An aircraft includes an airframe having a fixed-wing section and a plurality of articulated electric rotors, at least some of which are variable-position rotors having different operating configurations based on rotor position. A first operating configuration is a vertical-flight configuration in which the rotors generate primarily vertical thrust for vertical flight, and a second operating configuration is a horizontal-flight configuration in which the rotors generate primarily horizontal thrust for horizontal fixed-wing flight. Control circuitry independently controls rotor thrust and rotor orientation of the variable-position rotors to provide thrust-vectoring maneuvering. The fixed-wing section may employ removable wing panels so the aircraft can be deployed both in fixed-wing and rotorcraft configurations for different missions.
VTOL aircraft having fixed-wing and rotorcraft configurations
2023-08-15
Patent
Elektronische Ressource
Englisch
VTOL AIRCRAFT HAVING FIXED-WING AND ROTORCRAFT CONFIGURATIONS
Europäisches Patentamt | 2019
|VTOL AIRCRAFT HAVING FIXED-WING AND ROTORCRAFT CONFIGURATIONS
Europäisches Patentamt | 2019
|VTOL AIRCRAFT HAVING FIXED-WING AND ROTORCRAFT CONFIGURATIONS
Europäisches Patentamt | 2019
|VTOL AIRCRAFT HAVING FIXED-WING AND ROTORCRAFT CONFIGURATIONS
Europäisches Patentamt | 2020
|VTOL aircraft having fixed-wing and rotorcraft configurations
Europäisches Patentamt | 2024
|