The present invention relates to a pitch stabilizer (10) with a box structure suitable to provide stability for a rotorcraft. The pitch stabilizer (10) includes a vertical middle surface (15) and a fuselage (14). The pitch stabilizer (10) includes one or two pitch stabilizing assembly. One pitch stabilizing assembly is arranged on each side of the vertical middle surface (15), and each pitch stabilizing assembly includes an upper pitch stabilizing means (11), a lower pitch stabilizing means (12), and a wing tip element (13).

    회전날개 항공기에 안정성을 제공하기에 적합한 박스 구조를 갖는 피치 스태빌라이저(10)로서 수직 중간면(15) 및 동체(14)를 포함하며, 피치 스태빌라이저(10)는 하나 또는 두 개의 피치 스태빌라이징 조립체를 포함하는데, 수직 중간면(15)의 각 측에는 단지 하나의 피치 스태빌라이징 조립체가 있으며, 각 피치 스태빌라이징 조립체는 상측 피치 스태빌라이징 수단(11), 하측 피치 스태빌라이징 수단(12) 및 윙팁 요소(13)를 포함한다.


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    Title :

    ADVANCED PITCH STABILIZER


    Additional title:

    진보된 피치 스태빌라이저


    Contributors:

    Publication date :

    2015-06-08


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Korean


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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