To surely grasp an unlocked state of a cowl member while suppressing cost and time necessary for measures against forgetting of locking of an engine nacelle. An aircraft according to the present invention includes: an engine (3) that includes an engine main body (4, 5) outputting thrust force and an engine nacelle (7) surrounding the engine main body (4, 5); an engine pylon (2) that supports the engine main body (4, 5) to a main wing (1) and axially supports a cowl member (8) to be openable, the cowl member (8) configuring the engine nacelle (7); a locking part (30) that locks the cowl member (8) of the engine nacelle (7) in a closed state; and one or more light emitting sections (15) that are disposed inside the cowl member (8) and show an unlocked state of the cowl member (8).


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    Titel :

    AIRCRAFT, AIRCRAFT ENGINE, AND AIRCRAFT ENGINE NACELLE


    Weitere Titelangaben:

    FLUGZEUG, FLUGTRIEBWERK UND FLUGZEUGTRIEBWERKSGONDEL
    AÉRONEF, MOTEUR D'AÉRONEF ET NACELLE DE MOTEUR D'AÉRONEF


    Beteiligte:
    OONISHI TETSUYA (Autor:in) / SHIMOJO MASAHIRO (Autor:in) / SUZUKI TAKANORI (Autor:in)

    Erscheinungsdatum :

    2019-11-06


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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