De-ice system and apparatus for turbine engines

Number of patents in Portfolio can not be more than 2000

United States of America

PATENT NO 12253025
SERIAL NO

18588257

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Abstract

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A turbine engine includes a turbomachine having a compressor section, a combustion section, and a turbine section in serial flow order and together defining a working gas flow path; a thermal system operable with the turbomachine; a heat exchanger in fluid communication with the thermal system; and a plurality of elongated delivery devices in fluid communication with the compressor section of the turbomachine. The plurality of elongated delivery devices are configured to deliver a fluid from the compressor section to a surface of the heat exchanger.

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Patent Owner(s)

  • GENERAL ELECTRIC COMPANY

International Classification(s)

Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Rambo, Jeffrey Douglas Mason, US 100 506

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