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.


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    Title :

    AIRCRAFT LAMP


    Contributors:

    Publication date :

    2020-02-13


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    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



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