The invention relates to a locking system (801) for an aircraft nacelle, comprising a first part (803) intended to be mounted on a first component (703) of the aircraft nacelle and a second part (809) intended to be mounted on a second component (709) of the aircraft nacelle. The locking system (801) is configured such that the first portion (803) and the second portion (809) remain together when the locking system is in the closed position. The locking system includes at least one buffer member (815) and a load sensor (817) connected together and configured to compress the load sensor (817) between the buffer member (815) and another member (807) of the locking system (801) when the locking system is in a closed position.

    本发明涉及一种用于飞行器短舱的锁定系统(801),该锁定系统包括第一部分(803)和第二部分(809),该第一部分旨在安装在飞行器短舱的第一部件(703)上,该第二部分旨在安装在飞行器短舱的第二部件(709)上。锁定系统(801)被构造成使得当该锁定系统处于关闭位置时,第一部分(803)和第二部分(809)保持在一起。锁定系统包括至少一个缓冲部件(815)和载荷传感器(817),该至少一个缓冲部件和该载荷传感器连接在一起并被构造成当锁定系统处于关闭位置时,在缓冲部件(815)和锁定系统(801)的另一个部件(807)之间压紧载荷传感器(817)。


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    Titel :

    Locking system for aircraft nacelles


    Weitere Titelangaben:

    飞行器短舱的锁定系统


    Beteiligte:

    Erscheinungsdatum :

    20.02.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

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



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