The present invention relates to a propeller wind tunnel test apparatus. A technical object of the present invention is to provide the propeller wind tunnel test apparatus capable of preventing influence of the self-weight of a motor or the like on a thrust sensor, in advance. To the above object, the propeller wind tunnel test apparatus of the present invention comprises: a column unit including a fixed support member; a thrust sensor unit fixed to the column unit; a driving module provided in front of the thrust sensor unit; and a movement support unit movably supporting the driving module on the fixed support member.

    본 발명은 추력 센서에 모터 등의 자중이 미치는 영향을 미연에 막을 수 있는 프로펠러 풍동시험 장치를 제공하는 것이 그 기술적 과제이다. 이를 위해, 본 발명의 프로펠러 풍동시험 장치는, 고정 받침 부재를 포함하는 기둥부; 상기 기둥부에 고정되는 추력 센서부; 상기 추력 센서부의 앞에 구비되는 구동 모듈; 및 상기 구동 모듈을 상기 고정 받침 부재에 이동 가능하게 받치는 이동 받침부를 포함한다.


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    Title :

    Wind tunnel test apparatus for propeller


    Additional title:

    프로펠러 풍동시험 장치


    Contributors:
    CHO TAE HWAN (author) / KIM YANG WON (author)

    Publication date :

    2018-06-14


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Korean


    Classification :

    IPC:    G01M TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES , Prüfen der statischen oder dynamischen Massenverteilung rotierender Teile von Maschinen oder Konstruktionen / B64C AEROPLANES , Flugzeuge / 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



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