Hybrid carbon/fiberglass structural component for an aircraft

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United States of America Patent

PATENT NO 10131417
APP PUB NO 20180304983A1
SERIAL NO

15495152

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Abstract

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A hybrid carbon/fiberglass structural component or beam for an aircraft is constructed with layers of strips of glass fibers interspersed with layers of strips of unidirectional carbon fibers where the carbon fibers are oriented only in alignment with or along the longitudinal direction of the length of the beam thereby adding strength and stiffness to the beam while reducing weight and manufacturing costs.

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Patent Owner(s)

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

International Classification(s)

Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Andrews, Francis E Everett, US 6 59
Kismarton, Max U Renton, US 74 1026
Knowles, Devin E Kenmore, US 2 0

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