VTOL box-wing multirotor aerial vehicle
US12337959B2 · kind B2 · utility
Inventor
Key dates
| Filing date | Dec 29, 2022 |
| Grant date | Jun 24, 2025 |
| Priority date | — |
| Expiry date | Jun 7, 2043 |
Classification
- Technology area (CPC B)Performing Operations; Transporting
- CPC primaryB64C2009/005
- WIPO fieldTransport
- WIPO sectorMechanical engineering
Abstract
A VTOL (vertical take-off and landing) box-wing aerial vehicle with multirotor to provide VTOL flight includes a detachable cabin, fuselage base, a pair of first wings extending outward from the upper portion of the fuselage and a pair of second wings extending outwardly and from the lower portion of the fuselage. The first and second wings are spaced apart longitudinally and vertically. The pylon joints the first wing and second wing at the tip to form the box-wing. The pylon includes heading control rudder. Secured to the wing or pylon or both wing and pylon, a fixed rotor boom extending longitudinally to support a plurality of lift rotors for VTOL flight. In one configuration, the rotor boom is pivotable. Finally, the fuselage mounted push rotor propels the vehicle forward to generate lift from the wings. Furthermore, the wings are equipped with elevators and ailerons for flight control.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.