Vehicle, system, and method for vertical take-off and landing
Disclosed herein are a vehicle system and method for VTOL. The vehicle system includes: a carrier vehicle and a cruise vehicle. The carrier vehicle includes one or more fuselages, one or more wings, one or more attach units coupled to the one or more fuselages or to the one or more wings, and propulsion systems operable to provide, at least, substantially vertical thrust and substantially horizontal thrust. The cruise vehicle includes one or more fuselages for carrying passengers or cargo and one or more wings. The one or more attach units of the carrier vehicle are adapted to couple to the cruise vehicle to detachably engage.
1. A vehicle system for vertical take-off and/or landing (VTOL), comprising:
a carrier vehicle, comprising: one or more fuselages, one or more wings, one or more attach units coupled to the one or more fuselages or to the one or more wings, and propulsion systems operable to provide, at least, vertical thrust and horizontal thrust;
a cruise vehicle, comprising: one or more fuselages for carrying passengers or cargo, and one or more wings;
the one or more attach units of the carrier vehicle being adapted to couple to the cruise vehicle to detachably engage,
wherein the propulsion system of the carrier vehicle comprises:
one or more lift rotors coupled to the one or more fuselage or the one or more wings and operable to provide vertical thrust; and
one or more cruise rotors coupled to a fore or aft end of the one or more fuselages or the one or more wings and operable to provide horizontal thrust, and
wherein the one or more lift rotors comprise four pairs of lift rotors, the one or more fuselages of the carrier vehicle comprises two fuselages coupled with one wing, and the one or more cruise rotors comprises two push rotors coupled to two tails of the carrier vehicle.
2. The vehicle system of claim 1 , wherein each pair of lift rotors is operable to co-rotate or counter-rotate.
3. The vehicle system of claim 1 , wherein the carrier vehicle or the cruise vehicle further comprises landing gears, landing points, or landing skids.
4. The vehicle system of claim 1 , wherein the one or more attach units comprises a connector or an adjustable grappling arm.
5. The vehicle system of claim 1 , wherein the propulsion systems comprise one or more axial compressors.
6. The vehicle system of claim 1 , wherein the cruise vehicle comprises one or more pull rotors, one or more push rotors or both.
7. The vehicle system of claim 1 , wherein the cruise vehicle comprises one or more attach locations coupled to the one or more fuselages or to the one or more wings, the one or more attach units of the carrier vehicle being adapted to cooperate with the one or more attach locations of the cruise vehicle to detachably engage.
8. The vehicle system of claim 1 , wherein the carrier vehicle or cruise vehicle is fossil fuel, hydrogen, electric, or hybrid electric vehicle.
9. The vehicle system of claim 1 , wherein the carrier vehicle is manned or unmanned, and the cruise vehicle is manned or unmanned.
10. The vehicle system of claim 1 , wherein the cruise vehicle is a remote piloted aircraft.
11. The vehicle system of claim 1 , wherein the one or more lift rotors comprise four or more pairs of lift rotors.
12. A vehicle system for vertical take-off and/or landing (VTOL), comprising:
a carrier vehicle, comprising: one or more fuselages, one or more wings, one or more attach units coupled to the one or more fuselages or to the one or more wings, and propulsion systems operable to provide, at least, vertical thrust and horizontal thrust;
a cruise vehicle, comprising: one or more fuselages for carrying passengers or cargo, and one or more wings;
the one or more attach units of the carrier vehicle being adapted to couple to the cruise vehicle to detachably engage,
wherein the one or more wings of the carrier vehicle comprises a first wing coupled to the fuselage at a fore end of the fuselage and a second wing coupled to the fuselage at an aft end of the fuselage, and
wherein the propulsion systems of the carrier vehicle comprise a first pair of rotors coupled to either end of the first wing and a second pair of rotors coupled to either end of the second wing.
13. The vehicle system of claim 12 , wherein the first pair of rotors or the second pair of rotors is operable in a first orientation to provide vertical thrust, and the first pair of rotors or the second pair of rotors is operable in a second orientation to provide substantially horizontal thrust.
14. The vehicle system of claim 13 , wherein the first pair of rotors is coupled to either end of the first wino via pivots and a second pair of rotors is coupled to either end of the second wing via pivots.
15. The vehicle system of claim 12 , wherein the carrier vehicle or the cruise vehicle further comprises landing gears, landing points, or landing skids.
16. The vehicle system of claim 12 , wherein the one or more attach units comprises a connector or an adjustable grappling arm.
17. The vehicle system of claim 12 , wherein the cruise vehicle comprises one or more pull rotors, one or more push rotors or both.
18. A vehicle system for vertical take-off and/or landing (VTOL), comprising:
a carrier vehicle, comprising: one or more fuselages, one or more wings, one or more attach units coupled to the one or more fuselages or to the one or more wings, and propulsion systems operable to provide, at least, vertical thrust and horizontal thrust;
a cruise vehicle, comprising: one or more fuselages for carrying passengers or cargo, and one or more wings;
the one or more attach units of the carrier vehicle being adapted to couple to the cruise vehicle to detachably engage,
wherein the one or more wings of the carrier vehicle comprises a wing blended with the fuselage, and
wherein the blended wing has a triangle-like shape, and the propulsion systems comprise an aft rotor coupled to the wing at the aft apex of the wing, a left rotor coupled to the wing at the left apex of the wing and a right rotor coupled to the wing at the right apex of the wing.
19. The vehicle system of claim 18 , wherein the aft rotor, the left rotor, or the right rotor is operable in a first orientation to provide vertical thrust, and the aft rotor, the left rotor, or the right rotor is operable in a second orientation to provide horizontal thrust.
20. The vehicle system of claim 19 , wherein the aft rotor, the left rotor, and the right rotor are coupled to the wing via pivots.
21. The vehicle system of claim 18 , wherein the carrier vehicle or the cruise vehicle further comprises landing gears, landing points, or landing skids.
22. The vehicle system of claim 18 , wherein the one or more attach units comprises a connector or an adjustable grappling arm.
23. The vehicle system of claim 18 , wherein the cruise vehicle comprises one or more pull rotors, one or more push rotors or both.