Journal of Technology in Aerospace Engineering

Journal of Technology in Aerospace Engineering

Analysis, Design and Development of a Mini Jet Turbocharged Engine for Use in a Thermotronic Laboratory

Document Type : Scientific Extension

Authors
Kamyar Nikzadfar 1
Mahdi Garivani 2
Amir H. Zabihi 3
Ali Rezaei 4
1 Assistant Professor, Department of Mechanical Engineering, Babol Noshirvani University of Technology، Babol، Iran.
2 Researcher, epartment of Mechanical Engineering, Babol Noshirvani University of Technology. Babol.Iran
3 M. Sc. Student, Department of Mechanical Engineering, Babol Noshirvani University of Technology، Babol، Iran
4 B. Sc. Student, Department of Mechanical Engineering, Babol Noshirvani University of Technology، Babol، Iran
Abstract
Giventhe importance of air engine control systems and the necessity of developing this specialty in the country, the establishment of appropriate infrastructures for implementing applied research in this section field is very important. In order to establish a jet engine thermotronic control laboratory at Babol noshirvani University of Technology, an effort has been made to develop a turbojet engine cycle with measuring and control equipment.The turbocharger is used as the heart of the Brighton cycle in order to maintain the simplicity and functionality of the engine and change the performance parameters of the engine.The developed engine includes: refueling, fueling, combustion chamber, cooling, lubrication and measurement. After the initial design, Substandard has been manufactured and assembled. Finally, using the governing equations for the motor subtypes, the overall engine performance is analyzed and the engine's operation points are analyzed.
Keywords
Mini jet Engine
Thermotronic
Turbocharger
Jet Engine Control
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  • Receive Date 10 January 2019
  • Revise Date 13 May 2019
  • Accept Date 02 November 2019
  • First Publish Date 02 November 2019