Thermodynamic analysis of the apci skikda liquefaction process
Journal of Thermal Engineering 2023, Vol. 9, Issue 3, pp. 786-798; doi.org/10.18186/thermal.1300835
Abstract
Keywords: APCI; LNG; Mixed Refrigerant; COP; Exergy Efficiency; Optimization; Genetic Algorithm
Introduction
Today, liquefied natural gas (LNG) is considered one of the most important energy carriers. It is produced by three cryogenic gas liquefaction processes: cascade cycles with pure refrigerants, mixed refrigerant cycles and nitrogen expansion cycles. Mixed refrigerant processes are mainly divided into three types: single mixed refrigerant (SMR), dual mixed refrigerant (DMR) and cascaded mixed refrigerant cycles [1]. Among these mixed refrigerant processes,
the APCI-LNG process is the most widespread in the cryogenic industry, currently belongs to the majority of liquefaction plants in the international market, accounts for about 40% of the capital of LNG complexes and has a significant impact on utilities and operating costs. Many researchers have been conducting theoretical and experimental studies and have been interested to the optimization of this liquefaction process for more than three decades. Kikkawa et al. [2] simulated a uniform refrigerant liquefaction process using a pre-cooling loop and an expander
*Corresponding author. *E-mail address: chaim.23.derb@gmail.com This paper was recommended for publication in revised form by Regional Editor Ahmet Selim Dalkılıç Published by Yıldız Technical University Press, İstanbul, Turkey Copyright 2021, Yıldız Technical University. This is an open access article under the CC BY-NC license (http://creativecommons.org/licenses/by-nc/4.0/).
with the CHEMCAD III software. Process thermal efficiency has been evaluated based on the required power consumption to produce a unit of LNG, i.e., specific power consumption. The total required power consumption of the refrigerant compressors is 81.5MW which is equivalent to a specific power of 931 kJ/kg of LNG. Cao et al. [3] designed and simulated two types of small-scale NG liquefaction processes in a skid-mounted assembly, their results show that the N2-CH4 expansion cycle precedes the mixed refrigeration cycle due to the absence of propane pre-cooling. The power consumption of the compressors is more influential to specific power consumption, so compression with intercooling should be adopted to lessen the irreversible degree of compression process. Vatani et al. [4] considered two mixed refrigeration cycles for the design of an LNG production process with integrated natural gas liquids recovery. They formulated an optimization problem with minimization of specific energy consumption. Their results showed that not only liquefaction efficiency of the process is considerable (0.414 kWh/kg LNG) but also it can recover the ethane higher than 93.3%. This process can be used for large LNG plants in the natural gas refineries. It can also be said that the overall efficiency will be higher for the leaner feed gases. Wang et al. [5] optimized two types of C3MR processes by studying different objective functions, including shaft work consumption, exergy efficiency and operating expenses. They reported that tree work consumption is the best objective function for the optimization of these processes. Khan and Le [6] optimized SMR and C3MR processes using knowledge based optimization (KBO) method. By considering boiling point difference of the MR components, they improved the energy efficiency of the system. They reduced the compression energy requirement of an SMR process by 10% with warm particles model, while the exergy efficiency of the whole process increases 5%. Kumar and Mishra [7] presented a detailed review for cryogenic systems and made energy and exergy analysis of the system for liquefaction of various gases. Mehrpooya and Ansarinasab [8] conducted an energy and exergy analysis for the Linde SMR and APCI single mixed refrigeration processes. Their results show that the exergy efficiency and exergy destruction rate of the APCI process are 45% and 72.24MW respectively. Derbal al. [9] made an exergy analysis of the mixed refrigeration APCI-LNG Skikda and determined exergy efficiency and exergy destruction of the MR compressors and gas turbine. Their results show that the inlet temperature and inlet pressure of MR compressors has an impact on the evolution of the exergy efficiency. Wang et al. [10] experimentally investigated the effect of operating pressures and refrigerant flow compositions on the cycle performance; they concluded that the openings of two throttle valves had significant impacts on operating pressures. Hajji et al. [11] performed simulation and sensitivity analysis for two objective functions, specific energy and compressor energy consumption, by the Aspen HYSYS
process simulator and this was done to improve the overall performance and heat recovery of the LNG process output streams by changing the thermodynamic variables of the C3MR mixed refrigerant process. The results obtained show a greater improvement in the objective functions compared to other studies. He et al. [12] proposed a simulation-based optimization methodology to simultaneously determine the components and their respective fractions in the MR. Then; they performed energy and exergy analysis to reveal the relationships between the MR components and the process performance. Their results indicated that energy efficiency and exergy efficiency were strongly influenced by the selection of components for the MR. Aghazadeh et al. [13] carried out a comprehensive thermodynamic analysis and optimization of two new combined refrigeration cycles using the first and second thermodynamic laws and the assumption of a constant area model for the ejector. Their results show that the maximum thermal efficiency and exergy efficiency are 77.3% and 23.7% in cycle I and 87.5% and 23.9% in cycle II, respectively, by optimizing all design parameters. Rehman et al. [14] presented a systematic approach that includes the identification of improvement potentials in the single mixed refrigeration process SMR. To this end, sources of irreversibility are identified using an advanced exergy analysis to identify further improvement potential. The results reveal that 43% of the overall energy destruction associated with the base case of the SMR process can be avoided through process optimization or redesign. Genetic algorithm (GA) is a global optimization method applied for optimizing LNG process. Alabdulkarem et al. [15] applied GA for the optimization of the propane precooled mixed refrigeration cycle and reported the energy consumption of the MR at different compression pinch temperatures using a combination of GA and sequential quadratic programming. Xu et al. [16] modeled and optimized the PRICO process using GA and Aspen Plus software; the result shows that at about the 40th generation, the search identifies the optimal solution. They obtained a relationship between energy consumption and mixed refrigerant composition. Moein et al. [17] analyzed a single mixed refrigeration cycle (SMR) to determine the optimal operating conditions and optimized it with using GA. They minimized the total required work by optimizing eleven variables including the outlet pressures of all compressors and throttling valves and the molar flow rate of the MR components. The results showed that the total required work was reduced by 14% compared to the base case. Nikkho et al. [18] carried out a simulation of two small-scale modified single refrigeration processes for NG liquefaction. They used the GA method to optimize the specific energy consumption and the total exergy destruction rate of the process. Their results show that the specific energy consumption and the total exergy destruction rate are reduced by 19.4% and 25.4%, respectively. On the other
hand, the maximum total exergy efficiency of 47.51 % is obtained. The literature review shows that the APCI cycle is the most efficient for the production of LNG. In this context, fits our contribution. The objective of our work is to determine the efficiency of the APCI Skikda (Algeria) liquefaction process, compare it to other liquefaction processes and seek its improvement. To do so, this cycle will be thermodynamically analyzed. The energy analysis will lead to obtaining the COP of the cycle while the exergy analysis will allow the detection of irreversibilities within the process equipment and the evaluation of the exergy efficiency of the cycle. The effects of important parameters (compressor inlet gas temperature, expander inlet temperature and MCHE outlet temperature) on APCI process performance will be studied and the main results will be described. The genetic algorithm will be used as a method of performance optimization. The optimization results are described and
compared to those of the literature. The details of this work are represented in the following sections. APCI Process Description The APCI process used in Skikda LNG complex includes three refrigeration cycles (mixed refrigeration, propane refrigeration and external propane refrigeration). In this descriptive section, we limit ourselves to the mixed refrigeration cycle, subject of this work. It is mainly composed of a main cryogenic heat exchanger (MCHE), three compressors (C1, C2 and C3) and chillers (c4-c5-...-c11). The process is shown in Figure. 1. The NG flows through the HP, MP, BP propane feed gas coolers (c1, c2 and c3) at (22.46°C, 63 bar). The NG coming from the c3 cooler enters the scrubber column (SC) (Stream 4) at (-35.15°C,
61.56. bar). The head stream of the SC feeds the hot end
of the MCHE at (-38.99°C, 60.67 bar) (Stream 6) and then returns to the reflux drum (RD) at -55.33°C of the SC via
Legend E Expander c1-... c3 Gas cooler JT Thomson Joule valve RD Reflux Drum FD Flash Drum C1-…C3 Compressor P1, P2 Pump SD Separator Drum HX Heat exchanger c4-…c11 Chiller NS Nitrogen Stripper SC scrub column He.C Helium Compressor Ic1-…Ic3 Intercooler MCHE Main Cryogenic Heat Exchanger FG.C Fuel Gas Compressor
Figure 1. Schematic diagram of the APCI - Skikda liquefaction process.
efficiency of the APCI cycle has been evaluated in this study. The thermodynamic analysis is based on a numerical simulation performed with the Matlab® program. The energy equilibrium equations and the exergy equilibrium equations of the APCI cycle equipment are established by neglecting the pressure loss and the heat loss in the heat exchangers. This analysis was carried out on the basis of the assumptions presented in Table 2.
pump P1. Streams (12) to (40) constitute the MR loop. The mixed refrigeration system recovers the MR as steam from the shell side of the MCHE at -39.17°C (Stream 12). The MR discharged by compressors (C1, C2) is cooled in intercoolers (Ic1, Ic2) before being sent to the compressor suction (C3). After discharge from the compressor (C3), the MR is cooled in the intercooler (Ic3) to 40.76°C (Stream 18). The coolers (c4-...-c11) cool the MR from 40.76ºC to -35.69ºC before it enters the MCHE (Stream 30). The MR liquid leaving the MCHE mid-tip (Stream 31) is expanded by the E1 expander from 49.66 bar to 4.7 bar and returns to the exchanger through the Thomson Joule valve (Stream 33). The LNG expander E2 receives the liquefied natural gas from the cold end of the MCHE (Stream 44) at a pressure of
45.85. bar and expands it to a pressure of 21.79 bar (Stream
45) before it is admitted into the flash drum (FD) (Stream 46). The MR refrigerant from the separator (SD) feeds the exchanger (HX1) at -35.69ºC (Stream 37). The head product from the flash drum (FD) enters the exchanger (HX1) at -147.77ºC (Stream 46) to feed the helium compressor (He.C) (Stream 47) at -37.91ºC The exchanger (HX2) receives the hot LNG from the bottom of the flash drum (FD) at -147.77ºC (Stream 48). The LNG product at -160.55°C coming from the bottom of the nitrogen stripper (NS) (Stream 54) is sent to the LNG storage tank thanks to the P2 pump (Stream 55). The chemical composition of NG and MR are shown in Table 1.
Thermodynamic Analysis
In order to analyze the performance of the system, the influence of the inlet temperature of the compressors, the inlet temperature of the expander, the temperature of the NG after cooling in the MCHE, on the COP and the exergy
Table 2. Main assumptions for the thermodynamic analysis of the basic cycle
Energy Analysis The steady-state energy balance equation is expressed as:
Neglecting the kinetic and potential energy variations ( and gzk), the energy balance equations for each component can be written in terms of specific enthalpy as follows [19]:
m i ,in (hi',out − hi ,in ) = Wi m i ,in (hi ,out − hi= ) ,in
i=C1, C2, C3 where h'i,out is the enthalpy at entropy constant and ηc the compressor isentropic efficiency. For the expander, the energy equation is:
W= m j ,in (h j ,in − h j ,out= ) η j m j ,in (h j ,in − h'j ,out ) (4) j
j=E1, E2 where h'i,out is the enthalpy at entropy constant and ηi the expander isentropic efficiency. For heat exchangers HX1and HX2, the energy equation is:
For the MCHE, the energy equation is obtained from Figure 1: (6)
m NG ( h1 − h4 ) + m LNG ( h9 − h44 ) + m 19 ( h19 − h23 ) + m 24 ( h24 − h28 ) Q = W ∑W − ∑W net
i=C1, C2, C3; j=E1, E2 The input energy is the net work done on the system for the production of LNG, the output energy is the heat supplied by the refrigerants in the NG cooling stages. Exergy Analysis The exergy analysis of a process complements the energy analysis and is used to assess the work potential of the input and output material and heat streams, and to determine the location and magnitude of irreversibility losses. The state-specific exergy is determined from the following equation:
In this study, variations in kinetic and potential exergy have been neglected. By assuming a constant chemical composition of the flows, the chemical exergy term is cancelled out in the exergy balance equations. Therefore, the specific exergy for each arbitrary state can be considered equivalent to the physical exergy. The physical exergy is obtained from the following equation [20]:
where (s) and (h) are the specific entropy and enthalpy at the conditions specified for the species and the subscript 0 represents the environmental conditions. The general exergy balance can be expressed as a rate as follows [21-23]:
Table 3. Formulas used to calculate the exergy destruction of the cycle components Components
where E x ,in is the exergy at the input, E x ,out is the exergy at the output and ∆E x is the exergy destruction. The exergy destruction for each process component is calculated based on the well-known equations summarized as follows in Table 3. The total exergy destruction can be found as the sum of the exergy destruction of each component [24-27]:
The exergy efficiency of the cycle is defined as follows [19]: (11) The thermodynamic properties, including temperature, pressure, mass flow rate, enthalpy, entropy, exergy and steam fraction “x” at each point in the MR cycle of the APCI process are summarized in Appendix 1.
Optimization
The genetic algorithm (GA) is a heuristic search that mimics the process of natural selection and is commonly used to generate useful solutions to optimization problems [28]. The design of the liquefaction process is a highly nonlinear problem with many local optima. To solve the optimization problem, GA is chosen as the optimization method [29-31]. The GA starts working by producing an initialization population. During the optimization, there are several constraints to ensure that the process can run safely and stably. The GA will judge whether the constraints are satisfied or not. If the constraints are satisfied, the GA will calculate the objective function; otherwise, the penalty function will replace the objective function. The best population will be found when the objective function reaches the maximum or minimum value. The ‘Stochastic uniform’ method is used as a selection method in this paper, namely it stochastically chooses a number of chromosomes from the current population and selects the one with the best ‘fitness’. Breeding is carried out
by the ‘Scattered’ crossover method. Then chain mutations occur randomly with minor probability and a new individual is finally formed. In order to save the best solution from each generation, the corresponding optimal fitness solution is compulsively copied into the next generation. The parameters used for the GA are presented in Table 4, as for the variables used for the cycle optimization are presented in Table 5.
Objective Function In this work, the actual optimization problem is the minimization of the net energy consumption of the APCI cycle. In general, the exergy efficiency of the cycle has been defined as an objective function expressed as follows:
In this work, energy and exergy analyses were performed on the APCI cycle. Basic cycle performances described under the operating conditions are presented in Table 6. It consumes a net power of about 102.35 MW, while its COP and exergy efficiency are estimated at 2.66 and 59.99% respectively.
Table 6. Results of the thermodynamic calculation of the basic APCI cycle performances
Results And Discussion
In Eq. 12, X is an adjusted variable vector including the inlet temperature of the compressors (C1, C2 and C3), the inlet temperature of the expanders (E1, E2).
Exergy analysis is applied to assess the extent of exergy destruction in each component of the cycle shown in Figure 2. It is found that compressors occupy the highest proportion of the total exergy destruction rate estimated at 30.43 %, followed by coolers and intercoolers occupying 22.17%. Other important equipments with irreversible operations are the MCHE, expanders, heat exchangers and separators. They contribute respectively with a rate of 19.71%; 8.55%; 7.2% and 7.72% of the total exergy destruction of the liquefaction process. The energy destruction of the throttle valves and pumps are the lowest. Our results are in agreement with the work of the authors [35-38]. It is clear that reducing the exergy destruction in the compressors and coolers would be the best way to reduce the total exergy destruction of this liquefaction process. The main measures to reduce compressor exergy destruction are to adopt multi-stage compression, selecting reasonable inlet parameters and compression ratio for the compressor.
Table 5. Variables limits used for the cycle optimization Parameter
Figure 2. Distribution of exergy destruction rate of the basic cycle components
Thus, the outlet temperature of the compressors is reduced and the heat transfer temperature difference in the coolers is lower. The exergy destruction of the chillers is reduced due to the reduced heat transfer temperature difference. In this work, the numerical simulation of the key process parameters was carried out using the Aspen HYSYS software. The effects of compressor inlet temperature, NG temperature after cooling in the MCHE and MR expander inlet temperature on the COP and exergy efficiency of the APCI process were analyzed. The results proposed are shown in Figure 3; Figure 4 and Figure 5.
Figure 3. Effect of NG temperature after cooling in MCHE on the COP and exergy efficiency
Figure 3 shows the effects of the NG temperature after cooling in MCHE on the COP and exergy efficiency, where the heat transfer for the NG occurs under a pressure of
45.85. bar. It is seen that increasing the NG temperature
after cooling in MCHE induces a decrease in the COP and the exergy efficiency. On the other hand, the increase of the NG outlet temperature after cooling in MCHE induces a reduction of the input power required for the compressors (C1, C2 and C3), the total heat captured from the NG in the MCHE also decreases and finally the COP and exergy efficiency decrease. Figure 3 also shows that at -77°C the COP and exergy efficiency can also reach of about 1.78 and
23.10. %, respectively.
Figure 4 shows the influence of the inlet temperature of the compressors (C1, C2 and C3) on the COP and exergy efficiency, the inlet pressure of the compressors (C1, C2 and C3) is 4.3 bar; 20.61 bar and 31.80 bar respectively. It is seen that the COP and exergy efficiency decrease as the inlet temperature of the compressors (C1, C2 and C3) increases. This is due to the fact that the input power of the compressors increases as the input temperature of the compressors increases. On the other hand, Figure 4 also shows that the COP and exergy efficiency of C1 can also reach about 1.97 and 30.27% respectively; those of C2 about 2.23 and 53.25% respectively; and those of C3 about 2.26 and 63.28% respectively Table 7. Thus, a decrease in compressor inlet temperature would ensure better cycle performances. The effect of the inlet temperature of the E1 expander on the COP and exergy efficiency is shown in Figure 5 where the inlet pressure of the E1 expander is 49.66 bar. It is seen
Figure 4. Effect of compressors inlet temperature on the COP and exergy efficiency
Table 7. Cycle performance at maximum compressor inlet temperatures values Compressor
that the COP and exergy efficiency decrease with increasing inlet temperature of the E1 expander. This decrease is due to the increase in the power of the E1 expander. On the other hand, Figure 5 also shows that the COP and exergy efficiency of the E1 at -112°C can reach 1.84 and 26.33%, respectively. The results commented in Figure 3, Figure 4 and Figure 5 are in accordance with those obtained by the authors [37-38]. To validate simulation results proposed via Aspen HYSYS software, we run the model with basic cycle data as input and adjust it until the output produced matches the basic cycle results. This validation is represented in Table 8.
Figure 5. Effect of E1 expander inlet temperature on the COP and exergy efficiency
We note that the differences between the values of the parameters of the basic cycle and those proposed by simulation via HYSYS do not exceed 6.77%, which confirms the validity of our results. The optimization results indicate that the minimum power requirement for the three
Table 8. Validation of the numerical simulation results via Aspen HYSYS Parameter
compressors is about 101.84 MW and 1.17 MW for the two expanders. The optimal COP and exergy efficiency of the cycle are 2.70 and 62.26% respectively in Table. 9. From the results reported in Table 8 and Table 9, it can be deduced that the optimization allowed a decrease in the
power consumed by the compressors of 2.82%, a decrease in the exergy destruction of the cycle of 7.23%; an improvement of the COP and exergy efficiency of 1.48% and 3.64% respectively compared to the basic cycle. The results of the APCI cycle performance optimization obtained during this study are shown in Table 10 and compared with those of the literature. It is seen that the results are in agreement with previously published studies; they show a gain in compressor power consumption, a decrease in exergy losses and an improvement in the COP and exergy efficiency of the basic cycle studied. The differences between the recorded performances are due to the difference between the parameters of the operating conditions of these cycles (temperature, pressure, flow rate, chemical composition of MR and NG). The enhancement of the COP and exergy efficiency will result in a considerable reduction in NG consumption of the APCI process, hence an economic gain for the LNG Skikda Company.
Table 10. Comparison of APCI cycle optimization results with the literature Performances APCI cycle
Finally, the results obtained for the performances of the cycle APCI Skikda are in good agreement with the literature.
Conclusions
The mixed refrigeration cycle of the LNG- APCI Skikda process was thermodynamically studied. The results of the energy analysis showed that the net power of the basic APCI cycle is about 102.35 MW and its COP is 2.66. Exergy analysis pinpointed components whose irreversibility is high. The results of the exergy analysis showed that the total exergy destruction of the cycle is approximately 41 MW and its exergy efficiency is 60%. Compressors are the main energy consumer in the APCI process; they occupy with chillers the highest rate of the total exergy destruction 30.43% and 22.17% respectively. The reduction of their exergy losses can be achieved by an adequate choice of the compression ratio as well as the inlet temperature. In order to increase the performance of the APCI cycle, some key parameters have been analyzed. The results of the numerical simulation show that the compressor and expander inlet temperature as well as the NG temperature after cooling in the MCHE affect the COP and the exergy efficiency of the APCI cycle. COP and exergy efficiency will increase with decreasing compressor and expander inlet temperature and likewise with decreasing MCHE NG outlet temperature. To improve the performance of the basic cycle, an optimization was carried. The GA was used as an optimization method considering the net energy consumption as an objective function for the cycle optimization. The optimization results indicate that the power consumed by the compressors is reduced by 2.82% and the exergy destruction of the cycle by 7.23%. The optimal COP and exergy efficiency of the cycle are 2.70 and 62.26% respectively. They are improved by 1.48% and 3.64% respectively.
Nomenclature
Specific exergy, kJ/kg Exergy, MW Enthalpy, kJ/kg Enthalpy at constant entropy, kJ/kg Flow rate, kg/s Pressure, bar Rate of heat flow, MW Entropy, kJ/kg. K Temperature, K Power, MW Vapor fraction
Exergy efficiency Expander isentropic efficiency Exergy destruction
Abbreviations
APCI Air Products and Chemicals Inc C Compressor C3MR Propane pre-cooled mixed refrigerant COP Coefficient of performance KBO Knowledge Based Optimization LNG Liquefied Natural Gas MCHE Main Cryogenic Heat Exchanger MR Mixed Refrigerant NG Natural Gas SMR Single Mixed Refrigerant
Data Availability Statement
The authors confirm that the data that supports the findings of this study are available within the article. Raw data that support the finding of this study are available from the corresponding author, upon reasonable request.
Conflict Of Interest
The author declared no potential conflicts of interest with respect to the research, authorship, and/or publication of this article.
Ethics
There are no ethical issues with the publication of this manuscript.
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DERBAL, C.; HAOUAM, A. Thermodynamic analysis of the apci skikda liquefaction process. Journal of Thermal Engineering 2023, Vol. 9, pp. 786-798. https://doi.org/10.18186/thermal.1300835

