High-speed vertical take-off and landing aircraft
AssigneesThe Texas A&M University System, Oklahoma State University
InventorsMoble Benedict, David Allen Coleman, Atanu Halder
Life of this patent
Estimating the term…
Loading patent…
AssigneesThe Texas A&M University System, Oklahoma State University
InventorsMoble Benedict, David Allen Coleman, Atanu Halder
Estimating the term…
A high-speed vertical take-off and landing (HSVTOL) aircraft includes an airframe, a pair of inner wings coupled to and extending from the airframe, and a pair of wing rotors pivotably coupled to the pair of inner wings, wherein each of the pair of wing rotor has a rotatable configuration in which the wing rotor is freely rotatable entirely about a rotational axis of the wing rotor to generate vertically directed thrust that is applied to the airframe in a vertical take-off and landing (VTOL) mode of the HSVTOL aircraft, and a fixed configuration in which the wing rotor is locked into a defined angular orientation about the rotational axis in a forward cruise mode of the HSVTOL aircraft.
A high-speed vertical take-off and landing (HSVTOL) aircraft, comprising:
A high-speed vertical take-off and landing (HSVTOL) aircraft, comprising:
A high-speed vertical take-off and landing (HSVTOL) aircraft, comprising:
Dependencies are inferred from the claim text.