Title:
飛行体
Document Type and Number:
Japanese Patent JP7417254
Kind Code:
B2
Abstract:
[Summary][Problem to be Solved] To provide a aircraft that enables an efficient and safe transition from hovering to level-flight. [Solution] The aircraft according to the present invention includes a lift generating part, a thrust generating part capable of flying and hovering, a connecting part that displaceably connects the lift generating part and the thrust generating part so that the lift generating part can maintain a positive angle of attack with respect to the flying direction at least at the time of ascending. The lift generating part is a wing part having a main surface, and at least at the time of hovering, a propulsion direction by the thrust generating part is along a direction obliquely intersecting the vertical direction. At least at the time of hovering, the propulsion direction and the main surface form an obtuse angle. At least at the time of hovering, the propulsion direction is along the vertical direction.
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Inventors:
Youichi Suzuki
Application Number:
JP2019552643A
Publication Date:
January 18, 2024
Filing Date:
September 17, 2019
Export Citation:
Assignee:
Aeronext Co., Ltd.
International Classes:
B64C27/28; B64C27/08; B64C27/26; B64C29/00; B64C39/02; B64D27/40; B64U10/13
Domestic Patent References:
| JP2006327219A | ||||
| JP2007508998A | ||||
| JP2013501677A | ||||
| JP2017081360A | ||||
| JP2018526287A |
Foreign References:
| US20100327123 | ||||
| US20040075017 | ||||
| EP3162708A1 | ||||
| WO2018147810A1 |