Oblique blended wing body aircraft

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United States of America Patent

PATENT NO 9440740
SERIAL NO

13784438

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ATTORNEY / AGENT: (SPONSORED)

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Abstract

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An oblique wing aircraft designed for reduced surface area to volume ratio. The aircraft has an oblique wing comprising a forward swept wing segment and an aft swept wing segment. A center oblique airfoil section connects the forward and aft swept wing segments. The center oblique airfoil section has a larger chord near its centerline than the chords of either of the forward or aft swept wing segments. The chord of the center oblique airfoil section tapers down more rapidly than the forward or aft wing segments as the center oblique airfoil section extends outboard toward the forward and aft swept wings. Preferably, the aircraft is an all-wing aircraft.

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Patent Owner(s)

Patent OwnerAddress
ADVANCED PRODUCT DEVELOPMENT LLCST LOUIS MO 63131

International Classification(s)

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
McDonnell, William Randall St. Louis, US 7 54

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