ISSN ONLINE(23209801) PRINT (23209798)
Seema .S. Billur^{1}, Vaijanath V. Yerigeri^{2}, Ravi V. Yerigeri^{3}

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Heat recovery steam generator (HRSG) plays a key role on performance of combined cycle (CC). In this work, attention was focused on a dual pressure reheat (DPRH) HRSG to maximize the heat recovery and hence performance of CC. Deaerator, an essential open feed water heater in steam bottoming cycle was located to enhance the efficiency and remove the dissolved gasses in feedwater. Each of the heating section in HRSG is solved from the local flue gas condition with an aim of getting minimum possible temperature difference. For high performance, better conditions for compressor, HRSG sections, steam reheater and deaerator are developed. The CC system is optimized at a gas turbine inlet temperature of 1400â¦C due to the present available technology of modern gas turbine blade cooling systems. The exergetic losses in CC system are compared with each other. The present DPRH HRSG model has been compared and validated with the plant and published data.
KEYWORDS 
Combined cycle; dual pressure; deaerator; exergy analysis; heat recovery steam generator. 
1. INTRODUCTION 
Combined cycle (CC) power plants are gaining wider acceptance due to more and more availability of natural gas, now a days, because of their higher overall thermal efficiencies, peaking and twoshifting capabilities, fast startup capabilities and lesser cooling water requirements. Heat recovery steam generator (HRSG) plays a very important role in recovering the sensible heat of gas turbine exhaust for generating steam, at required pressure and temperature, suitable to steam turbine for further power generation. Heat recovery from the HRSG has to be maximized for higher CC efficiency. Plant designs need to be adjusted to the specific project parameters to achieve optimum results. The optimization of the HRSG is particularly interesting for the combined plants design in order to maximize the work obtained in the vapor cycle. A detailed optimization of the HRSG is a difficult problem, depending on several variables. These include the number of pressure levels, the pressures, the mass flow ratio, and the inlet temperatures to the HRSG sections. 
Recently, researchers paying much attention towards the heat recovery steam generator to improve the CC performance. Pasha & Sanjeev (1995) presented a discussion about the parameters which influence the type of circulation and the selection for HRSG. Ongiro et al (1997) developed a numerical method to predict the performance of the HRSG for the design and operation constraints. Ganapathy et al (1988) described the features of the HRSG used in the Cheng cycle system. In this system, a large quantity of steam is injected into a gas turbine to increase electrical power output. Subrahmanyam et al (1995)d iscussed about the various factors affecting the HRSG design for achieving highest CC efficiency with cheaper, economical and competitive designs and with highest requirements to meet the shorter deliveries. 
Noelle & Heyen (2004) designed the oncethrough HRSG which is ideally matched to very high temperature and pressure, well into the supercritical range. Ragland & Stenzel (2000) compared four plant designs using natural gas with a view of cost benefits achieved through HRSG optimization. Casarosa et al (2004) determined the operating parameters means both thermodynamic and thermo economic analysis, minimizing a suitable objective function by analytical or numerical mathematical methods. The optimal design and operation of a HRSG is possible with minimization of entropy generation (Nag & De 1997). Reddy et al (2002) applied second law analysis for a waste HRSG which consists of an economizer, an evaporator and a super heater. Introducing multi pressure steam generation in the HRSG of a combined power plant improves the performance of the plant than that of a corresponding single pressure system (De & Biswal 2004). 
Pelster et al (2001) compared the results of a reference CC with the dual and triple pressure HRSGs and also with and without steam reheating models. Bassily (2005, 2007) modelled a dual and triple pressure reheat CC with a preset in constraints on the minimum temperature difference for pinch points, the temperature difference for superheat approach, the steam turbine inlet temperature and pressure, the stack temperature, and the dryness fraction at steam turbine outlet without a deaerator in steam bottoming cycle. Srinivas (2009) suggested an improved location for a deaerator in a triple pressure HRSG. A literature review has shown that the DPRH HRSG has not been modelled and analysed parametrically with a deaerator. The purpose of this work is to optimize the DPRH HRSG in the CC with a deaerator. The variations in CC performance are plotted with the compressor pressure ratio, gas turbine inlet temperature, HRSG HP, steam reheat pressure and deaerator pressure. From the present thermodynamic modelling, the optimized conditions to air compressor, HP steam, LP steam, steam reheater and deaerator have been developed. 2. Thermodynamic model of the CC with DPRH HRSG The optimized model in HRSG improves the steam generation rate and hence steam turbine output. Schematic flow diagram for CC is shown in figure 1. Simple gas cycle gives higher efficiency at lowcompressor ratio compared to the intercooledreheat model and hence in this work simple gas cycle is selected as a topping cycle in CC (Srinivas et al 2007). Figure 2 shows the temperatureentropy diagram for the CC shown in figure 1. Steam cycle with a reheater is taken as a bottoming cycle in CC. In steam cycle a deaerator is located to gain higher efficiency as well as to remove the dissolved gasses in feed water. Condensate preheater is arranged in the HRSG as a last heat transfer surface to improve the heat recovery. 
The temperatureheat transferred diagram for DPRH heat recovery is depicted in figure 3. TheCCis modelled withDPRHconfiguration in HRSG. An attempt has been made to improvethe heat recovery with parametric analysis. In this work, steam temperatures and low pressure (LP) are not getting fixed as in a regular method. Those are (except HP pressure and deaerator pressure) determined with the local flue gas temperature in heating sections of HRSG. 
Pinch point (PP)minimum temperature difference between gas turbine exhaust leaving the evaporator and saturation temperature of steam in evaporators and terminal temperature difference (TTD)temperature difference between exhaust entry and super heated steam in super heaters are maintained constant. Their choice is the consequence of a compromise between thermodynamic efficiency and investment costs (Franco & Russo 2002). 15K approach point (temperature difference between saturated steam and incoming water) is assumed in economizers. 
3. Thermodynamic analysis of the CC 
The assumptions made for the analysis of the CC are tabulated in table 1. The fuel to electricity efficiency of the CC is determined based on the lower heating value (50, 145 kJ/kg) of the fuel. The net work output of CC in percent of standard chemical exergy of the fuel (52, 275 kJ/kg) is expressed as exergy efficiency of CC (Kotas 1995). For an isentropic compression process, the change in the entropy for air is zero i.e. s = 0. The isentropic efficiency (Eq. 1 and 
2) for compressor and gas turbine is determined from pressure ratio (rc), specific heat ratio (γ) and polytrophic state efficiency (η∞). 
In Eq. (1) and (2), η∞c and η∞gt are the polytrophic efficiencies of compressor and gas turbine respectively. For an isentropic compression process, the change in entropy for air is 
In Eq. (3), ‘R’ is the universal gas constant. The temperature of air after isentropic compression is estimated from the iteration of entropy change equation in compressor (Eq. 3). Then the actual temperature of compressed air is iterated from compressor isentropic efficiency (ηc) and enthalpies. 
The combustion equation in gas turbine combustion chamber is 
CH4+X(O2+3.76N2)→CO2+2H20+(x2)O2+3.76xN2 
In combustion equation (Eq. 4), ‘x’ is the amount of air to be supplied at a fixed adiabatic flame temperature. The exergy balance equation for combustion chamber (Eq. 5) results the value of ‘x’ (Eq. 6). The exergy balance equation in gas turbine combustion chamber, 
IV. RESULTS AND DISCUSSIONS 
CC with DPRH HRSG has been studied parametrically to find the maximum obtainable output and efficiency from the power system. Deaerator pressure at which steam is trapped to heat the feed water is a key parameter to get the optimum heat recovery from the exhaust. Sensitivity analysis has been carried out with the gas turbine inlet temperature, compressor pressure ratio, steam reheat pressure ratio and deaerator temperature ratio. All the plots are prepared at an air flow rate of 625 kg s−1. Deaerator location is expressed in dimensionless form, defined as the ratio of difference in saturation temperatures of deaerator and condenser to the overall saturation temperature difference in the bottom cycle (Eq. 19). 
Figure 4 shows the effect of compressor pressure ratio for different values of gas turbine inlet temperature on CC power and efficiencies. In all the following figures (a) net electric power output, (b) fuel to electricity efficiency i.e. exergy efficiency and (c) exergy efficiency are developed against the CC key parameters. The difference in exergy of fuel and total exegetic losses gives the net work output (Eq. 18). The heating value of fuel is slightly less than the exergy of fuel. Generator efficiency has been considered in determining the fuel to electricity efficiency. Therefore, both the fuel to electricity efficiency and efficiency of CC are nearer to each other as shown in all the plots. The compressor pressure ratio is varied in such a way that the gas turbine exit temperature should not be less than 600°C. Due to limitation of steam maximum temperature (600°C), the resulted range of feasible compressor pressure ratio is 8 to 12 at a gas turbine inlet temperature of 1200°C. This range is 10 to 18 at 1300°C and 14 to 26 at 1400°C. The gas inlet temperature to HRSG is high at low pressure ratio and due to this reason; more quantity of steam can be generated in HRSG. This results in high output and efficiencies as shown. The pressure ratio corresponding to high performance increases from 10 to 14 with an increase in gas turbine inlet temperature of 1200°C to 1400°C. 
Figure 4 shows the effect of compressor pressure ratio for different values of gas turbine inlet temperature on CC power and efficiencies. In all the following figures (a) net electric power output, (b) fuel to electricity efficiency i.e. exergy efficiency and (c) exergy efficiency are developed against the CC key parameters. The difference in exergy of fuel and total exergetic losses gives the net work output (Eq. 18). The heating value of fuel is slightly less than the exergy of fuel. Generator efficiency has been considered in determining the fuel to electricity efficiency. Therefore, both the fuel to electricity efficiency and exergy efficiency of CC are nearer to each other as shown in all the plots. The compressor pressure ratio is varied in such a way that the gas turbine exit temperature should not be less than 600°C. Due to limitation of steam maximum temperature (600°C), the resulted range of feasible compressor pressure ratio is 8 to 12 at a gas turbine inlet temperature of 1200°C. This range is 10 to 18 at 1300°C and 14 to 26 at 1400°C. The gas inlet temperature to HRSG is high at low pressure ratio and due to this reason; more quantity of steam can be generated in HRSG. This results in high output and efficiencies as shown. The pressure ratio corresponding to high performance increases from 10 to 14 with an increase in gas turbine inlet temperature of 1200°C to 1400°C. 
Figure 5 presents the effect of compressor pressure ratio with HRSG HP on CC performance. The H combined cycle system will be the first power plant to achieve 60 percent efficiency and will operate at high temperature of 1430°C. This has been achieved by advances in materials and cooling system technology. Therefore, all the performance characteristics curves are developed at a gas turbine inlet temperature of 1400°C. At 1400°C, the compressor pressure ratio is varied from 14 to 26 as discussed in the previous section. HRSG HP is varied from 50 to 200 bar. The power output is high at low pressure ratio irrespective of HRSG HP in the preselected pressure ratio range (14–26). But with respect to exergy and exergy efficiencies, the optimum pressure ratio decreases with an increase in HRSG HP. The effect of steam reheat pressure expressed in a fraction of HRSG HP has been depicted in Figure 6 at different values of HRSGHP. The optimum steam reheat pressure ratio increases with an increase in HRSG HP. But due to the limitation in dryness fraction (0·8) at steam turbine exit, the steam reheat pressure ratio is limited to 0·5 in the present work at HRSG HP of 200 bar. 
Figure 7 generates the effect of deaerator temperature ratio as defined in Eq. (19) on CC performance at different sets of HRSG HPs. The optimum deaerator temperature ratio is found in between 0·25 and 0·3 with the variation of HRSG HP from 50 bar to 200 bar. 
Figure 8 compares the exergetic losses of cycle components in percent of standard chemical exergy of fuel. The second low evaluation is useful to identify the major losses to focus the attention on the weak areas for further improvements. The major exergetic loss occurs in gas turbine combustion chamber in the order of 27·5 percent and the minor exergetic loss is in deaerator. With a steam injection in combustion chamber, this major exergetic loss can be decreased (Srinivas et al 2007, 2008). Next to GTCC, considerable level of exergy is destroyed in compressor, gas turbine, HRSG and exhaust in the range of 2 to 3 percent. The present DPRH HRSG model results are compared and validated with ABB– Alstom, greatest manufacturers of CC plants in the world and the literature results. This comparison is presented in table 2. The inlet conditions for DPRH HRSG are chosen from ABB plant. However, the present HRSG layout with a deaerator adopted here are quite different from those of comparison. The main differences we can find between the plant data and present work are the value of the HRSH HP and reheat pressures. It can be supposed that all the other differences that arise from the comparison (pressures and the flow rates) are a consequence of this primary characteristic that influences the properties of the thermal cycles deeply. 
Figure 8. Comparison of exergetic losses in CC components in per cent of standard chemical exergy input of fuel. In the present work, the HRSG LP is more than from the observations. It is due to inclusion of deaerator at a pressure below the LP level. Remaining all the results are in agreement with the plant and literature results. 
V. CONCLUSIONS 
In a CC power generation system, a DPRH HRSG has been critically examined. For a given set of gas turbine inlet temperature, the feasible range of compressor pressure ratio has been developed. For a maximum steam temperature of 600°C, the feasible compressor ratios are 8–12, 10–18 and 14–26 for a gas turbine inlet temperature of 1200°C, 1300°C and 1400°C Table 2. Comparison of heat recovery details with the plant data and published results at Tg,HRSGin = 650°C and mg = 386·7 kg s−1. 
respectively. Out of this range, the optimum compressor pressure ratio decreases with an increase in HRSG HP. The optimum deaerator temperature ratio is suggested at 0·25 to 0·3. 
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