2019
DOI: 10.1051/e3sconf/201912801027
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Thermal performance of a gas turbine based on an exergy analysis

Abstract: This work concerns the calculation and the analysis of the thermal performance of the components ofan MS 7001 type gas turbine with a nominal power of 87 MW using the concept of exergy. The exergy balance is used in addition to the energy balance to estimate the irreversibility of the air compressor, the combustion chamber and the turbine. The exergy analysis is carried out by applying the equilibrium equations obtained from the general definitions of the irreversibility of the thermodynamic processes and the … Show more

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Cited by 7 publications
(5 citation statements)
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“…Also, it gets less than the standard temperature of 15 • C. Moreover, the lower exergy efficiency obtained in higher Ta. Also, it gets less than the standard temperature of 15 • C, which is consistent with most recent researchers [15,16,22]. The obtained results clearly show the effect of temperature on the energy efficiency available for the simulation results.…”
Section: Effect Of Change In T a On The Exergy Efficiencysupporting
confidence: 90%
“…Also, it gets less than the standard temperature of 15 • C. Moreover, the lower exergy efficiency obtained in higher Ta. Also, it gets less than the standard temperature of 15 • C, which is consistent with most recent researchers [15,16,22]. The obtained results clearly show the effect of temperature on the energy efficiency available for the simulation results.…”
Section: Effect Of Change In T a On The Exergy Efficiencysupporting
confidence: 90%
“…Investigations dealing with experimental investigations based on second law in gas turbines and power plants are rarely reported [ 57 , 58 , 59 , 60 , 61 , 62 ]. Regarding gas turbines, Ibrahim et al [ 57 ] conducted energy and exergy analysis of gas turbine power plants, including the compressor, combustion chamber and turbine.…”
Section: Experimental Investigations and 1d Calculations Of Exergy An...mentioning
confidence: 99%
“… Application Components with Reacting Flow 1D RANS LES DNS Entropy Source Terms Calculation Method Exp. Power plant Combustion Chamber [ 57 , 58 , 59 , 60 , 61 , 63 , 65 , 67 , 68 ] - - - Skeletal [ 57 , 58 , 68 ] Stationary gas turbine Combustion Chamber [ 71 , 72 , 73 ] - - - Skeletal - Aircraft gas turbine Combustion Chamber [ 74 , 75 , 76 , 77 , 78 , 79 ] - - …”
Section: Table A1mentioning
confidence: 99%
“…MS-7001 turbine is a special purpose gas turbine produced by General Electric (GE) which is used in various industrial applications. It is important to note that the feasibility of an intake air cooling system for MS-7001 turbine will depend on the particular specifications and installation conditions (Haouam et al, 2019 andKhawaji et al, 1997).…”
Section: Introductionmentioning
confidence: 99%