Combustor for a turbine engine having a fuel-air mixer including a set of mixing passages

Number of patents in Portfolio can not be more than 2000

United States of America

PATENT NO 12215866
APP PUB NO 20230266009A1
SERIAL NO

17734469

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Abstract

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A turbine engine can include a compressor section, a combustion section, and a turbine section in axial flow arrangement. The combustion section can include a combustor having a fuel-air mixer. The fuel-air mixer can include a body with at least an air passage, as well as a set of mixing passages.

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Patent Owner(s)

  • GENERAL ELECTRIC COMPANY

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Chiranthan, R Narasimha Bengaluru, IN 30 20
Giridharan, Manampathy G Evendale, US 51 773
Naik, Pradeep Bengaluru, IN 143 287
Patra, Ajoy Bengaluru, IN 52 37
Vukanti, Perumallu Bengaluru, IN 85 132

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