Methods for fabricating solid laminate stringers on a composite panel

Number of patents in Portfolio can not be more than 2000

United States of America

PATENT NO 12220890
APP PUB NO 20210252817A1
SERIAL NO

16793559

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Abstract

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A method of fabricating a solid laminate stringer on a composite panel, including unspooling one or more composite layers onto the composite panel; compacting the one or more composite layers unspooled onto the composite panel; cutting the one or more composite layers unspooled onto the composite panel; and curing the one or more composite layers unspooled onto the composite panel, wherein the one or more composite layers are unspooled continuously along a length corresponding to a length of the solid laminate stringer.

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Patent Owner(s)

  • THE BOEING COMPANY

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Cheng, Jiangtian Mukilteo, US 24 62

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