일 실시예에 따른 항공기는, 항공기 상태정보를 검출하는 상태정보 검출부; 상기 항공기 상태정보에 기초하여 비상착륙 상황인지 여부를 판단하고 예상되는 비상착륙지점을 계산하는 제어부; 소리 및 빛 중 적어도 하나를 이용하여 상기 비상착륙지점을 향해 경고 정보를 출력하는 외부 출력부; 및 내부 및 외부 중 적어도 일부에 상기 상태정보 검출부, 상기 제어부 및 상기 외부 출력부가 구비되는 동체부;를 포함할 수 있다.

    An embodiment aircraft includes an aircraft body including a fuselage, a status information detection device disposed in or on the aircraft body, a controller disposed in or on the aircraft body and configured to determine whether an emergency landing situation exists based on aircraft status information detected by the status information detection device and, in response to a determination that the emergency landing situation exists, calculate an expected emergency landing point, and an external output device disposed in or on the aircraft body and configured to output warning information toward the expected emergency landing point, wherein the warning information includes a sound or a light.


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    Title :

    AIRCRAFT WITH EMERGENCY LANDING ZONE WARNING SYSTEM


    Additional title:

    비상착륙지점 경고 시스템을 구비한 항공기


    Publication date :

    2025-06-12


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Korean


    Classification :

    IPC:    G08B SIGNALLING OR CALLING SYSTEMS , Signalisier- oder Rufsysteme / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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