[go: up one dir, main page]

Padwal et al., 2016 - Google Patents

Experimental characterization of gelled Jet A1 spray flames

Padwal et al., 2016

Document ID
9430697393797201199
Author
Padwal M
Mishra D
Publication year
Publication venue
Flow, Turbulence and Combustion

External Links

Snippet

Gelled propellants provide energetic performance similar to conventional liquid propellants and safety during storage and handling like a solid propellant. Experiments on unconfined gelled Jet A1 spray flames and the comparison with ungelled spray flames are reported for …
Continue reading at link.springer.com (other versions)

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23DBURNERS
    • F23D11/00Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space
    • F23D11/36Details, e.g. burner cooling means, noise reduction means
    • F23D11/44Preheating devices; Vaporising devices
    • F23D11/441Vaporizing devices incorporated with burners
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/28Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • F23R3/286Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply having fuel-air premixing devices
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/02Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/04Air inlet arrangements
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23DBURNERS
    • F23D14/00Burners for combustion of a gas, e.g. of a gas stored under pressure as a liquid
    • F23D14/46Details, e.g. noise reduction means
    • F23D14/62Mixing devices; Mixing tubes
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23CCOMBUSTION APPARATUS USING FLUENT FUEL
    • F23C6/00Combustion apparatus characterised by the combination of two or more combustion chambers or combustion zones, e.g. for staged combustion
    • F23C6/04Combustion apparatus characterised by the combination of two or more combustion chambers or combustion zones, e.g. for staged combustion in series connection
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23CCOMBUSTION APPARATUS USING FLUENT FUEL
    • F23C2900/00Special features of, or arrangements for combustion apparatus using fluid fuels or solid fuels suspended in air; Combustion processes therefor
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23DBURNERS
    • F23D2900/00Special features of, or arrangements for burners using fluid fuels or solid fuels suspended in a carrier gas
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23CCOMBUSTION APPARATUS USING FLUENT FUEL
    • F23C7/00Combustion apparatus characterised by arrangements for air supply
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23CCOMBUSTION APPARATUS USING FLUENT FUEL
    • F23C2203/00Flame cooling methods otherwise than by staging or recirculation
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23DBURNERS
    • F23D2206/00Burners for specific applications
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R2900/00Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23CCOMBUSTION APPARATUS USING FLUENT FUEL
    • F23C99/00Subject-matter not provided for in other groups of this subclass

Similar Documents

Publication Publication Date Title
Schefer Hydrogen enrichment for improved lean flame stability
Padwal et al. Experimental characterization of gelled Jet A1 spray flames
Zhang et al. Combustion and emissions characteristics of dual-channel double-vortex combustion for gas turbine engines
Shen et al. Combustion characteristics of ignition processes for lean premixed swirling combustor under visual conditions
Wang et al. Effects of confinement length of the central toroidal recirculation zone partly confined by the small pilot stage chamber on ignition characteristics
Huang et al. Experimental investigation on spray and ignition characteristics of plasma actuated bluff body flameholder
Hwang et al. An experimental study on flame stability and pollutant emission in a cyclone jet hybrid combustor
Garai et al. Experimental investigation of spray characteristics of kerosene and ethanol-blended kerosene using a gas turbine hybrid atomizer
Li et al. Effects of fuel injection on the combustion and emission performance of a trapped vortex combustor
Wei et al. Experimental study of combustion instability and emission characteristics of ethanol/ammonia co-firing swirl flame
Wang et al. Combustion and emission performance of a trapped-vortex gas turbine combustor fueled by RP-3 kerosene
Kasabov et al. Experimental study on lifted flames operated with liquid kerosene at elevated pressure and stabilized by outer recirculation
Pourhoseini et al. Effect of water–Kerosene emulsified fuel on radiation, NO x emission and thermal characteristics of a liquid burner flame in lean combustion regime
Burguburu et al. Effects of H2 enrichment on flame stability and pollutant emissions for a kerosene/air swirled flame with an aeronautical fuel injector
Sharma et al. Combustion Characteristics of a Peripheral Vortex Reverse Flow Combustor With Coaxial Fuel Injection
Zeng et al. Effect of confinement on combustion characteristics in lean direct injection combustion system
WO2019159921A1 (en) Fuel combustion device and combustion method
Archer et al. The role of confinement on flow dynamics under fuel lean combustion conditions
CN117571913A (en) Experimental-grade ammonia coal combustion test system and combustion control method for industrial boilers
Ahmad et al. Experimental investigation of a Jet-A1 fuelled peripheral vortex reverse flow combustor
Zhang et al. Influence of air-assisted atomizer structure on ignition and flame propagation in a trapped-vortex cavity
Biswal et al. Characterization of Flame Morphology for Twin Fluid Atomizer-Based Swirl Stabilized Combustor
Xie et al. Ethanol spray tubular flame established in a swirling air flow
Zhu et al. Experimental investigation on dynamics of spray atomization, ignition, and flame propagation in an annular combustor
JP2004053144A (en) In-cylinder swirl combustor