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DOE OSTI · 1346054

Variable volume combustor with aerodynamic support struts

Abstract

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 supporting the fuel nozzles and providing the flow of fuel therethrough. The support struts may include an aerodynamic contoured shape so as to distribute evenly a flow of air to the micro-mixer fuel nozzles.

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BibTeXRIS

Ostebee, Heath Michael, Johnson, Thomas Edward, Stewart, Jason Thurman, Keener, Christopher Paul. 2017-03-07. Variable volume combustor with aerodynamic support struts. https://www.osti.gov/biblio/1346054

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