Fuselage structure for accommodating tails and canards of different sizes and shapes

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United States of America Patent

PATENT NO 9849966
SERIAL NO

14975115

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Abstract

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An aircraft includes a fuselage with structural interfaces for connection to any one or more of a variety of vertical tails, horizontal tails and canards. Vertical tails, horizontal tails and/or canards of different sizes, shapes, sweep angles, box chords, and/or root chords may connect to the fuselage without changing the structural layout or configuration of the fuselage structural interfaces.

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Patent Owner(s)

Patent OwnerAddress
THE BOEING COMPANY100 N RIVERSIDE CHICAGO IL 60606

International Classification(s)

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Schmidt, Gregory M Lake Forest Park, US 4 10
Walton, Samuel Thomas Seattle, US 1 0

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