VTOL AIRCRAFT HAVING FIXED-WING AND ROTORCRAFT CONFIGURATIONS

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VTOL AIRCRAFT HAVING FIXED-WING AND ROTORCRAFT CONFIGURATIONS

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BAITY SEAN MARSHALL / BILLINGSLEY DAVID D / GALLOWAY BRAD S / CHAPMAN RICHARD M

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.

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Titel :

VTOL AIRCRAFT HAVING FIXED-WING AND ROTORCRAFT CONFIGURATIONS

Weitere Titelangaben:

VERTIKAL STARTENDES UND LANDENDES (VTOL) FLUGZEUG MIT STARRFLÜGEL- UND DREHFLÜGLERKONFIGURATIONEN
AÉRONEF ADAV AYANT DES CONFIGURATIONS À AILES FIXES ET DE GIRAVION

Beteiligte:

BAITY SEAN MARSHALL (Autor:in) / BILLINGSLEY DAVID D (Autor:in) / GALLOWAY BRAD S (Autor:in) / CHAPMAN RICHARD M (Autor:in)

Erscheinungsdatum :

2020-09-09

Medientyp :

Patent

Format :

Elektronische Ressource

Sprache :

Englisch

Klassifikation :

IPC:

B64C AEROPLANES , Flugzeuge

VTOL AIRCRAFT HAVING FIXED-WING AND ROTORCRAFT CONFIGURATIONS

VTOL AIRCRAFT HAVING FIXED-WING AND ROTORCRAFT CONFIGURATIONS

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