High temperature composite inlet

Number of patents in Portfolio can not be more than 2000

United States of America Patent

PATENT NO 9771866
APP PUB NO 20160305321A1
SERIAL NO

14609254

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Abstract

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An inlet for an aircraft nacelle may comprise a nanoreinforced polyimide composite lip skin. The nanomaterials may increase thermal conductivity and decrease microcracking in the lip skin. A lip skin for an inlet with an electric heater may comprise a surface layer, an outer composite skin, an electric heater, an inner composite skin, and a thermal barrier coating. A lip skin for an inlet with a pneumatic deicing system may comprise a surface layer, a composite skin, and a thermal barrier coating.

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Patent Owner(s)

Patent OwnerAddress
ROHR INC850 LAGOON DRIVE CHULA VISTA CA 91910

International Classification(s)

Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Kruckenberg, Teresa La Mesa, US 14 53
Pujar, Vijay V San Diego, US 77 197

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