Improvement of Gas Turbine Performance Using Multi-Stage Inlet Air Cooling System

Authors

  • Hisham Tolba Mechanical Power Engineering Department, Faculty of Engineering-Mattaria, Helwan university, Cairo, Egypt.
  • Rafea A. El-Maksoud Mechanical Power Engineering Department, Faculty of Engineering-Mattaria, Helwan university, Cairo, Egypt.
  • Karim Emara Mechanical Power Engineering Department, Faculty of Engineering-Mattaria, Helwan university, Cairo, Egypt.

Keywords:

Gas turbine, inlet air, cooling system, fogging cooling system, chiller cooling system, performance

Abstract

Gas turbines play a significant role as an energy source if it has been designed according to the ISO operating conditions taking into consideration the operating conditions varied with the variation of the ambient conditions.

This work aims to determine the effect of many parameters like the temperature at the compressor inlet, relative humidity, pressure ratios, and polytropic efficiency on each component of gas turbine performance (compressor, combustion chamber, and turbine). In this work, the Engineering Equation Solver (EES) software is used to calculate exergy destruction, net power, and all efficiencies (1st law and 2nd efficiency). After that, the validation of the code generated through EES software is performed using the actual performance data from the Heliopolis gas turbine power plant 25 MW. model, (GE GT-TM) made by GE.

The results show the performance of the overall gas turbine behaves with and without a multi-stage cooling system.

 In addition, the effect of using the new inlet air cooling system on the gas turbine performance improvement under different conditions is determined. It is worth mentioning that the maximum power output increase is about 14.3% at the maximum ambient temperature (313oK). While the change of the 1st low efficiency and the 2nd low efficiency are so small it could be neglected. Also, the results illustrate that first and second law efficiencies provide quantitative and qualitative compressor performance assessments.

The present multi-stage cooling system reduces the back-period cost if it uses a chiller system. Adding a chilling system before the fogging cooling system reflects the downsizing of the chilling system. This means low initial capital investment costs and low total annual costs. In addition, the multi-stage cooling system capital cost will be cashback during the first year regarding recovered power price

References

Mohtaram Soheil, Chen Wen, T. Zargar, Ji Lin, "Energy-exergy analysis of compressor pressure ratio effects on thermodynamic performance of ammonia water combined cycle", Energy Conversion and Management 134 (2017).

R. K. Dinindu, "Effect of cooling charge air on the gas turbine performance and feasibility of using absorption refrigeration in the “Kelanitissa” power station, Sri Lanka", Master of Science Thesis, STOCKHOLM, (2014).

N.N. Farah, Espindola Juan, M. S. Osama, and S. Amano Ryoichi, "Energy, Exergy, and Emission Analysis on Industrial Air Compressors”, Journal of Energy Resources Technology, (2021).

M. M. El-Awad, M. A. Siraj and H. A. Saeed, "Feasibility of Gas Turbine's Inlet-Air Cooling by Air Washing and Evaporative Cooling in the Dry and Hot Climate ", UofKEJ Vol. 2 Issue 1 pp. 10-15 (February2012).

K. Ibrahim Thamir, M. M. Rahman, and N. Abdalla Ahmed, " Optimum Gas Turbine Configuration for Improving the performance of Combined Cycle Power Plant", Available online at www.sciencedirect.com, Procedia Engineering 15, 4216 – 4223, (2011).

S.K. Abhishek, A. Singhania, A. Kumar, R. Ranendra, and M.B. Kumar, " Improvement of Gas Turbine Power Plant Performance: A Review", International Journal of Innovative Research in Engineering & Management (IJIREM) ISSN: 2350-0557, Volume-4, Issue-3, (May-2017).

Siemens Power and Gas Division, Bid Ref. No. EG1020 (2015/05) PG ES SGEA PROP, II_0004010000_EG1020 _ EKH_ Gas Compressor_R2.doc, Rev:2, Vol / Section: II / 0.4.1, page: 7 of 9, EEHC, Cairo Egypt, (2015).

S.H. Yousef, Najjar, and M. Ahmad Abubaker, "Indirect evaporative combined inlet air cooling with gas turbines for green power technology", international journal of refrigeration 59, (2015) 235–250.

Masheiti Salah, Abdusamad Jamal, Shamekh Awad, and Bodalal Awad, " Improvement of overall performance of Benghazi North combined power plant by retrofitting the Inlet Cooling with a single effect absorption chiller", 3rd International Conference on Renewable Energies for Developing Countries (REDEC), (2016).

B. Mohanty, and G. Paloso, “Enhancing gas turbine performance by intake air cooling using an absorption chiller”. Heat Recovery Systems and CHP 15 41-50, (1995).

D.A. Kolp, W.M. Flye, and H.A. Guidotti, “Advantages of air conditioning and supercharging an LM6000 gas turbine inlet, engineering for gas turbine and power”, Transactions of the ASME 117, 513–527, (1995).

Kareem Emara, Ahmed Emara, El Sayed Abdel Razek, “Turbocharger Selection and Matching Criteria in A Heavy-Duty Diesel Engine”, International Journal of Scientific & Engineering Research Volume 7, Issue 12, December-2016 ISSN 2229-5518.

K.N. Abdalla, and Z.A.M. Adam, “Enhancing gas turbine output through inlet air cooling”. Sudan Engineering Society Journal 7-14 52, (2006).

Abdelghany Tarek, "Effect of Climatic Conditions on Gas Turbines Performance", Master of Science Thesis, Helwan University, Cairo, (2021).

S.S. Ali and Safari Mahbod, " Study and Comparison of Inlet Air Cooling Technique of Gas Turbines and Their Effects on Increase of the Efficiency and Outlet Power", International Journal of Materials, Mechanics and Manufacturing, Vol. 2, No. 4, (November 2014).

Saleh S. Baakeem, Jamel Orfi, Hany Al-Ansary,” Performance improvement of gas turbine power plants by utilizing turbine inlet air-cooling (TIAC) technologies in Riyadh, Saudi Arabia”, Applied Thermal Engineering, Volume 138, 25 June 2018, Pages 417-432.

Muhammad Reshaeel, Adeel Javed, Ahmad Jamil, Majid Ali, Mariam Mahmood, Adeel Waqas, “Multiparametric optimization of a reheated organic Rankine cycle for waste heat recovery-based repowering of a degraded combined cycle gas turbine power plant”, Energy Conversion and Management, Volume 254, 15 February 2022, 115237.

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Published

2022-03-19

How to Cite

Tolba , H., A. El-Maksoud, R., & Emara, K. (2022). Improvement of Gas Turbine Performance Using Multi-Stage Inlet Air Cooling System. International Journal of Sciences: Basic and Applied Research (IJSBAR), 62(1), 79–95. Retrieved from https://www.gssrr.org/index.php/JournalOfBasicAndApplied/article/view/13887

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