Variable volume combustor with aerodynamic fuel flanges for nozzle mounting

The present application provides a combustor for use with a gas turbine engine. The combustor may include a number of micro-mixer fuel nozzles and a fuel injection system for providing a flow of fuel to the micro-mixer fuel nozzles. The fuel injection system may include a number of support struts su...

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Bibliographic Details
Main Authors Johnson Thomas Edward, McConnaughhay Johnie Franklin, Keener Christopher Paul, Ostebee Heath Michael
Format Patent
LanguageEnglish
Published 20.09.2016
Subjects
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