VTOL aerial vehicle
First Claim
1. An aircraft capable of vertical takeoff and landing, stationary flight and forward flight, comprising:
- a fuselage having a forward portion, an aft portion, a top surface and a bottom surface;
a duct extending vertically through said fuselage, said duct including an inlet on said top surface of the fuselage and an outlet on the bottom surface of said fuselage;
a lift fan having first and second counter rotating rotors disposed within said duct, the rotational axis of said rotors defining a vertical reference axis, wherein said first and second counter rotors define a toroidal fan, wherein a diameter of a hub of said toroidal fan is larger than a blade length of said first and second rotors and wherein an area below said hub of said toroidal fan forms a payload bay for said aircraft;
at least one engine operative to rotate said rotors; and
a pair of wing sets, wherein each wing set includes;
a first wing having a wing root connected to said fuselage forward of said vertical reference axis; and
a second wing having a wing root connected to said fuselage aft of said vertical reference axis, wherein a distal portion of said first and second wings are connected.
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Accused Products
Abstract
An aircraft capable of vertical take-off and landing is provided. The aircraft includes a fuselage having a forward portion and an aft portion. A lift fan extends though a duct, which extends through the fuselage. The aircraft further includes a pair of wing sets where each set of wings include first and second wings. Each set of wings has a first wing with a first wing root interconnected to the fuselage forward of a central axis of the lift fan and a second wing having a second wing root interconnected to the fuselage aft of the central axis of the lift fan. The tips of each set of wings are connected. The aircraft further includes a pusher fan.
60 Citations
27 Claims
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1. An aircraft capable of vertical takeoff and landing, stationary flight and forward flight, comprising:
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a fuselage having a forward portion, an aft portion, a top surface and a bottom surface; a duct extending vertically through said fuselage, said duct including an inlet on said top surface of the fuselage and an outlet on the bottom surface of said fuselage; a lift fan having first and second counter rotating rotors disposed within said duct, the rotational axis of said rotors defining a vertical reference axis, wherein said first and second counter rotors define a toroidal fan, wherein a diameter of a hub of said toroidal fan is larger than a blade length of said first and second rotors and wherein an area below said hub of said toroidal fan forms a payload bay for said aircraft; at least one engine operative to rotate said rotors; and a pair of wing sets, wherein each wing set includes; a first wing having a wing root connected to said fuselage forward of said vertical reference axis; and a second wing having a wing root connected to said fuselage aft of said vertical reference axis, wherein a distal portion of said first and second wings are connected. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13, 14, 15, 16, 17, 18, 19, 20, 21, 22, 23, 24, 25, 26)
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27. An aircraft capable of vertical takeoff and landing, stationary flight and forward flight, comprising:
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a fuselage having a forward portion, an aft portion, a top surface and a bottom surface; a duct extending vertically through said fuselage, said duct including an inlet on said top surface of the fuselage and an outlet on the bottom surface of said fuselage; a lift fan having first and second counter rotating rotors disposed within said duct, the rotational axis of said rotors defining a vertical reference axis; at least one pair of puffer jets, wherein said puffer jets are connected to said lift fan via ducting; at least one engine operative to rotate said rotors; and a pair of wing sets, wherein each wing set includes; a first wing having a wing root connected to said fuselage forward of said vertical reference axis; and a second wing having a wing root connected to said fuselage aft of said vertical reference axis, wherein a distal portion of said first and second wings are connected.
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Specification