体(10),至少两个上成形体(7)包括两个紧固装置(8),以便使得每个紧固装置将罐(2)的紧固点(9)连接到上成形体(7),至少一个下成形体(10)包括两个第二紧固装置(11),以便使得每个第二紧固装置将罐(2)的第二紧固点(12)连接到下成形体(10)。紧固系统(1)允许操作者接近能够被紧固系统(1)紧固的罐。


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    Titel :

    Fastening system and aircraft integrated with such fastening system


    Weitere Titelangaben:

    紧固系统和集成有这种紧固系统的飞行器


    Beteiligte:
    MERTES ANDREAS (Autor:in)

    Erscheinungsdatum :

    2024-05-10


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

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



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