Title:
FLIGHT VEHICLE
Document Type and Number:
WIPO Patent Application WO/2023/062691
Kind Code:
A1
Abstract:
This flight vehicle comprises: attachment sections that are disposed at the tips of a pair of fixed wings disposed to the left and the right with a main body therebetween, and that have side surfaces on sides facing away from the main body; front support columns disposed to the attachment sections on the front side thereof in the travel direction of the flight vehicle; rear support columns disposed on the attachment sections on the rear side thereof in the travel direction of the flight vehicle; aircraft propellers attached to the tips of the front support columns and aircraft motors for rotating said propellers; and multicopter propellers attached respectively to the rear bottom side of the rear support columns and to the tips of extended support columns that extend upward from the front side of the front support columns, and multicopter motors for rotating said propellers. The aircraft motors rotate the aircraft propellers in a direction so that air flowing through the aircraft propellers will suppress vortex flow generated due to pressure differences between above and below the fixed wings.
Inventors:
NOMURA MAKOTO (JP)
Application Number:
PCT/JP2021/037597
Publication Date:
April 20, 2023
Filing Date:
October 11, 2021
Export Citation:
Assignee:
SANKYO MOKKO CO LTD (JP)
International Classes:
B64C27/26
Foreign References:
| US20190337612A1 | 2019-11-07 | |||
| JP2021154802A | 2021-10-07 |
Attorney, Agent or Firm:
MOMOSE Naoyuki (JP)
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