Methods and components for wing-to-fuselage integration

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United States of America Patent

PATENT NO 9828083
SERIAL NO

14541379

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ATTORNEY / AGENT: (SPONSORED)

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Abstract

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A method for wing-to-fuselage integration is disclosed. The method includes attaching a fitting to a wing box assembly of an aircraft at an early stage of integration and then attaching the fitting to a stub beam attached to a fuselage panel of the aircraft at a later stage of integration. The fitting eliminates the need to attach the stub beam directly to the wing box assembly.

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Patent Owner(s)

Patent OwnerAddress
THE BOEING COMPANY100 N RIVERSIDE CHICAGO IL 60606-1596

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Adedeji, Oladele A Lynnwood, US 2 0
Erickson, Marcus A Snohomish, US 3 22
Lockin, Charles B Bothell, US 4 3
Puzey, Kevin R Lake Stevens, US 2 0

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