Title:
VERTICAL TAKE-OFF AND LANDING AIRCRAFT, AND VERTICAL TAKE-OFF AND LANDING AIRCRAFT CONTROLLER, CONTROL METHOD, AND CONTROL PROGRAM
Document Type and Number:
WIPO Patent Application WO/2018/083839
Kind Code:
A1
Abstract:
A vertical take-off and landing aircraft equipped with: an airframe main section; a frame which defines a quadrant center inside the airframe main section in a planar pattern, and supports the airframe main section so as to generate independent lift in the same direction in each quadrant among the first through fourth quadrants positioned around the quadrant center; first propellers provided via a rotating shaft provided in the frame in each of the first through fourth quadrants; and a second propeller which rotates in the same direction as does the first propeller and is provided in the first quadrant via a rotating shaft provided in the frame. Furthermore, the direction of rotation in the first and third quadrants is the opposite direction from the direction of rotation in the second and fourth quadrants.
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Inventors:
SUZUKI HIDEO (JP)
SUZUKI SACHIHIRO (JP)
MATSUSHITA KOTARO (JP)
HANADA MASAKI (JP)
SHINOHARA TORU (JP)
NIIJIMA NORIKO (JP)
NAKAMURA TADAO (JP)
SUZUKI SACHIHIRO (JP)
MATSUSHITA KOTARO (JP)
HANADA MASAKI (JP)
SHINOHARA TORU (JP)
NIIJIMA NORIKO (JP)
NAKAMURA TADAO (JP)
Application Number:
PCT/JP2017/024917
Publication Date:
May 11, 2018
Filing Date:
July 07, 2017
Export Citation:
Assignee:
SUZUKI HIDEO (JP)
International Classes:
B64C27/08; B64C39/02; B64D27/24
Domestic Patent References:
| WO2015199535A1 | 2015-12-30 |
Foreign References:
| US20140062754A1 | 2014-03-06 | |||
| JP2016147565A | 2016-08-18 | |||
| JP2016524567A | 2016-08-18 |
Attorney, Agent or Firm:
SUZUKI Sohbe (JP)
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