Vertical take-off and landing (VTOL) winged air vehicle with complementary angled rotors
First Claim
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1. A method comprising:
- providing substantially equal thrust to a top port motor, a bottom port motor, a top starboard motor, and a bottom starboard motor of a vertical takeoff and landing (VTOL) aircraft to achieve a vertical take-off, wherein the top and bottom port motors are disposed at a first end of a wing, wherein the top and bottom starboard motors are disposed at a second end of the wing distal from the first end of the wing, wherein the top and bottom starboard motors are angled away from each other within a first plane generally perpendicular to a plane of the wing; and
wherein the top and bottom port motors are angled away from each other within a second plane generally perpendicular to the plane of the wing;
increasing thrust to the top motors, and decreasing thrust to the bottom motors to produce a net moment about a center of mass of the VTOL aircraft and cause the aircraft to pitch forward; and
increasing thrust to the top motors, and increasing thrust to the bottom motors to achieve horizontal flight, wherein the wing of the VTOL aircraft provides primary lift in horizontal flight.
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Abstract
Systems, devices, and methods for an aircraft having a fuselage (110); a wing (120) extending from both sides of the fuselage; a first pair of motors (132b, 133b) disposed at a first end of the wing; and a second pair of motors (142b, 143b) disposed at a second end of the wing; where each motor is angled (381, 382, 391, 392) to provide a component of thrust by a propeller (134, 135, 144, 145) attached thereto that for a desired aircraft movement applies a resulting torque additive to the resulting torque created by rotating the propellers.
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Citations
20 Claims
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1. A method comprising:
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providing substantially equal thrust to a top port motor, a bottom port motor, a top starboard motor, and a bottom starboard motor of a vertical takeoff and landing (VTOL) aircraft to achieve a vertical take-off, wherein the top and bottom port motors are disposed at a first end of a wing, wherein the top and bottom starboard motors are disposed at a second end of the wing distal from the first end of the wing, wherein the top and bottom starboard motors are angled away from each other within a first plane generally perpendicular to a plane of the wing; and
wherein the top and bottom port motors are angled away from each other within a second plane generally perpendicular to the plane of the wing;increasing thrust to the top motors, and decreasing thrust to the bottom motors to produce a net moment about a center of mass of the VTOL aircraft and cause the aircraft to pitch forward; and increasing thrust to the top motors, and increasing thrust to the bottom motors to achieve horizontal flight, wherein the wing of the VTOL aircraft provides primary lift in horizontal flight. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13, 14, 15, 16, 17, 18, 19, 20)
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Specification