Rancang Bangun Ignition System Untuk Turbocharger Gas Turbine Engine dengan Inducer Diameter 1,75 Inch

  • M. Zuhal Fachri A Politeknik Penerbangan Indonesia Curug
  • Wira Gauthama Politeknik Penerbangan Indonesia Curug
  • Zulham Hidayat Politeknik Penerbangan Indonesia Curug
Keywords: gas turbine engine, ignition system, turbocharger

Abstract

Turbocharger is a centrifugal compressor that obtain  power from turbines whose power source comes from vehicle exhaust gases. In this design, the turbocharger acts as  the compressor and turbine functions. The goal of designing the ignition system is that the system can produce strong sparks which  burn the fuel  entering the combustion chamber. Thus maintaining the operational of the engine. From the calculation, it was found that the energy  required  to burn 0.013 kg / s LPG gas was 0.164 kW and the energy generated  from the ignition system design was 326,286 kW. In conclusion, the ignition system can supply the amount of   energy to burn 0.0013 kg / s LPG gas. In the turbocharger experiment, the gas turbine engine can light up and operate normally and continuously.

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Published
2021-06-30
How to Cite
1.
M. Zuhal Fachri A, Wira Gauthama, Hidayat Z. Rancang Bangun Ignition System Untuk Turbocharger Gas Turbine Engine dengan Inducer Diameter 1,75 Inch. JIA [Internet]. 2021Jun.30 [cited 2024Apr.24];14(02):7-16. Available from: https://journal.ppicurug.ac.id/index.php/jurnal-ilmiah-aviasi/article/view/405