Gas Turbine Exhaust Research Articles

A Custom, High-Channel Count Data Acquisition System for Chemical Species Tomography of Aero-Jet Engine Exhaust Plumes

The fiber-laser imaging of gas turbine exhaust species project aims to provide a video-rate imaging (100 frames/s) diagnostic tool for application to the exhaust plumes of the largest civil aero-jet engines. This remit, enabled by chemical species tomography (CST) currently targeting carbon dioxide (CO2), requires system design that facilitates expansion of multiple parameters. Scalability is needed in order to increase imaging speeds and spatial resolutions and extends the system toward other pertinent gases such as the oxides of nitrogen and sulfur and unburnt hydrocarbons. This paper presents a fully scalable, noninvasive instrument for installation in a commercial engine testing facility, technical challenges having been tackled iteratively through bespoke optical and mechanical design, and it specifically presents the high-speed data acquisition (DAQ) system required. Measurement of gas species concentration is implemented by tunable diode laser absorption with wavelength modulation spectroscopy (TDLAS-WMS) using a custom, high-speed 10–40-MS/s/channel 14-bit DAQ. For CO2 tomography, the system uses six angular projections of 21 beams each. However, the presented DAQ has capacity for 192 fully parallel 10-Hz–3-MHz differential inputs, achieving a best-case signal-to-noise ratio (SNR) of 56.5 dB prior to filtering. A 12 Ethernet-connected digitization nodes based on field-programmable gate array technology with software control are distributed around a 7-m-diameter mounting “ring.” Hence, the high data rates of 8.96-Gb/s per printed circuit board and 107.52 Gb/s for the whole system can be reduced by using local digital lock-in amplifiers. We believe that this DAQ system is unique in both the TDLAS and CST literatures.

Gas Turbine Exhaust System Health Management Based on Recurrent Neural Networks

Predictive maintenance of gas turbine exhaust system plays an important role in reducing the risk of failure and improving the safety of gas turbine operation. This paper proposed an effective method based on the recurrent neural networks (RNNs) and statistical process control chart to predict the condition of the gas turbine exhaust system. Firstly, the fuel flow and air flow of the input gas chamber are used to predict exhaust gas temperature by an RNN model. Secondly, an Xbar-s statistical process control chart is constructed via comparing the current exhaust gas temperature predicted by RNN with that measured by sensors. Then the chart can be used to monitor whether there are failures in gas turbine exhaust system and temperature sensors. This is the first time that recurrent neural networks are used to address the health management of gas turbine exhaust system. And the sensor failure is also taken into consideration. Finally, the proposed approach is evaluated in the numerical experiment.

Southern Iraq gas station conversation to integrated solar combined cycle

Iraq has a big shortage in the electrical system and this is because of repeated wars that have destroyed the country’s economy and infrastructure. In order to improve the situation and progress of the country we see that the exploitation of huge and neglected land, where Iraq has a very featured site can make it a factory for the production of electric power through the exploitation of the vast areas as fields of cells and solar plants to produce electricity. Iraq is characterized by the number of sunny hours during the year and estimated more than 3300 hours. Also, the solar radiation in Iraq, which exceeds 2000 kWh/m2. Where the production of electricity enough to meet the needs of Iraq and neighboring countries. In this paper we will discuss the development of gas station in southern Iraq by taking advantage of the sun’s rays falling and recycling of combustion products from the gas station. The plant consists of 200MW conventional gas turbine plant and two steam turbines of 75MW and 65MW powered by the solar field and gas turbine exhaust. With high insolation during the summer month of June the plant can achieve up to 25% of solar fraction with Integrated Solar Combined Cycle (ISCC) plant.

ВИБІР ТЕПЛОВОГО НАВАНТАЖЕННЯ АПАРАТІВ ОХОЛОДЖЕННЯ ПОВІТРЯ НА ВХОДІ ГТУ В РІЗНИХ КЛІМАТИЧНИХ УМОВАХ

It is proposed the definition of the installed (rational) refrigeration capacity of a waste heat-recovery absorption-ejector chiller that utilizes the heat of the exhaust gases of a gas turbine unite to cool the air at the inlet. Since the effect of air cooling, in particular in the form of a reduction in the specific fuel consumption, depends on its depth (the magnitude of the decrease in air temperature) and duration, it is proposed to determine it by the annual fuel economy. As an example of air cooling at the inlet of a gas turbine unit, the value of reducing specific fuel consumption due to cooling the air at the inlet to the temperature of 15 °C by an absorption lithium-bromide chiller and two-stage air cooling: to a temperature of 15 °C in an absorption lithium-bromide chiller and down to 10 °C – in a refrigerant ejector chiller as the stages of a two-stage absorption-ejector chiller, depending on the installed (design) refrigeration capacity is analyzed.It is shown that proceeding from the different rate of increment of the annual reduction in the specific fuel consumption due to the change in the thermal load in accordance with the current climatic conditions, it is necessary to choose such design heat load for the air cooling system (installed refrigeration capacity of the chillers), which ensures the achievement of the maximum or close to annual reduction in the specific fuel consumption at relatively high rates of its increment. In order to determine the installed refrigeration capacity, which ensures the maximum annual refrigeration capacity (annual production of cold), the dependence of the increment of annual fuel economy from the installed refrigeration capacity is analyzed. Based on the results of the investigation, it was proposed to determine the rational thermal load of the air cooling system (installed - the design refrigeration capacity of the chiller) in accordance with the changing climatic conditions of operation during the year, which provides a maximum annual reduction in the specific fuel consumption at relatively high rates of its increment

Gas turbine exhaust gas heat recovery by organic Rankine cycles (ORC) for offshore combined heat and power applications - Energy and exergy analysis

Effective heat and power supply to offshore installations leads to environmental benefits, but the efficiency is often limited by requirements and constraints connected to the offshore environment. An exergetic analysis of gas turbines exhaust heat recovery on offshore platforms is performed to identify optimal approaches to produce heat and power. Two different configurations are presented, with heat delivery at two temperature levels and power production by an organic Rankine cycle (ORC). In one system (cascade), the high temperature heat is taken from the exhaust after the ORC, while low temperature heat is taken from the ORC condenser. Alternatively, high and low temperature heat is taken from the exhaust gas before the ORC feeds on the remaining exhaust thermal energy (series system). Four different working fluids (three siloxanes, one refrigerant) are considered. In addition, the exergetic effects of the heat loads and heat source temperatures are investigated. The results revealed that MM and R124 are the best working fluids for the cascade and series system, respectively. A recuperated ORC in the series system improve the siloxane results, with MM as the best working fluid. Moreover, decreasing the ORC minimum pressure in the series system makes considerable improvement.

Design optimisation of separate-jet exhausts for the next generation of civil aero-engines

ABSTRACTThe next generation of civil large aero-engines will employ greater bypass ratios compared with contemporary architectures. This results in higher exchange rates between exhaust performance and specific fuel consumption (SFC). Concurrently, the aerodynamic design of the exhaust is expected to play a key role in the success of future turbofans. This paper presents the development of a computational framework for the aerodynamic design of separate-jet exhaust systems for civil aero-engines. A mathematical approach is synthesised based on class-shape transformation (CST) functions for the parametric geometry definition of gas-turbine exhaust components such as annular ducts and nozzles. This geometry formulation is coupled with an automated viscous and compressible flow solution method and a cost-effective design space exploration (DSE) approach. The framework is deployed to optimise the performance of a separate-jet exhaust for very-high-bypass ratio (VHBR) turbofan engine. The optimisations carried out suggest the potential to increase the engine’s net propulsive force compared with a baseline architecture, through optimum exhaust re-design. The proposed method is able to identify and alleviate adverse flow-features that may deteriorate the aerodynamic behaviour of the exhaust system.

Energy and Exergy Analysis of the S-CO2 Brayton Cycle Coupled with Bottoming Cycles

Supercritical carbon dioxide (S-CO2) Brayton cycles (BC) are soon to be a competitive and environment friendly power generation technology. Progressive technological developments in turbo-machineries and heat exchangers have boosted the idea of using S-CO2 in a closed-loop BC. This paper describes and discusses energy and exergy analysis of S-CO2 BC in cascade arrangement with a secondary cycle using CO2, R134a, ammonia, or argon as working fluids. Pressure drop in the cycle is considered, and its effect on the overall performance is investigated. No specific heat source is considered, thus any heat source capable of providing temperature in the range from 500 °C to 850 °C can be utilized, such as solar energy, gas turbine exhaust, nuclear waste heat, etc. The commercial software ‘Aspen HYSYS version 9’ (Aspen Technology, Inc., Bedford, MA, USA) is used for simulations. Comparisons with the literature and simulation results are discussed first for the standalone S-CO2 BC. Energy analysis is done for the combined cycle to inspect the parameters affecting the cycle performance. The second law efficiency is calculated, and exergy losses incurred in different components of the cycle are discussed.

Thermoeconomic analysis and multiobjective optimization of a combined gas turbine, steam, and organic Rankine cycle

AbstractBecause of the fossil fuels crisis in recent years, efficient working of power producing cycles has gained considerable importance. This study presents a detailed exergoeconomic analysis of a proposed combination of a gas turbine (GT), a steam Rankine cycle (SRC), and an organic Rankine cycle (ORC), which are coupled together to obtain the maximum heat recovery of the GT exhaust gas. The proposed cycle was analyzed from both thermodynamic and economic viewpoints. The exergy efficiency and product cost rate of the introduced cycle were optimized simultaneously using multiobjective optimization with seven decision variables, including steam turbine inlet pressure and temperature, ORC turbine inlet pressure, ORC and steam turbine back pressures, and pinch point of heat exchangers. Sensitivity analysis revealed that the steam turbine back pressure and inlet pressure had the highest impact on product cost rate and exergy efficiency, followed by ORC turbine inlet pressure and back pressure. Also, the exergoeconomic analysis showed that the combustion chamber had the highest sum of exergy destruction costs and investment costs; more attention should thus be paid to its design procedure. Under the design conditions, the exergy efficiency of 40.75% and product cost rate of 439 million $/year could be achieved.

Thermoeconomic analysis of a gas turbine and cascaded CO2 combined cycle using thermal oil as an intermediate heat-transfer fluid

This paper reports an investigation of a gas turbine (GT) and two-stage cascaded supercritical and transcritical CO2 (s-CO2/t-CO2) combined power cycle using liquefied natural gas (LNG) as a low-temperature heat sink. This cycle may be well-suited for installation near LNG import terminals. GT exhaust supplies input heat to an intermediate s-CO2 cycle through a thermal oil loop. Waste heat from the s-CO2 cycle and residual heat from the GT cycle drives a lower temperature t-CO2 cycle. The t-CO2 cycle is LNG-cooled. A solution procedure is performed to perform a coupled analysis of the thermodynamic and economic performance of this combined cycle. Results show that the GT-cascade CO2 combined cycle has an optimal operating point determined by the s-CO2 compressor inlet conditions. Genetic algorithm (GA) optimization indicates that a Taurus 60 GT-cascaded CO2 combined cycle could reach 51.44% efficiency. For 20-year lifetime and 5% rate of interest, thermoeconomic optimization (after-tax profit, ATP as objective) results show ATP, levelized cost of electricity (LCOE) and net power are $2.935 × 106, $0.0420 kWh−1 and 8.886 MW, respectively. Findings suggest that the GT-cascaded CO2 combined cycle is an efficient and commercially viable technology for power generation.

Techno-economic analysis of waste heat recovery systems for wet-cooled combined cycle power plants

Increasing ambient temperature negatively impacts the performance of natural gas combined cycle (NGCC) power plants. There have been multiple approaches to mitigate this performance reduction by chilling the compressor inlet air of the gas turbine, as well as by recovering the waste heat emanating from the power plant to generate additional power. In the present study, a detailed techno-economic assessment on the application of different types of waste heat recovery systems used to chill the compressor inlet air has been assessed. A simplified thermodynamic and heat transfer model is developed to predict the performance of an evaporatively cooled NGCC at varying ambient conditions. By taking typical meteorological year (TMY3) hourly weather data for two different locations – Los Angeles, California and Houston, Texas – the yearly output for a 565 MW plant is predicted at a 100% capacity factor. The feasibilities of different waste heat recovery (WHR) systems including a flue gas driven absorption chiller, a steam driven absorption chiller, and an electrically driven vapor compression chiller are assessed by calculating the levelized cost of electricity (LCOE) for each scenario. The results of the analysis showed that, for a fixed WHR system costs (i.e., $ per kWth), the system powered by flue gas generated the smallest LCOE, followed by the mechanically-driven vapor compression, steam-heated chiller, and, finally, the gas turbine exhaust chiller for both the locations at all COP combinations. The analysis also investigated the impact of fixed investments cost, and the flue gas system again yielded the smallest LCOE, while still yielding a lower LCOE than at baseline case over a wide range of COP and tolerable cooling costs for both locations.

Studies on Stepped Air Ejector Diffusers incorporating Heat Transfer Effects

Abstract Air ejector diffusers are employed in gas turbine exhaust systems to cool the exhaust gases. These diffusers are developed as passive devices, which use the energy of the main flow to entrain the relatively cool ambient air through the annular slot openings. Multiple slot openings are provided along the length of ejector diffusers to lower the temperatures of the exhaust gases. This paper presents results of a 3-D numerical study carried out at a fixed Reynolds Number of 2.5×105 with a corresponding inlet Mach number of about 0.22 on three configurations of a non-circular ejector diffuser having an overall area ratio of 9. The three configurations being investigated are the best diffuser configurations established on the basis of cold flow studies reported in literature. The results are presented in terms of temperature distribution, entrainment mass flux rates and static pressure recovery. The results show that the higher number of slot openings improves cooling in the ejector diffuser as compared to thicker interfaces or inclination at the slot inlet.

Exergetic optimization and comparison of combined gas turbine supercritical CO2 power cycles

For developing a sustainable power system, the key is to maximize the use of available resources with a minimal impact on the environment. One technique for achieving this is exhaust heat recovery. In this paper, three gas turbine exhaust heat recovery supercritical carbon dioxide combined power cycles are presented. They are combined gas turbine-recompression cycle, combined gas turbine-preheating cycle, and combined gas turbine-simple regenerative cycle. For all the cycles, thermodynamic models are developed and the influence of varying mass flow rates, compression ratio, and mass split/recompression percentages in different components of all three cycles are investigated. Using genetic algorithm, exergetic optimization is done to find the optimal configuration for each cycle. The reduction in CO2 emissions in presented cycles against fossil fuel power cycles is also assessed. Additionally, a comparison with a simple gas turbine (SGT) and an air bottoming combined cycle (ABC) is presented. The results indicate that owing to exhaust exergy recovery, there is a significant improvement in the energetic and exergetic performance of combined gas turbine-supercritical CO2 power cycles compared to that of SGT and ABC. The sum of exergy destruction and exergy loss in the combined cycles is lower as compared to the sum in SGT. The reduction in losses compared to SGT is 22.89% in the case of the combined gas turbine recompression cycle and 35.8% in the case of the combined gas turbine preheating cycle (CGTPHC). Moreover, the energetic and exergetic performances of the bottoming supercritical CO2 recompression cycles (BRECs) are better than those of the bottoming supercritical CO2 preheating cycle owing to lower exergy destruction in the components of BREC. As a result of comparative analysis based on the exergetic performance and environmental impact, the CGTPHC is selected as an appropriate option for gas turbine exhaust exergy recovery.

Optimization Research of S-CO2 Compound Brayton Cycle Based on Genetic Algorithm

Supercritical carbon dioxide (S-CO2) has the advantages of large density and small viscosity. Being used in the power circulation system, it can make the system compact and reduce the cost, so it has great potential in engineering application. In this paper, the residual heat recycling system with S-CO2 as the working material is studied. The computational model of S-CO2 Brayton cycle is built to analyse its characteristics. The cycle efficiency, output network and other parameters of the bottom cycle under the standard working conditions are obtained. Meanwhile, the parameters of the inlet and outlet of the components are optimized by genetic algorithm, and the parameters of the system components are obtained when the best cycle network is achieved. This study provides some reference for the field of residual heat utilization, including the gas turbine exhaust.

Design and performance investigation of a biogas fueled combined cooling and power generation system

Nowadays, different renewable sources and energy storages are attracting world attention due to the major concerns about the excessive emissions and the global energy crisis. Hence, this paper studies design and performance investigation of a biogas fueled building cooling and power system, which comprises of an air compressor, an air preheater, a combustion chamber, a gas turbine, some compression chillers and aggregated plug-in electric vehicles. In the proposed coproduction facility, biogas is used as an alternative fuel to reduce the total greenhouse gas emissions and increase the economic saving in the consumption of fossil fuels. The feasibility and robust performance of this microgrid is evaluated under extremely-hot summer days. Three compression chillers are installed to satisfy total cooling demand of a large hotel building located in Ahwaz, Iran. Moreover, the total energy requirement of chillers and building electricity demand is supplied through the biogas driven gas turbine cycle. A mid-high temperature waste heat is recovered from the exhaust gases of gas turbine to be used in the air preheating stage. A comprehensive thermodynamic analysis is developed to solve a mixed integer non-linear programming problem with the aim of minimizing total electricity procurement cost of the proposed zero-emission cogeneration micro-plant taking into account the operational constraints of gas turbine cycle, compression chillers, and electric drive vehicles.

소형 터보샤프트 엔진의 구성품 설계

Aerodynamic design of turbomachines inside a small turboshaft engine has been performed. The engine is a twin spool turboshaft engine, which consists of a gas generator and axial type power turbine followed by. The gas generator consists of a centrifugal compressor-radial turbine spool. To minimize specific fuel consumption of the engine, heat exchange occurs between compressor outlet air and power turbine exhaust gas. To supply sufficiently decelerated and radially de-swirled flow to the heat exchanger, two-staged cascade diffuser was introduced at the compressor diffuser row. Mass flow rate is controlled by the radial turbine nozzle throat. The design results showed that aerodynamic performances are higher than design requirements. For this reason, stage matching between adjacent components is required. In this study, stage matching between the radial turbine and the power turbine was considered. CFD result revealed that flow capacity of the axial turbine is high for adequate stage matching, so flow path has been adjusted to produce required power both from radial and axial turbines.

ОХОЛОДЖЕННЯ ПОВІТРЯ НА ВХОДІ ГТУ З ВИКОРИСТАННЯМ РЕЗЕРВУ ХОЛОДОПРОДУКТИВНОСТІ АБСОРБЦІЙНО-ЕЖЕКТОРНОЇ ХОЛОДИЛЬНОЇ МАШИНИ В БУСТЕРНОМУ ПОВІТРООХОЛОДЖУВАЧІ

The processes of gas turbine unit two-stage intake air cooling by absorption lithium-bromide chiller as a high temperature cooling stage to the temperature of about 15 °C and by refrigerant ejector chiller as a low temperature cooling stage to the temperature of about 10 °C through utilizing the turbine exhaust gas waste heat for hour-by-hour changing ambient air temperatures and changeable heat loads on the air coolers as consequence during 10 days of July 2017 (10–12.07.2017) for climatic conditions of the south of Ukraine are analyzed. The computer programs of the firms-producers of heat exchangers were used for gas turbine unit inlet air cooling processes simulation.It is shown that at decreased heat loads on the air coolers an excessive refrigeration capacity of combined absorption-ejector chiller exceeding current heat loads is generated which can be used for covering increased heat loads on the air coolers and to reduce the refrigeration capacity of the absorption-ejector chiller. To solve this task the refrigeration capacity required for gas turbine unit inlet air cooling is compared with an excessive refrigeration capacity of the absorption-ejector chiller exceeding current heat loads summarized during 10 days.The system of gas turbine unit inlet air cooling with a booster stage of precooling air and a base two-stage cooling air to the temperature of about 10 °C by absorption-ejector chiller has been proposed. An excessive refrigeration capacity of the absorption-ejector chiller generated during decreased heat loads on the gas turbine unit inlet air coolers that is collected in the thermal accumulator is used for gas turbine unit inlet air precooling in a booster stage of air coolers during increased heat loads on the air coolers. The results of gas turbine unit inlet air cooling processes simulation proved the reduction of refrigeration capacity of the absorption-ejector chiller by about 50 % due to the use of a booster stage for precooling air at the expanse of an excessive absorption-ejector chiller refrigeration capacity served in the thermal accumulator. The conclusion has been made about the efficient use of a booster stage of gas turbine unit inlet air cooler for precooling air by using an excessive refrigeration potential of absorption-ejector chiller saved in the thermal accumulator

Investigation of a combined molten carbonate fuel cell, gas turbine and Stirling engine combined cooling heating and power (CCHP) process by exergy cost sensitivity analysis

An integrated combined cooling, heating and power process is investigated and analyzed by advanced exergy cost analysis method. In this process molten carbonate fuel cell, gas turbine and Stirling engine are used for providing the required power (6482 kW). A double effect H2O-Li/Br absorption refrigeration cycle supplies 980 kW cooling. Fuel cell exhaust heat is used to drive Stirling engine and absorption chiller. Also, gas turbine exhaust heat is used to produce steam for heating (2136.6 kW). The main result extracted from the endogenous and exogenous parts shows that cost interactions between the equipment in this hybrid system is not strong. Heat exchangers investment cost and exergy destruction cost are avoidable and unavoidable respectively, while opposite behavior is exhibited by the compressors. From avoidable exergy destruction cost point of view, compressor C-1 and from avoidable investment cost point of view, heat exchangers have high improvement potential. Also effects of key parameters on the exergoeconomic factor and exergy destruction cost rate are studied through the sensitivity analysis. Finally, three strategies are recommended for removing the inefficient costs and improving the system performance.

Optimization of Supercritical CO2 Brayton Cycle for Simple Cycle Gas Turbines Exhaust Heat Recovery Using Genetic Algorithm

For the application of waste heat recovery (WHR), supercritical CO2 (S-CO2) Brayton power cycles offer significant suitable advantages such as compactness, low capital cost, and applicability to a broad range of heat source temperatures. The current study is focused on thermodynamic modeling and optimization of recuperated (RC) and recuperated recompression (RRC) configurations of S-CO2 Brayton cycles for exhaust heat recovery from a next generation heavy duty simple cycle gas turbine using genetic algorithm (GA). This nongradient based algorithm yields a simultaneous optimization of key S-CO2 Brayton cycle decision variables such as turbine inlet temperature, pinch point temperature difference, compressor pressure ratio, and mass flow rate of CO2. The main goal of the optimization is to maximize power out of the exhaust stream which makes it single objective optimization. The optimization is based on thermodynamic analysis with suitable practical assumptions which can be varied according to the need of user. The optimal cycle design points are presented for both RC and RRC configurations and comparison of net power output is established for WHR. For the chosen exhaust gas mass flow rate, RRC cycle yields more power output than RC cycle. The main conclusion drawn from the current study is that the choice of best cycle for WHR actually depends heavily on mass flow rate of the exhaust gas. Further, the economic analysis of the more power producing RRC cycle is performed and cost comparison between the optimized RRC cycle and steam Rankine bottoming cycle is presented.

A systematic procedure to optimize Integrated Solar Combined Cycle power plants (ISCCs)

This study aims to find the optimal way to integrate a parabolic trough solar field into a gas fired combined cycle. The combined cycle studied here is composed of a gas turbine and a triple pressure bottoming Rankine cycle. A general layout is proposed and allows the integration of the solar source at all levels of temperature. A thermodynamic model is proposed to evaluate the performance of the system and then coupled to a constrained nonlinear optimization algorithm that uses a hybrid optimization technique combining Particle Swarm Optimization (PSO) and Gravitational Search Algorithm (GSA). This gives the optimal configuration of the heat exchanger networks used to harvest the solar source and the exhaust gases of the gas turbine. The effect of the system’s main parameters on the solar integration performance was investigated such as the amount of the solar heat rate injected to the bottoming cycle, the mass flow rate of the solar source, the inlet temperature of the solar source and the outlet temperatures of the high pressure super-heater n°1 and the re-heater n°1. The approach used here is general and gives finally the real potential of the integration of a parabolic trough solar field into a combined cycle.

Analysis of Efficiency of the Ship Propulsion System with Thermochemical Recuperation of Waste Heat

One of the basic ways to reduce polluting emissions of ship power plants is application of innovative devices for on-board energy generation by means of secondary energy resources. The combined gas turbine and diesel engine plant with thermochemical recuperation of the heat of secondary energy resources has been considered. It is suggested to conduct the study with the help of mathematical modeling methods. The model takes into account basic physical correlations, material and thermal balances, phase equilibrium, and heat and mass transfer processes. The paper provides the results of mathematical modeling of the processes in a gas turbine and diesel engine power plant with thermochemical recuperation of the gas turbine exhaust gas heat by converting a hydrocarbon fuel. In such a plant, it is possible to reduce the specific fuel consumption of the diesel engine by 20%. The waste heat potential in a gas turbine can provide efficient hydrocarbon fuel conversion at the ratio of powers of the diesel and gas turbine engines being up to 6. When the diesel engine and gas turbine operate simultaneously with the use of the LNG vapor conversion products, the efficiency coefficient of the plant increases by 4%–5%.