Aircraft panel assembly

Number of patents in Portfolio can not be more than 2000

United States of America

PATENT NO 12162600
APP PUB NO 20220024556A1
SERIAL NO

17298501

Stats

ATTORNEY / AGENT: (SPONSORED)

Importance

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Abstract

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An aircraft panel assembly with a panel and a plurality of stiffeners on the panel is disclosed. Each stiffener has an attachment part attached to the panel and a structural part spaced apart from the panel. A rib foot beam crosses the stiffeners at a series of intersections. At each intersection the rib foot beam is located between the panel and the structural part of a respective one of the stiffeners.

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First Claim

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Patent Owner(s)

Patent OwnerAddress
AIRBUS OPERATIONS LIMITEDBRISTOL BS34 7PA

International Classification(s)

Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Gaitonde, John Martin Bristol, GB 5 4
Heaysman, Chris Bristol, GB 5 4
Seegel, Hauke Hamburg, DE 31 75

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