Preliminary Design of Heavy Duty Industrial Gas Turbine
ElDemerdash, A., ElShaer, A., Hamid, A., khairy, A., Samir, A., Shehta, A., Maher, A., Adel, M., Elgamal, M., El-Sayed, A., Emeara, M. (2017). Preliminary Design of Heavy Duty Industrial Gas Turbine. EKB Journal Management System, 2(Second International Undergraduate Research Conference, IUGRC), 52-52. doi: 10.21608/iugrc.2017.90665
Ahmed ElDemerdash; Ahmed ElShaer; Ahmed Hamid; Ahmed khairy; Ahmed Samir; Ahmed Shehta; Andrew Maher; Mohamed Adel; Mostafa Elgamal; Ahmed F. El-Sayed; Mohamed S. Emeara. "Preliminary Design of Heavy Duty Industrial Gas Turbine". EKB Journal Management System, 2, Second International Undergraduate Research Conference, IUGRC, 2017, 52-52. doi: 10.21608/iugrc.2017.90665
ElDemerdash, A., ElShaer, A., Hamid, A., khairy, A., Samir, A., Shehta, A., Maher, A., Adel, M., Elgamal, M., El-Sayed, A., Emeara, M. (2017). 'Preliminary Design of Heavy Duty Industrial Gas Turbine', EKB Journal Management System, 2(Second International Undergraduate Research Conference, IUGRC), pp. 52-52. doi: 10.21608/iugrc.2017.90665
ElDemerdash, A., ElShaer, A., Hamid, A., khairy, A., Samir, A., Shehta, A., Maher, A., Adel, M., Elgamal, M., El-Sayed, A., Emeara, M. Preliminary Design of Heavy Duty Industrial Gas Turbine. EKB Journal Management System, 2017; 2(Second International Undergraduate Research Conference, IUGRC): 52-52. doi: 10.21608/iugrc.2017.90665

Preliminary Design of Heavy Duty Industrial Gas Turbine

The International Undergraduate Research Conference
Article 39, Volume 2, Second International Undergraduate Research Conference, IUGRC, 2017, Page 52-52  XML PDF (553.27 K)
Document Type: Original Article
DOI: 10.21608/iugrc.2017.90665
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Authors
Ahmed ElDemerdash1; Ahmed ElShaer1; Ahmed Hamid1; Ahmed khairy1; Ahmed Samir1; Ahmed Shehta1; Andrew Maher1; Mohamed Adel1; Mostafa Elgamal1; Ahmed F. El-Sayed2; Mohamed S. Emeara3
1Zagazig University, Egypt.
2Professor of Aerospace and Mechanical Engineering, Mechanical Power Dept., Faculty of Engineering, Zagazig University, Egypt.
3Lecturer Assistant, Mechanical Power Dept., Faculty of Engineering, Zagazig University, Egypt.
Abstract
Industrial gas-turbine engine had many developments in the past 60 years and becomes the common power plant. Egypt, middle east and Africa is considered one of the biggest region for gas turbine markets. The main aim of the present project is to submit a preliminary design for gas turbine. This is to improve engine performance in the world markets. Engine developments in gas-turbine design have endeavors of larger net-power, low noise and emission as well as better fuel economy. These goals were achieved by increasing of the compressor pressure ratio (PR), turbine inlet temperature (TIT) as well as using modifications of gas-turbine cycle and cooling techniques for both turbines and combustion chamber. Such modifications led to improvements in cycle efficiency, decreases in specific fuel consumption (SFC) and increase the net power. This paper presents a parametric study and design point selection of a heavy duty industrial gas-turbine engine (close to GE-F9). This engine is one of the products of GE Aviation Company. Performance analysis is performed using MATLAB program codes.
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