"Low NOx Flameless Combustion for Jet Engines and Gas turbines"
"Low NOx Flameless Combustion for Jet Engines and Gas turbines"
"Low NOx Flameless Combustion for Jet Engines and Gas turbines"
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MODIFIED CONCEPTConventional <strong>Flameless</strong> <strong>for</strong> <strong>Gas</strong>TurbineInletMaincombustionExhaust14-18% O2New design <strong>for</strong>Aero-engineHeat extraction21 % O2InletMaincombustionExhaustADVANTEGEOUS:•COOLER FLAME•NEED FOR LOWERRECIRCULATION RATIO5-8 % O29 th Israeli Symposium on <strong>Jet</strong><strong>Engines</strong> <strong>and</strong> <strong>Gas</strong> Turbines,October 7 2010,Technion, IstarelMODIFIED FLAMELESS COMBUSTOR WITHINTERNAL HEAT EXCHANGER.29Turbo <strong>and</strong> <strong>Jet</strong>Engine LaboratoryTechnion – Israelwww. jet-engine-lab.technion.ac.il
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