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IRJET- Performance Analysis of 4-Stroke SI Engine with HHO Generator by Morse Test
1.
International Research Journal
of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 05 Issue: 11 | Nov 2018 www.irjet.net p-ISSN: 2395-0072 © 2018, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 1001 Performance Analysis of 4-stroke SI Engine with HHO Generator by Morse Test Prof. Mrs. Namrata V. Lotia1, Zeeshan Jamal2, Jafar Sadique3, M. Mohsin Raza4 1,2,3,4Anjuman college of Engg. and Technology, Rastrasant Tukdoji Maharaj Nagpur University, Maharashtra, India ---------------------------------------------------------------------***--------------------------------------------------------------------- Abstract – Earth today is facing the increasing cost of gasoline and other oil products. Automotive innovators and manufacturers are working to increase vehicle mileage while still meeting today’s strict emissions and greater power requirements. An efficient way to increase the fuel economy and power of the engine is to add hydrogen to the air/fuel mixture in a conventional SI engine. In this work, the performance of an SI engine powered with petrol and HHO as fuel supplement was compared with only gasoline-fuelled engine using Morse Test. To study the effect we constructed a simple integrated HHO generation system and evaluated the effect of hydroxyl gas (HHO) addition, as an engine performance improver, into gasoline fuel on engine. HHO cell was designed, fabricated and for appropriate HHO gas productivity per input power. The performancewasmeasured in terms of the engine torque (T), brake power (BP), thermal efficiency (ƞth), brake specific fuel consumption (BSFC) by utilizing Morse Test Method The Hydroxyl gas (HHO) was produced by the process electrolysis using Potassium hydroxide (KOH) in a leak proof cylindrical chamber. Utilizing an on board integrated generation system of the gas reduces the risk of storage (hydrogen is highly inflammable and its leak is undetectable). At economy and higher engine speeds the HHO system with petrol fuel yields higher engine efficiency and reduced fuel consumption compared to pure petrol fuelled engine operation. Key Words: Morse Test, 4-Storke SI Engine,HHOGenerator, Heat Balance Sheet, Thermal and Mechanical Efficiency. 1. INTRODUCTION There are different possible solutions for the problem of using fossil fuels, but most of them would require years of development and research. This method involves burning hydrogen gas along with hydrocarbon fuels in engine. Combustion of fossil fuels has caused serious problems to the environment and most adverse effect of combustion on environment by fossils fuel combustion are emission of NOx, CO, CO2, and unburned hydrocarbons which leads to ozone depletion. Hydrogen has long been considered as a fuel entirely from the plethora of renewable resource water with some unique and desirable properties, for application as a fuel in engines. It is the only fuel that can be produced, through the expenditure of relatively much energy. Hydrogen combustion in oxygen produces onlywater.Theseattributes makes it an excellent fuel to significantlymeettheincreasing strict environmental controls of exhaust emissions from combustion engines, including the reduction of greenhouse gases that are emitted. The use of H2 with conventional fuels offers reduction in exhaust gas emission and also opportunities of optimizing engine performance. The use of Hydrogen helps to reduce their use and hence prevent the depletion of these non-renewable fossil fuels. The principle of this type of combustion is to add a proportion of hydrogen gas to the combustion reactions of spark ignition engines. The theory of this concept is that the addition of hydrogen as a supplement to the fuel can increase lean operation limit, improve the lean burn ability, and decrease burn duration. Thus the use of hydrogen in IC engines not only help in increasing the efficiency of it but also to reduce pollution and suppress the toxic gases like carbon monoxide, nitrous oxide emission etc.. 1.1 MORSE TEST The Indicated Power (IP) andthe mechanicalefficiencyof a multi-cylinder SI engine is calculated by this method. During the test the engine is run at a constant speed (3000 rpm in our test) and at the same throttle opening. First the Brake Power (BP) of the engine withallcylindersoperativeis measured with the help of a dynamometer. Now, the Brake power of the engine is measured witheachcylinderrendered in cut off position one by one by shorting the spark plug of that particular cylinder. When any cylinder is cut off, the speed goes down. Before taking any reading, the initial speed must be restored by adjusting the load. Consider the case of a 4-cylinder engine. Let, BP= Brake power of the engine with all cylinder in operation BP1= BP of the engine with cylinder no. 1 cut off BP2= BP of the engine with cylinder no. 2 cut off BP3= BP of the engine with cylinder no. 3 cut off BP4= BP of the engine with cylinder no. 4 cut off IP1, IP2, IP3 and IP4 = IP of the engine 1, 2, 3, 4 cut off FP1 FP2 FP3 and FP4 = Frictional power loss of cylinder 1, 2, 3, 4 respectively
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International Research Journal
of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 05 Issue: 11 | Nov 2018 www.irjet.net p-ISSN: 2395-0072 © 2018, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 1002 Therefore when all cylinder are operative then, BP = (IP1 – FP1) + (IP2 –FP2) + (IP3 –FP3) + (IP4 – FP4) = (IP1 +IP2 + IP3 + IP4) – (FP1 +FP2 +FP3 +FP4) When cylinder No.1 is cut off, it does not develop any power on the contrary; some power is lost due to friction between cylinder and piston. Then, BP1= (IP2 +IP3 + IP4) – (FP1 +FP2 +FP3+FP4) From the above equations, BP – BP1= IP1 Similarly, BP – BP2= IP2 BP – BP3= IP3 and BP – BP4= IP4 Therefore, total IP of the engine= IP1 +IP2 + IP3 + IP4 = IP and mechanical efficiency is BP/IP. When the Morse test is carried out following precautions must be taken: The Brake Power(BP) should be measured as soon as possible after making cylinder cut off The dynamometer load should be adjusted to bring the speed to its constant value. 2. HHO GENERATOR A HHO Generator is a device that uses the process of electrolysis to convert water into two molesofHydrogenand one mole of Oxygen (HHO). This gas, also known as Brown's Gas, is a very cheap and clean, powerful fuel. Efficient HHO Generators are capable of using Distilled Water only, but most HHO Generators used an electrolyte, or catalyst in addition to the distilled water. The most easily available and cheap catalyst is potassium hydroxide KOH. Water + KOH +Electric current = clean, cheap fuel Through the simple process of running electric current through the water, the atoms 'split' back into their original elemental forms. This process is known as electrolysis. Electrical current runs through the water and all the Hydrogen atoms run towards the negatively charged electrode. Any HHO generator simply adds 'free' hydrogen and oxygen in a gaseous stateto the combustionprocess.The mixture of this burns so hot, and so fast, it helps to COMPLETE the combustion process of the original gasoline. Fig 1: HHO Generator with bubbler arrangement When water is introduced with electrical current/voltage it has a tendency to become excited and divides into its primary elements of Hydrogen and Oxygen. The produced Hydrogen and Oxygen are now in a gaseous state from the liquid water. It's been said by others that the two elements have been split apart from one another into their sub- diatomic molecular state. The process is as follows, you start with water and Potassium Hydroxide. DC current is passed through the solution, the H2O breaks into H2 and O (we call it HHO). HHO is introduced into the engine by use of the engines vacuum. The HHO combines with the gasoline and air in the carburetor and is burnt in the combustion chamber. After combustion, it converts to H2O. Since, the hydrogen gas is highly inflammable, odorless and colorless, it becomes difficult to detect its leak. As a preventive measure, we installed a bubbler just after the electrolytic cell. The bubbler is filled with regular water and works as a shield between gas source and possibility of any spark from the engine, which may lead to any fire and explosion in the electrolytic cell. It also useful in controlling the amount of HHO gas to the engine. The actual HHO generator is shown in Fig 2. Fig 2: Actual HHO generator 3. EXPERIMENTAL SETUP The Experimental setup consists of a 4-Stroke four- Cylinder Maruti Esteem VXI Engine. The carburetor of the engine is connected with HHO intake hose pipewhichcomes directly from the electrolytic generator.Fuel issuppliedfrom the petrol tank to a burette to measure the quantity of fuel supplied to the engine. The line diagram of the experimental Kit can be seen in fig 3.
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International Research Journal
of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 05 Issue: 11 | Nov 2018 www.irjet.net p-ISSN: 2395-0072 © 2018, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 1003 Fig 3: Line diagram of experimental setup ENGINE SPECIFICATION: Engine : Maruti Esteem VXI Type : 4stroke, 4-Cylinder, SI Engine Cubic Capacity : 1298cc Max Power : 85bhp at 6000rpm Max Torque : 110Nm at 4500rpm Rope brake dynamometerisusedtomeasuretheTorque of the engine. Two spring balances are attached to the rope at the tight side and one at the slack side and are tangential to brake drum. The speed is measured with the help of a Digital Tachometer. Readings are taken with and without HHO input to the engine and calculationsaretabulatedin the table Fig 3: Actual experimental setup 4. OBSERVATION TABLE AND CALCULATIONS The test was carried out in the Heat Engine Lab of Anjuman College of Engineering and Technology. The readings were tabulated with the conventional cycle (without HHO) as well as with the addition of HHO with Petrol. Rpm of the shaft was measured with the help of a digital Tachometer and the temperature at the inlet and outlet of cooling water and gases were measured with the help of Thermocouples. The dynamometer has thefollowing dimensions; Dynamometer drum radius (Rd) = 0.118m Thickness of the rope (t) = 0.01m Morse test Sample Calculations: Torque( T ) : T= (W-S)×9.81×(Rd + t2) a) Torque when all cylinders are working T= (133.3-44.2) × 9.81 × 0.123 T= 107.6 Nm b) Torque when 1st cylinder is cut off T1= (93.1-30.7) × 9.81 × 0.123 T1 = 75.2 Nm c) Torque when 2nd cylinder is cut off T2 = (92.4 – 28.7) × 9.81 × 0.123 T2 = 76.7 Nm d) Torque when 3rd cylinder is cut off T3 = (91.1 – 29.9) × 9.81 × 0.123 T3 = 74.3 Nm e) Torque when 4th cylinder is cut off T4= (93.1 – 30.8) × 9.81 × 0.123 T4 = 75.5 Nm Brake Power (BP) = 2πNT/60 Where; N=3000rpm i) Brake power when all cylinders are operating BP = (2π×3000×107.6)/60 BP = 33.8 Kw ii) Brake power when 1st is cut off BP1= (2π×3000×75.2)/60 BP1= 23.6 Kw iii) Brake power when 2nd is cut off BP2= (2π×3000×76.7)/60 BP2= 24 Kw iv) Brake power when 3rd is cut off BP3= (2π×3000×74.3)/60
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International Research Journal
of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 05 Issue: 11 | Nov 2018 www.irjet.net p-ISSN: 2395-0072 © 2018, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 1004 BP3= 23.3 Kw v) Brake power when 4th is cut off BP4= (2π×3000×75.5)/60 BP4= 23.7 Kw Indicated Power (IP) Utilizing Morse Test for calculation of Indicated Power; IP1 = BP - BP1 = 33.8 - 23.6 = 10.2 Kw IP2 = BP – BP2 = 33.8 – 24 = 9.8 Kw IP3 = BP – BP3 = 33.8 – 23.3 = 10.5 Kw IP4 = BP – BP4 = 33.8 – 23.7 = 10.1 Kw Therefore, the total Indicated power is given as IP = IP1 +IP2 + IP3 + IP4 IP = 10.2+9.8+10.5+10.1 IP = 40.6 Kw Table: 1 Calculation table of BP and IP with conventional cycle (Only Petrol) Petrol Sr. No W (kg) S (kg) W-S (kg) Torque (Nm) BP (Kw) IP (Kw) 1 133.3 44.2 89.2 107.6 33.8 40.6 2 93.1 30.7 62.4 75.2 23.6 10.2 3 92.4 28.7 63.7 76.7 24 9.8 4 91.3 29.9 61.4 74.3 23.3 10.5 5 93.1 30.8 62.3 75.5 23.7 10.1 Mechanical Efficiency (ƞmech) Ƞmech = B.P/I.P =33.8/40.6 = 83.25% Fuel Air Ratio (mf/ma) Fuel Air Ratio = mf/ma Where; ma = ρair × Cd × Ao × (2×g×hm×( ( ρm/ρair) – 1) )1/2 Where; ρair = Density of Air (1.16Kg/m3) Cd = Co-efficient of discharge of orifice = 0.65 Ao = Area of Orifice = 1.539×10-3 m2 hm = Manomeric pressure head (0.03m) ρm = Density of Manometric fluid = 1000 Kg/m3 Hence, ρm/ρair = 1000/1.16 = 862.06 Therefore, ma = 1.16×0.62×1.539×10-3×(2×9.81×0.03×((862.06)–1)1/2 ma = 25×10-3 Kg/s mf = 10cc × ρf/Tf Where; ρf = Density of Fuel (0.78 Kg/m3) Tf = Time for 10cc Fuel Consumption = 3.65sec mf = 0.01 × 0.78/3.65 mf = 2.14 × 10-3 Kg/sec Hence; Fuel Air Ratio = mf/ma mf/ma = 0.085 Thermal Efficiency Ƞth = Power/(mf × Cv) Where Cv is the calorific value of fuel (48000 KJ/Kg) Ƞth = 33.8/(2.14 × 10-3 × 48000) Ƞth = 32.8% Brake Specific Fuel Consumption(BSFC) BSFC = mf × 3600/BP = 2.14 × 10-3 × 3600/33.7 = 0.227 Kg/Kw-hr Heat Balance Sheet (Without HHO) The inlet temperature (t1) and outlet temperature (t2) of the cooling water is measured withthehelpof Thermocouple. Similarly t3 and t4 are the inlet and outlet temperature of the exhaust gases when all cylinders are in operating condition. IP = 40.6 Kw BP = 33.8 Kw mf = 2.14 × 10-3 Kg/sec ma = 25×10-3 Kg/s I. Heat Supply (Qs) = mf × Cv = 2.14 × 10-3 × 48000 = 102.72 Kw II. Heat Equivalent to BP = 33.8 Kw III. Heat Carried by Cooling Water = mw × Cp × (t2-t1) = 0.109 × 4.187 × (83.6-72.8) = 4.93 Kw
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International Research Journal
of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 05 Issue: 11 | Nov 2018 www.irjet.net p-ISSN: 2395-0072 © 2018, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 1005 IV. Heat Carried by exhaust gases(Qg) Qg = mg × CPg × (t4 –t3) Where; mg = mf + ma mg = 2.14 × 10-3 + 25×10-3 mg = 0.027 Kg/sec Hence, Qg = 0.027 × 1.005 × (184.8 - 32) = 4.14 Kw V. Un-accounted Heat Loss Qa = Qs – (Sum of losses) = 102.72 – (33.8+4.93+4.14) = 59.85 Kw HEAT BALANCE SHEET (Without HHO) Table: 2 Heat Balance Sheet for petrol (Without HHO) Energy Input Sr. no Particular Quantity (Kw) % 1 Heat Supplied 102.7 100% Energy Output Sr. no Particular Quantity (Kw) % 1 Heat Equivalent to BP 33.8 32.91% 2 Heat Carried By Cooling Water 4.93 4.8% 3 Heat Carried By Exhaust gases 4.14 4.03% 4 Un-accounted heat losses 59.85 58.2% Similarly the whole calculation can be obtained for the cycle with HHO as supplement. Below is the calculation table and heat balance sheet for the combustion cycle with HHO. Table: 3 Calculation table of BP and IP with HHO as supplement Petrol + HHO Sr. No W (kg) S (kg) W-S (kg) Torque (Nm) BP (Kw) IP (Kw) 1 147.8 48.2 99.6 120.1 37.7 45.4 2 100.9 31.8 69.1 83.3 26.1 11.6 3 100.1 30.4 69.7 84.1 26.4 11.3 4 101.1 31.2 69.9 84.3 26.4 11.3 5 100.7 30.7 70.0 84.4 26.5 11.2 Mechanical Efficiency (ƞmech) Ƞmech = B.P/I.P = 37.7/45.4 = 83.04% Fuel Air Ratio (mf/ma) ma = 1.16×0.62×1.539×10-3×(2×9.81×0.03×((862.06)–1)1/2 ma = 25×10-3 Kg/s mf = 10cc × ρf/Tf Where; ρf = Density of Fuel (0.78 Kg/m3) Tf = Time for 10cc Fuel Consumption (4sec) mf = 0.01 × 0.78/4 mf = 1.95 × 10-3 Kg/sec Hence; Fuel Air Ratio = mf/ma mf/ma = 0.0755 and mg = mf + ma mg = 26.95 × 10-3 Kg/sec Brake Specific Fuel Consumption(BSFC) BSFC = mf × 3600/BP = 1.195 × 10-3 × 3600/37.7 = 0.186 Kg/Kw-h HEAT BALANCE SHEET (With HHO) Table: 4 Heat Balance Sheet for petrol (With HHO) Energy Input Sr. no Particular Quantity (Kw) % 1 Heat Supplied 93.6 100% Energy Output Sr. no Particular Quantity (Kw) % 1 Heat Equivalent to BP 37.7 40.2 2 Heat Carried By Cooling Water 5.93 6.33 3 Heat Carried By Exhaust gases 4.29 4.5 4 Un-accounted heat losses 45.68 48.8
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International Research Journal
of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 05 Issue: 11 | Nov 2018 www.irjet.net p-ISSN: 2395-0072 © 2018, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 1006 5. GAS ANALYSIS GRAPHS: The following charts shows the emission of hydrocarbons and carbon monoxidesagainsttheBrakepoweroftheengine. The emission of CO before and after addition of HHO to the fuel is shown in chart 1. It is clear that using a blend of HHO gas reduces the presence of carbon monoxide in the exhaust gas emitted. This is due to reduction in the gasoline consumption. BP vs CO (%volume) 0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 4 8 12 16 Brake Power (Kw) CO(%volume) With HHO without HHO Chart: 1 Brake power vs CO In Chart:2, it is clear that, the unburned hydrocarbons increases with the load. This increase in the hydrocarbons is due to the increase in introduction of fuel in the combustion chamber. Hence, more HC remains unburned and is emitted as exhaust. When HHO is added to the fuel as supplement enhances the fuel oxidation process and result in the complete combustion of the hydrocarbons in the fuel. BP vs HC 0 50 100 150 200 4 8 12 16 Brake Power (Kw) HC(ppmvolume) With HHO Without HHO Chart: 2 Brake power vs HC 6. CONCLUSIONS: The effect of adding proportionate amount of HHO mixture on the performance of the given 4-stroke four cylinder SI engine was evaluated. The following improvements in the parameters can be observed Complete combustion was achieved by adding the HHO to petrol leading to less emission of hydrocarbons and Carbon monoxides. The fuel consumption reduced by 8.87% The Thermal efficiency of the system decreased because of the increase input of heatduetoaddition of Hydrogen. The Mechanical efficiency however remained approximately same. The BSFC was also from 0.227 Kg/Kw-hr to 0.186 Kg/Kw-hr. REFERENCES [1] Suryakant Sharma, Deepak Bhardwaj and Vinay Kumar, “Effect on performance of engine by injectinghydrogen” International Journal of Mechanical Engineering and Robotics Research July 2013. [2] Sebastian Verhelst, Thomas Wallner, “Hydrogenfueled internal combustion engines”, Progress in Energy and Combustion Science, Vol. 35 (2009), Page no. 490–527. [3] A text book of ‘Internal Combustion Engines’ by V. Ganeshan, Tata McGraw Hill Education Private Limited . [4] Ammar A. Al-Rouson, 2010. An International Journal on ‘Reduction of fuel consumption in gasoline engines by introducing HHO gas into intake manifold’,Publishedby Elsevier Ltd. AUTHORS Prof. Mrs. Namrata V. Lotia Assistant Professor, Anjuman College of Engineering and Technology, Nagpur, India. Nagpur University (RTMNU) Zeeshan Jamal. Student of B.E Anjuman College of Engineering and Technology, Nagpur, India. Nagpur University (RTMNU) Jafar Sadique. Student of B.E Anjuman College of Engineering and Technology, Nagpur, India. Nagpur University (RTMNU) Mohammad Mohsin Raza. Student of B.E Anjuman College of Engineering and Technology, Nagpur, India. Nagpur University (RTMNU)
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