Abstract—Design of a gas turbine combustor is still difficult and an uncertain part of aero engine design process because of complex simultaneous processes such as turbulent mixing, reaction, multiphase flow and heat transfer. Therefore, having a proven design and experimental methodologies is so important to achieve combustor design targets in aero engine gas turbine projects. The present work provides an overview of an aero gas turbine combustor with airblast atomizer design, production and rig test process.
Index Terms—Combustor, turbojet, propulsion, airblast atomizer, gas turbine.
Ahmet Topal is with TUSAŞ Motor Sanayii A.Ş., Eskişehir, 26003, Turkey (e-mail: ahmet.topal@tei.com.tr).
Onder Turan is with Anadolu University, Faculty of Aeronautics and Astronautics, TR-26470, Eskisehir, Turkey (e-mail: onderturan@anadolu.edu.tr)
Sıtkı Uslu is with TOBB University of Economics and Technology, Department of Mechanical Engineering, Sogutozu Cad. No. 43, 06560 Ankara/Turkey (e-mail: suslu@tobbetu.edu.tr).
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Cite: Ahmet Topal, Onder Turan, and Sıtkı Uslu, "Design, Manufacturing and Rig Test of a Small Turbojet Engine Combustor with Airblast Atomizer," International Journal of Materials, Mechanics and Manufacturing vol. 3, no. 2, pp. 97-100, 2015.
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