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

Kamyar Nikzadfar, Mahdi Garivani, Amir Hossein Zabihi, Ali Rezaie

Research output: Contribution to journalArticlepeer-review

Abstract

Given the 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.
Original languageEnglish
Pages (from-to)1-11
Number of pages11
JournalJournal of Technology in Aerospace Engineering
Volume3
Issue number1
Publication statusPublished - 2 Jul 2019
Externally publishedYes

Keywords

  • Mini jet engine
  • Thermotronic
  • Turbocharger
  • Jet engine control

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