Title:
AERIAL VEHICLE AND FLYING METHOD OF AERIAL VEHICLE
Document Type and Number:
WIPO Patent Application WO/2021/024323
Kind Code:
A1
Abstract:
[Problem] The present invention provides an aerial vehicle which has a more basic structure and has safety measures. [Solution] An aerial vehicle according to the present invention comprises: a thrust unit including a plurality of rotor blades for generating thrust; a tail assembly; a fuselage connecting the thrust unit and the tail assembly; a main wing provided at an approximate center of the fuselage; and a control unit that controls at least the main wing. When the aerial vehicle lands, the control unit controls the main wing so that a part of the main wing is a lower end. The main wing is constituted by two fixed wings, and when the aerial vehicle lands, the two fixed wings slope downward in a substantially straight line as the fixed wings progress rearward while being symmetrical on both sides of the fuselage in a substantially inverted V-shape. This makes it possible to provide an aerial vehicle which has a more basic structure and has safety measures.
Inventors:
SUZUKI YOICHI (JP)
Application Number:
PCT/JP2019/030590
Publication Date:
February 11, 2021
Filing Date:
August 02, 2019
Export Citation:
Assignee:
AERONEXT INC (JP)
International Classes:
B64C39/02; B64C27/08; B64C29/02
Foreign References:
| US20130206921A1 | 2013-08-15 | |||
| JP2007508998A | 2007-04-12 |
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