고정익 항공기를 위한 비행 조종 장치는 제1포트 날개(115) 및 제1스타보드 날개(120), 제1포트 로터(155)와 제1포트 전동기(135) 사이에 연결되는 제1포트 스와시 판(145), 제1포트 날개(115)에 연결되는 제1포트 전동기(135), 제1스타보드 로터(130)와 제1스타보드 전동기(140) 사이에 연결되는 제1스타보드 스와시 판(150), 제1스타보드 날개(120)에 연결되는 제1스타보드 전동기(140)를 포함한다.

    A flight control apparatus for fixed-wing aircraft includes a first port wing (115) and first starboard wing (120), a first port swash plate (145) coupled between a first port rotor 155) and first port electric motor (135), the first port electric motor (135) coupled to the first port wing (115), and a first starboard swash plate (150) coupled between a first starboard rotor (130) and first starboard electric motor (140), the first starboard electric motor (140) coupled to the first starboard wing (120).


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    Title :

    VERTICAL TAKEOFF AND LANDING VTOL AIR VEHICLE


    Additional title:

    수직 이착륙(VTOL) 공중 비행체


    Publication date :

    2020-09-02


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Korean


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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