An embodiment of the present invention is a thrust measuring device of a thrust generator that generates an ascending thrust of an elevating aircraft, comprising: a frame unit; a mount unit disposed on the frame unit and detachably installed in the thrust generator; a connecting rod having an upper end connected to the mount unit and extending long in the vertical direction toward a lower portion of the frame unit; and a load cell unit connected to the lower end of the connecting rod and disposed under the frame unit for measuring the thrust of the thrust generator transmitted through the mount unit and the connecting rod when the thrust generator is operated. An object of the present invention is to provide the thrust measuring device of a thrust generator for an elevating aircraft that can accurately measure the thrust generated from the thrust generator by directly installing the thrust generator.

    본 발명의 실시예는 승강 비행체의 상승 추력을 발생하는 추력발생기의 추력 측정 장치로서, 프레임 유닛, 상기 프레임 유닛의 상부에 배치되고 상기 추력발생기가 착탈 가능하게 설치되는 마운트 유닛, 상기 마운트 유닛에 상단부가 연결되고 상기 프레임 유닛의 하부를 향해 상하 방향으로 길게 연장된 연결 로드, 및 상기 연결 로드의 하단부와 연결되고 상기 프레임 유닛의 하부에 배치되며 상기 추력발생기의 작동시 상기 마운트 유닛과 상기 연결 로드를 통해 전달되는 상기 추력발생기의 추력을 측정하는 로드셀 유닛을 포함한다.


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    Titel :

    THRUST MEASURING APPARATUS FOR THRUST GENERATOR OF SMALL UAV


    Weitere Titelangaben:

    승강 비행체용 추력발생기의 추력 측정 장치


    Beteiligte:
    BAEK JIN WOOK (Autor:in) / YU HYEONG MIN (Autor:in)

    Erscheinungsdatum :

    2021-10-28


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Koreanisch


    Klassifikation :

    IPC:    B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen / B64C AEROPLANES , Flugzeuge / G01L Messen von Kraft, mechanischer Spannung, Drehmoment, Arbeit, mechanischer Leistung, mechanischem Wirkungsgrad oder des Drucks von Fluiden , MEASURING FORCE, STRESS, TORQUE, WORK, MECHANICAL POWER, MECHANICAL EFFICIENCY, OR FLUID PRESSURE



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