Disclosed are a rotor head of a flight vehicle and an unmanned helicopter. The rotor head of a flight vehicle comprises: a top propeller unit having a plurality of rotor blades; a rotor drive shaft unit of which an upper end is joined to the top propeller unit to transmit a rotating force generated in a propeller drive unit to the top propeller unit; and a tilt adjustment unit joined to a lower end of the top propeller unit to adjust an angle of an rotating surface of the top propeller unit. Therefore, an angle of a rotating surface of the rotor blades can be accurately and freely adjusted through a tilt rotating unit.

    비행체의 로터헤드 및 무인헬기가 개시된다. 상기 비행체의 로터헤드는, 복수 개의 로터 블레이드를 구비하는 탑 프로펠러부, 상단이 상기 탑 프로펠러부와 결합되어 프로펠러 구동부에서 생성된 회전력을 상기 탑 프로펠러부로 전달하는 로터 구동축부, 및 상기 탑 프로펠러부의 하단과 결합되어 상기 탑 프로펠러부의 회전면의 각도를 조절하는 틸트 조절부를 포함하는 것을 특징으로 한다.


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    Title :

    ROTOR HEAD OF FLIGHT VEHICLE AND UNMANNED HELICOPTER


    Additional title:

    비행체의 로터헤드 및 무인헬기


    Contributors:

    Publication date :

    2016-05-10


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Korean


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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