Hydrogen oxygen steam generator integrating with renewable energy resource for electricity generation

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Available online at www.sciencedirect.com Energy Procedia 29 (2012 ) 12 20 World Hydrogen Energy Conference 2012 Hydrogen oxygen steam generator integrating with renewable energy resource for electricity generation Saif A. Alabbadi* Coventry University. Amman, 2280 sweileh 11910, Jordan Abstract Renewable hydrogen energy system produces oxygen as by product from water electrolysis process, the produced oxygen is vented out to the surrounding and not utilized. Hydrogen combustion with a stoichiometric ratio of pure oxygen produces steam at a very high temperature, Steam temperature can be controlled by injection of liquid water into the combustion chamber. The main objectives of this study is to utilize the oxygen and hydrogen produced from water electrolysis using renewable energy resource in H 2 /O 2 steam generator to supply steam for a turbine drive an electric generator, and to study the feasibility of using H 2 /O 2 steam generator with a steam turbine unit to provide electric power as a primary or a secondary source of energy. 2012 2012 Published The Authors. by Elsevier Published Ltd. by Selection Elsevier and/or Ltd. peer-review under responsibility of Canadian Hydrogen and Fuel Cell Association Open access under CC BY-NC-ND license. Selection and/or peer-review under responsibility of Canadian Hydrogen and Fuel Cell Association Keywords: Type your keywords here, separated by semicolons ; 1. Introduction Global warming effect as a result of green house gases emissions from fossil fuels consumption, and the unease about availability and prices of fossil fuels as well as large increase in energy demands have boosted the requirements for developing the renewable energy resources. [1] Nowadays the conventional technology to generate electricity is steam power plant which is either using fossil or nuclear fuels, and gas turbine power plant which is using fossil fuels. * Corresponding author. Tel.: 00962-79585-3687. E-mail address: salabbadi@live.com. 1876-6102 2012 Published by Elsevier Ltd. Selection and/or peer-review under responsibility of Canadian Hydrogen and Fuel Cell Association. Open access under CC BY-NC-ND license. doi:10.1016/j.egypro.2012.09.003

Saif A. Alabbadi / Energy Procedia 29 ( 2012 ) 12 20 13 In steam power plant the steam is generated by burning fuel to heat up water. The combustion of pure hydrogen and pure oxygen in a stoichiometric ratio is exothermic reaction and produce steam at very high temperature, water can be added to the reaction to reduce the steam temperature for the desired application. Hydrogen oxygen steam generator technology was derived from hydrogen oxygen combustion in rocket technology. Hydrogen and oxygen can be produced from water electrolysis process using renewable energy resource (solar energy, wind energy) or a combination of both depends on the weather availability. Nomenclature m steam mass flow rate (kg/s) m f V hydrogen mass flow rate (kg/s) flow velocity (m/s) A orifice cross section area (m 2 ) T temperature (K) P absolute pressure (Pa) ρ density of steam (kg/m 3 ) R steam gas constant (461.5 J/kg.K) M Mach number C speed of sound K ratio of specific heat constant pressure and specific heat constant volume (1.33) P o T o P t P net η th η overall LHV stagnation pressure (Pa) stagnation temperature (K) turbine shaft power (kw) net electric power (kw) thermal efficiency overall efficiency lower heat value of hydrogen (119.9 x 10 3 kj/kg) 2. H 2 /O 2 steam generator The working principle of H 2 /O 2 steam generator is taken from the H 2 /O 2 rocket combustion technology. The combustion of pure hydrogen and pure oxygen in a stoichiometric mixture produce superheated steam (H 2 O) with a temperature reach in flame zone around 3000 0 C [2], as shown in the chemical equation below, for every two moles of hydrogen react with one mole of oxygen in combustion chamber produce steam at high temperature in range 1000-1500 0 C. [3]

14 Saif A. Alabbadi / Energy Procedia 29 ( 2012 ) 12 20 2H 2 + O 2 2H 2 O + heat This reaction is highly exothermic therefore, liquid water is added to the reaction to reduce the steam temperature, so it can be utilized in a steam turbine. Steam generator is a device to burn stoichiometric mixture of hydrogen and oxygen in combustion chamber to produce high temperature superheated steam Figure 1 shows hydrogen oxygen steam generator device. The mixture of hydrogen and oxygen are ignited in the ignition chamber, then the combustion takes place in the combustion chamber, the temperature controlled in the combustion chamber by liquid water injection, after that the steam compose at evaporation chamber. The steam generator efficiency is 100% since no emissions and no thermal losses. [2] Table 1 shows some steam characteristics produced by the hydrogen oxygen steam generator and steam from the conventional method. Figure 1: hydrogen oxygen steam generator. [4] Table 1: steam characteristics produced by the H 2 /O 2 steam generator and steam by the conventional method. [3] Steam generator Conventional (boiler) H 2 /O 2 steam generator Fuel Nuclear, oil, coal Hydrogen Oxidizer Air Oxygen Maximum steam temperature ( 0 C) Efficiency (%) Starting time (second) Pollutants 535-600 90-94 >10 4 CO 2, NO x, SO x, Ash 1000-1500 98-99.5 <50 None

Saif A. Alabbadi / Energy Procedia 29 ( 2012 ) 12 20 15 Saif A. Alabbadi/ Energy Procedia 00 (962) 79585 3687 3. Hydrogen oxygen production Typical method of hydrogen and oxygen production is steam reforming of natural gas, and cryogenic air separation respectively. Using renewable energy resource (wind or solar) in water electrolysis process to produce hydrogen and oxygen from electrolyser, either alkaline or proton exchange membrane (PEM) is effective method of production from free source of energy. The advantages are high purity of hydrogen and oxygen, no CO 2 emissions because no fossil fuel used, and reduces the cost of production of the hydrogen and oxygen since the energy resource is free. One mole of water produces one mole of hydrogen and half mole of oxygen from water electrolysis process. Theoretically, every one liter of water produces 1.24 Nm 3 of hydrogen and 0.62 Nm 3 but actually the water utilization is 25% higher. [5] 4. System design Figure 2: shows a schematic diagram of the H 2 /O 2 steam turbine power unit integrated with renewable energy resource. From figure 2 the components are renewable energy resource (solar or wind or combination of both), electrolyser (alkaline or PEM), including electrolyser auxiliary unit (water pumps, gas drier, and deoxidizer), hydrogen compressor, oxygen compressor, hydrogen storage system, oxygen storage system, hydrogen and oxygen supply system, hydrogen oxygen steam generator, steam turbine, electric generator, condenser, and the water reservoir. The renewable energy resource provide electric power for the hydrogen and oxygen production unit (electrolyser, auxiliary unit, compressors, and the storage system) then the hydrogen and oxygen are supplied to the H 2 /O 2 steam generator for steam production. Turbine is fed by steam to produce work for electricity generation. The exhaust steam is passed through condenser then to the main water reservoir. The oxygen production is equal to half of the hydrogen production and the oxygen mass flow rate

16 Saif A. Alabbadi / Energy Procedia 29 ( 2012 ) 12 20 supplied to the steam generator is equal to half of the hydrogen mass flow rate. The water mass flow rate supplied to the reservoir from the condenser is bigger than the mass flow rate needed to control the temperature in the combustion chamber consequently water is fed to the electrolyser to produce hydrogen and oxygen again. The system operates as a closed cycle. 4.1 Desired Steam Turbine Parameters Assumption has been made to determine the turbine inlet temperature, pressure and mass flow rate. The electrical loads demand is assumed to be 750 kw. Therefore, the shaft power of the steam turbine depends on the efficiency of the electric generator, which is assumed to be 90%. Steam turbine power = 750 / 0.9 = 834 kw The turbine mechanical power should be 834 kw to supply 750 kw electrical power. Steam turbine isentropic efficiency is determined by the manufacturer based on the interior design of the turbine. Typical isentropic efficiency ranging from 20-90%, isentropic efficiency has been assumed to be 65 %, according to the power output and the isentropic efficiency. The turbine inlet temperature, pressure, mass flow rate, and exhaust pressure have been assumed to meet the power output and isentropic efficiency of the steam turbine using turbine steam consumption calculator version 2.2, (2007) from Wayne Jayes and Harvey Wilson, (free software). Turbine inlet temperature: 450 0 C Turbine inlet pressure: 6 MPa Turbine exhaust pressure: 150 saturated steam Steam mass flow rate: 1.6 kg/s 4.2 H 2 /O 2 steam generator design From the steam turbine parameters, the hydrogen oxygen steam generator must supply steam at pressure 6 MPa, and temperature 450 0 C with a steam mass flow rate 1.6 kg/s these are the design conditions. The temperature of the combusting gases (hydrogen and oxygen) is controlled by the number of moles of the liquid water injected in the combustion chamber. Control volume of the steam generator shown in figure 3. Figure 3: steam generator control volume. The steam generator is assumed to be adiabatic, isentropic, and constant pressure device, there is no change in kinetic and potential energy. As well as there is no dissociation since the temperature less than 2500 K. Z H 2 + (Z/2) O 2 + X H 2 O liquid 88.89 H 2 O steam This equation shows the stoichiometric reaction of (Z) moles of hydrogen and (Z/2) moles of oxygen with (X) moles of liquid water to produce 88.89 mole per second of steam. The (X) means number moles of the liquid water to be injected in the combustion chamber to reach the desired steam temperature.

Saif A. Alabbadi / Energy Procedia 29 ( 2012 ) 12 20 17 Solve the combustion equation for 450 0 C of adiabatic flame temperature to find the moles number of liquid water injected in the combustion chamber. The adiabatic flame temperature rise will be very small due to the pressure increase. [6] Z H 2 + (Z/2) O 2 + 70.52 H 2 O liquid 88.89 H 2 O steam From the balance of the combustion reaction equation to burn the hydrogen with a stoichiometric ratio of oxygen 18.37 H 2 + 9.185 O 2 + 70.52 H 2 O liquid 88.89 H 2 O steam burn 36.74 g/s of hydrogen with 293.92 g/s of oxygen and 1269.36 g/s of injected water liquid to produce 1600 g/s of steam at 450 0 C. The steam pressure is determined by sizing the exit orifice diameter of the H 2 /O 2 steam generator, since the combusted gases follow the compressible flow. Critical flow (choked flow) of compressible gas is defined that the flow result when the ratio of the back pressure to the chamber pressure is less than the critical pressure ratio which is equal to 0.528 for the ideal gases, this also mean that the flow velocity at the exit of the orifice is one Mach (sonic flow). The flow through the orifice is assumed to be isentropic, adiabatic, and frictionless. The mass flow rate m = ρ V A...(1) From an ideal gas law ρ = P / RT...(2) Mach number is M = V / C...(3) The speed of sound is defined as C = KRT...(4) Since Mach number value is unity, substitute equation 2,3, and 4 in 5 m = P/RT x KRT A...(5) Where P and T in equation (5) are representing the pressure and temperature at the orifice and they are related to the stagnation pressure and temperature, but since the flow is isentropic, this means the stagnation pressure and temperature are constant. The stagnation pressure and temperature are stated by the equations below. P o /P = [1 + ((K-1)/2) M 2 ] K/K-1 T o /T = 1 + ((K-1)/2) M 2 Substitute for M = 1, and K = 1.33

18 Saif A. Alabbadi / Energy Procedia 29 ( 2012 ) 12 20 P = 0.54 P o...(6) T = 0.86 T o...(7) Substitute equations 6 and 7 in equation 5, then the equation of the mass flow rate through the orifice become m = (0.54P o / 0.86T o R) A K R 0.86T o The flow velocity inside the combustion chamber is assumed to be zero, consequently the stagnation pressure and temperature is the same as the static pressure and temperature. Substitute in the above equation for the mass flow rate is 1.6 kg/s, pressure 6 MPa, and the temperature 723 K. The diameter needed is 17 mm. 4.3 Steam Power Unit Efficiency Calculations η th = (P t / m f x LHV) x 100% = 18.9 % η overall = ( P net / m f x LHV) x 100% = 17 % 4.4 Hydrogen oxygen production unit The electrolyser production rate, hydrogen and oxygen storage system depends on the consumption (kg/hr). As well as the renewable energy resource (wind or solar), should match the electrolyser capacity to ensure sufficient production of hydrogen and oxygen. From the combustion equation the hydrogen and oxygen consumption is 132.3 kg/hr, 1058.2 kg/hr respectively. Based on that the hydrogen and oxygen storage capacity under pressure 200 bar should be 177 m 3 (35319 Nm 3 ), 89 m 3 (17773 Nm 3 ) respectively, to guarantee 24 hours of autonomous operation for the steam power unit if there is no electrical power supplied from the renewable energy resource to the electrolyser.

Saif A. Alabbadi / Energy Procedia 29 ( 2012 ) 12 20 19 5. Conclusion This study has been focused exclusively on the design of the hydrogen oxygen steam generator connected to a steam turbine drive an electric generator to supply electrical power as a secondary or primary source of energy. The work presented in this study leads to clear understanding for the working principle of the hydrogen oxygen steam generator. The hydrogen and oxygen are produced from water electrolysis using renewable energy resource. The hydrogen oxygen steam generator design is defined by finding the steam exit temperature, pressure, and the steam mass flow rate. These parameters were determined according to the turbine operation conditions. The steam temperature can be controlled based on the moles number of the liquid water injected inside the combustion chamber, and the steam pressure depends on the sizing of the exit orifice. The thermal and overall efficiency can be enhanced only by increasing the inlet pressure, temperature, turbine isentropic efficiency, and electric generator efficiency together and reduce the exit pressure from the turbine, because that will reduce the steam consumption which means that will reduce the mass flow rate of the hydrogen and oxygen entering the combustion chamber. References [1] JANON, A. (2009) Wind-Hydrogen Energy Systems for Remote Area Power Supply. Unpublished thesis (PhD). Melbourne: Royal Melbourne Institute of Technology University. [2] SHERIF, S.A. BARBIR, F. and VEZIROGLU, T. N (2005) Wind Energy and Hydrogen Economy- Review of the Technology, Solar Energy, 78, 647-660 [3] MALYSHENKO, S. GRYZANOV, A. and FILATOV, N. (2004) High Pressure H 2 /O 2 Steam Generators and Their possible Applications, International Journal of Hydrogen Energy, 29, 589-596. [4] HAIDN, O. J. et al (1998) Improved Combustion Efficiency of A H 2 /O 2 Steam generator fro Spinning Reserve Applications, International Journal of Hydrogen Energy, 23, 491-497. [5] BARBIR, F. (2005) PEM Electrolysis for Production of Hydrogen from Renewable Energy Resource, Solar Energy, 78, 661-669 [6] GLASSMAN, I. and YETTER, R. (2008) Combustion. 4 th ed. Oxford: Elsevier.

20 Saif A. Alabbadi / Energy Procedia 29 ( 2012 ) 12 20 Bibliography CENGEL, Y. A. and BOLES, M. A. (2006) Thermodynamics an Engineering Approach. 5 th ed. New York: McGraw-Hill. HAIDN, O. J. et al (1998) Improved Combustion Efficiency of A H 2 /O 2 Steam generator fro Spinning Reserve Applications, International Journal of Hydrogen Energy, 23, 491-497. MIDILLI, A. et al. (2005) On hydrogen and Hydrogen Energy Strategies Current Status and Needs, Renewable and Sustainable Energy Reviews, 9, 255-271. NEAGU, C et al. (2000) The Electrolysis of Water: An Actuation principles for MEMS with a Big Opportunity, Mechatronics, 10, 571-581. SONNTAG, R. BORGNAKKE, C. and VAN WYLEN, G. (1998) Fundamentals of Thermodynamics. 5 th ed. New York: John Wiley and Sons. STERNFELD, H. J. (1995) Capacity Control of Power Stations by H 2 /O 2 Rocket Combuster Technology, Acta Astronautica, 37, 11-19.