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Title:
VERTICAL TAKEOFF AND LANDING TYPE HYBRID DRONE
Document Type and Number:
WIPO Patent Application WO/2020/130333
Kind Code:
A1
Abstract:
The present invention relates to a vertical take-off and landing type hybrid drone comprising: a pair of front rotary rotors, which are formed on a fixed blade, perform a vertical rotation operation so that vertical taking-off and landing are performed, and respectively perform independent control in order to control the rockshaft of the drone; a rear rotary rotor which is formed on a tail wing and which provides propulsion during flight of the drone; a dual receiver for receiving a plurality of flight control signals; and a rotor control unit for analyzing the plurality of flight control signals transmitted from the dual receiver, and controlling the driving of the front and rear rotary rotors by selecting the flight control signal having a small error.

Inventors:
KIM MU SEON (KR)
Application Number:
KR2019/014817
Publication Date:
June 25, 2020
Filing Date:
November 04, 2019
Export Citation:
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Assignee:
KOREAUAV CO LTD (KR)
International Classes:
B64C39/02; B64C11/46; B64C29/00; B64D27/24; B64D45/00
Domestic Patent References:
WO2017208037A12017-12-07
Foreign References:
US20160083115A12016-03-24
US20160200436A12016-07-14
KR20150058197A2015-05-28
KR102010964B12019-08-16
Attorney, Agent or Firm:
JUNG, Chang Su (KR)
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