According to the present invention, an optical window cover device for an aircraft is characterized in that it is adapted to cover an optical window formed in the aircraft with a cover which does not transmit electromagnetic waves during a flight course in which the function of transmitting electromagnetic waves is not required, and to detach the cover covering the optical window from the aircraft during the end of flight phase, when the operation of an electromagnetic wave transceiver mounted inside the aircraft begins.

    본 발명에 따른 비행체용 광학창 덮개 장치는, 전자기파 투과기능이 필요하지 않은 비행구간 동안 비행체에 형성된 광학창을 전파를 투과하지 않는 덮개로 덮어 레이다파를 전반사시키거나 흡수하고, 상기 비행체 내부에 탑재한 전자기파 송수신기의 작동이 시작되는 비행 종말단계에서 상기 광학창을 덮고 있는 덮개를 상기 비행체로부터 분리시키도록 이루어진 것을 특징으로 한다.


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    Titel :

    Optical window covering device for air-vehicle


    Weitere Titelangaben:

    비행체용 광학창 덮개 장치


    Beteiligte:
    LEE WOO YONG (Autor:in) / CHA JIN HYUN (Autor:in) / AHN JOONG KI (Autor:in) / KO DUCK KON (Autor:in)

    Erscheinungsdatum :

    24.10.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Koreanisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / H01Q Antennen , ANTENNAS, i.e. RADIO AERIALS / H05K PRINTED CIRCUITS , Gedruckte Schaltungen



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