Methods and apparatus for monitoring and fixing holes in composite aircraft

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United States of America Patent

PATENT NO 9586699
SERIAL NO

14167766

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Abstract

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Methods and apparatus are described for repairing a damaged area of an airplane fuselage made from fiber-reinforced composite material. In one embodiment, an intelligent patch is provided comprising a first electronic communication device to communicate information from at least one sensor regarding the presence of compression induced microfractures within the patch.

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Patent Owner(s)

Patent OwnerAddress
SMART DRILLING AND COMPLETION INC3123 - 198TH PLACE S E BOTHELL WA 98012

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Skerl, Tomislav Houston, US 8 46
Vail,, III William Banning Bothell, US 25 279

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