"Low NOx Flameless Combustion for Jet Engines and Gas turbines"

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10090807060504020252015present3020100Noise (dB)Nox, CO, UHC(%)FuelConsumption(%)MaintananceCost (%)2025present• NOx, CO & UHC emissions are to be reduced by 70% by year2015 and 80% by year 2025• Fuel Consumption & CO 2 emission to be cut by 15% by year 2015and 25% by year 202520159 th Israeli Symposium on JetEngines and Gas Turbines,October 7 2010,Technion, IstarelAnticipated Future Projections ofEngine performance2Turbo and JetEngine LaboratoryTechnion – Israelwww. jet-engine-lab.technion.ac.il
Page 5 and 6: ppm NOx200 ..........…100........
Page 9: FLAMELESS OXIDATION METHOD FOR NOx
Page 12 and 13: NormalCombustionTemp. of Reactants
Page 14 and 15: INDICATIONS OF INCOMPLETE COMBUSTIO
Page 16 and 17: 9 th Israeli Symposium on JetEngine
Page 18: 9 th Israeli Symposium on JetEngine
Page 21 and 22: 9 th Israeli Symposium on JetEngine
Page 23 and 24: PRELIMINARY DESIGN MODIFICATIONSCOM
Page 25 and 26: • FLOXCOM COMBUSTOR HAS LARGE STA
Page 27 and 28: Mesh of simulated regionVelocity fi
Page 29 and 30: MODIFIED CONCEPTConventional Flamel
Page 31 and 32: פתח הזרמתאוויראזור
Page 33 and 34: DIFFUSIONFLAMELESS9 th Israeli Symp
Page 35 and 36: To outletCH 4inletAir inlet| | | |
Page 37 and 38: RECIRCULATION REGIONTo outlet9 th I
Page 39 and 40: T KexperimentsimulationTHERE IS STI
Page 41 and 42: LNG/ LH2 Main Combustor Kerosene/ B
Page 43 and 44: GE-90U 2 C T 1 c 1 P c9'9' n ' p
Page 45 and 46: T2 T3[ x3] [ x3]T1[ x3]Air InExhaus

"Low NOx Flameless Combustion for Jet Engines and Gas turbines"

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