Vertical take-off and landing (VTOL) winged air vehicle with complementary angled rotors

Number of patents in Portfolio can not be more than 2000

United States of America Patent

PATENT NO 10370095
APP PUB NO 20180002003A1
SERIAL NO

15612671

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ATTORNEY / AGENT: (SPONSORED)

Importance

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Abstract

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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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First Claim

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Patent Owner(s)

  • AEROVIRONMENT, INC.

International Classification(s)

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Lindsey, Quentin Canoga Park, US 12 36
Won, Henry Thome Simi Valley, US 13 68

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