Title:
航空機及び航空機を飛行させる方法
Document Type and Number:
Japanese Patent JP7414310
Kind Code:
B2
Abstract:
Airframes configured for stable in-flight transition between forward flight and vertical takeoff and landing are described herein. In one embodiment, an aircraft can include a fuselage, opposed wings extending from opposed sides of the fuselage, and a plurality of engines. At least one engine can be mounted to each of the opposed wings and at least a portion of each opposed wing including at least one of the plurality of engines can rotate relative to the fuselage around a rotation axis that is non-perpendicular and transverse to a longitudinal axis of the fuselage. Rotating portions of the wings including at least one of the plurality of engines in the described manner can provide a stable and smooth transition between vertical and forward flight.
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Inventors:
Petrov, Val
Application Number:
JP2022081615A
Publication Date:
January 16, 2024
Filing Date:
May 18, 2022
Export Citation:
Assignee:
PTERODYNAMICS INC.
International Classes:
B64C29/00; B64C27/28; B64C27/58
Domestic Patent References:
| JP2014113937A | ||||
| JP154394C2 |
Foreign References:
| KR100822366B1 | ||||
| US20150336663 | ||||
| US20140117150 | ||||
| US2674422 | ||||
| US3937424 | ||||
| US1556414 | ||||
| US9550567 | ||||
| WO2014177589A1 | ||||
| WO2017184270A2 | ||||
| GB447577A |
Attorney, Agent or Firm:
Patent Attorney Corporation R&C