Title:
VERTICAL TAKEOFF AND LANDING AIRCRAFT
Document Type and Number:
WIPO Patent Application WO/2019/066484
Kind Code:
A1
Abstract:
The present invention relates to a vertical takeoff and landing aircraft. According to one embodiment of the present invention, the vertical takeoff and landing aircraft comprises: a flight fuselage (F) on which a main wing (3) and auxiliary wings (W1, W2) are mounted; a pair of front propellers (7) respectively mounted at both sides of the flight fuselage (F) so as to be variable in the horizontal and vertical directions; a rear propeller (9) mounted on the auxiliary wings (W1, W2) provided at the rear of the flight fuselage (F), so as to be variable in the horizontal and vertical directions; front and rear variable parts (11, 13) mounted on the flight fuselage (F) and the auxiliary wings (W1, W2) so as to vary the front propellers (7) and the rear propeller (9) in the vertical or horizontal direction; and a control part (50) for controlling the front and rear variable parts (11, 13).
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Inventors:
HONG SEUNG-IL (KR)
Application Number:
PCT/KR2018/011414
Publication Date:
April 04, 2019
Filing Date:
September 27, 2018
Export Citation:
Assignee:
HONG SEUNG IL (KR)
International Classes:
B64C29/00; B64C11/00; B64C11/48
Foreign References:
| KR20090101413A | 2009-09-28 | |||
| JP2016172557A | 2016-09-29 | |||
| KR200286578Y1 | 2002-08-22 | |||
| KR20160116748A | 2016-10-10 | |||
| KR20030049796A | 2003-06-25 |
Attorney, Agent or Firm:
IPUS PATENT & LAW FIRM (KR)
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