Title:
MULTICOPTER
Document Type and Number:
WIPO Patent Application WO/2019/244462
Kind Code:
A1
Abstract:
[Problem] To provide a multicopter with low energy consumption and having a high degree of freedom for miniaturization design. [Solution] The present invention has: a fuselage 12; N number of first lift generators 30 which are located on a first concentric circle C1 approximately centered on the center of gravity of the fuselage 12, and arranged in a bilaterally symmetrical manner at each of the front and rear of the fuselage 12; and M number of second lift generators 70 which are located on a second concentric circle C2 having a larger diameter than the first concentric circle C1 approximately centered on the center of gravity G of the fuselage 12 and are located on the central axis X extending in the front-rear direction of the fuselage 12, and which are arranged at the front and rear of the fuselage 12 (where N > M).
Inventors:
TSUTSUMI DAIKO (JP)
MINAGAWA YOSHITAKA (JP)
KATO MASASHI (JP)
ISHITSUKA YUJI (JP)
MINAGAWA YOSHITAKA (JP)
KATO MASASHI (JP)
ISHITSUKA YUJI (JP)
Application Number:
PCT/JP2019/016641
Publication Date:
December 26, 2019
Filing Date:
April 18, 2019
Export Citation:
Assignee:
HONDA MOTOR CO LTD (JP)
International Classes:
B64C27/08; B64C39/02; B64D27/24
Domestic Patent References:
| WO2016136848A1 | 2016-09-01 |
Foreign References:
| JP2010132280A | 2010-06-17 | |||
| JP2016522113A | 2016-07-28 | |||
| JP2009513435A | 2009-04-02 | |||
| CN107416194A | 2017-12-01 |
Attorney, Agent or Firm:
OSHIMA & PARTNERS (JP)
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