개선된 공기역학적 성능을 가지고 중간- 높은 입사각에서 매우 양호한 공기역학적 거동 및 방향 안정성을 유지하기 위한 항공기(10). 상기 항공기(10)는 형성된 날개(18,20)들이 연결된 동체(12) 및 노우즈(52)를 포함한다. 상기 항공기(10)는, 날개의 리딩 엣지를 시작위치(root)연장시키는 연장부(LEX)의 와류 제어장치(72)를 포함하여 중간- 높은 입사각에서 상기 LEX에 의해 발생된 와류의 폭발을 균형상태로 만든다. 상기 항공기는 항공기의 적어도 한 개의 고온부분에서 입사 레이더 파를 소멸(dissipating)시키는 적어도 한 개의 소멸 장치를 포함하고 분리될 수 있는 장비를 포함한다.

    An aircraft (10) with improved aerodynamic performances is adapted to keep the directional stability and a very good aerodynamic behavior at medium-high incidence. The aircraft (10) includes a fuselage (12) to which shaped wings (18, 20) are associated, and a nose (52). The aircraft (10) also includes a vortex control device (72) of the extension of the leading edge of the wing at the root (LERX), shaped in order to symmetrize the bursting of the vortices generated by such LERX with a medium-high incidence. Said aircraft comprises removable equipment with at least one dissipation device of incident radar waves, on at least one hot portion of the aircraft.


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    Titel :

    AIRCRAFT WITH IMPROVED AERODYNAMIC PERFORMANCE


    Weitere Titelangaben:

    개선된 공기역학적 성능을 가진 항공기


    Erscheinungsdatum :

    2018-03-20


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Koreanisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64C AEROPLANES , Flugzeuge



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