The present invention relates to aircraft circular alignment multiple control surfaces and a control method thereof, which are able to put together the control surfaces hanging on the wings of an aircraft by the control surfaces connected to a servo by being aligned in a circular shape into a duct, to make the wings of the aircraft more stable in structural terms, and to allow a user to intuitively check the motion characteristics of the aircraft at a glance. That is, the aircraft circular alignment multiple control surfaces comprise: a duct placed to mount the servo and the control surfaces; the servo aligned in circular shape on a rear side of the duct; the control surfaces aligned in a circular shape on a rear side of the duct and connected to the servo; a thrust generation apparatus in the duct to be connected to a fan; a flight control apparatus placed on the fuselage of the aircraft; and a sensitivity input apparatus placed in the flight control apparatus. Accordingly, the present invention has effects to put together the control surfaces hanging on the wings of the aircraft by the control surfaces connected to the servo by being aligned in a circular shape into the duct, to make the wings of the aircraft more stable in structural terms, and to allow the user to intuitively check the motion characteristics of the aircraft at a glance.

    본 발명은 항공기 원형 정렬 다중 조종면 및 제어 방법에 관한 것으로서, 원형으로 정렬되어 서보에 연결된 조종면에 의하여 항공기 날개에 달려있던 조종면을 덕트로 모아 항공기 날개의 구조적으로 더욱 안정적으로하면서 항공기 운동 특성을 직관적으로 한눈에 확인하도록 함을 목적으로 한 것이다. 즉, 서보와 조종면을 장치할 수 있게 구비한 덕트, 덕트 후방에 원형으로 정렬한 서보, 덕트 후방에 원형으로 정렬되어 서보에 연결된 조종면, 덕트 내부에 팬과 연결된 추력발생장치, 항공기 동체에 구비된 비행제어장치, 비행제어장치 내부에 구비된 민감도입력장치로 구성한 것이다. 따라서, 본 발명은 원형으로 정렬되어 서보에 연결된 조종면에 의하여 항공기 날개에 달려있던 조종면을 덕트로 모아 항공기 날개의 구조적으로 더욱 안정적으로하면서 항공기 운동 특성을 직관적으로 한눈에 확인할 수 있는 효과를 갖는 것이다.


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    Titel :

    AIRCRAFT CIRCULAR ALIGNMENT MULTIPLE CONTROL SURFACES AND METHOD OF CONTROL


    Weitere Titelangaben:

    항공기 원형 정렬 다중 조종면 및 제어방법


    Beteiligte:
    CHO YUN SANG (Autor:in)

    Erscheinungsdatum :

    2021-04-07


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Koreanisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / G05D SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES , Systeme zum Steuern oder Regeln nichtelektrischer veränderlicher Größen



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