“…Also note that all of these values considering that the best NOx reduction value at the three conditions W/F ratio 0.2, 0.3 and 0.4 is at injected water inclination angle 45° due to the explained reason before. The results are in agreement practically with Ayed et al, [16] and Luo et al, [17].…”
Section: Effect Of Nox With Different Lpg Fuel Flowrates At Fixed W/fsupporting
confidence: 92%
“…It provides the air to the combustion chamber for a fuel burning combustion. The discharge from the air compressor end is connected with the primary air pipe which is fitted into the fuel nozzle pipe by 45 degree angle and 10 cm before the nozzle tips, the connection is through a flexible hose and an air control valve (17) to adjust the inlet air for the combustion process and measured the air flowrate with a similar rotameter of the gas fuel as well [23]. For the water injection kit, the water is injected through a clean glucose lashes with a calibrated ruler from 1 to 500 mm/min (18) and hanged on an ironed stand with a height 130 cm from the injection point to be simulated as a head tank [21].…”
Section: Fig 1 Schematic Of the Experimental Test Rigmentioning
Direct Water Injection (DWI) is commonly used in many nitrogen oxides (NOx) emissions control applications due to its effect to reduce the adiabatic flame temperature. In this paper an experimental test rig is designed to study the effect of water injection spray inside a simulated gas turbine combustor from the gas fuel. The practical work introduced by the chemical reaction methodology followed by the experiment which was presented and discussed carefully. Results are obtained in term of the exhaust gas temperature and different injection parameters including position, direction and fuel mass flow rate on the nitrogen oxide emission value in PPM (Parts per Million) at different conditions. The results showed that the best water injection effect was obtained at 45° degree inside the primary air zone. Injection location has a major effect on the NOx reduction as the best injected location is the Primary air zone compared with the direct fuel nozzle tip due to the increase of the water droplets residence time inside the combustor and perform a vortex that will affect the reduction of exhaust gas temperature and NOx emission respectively. The huge impact was observed at LPG (Liquefied Petroleum gas) flowrate 2.7L/min and water to fuel ratio about 0.4 as the NOx value was decreased about 73% from almost 381 PPM to 73 PPM. The chemical reaction arrangement order methodology presented good agreement with the experimental results at different fuel flow rate and equivalence ratio. The chemical Reaction equations were implemented to calculate the different adiabatic flame temperatures which is experimentally known as the exhaust gas temperature and impacted directly the NOx emission results.
“…Also note that all of these values considering that the best NOx reduction value at the three conditions W/F ratio 0.2, 0.3 and 0.4 is at injected water inclination angle 45° due to the explained reason before. The results are in agreement practically with Ayed et al, [16] and Luo et al, [17].…”
Section: Effect Of Nox With Different Lpg Fuel Flowrates At Fixed W/fsupporting
confidence: 92%
“…It provides the air to the combustion chamber for a fuel burning combustion. The discharge from the air compressor end is connected with the primary air pipe which is fitted into the fuel nozzle pipe by 45 degree angle and 10 cm before the nozzle tips, the connection is through a flexible hose and an air control valve (17) to adjust the inlet air for the combustion process and measured the air flowrate with a similar rotameter of the gas fuel as well [23]. For the water injection kit, the water is injected through a clean glucose lashes with a calibrated ruler from 1 to 500 mm/min (18) and hanged on an ironed stand with a height 130 cm from the injection point to be simulated as a head tank [21].…”
Section: Fig 1 Schematic Of the Experimental Test Rigmentioning
Direct Water Injection (DWI) is commonly used in many nitrogen oxides (NOx) emissions control applications due to its effect to reduce the adiabatic flame temperature. In this paper an experimental test rig is designed to study the effect of water injection spray inside a simulated gas turbine combustor from the gas fuel. The practical work introduced by the chemical reaction methodology followed by the experiment which was presented and discussed carefully. Results are obtained in term of the exhaust gas temperature and different injection parameters including position, direction and fuel mass flow rate on the nitrogen oxide emission value in PPM (Parts per Million) at different conditions. The results showed that the best water injection effect was obtained at 45° degree inside the primary air zone. Injection location has a major effect on the NOx reduction as the best injected location is the Primary air zone compared with the direct fuel nozzle tip due to the increase of the water droplets residence time inside the combustor and perform a vortex that will affect the reduction of exhaust gas temperature and NOx emission respectively. The huge impact was observed at LPG (Liquefied Petroleum gas) flowrate 2.7L/min and water to fuel ratio about 0.4 as the NOx value was decreased about 73% from almost 381 PPM to 73 PPM. The chemical reaction arrangement order methodology presented good agreement with the experimental results at different fuel flow rate and equivalence ratio. The chemical Reaction equations were implemented to calculate the different adiabatic flame temperatures which is experimentally known as the exhaust gas temperature and impacted directly the NOx emission results.
“…The DRG method was first applied to a model system of ethylene combustion (Lu and Law 2005;Luo et al 2011) with a full scheme of 70 species. A value of ε of 0.16 gave a skeleton scheme of 33 species, i.e.…”
“…The DRGEP approach has been applied adaptively in order to produce on-the-fly reduced mechanisms for n-heptane (Shi et al 2010b) and gasoline surrogate mixtures (Liang et al 2009b;Shi et al 2010a) in simulations of homogeneous charge compression ignition. Other applications of the DRG method and its extensions to skeletal model reduction include modelling the high-temperature combustion of H 2 /CO/C 1 ÀC 4 hydrocarbons (Wang 2013), methane oxidation (Jiang and Qiu 2009), nitrogen oxide emissions and their control (Lv et al 2009;Luo et al 2011), the combustion of n-heptane (Liang et al 2009a;Wang et al 2013;Bahlouli et al 2014), surrogate jet fuels (Naik et al 2010), methyl decanoate (a large methyl ester used as a surrogate for biodiesel, (Seshadri et al 2009)), surrogate biofuels (Luo et al 2010a, b;Malik et al 2013) and the oxidation of iso-octane (Kelley et al 2011). The number of species required in the locally reduced models varies throughout the calculations but reaches a maximum of about one third of the number of initial species.…”
“…However, methane (CH 4 ) and ethylene (C 2 H 4 ) are short chain hydrocarbons that are major products resulting from thermally cracked kerosene. Additionally, fuel components with dramatically different chemical properties such as methane and ethylene can be used as surrogate mixtures for more complex fuels (Luo et al, 2011). As a result methane and ethylene are often used as surrogate fuels in both simulations and experimentation (Wu et al, 2017).…”
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