Internally stiffened composite panels and methods for their manufacture

Number of patents in Portfolio can not be more than 2000

United States of America Patent

PATENT NO 8128028
APP PUB NO 20100252681A1
SERIAL NO

11626766

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ATTORNEY / AGENT: (SPONSORED)

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Abstract

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Internally stiffened composite panels and associated manufacturing methods. An internally stiffened composite panel can include a first face sheet, a second face sheet offset from the first face sheet, and at least one core portion sandwiched between the first and second face sheets. The composite panel can further include a stiffener disposed between the first and second face sheets adjacent to the core portion. The stiffener can have a first attachment portion attached to the first face sheet, a second attachment portion attached to the second face sheet, and an intermediate portion extending between the first and second attachment portions. One or both of the first and second attachment portions can be configured to engage a fastener, such as a blind fastener, for attaching a part to the composite panel.

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Patent Owner(s)

  • THE BOEING COMPANY

International Classification(s)

Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Grillos, Emmanuel J Bellevue, US 2 64

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