According to the present invention, a horizontal stabilizer comprises a pair of half horizontal stabilizers which are bilateral symmetry, wherein the half horizontal stabilizer includes: an A section; a B section; a C section surrounding the outside of the A section and the B section; and a cap covered on one end of the C section. The A section, B section and the C section are formed by a thermoplastic resin matrix in which carbon fiber is contained. When the present invention is used, the horizontal stabilizer can be quickly formed with a simple structure so that weight lightening and price competitiveness of the horizontal stabilizer are improved.

    본 발명에 따른 수평꼬리날개는, 좌우 대칭인 수평꼬리반쪽날개 한 쌍으로 구성되며, 상기 수평꼬리반쪽날개는, A구역과, B구역과, 상기 A구역 및 상기 B구역의 외곽을 감싼 C구역과, 상기 C구역의 일단에 씌워진 캡을 포함하며, 상기 A구역, 상기 B구역, 상기 C구역은 탄소섬유가 포함된 열가소성 수지매트릭스로 형성된 것을 특징으로 한다. 본 발명을 사용하면, 수평꼬리날개를 단순한 구조로 신속하게 만들 수 있어, 수평꼬리날개의 경량화 및 가격경쟁력이 향상된다.


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    Title :

    HORIZONTAL STABILIZER AND APPARATUS AND METHOD FOR MANUFACTURING THE SAME


    Additional title:

    수평꼬리날개 및 이를 제조하는 장치 및 방법


    Contributors:

    Publication date :

    2020-03-18


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Korean


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B32B LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM , Schichtkörper, d.h. aus Ebenen oder gewölbten Schichten, z.B. mit zell- oder wabenförmiger Form, aufgebaute Erzeugnisse / 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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