본 발명의 일 실시예에 따르면, 제1축을 따라 연장 형성되는 비행본체부와, 비행본체부의 양측에 위치 고정되는 한 쌍의 날개부 및 비행본체부의 내측에 배치되는 덕티드팬부를 포함하고, 덕티드팬부는 비행본체부의 상기 제1축에 직교하는 제2축을 회전 중심축으로 하여 회전력을 발생시키는 팬블레이드부와, 팬블레이드부의 외측에 배치되며, 비행본체부에 대하여 미리 설정된 각도만큼 회전 가능한 베인부를 포함하는 것을 특징으로 하는 수직 이착륙 비행 장치를 제공한다.

    One embodiment of the present invention provides a vertical take-off and landing flight system, comprising: a flight main body part extending along a first axis; a pair of wing parts fixed in position on both sides of the flight main body part; and a ducted fan part disposed on the inside of the flight main body part, wherein the ducted fan part includes: a fan blade part for generating a rotational force with a second axis orthogonal to the first axis of the flight main body part as a central axis of rotation; and a vane part disposed on the outside of the fan blade part, and rotatable by a preset angle with respect to the flight main body part. An object of the present invention is to be able to generate thrust together with the ducted fan part that generates lift in emergency situations such as failure of a thrust generating part.


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    Title :

    Vertical take-off and landing aerial apparatus


    Additional title:

    수직 이착륙 비행 장치


    Publication date :

    2025-05-07


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Korean


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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