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DOE OSTI · 1324683

Variable volume combustor with nested fuel manifold system

McConnaughhay, Johnie Franklin·Keener, Christopher Paul·Johnson, Thomas Edward·Ostebee, Heath Michael
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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, a fuel manifold system in communication with the micro-mixer fuel nozzles to deliver a flow of fuel thereto, and a linear actuator to maneuver the micro-mixer fuel nozzles and the fuel manifold system.

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BibTeXRIS

McConnaughhay, Johnie Franklin, Keener, Christopher Paul, Johnson, Thomas Edward, Ostebee, Heath Michael. 2016-09-13. Variable volume combustor with nested fuel manifold system. https://www.osti.gov/biblio/1324683

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