Disclosed is an aircraft lamp including a lamp outer case constituted of a lamp housing having an opening and a cover mounted to the lamp housing in a state of closing the opening, the lamp outer case having an inner space formed as an arrangement space, and a light source disposed in the arrangement space, a portion of the lamp housing is provided as a heat sink that releases heat generated when the light source is driven to an outside of the lamp housing, the heat sink is provided with a hole forming portion, and the hole forming portion is formed with an air vent hole communicating with the arrangement space and the outside of the lamp housing.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    AIRCRAFT LAMP


    Beteiligte:
    YODA TAKASHI (Autor:in)

    Erscheinungsdatum :

    2020-02-13


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F21V FUNCTIONAL FEATURES OR DETAILS OF LIGHTING DEVICES OR SYSTEMS THEREOF , Funktionsmerkmale oder Einzelheiten von Leuchten oder Beleuchtungssystemen



    AIRCRAFT LAMP

    SAWADA SHIGEO / SHOJI AKIO / URUSHIBATA MIKIO | Europäisches Patentamt | 2021

    Freier Zugriff

    AIRCRAFT LAMP

    YODA TAKASHI | Europäisches Patentamt | 2020

    Freier Zugriff

    Aircraft lamp

    TSUKAMOTO MICHIO / SAWADA SHIGEO | Europäisches Patentamt | 2023

    Freier Zugriff

    AIRCRAFT LAMP

    Europäisches Patentamt | 2021

    Freier Zugriff

    AIRCRAFT LAMP

    MUKAI TOMOYUKI / SHIMIZU HIROTO | Europäisches Patentamt | 2020

    Freier Zugriff