Article Per Year (5 Year)
p-Index From 2020 - 2025
0.562
P-Index
This Author published in this journals
All Journal Langit Biru: Jurnal Ilmiah Aviasi
M. Zuhal Fachri A
Politeknik Penerbangan Indonesia Curug
Decision Sciences, Operations Research & Management Education Engineering Environmental Science Transportation

Published : 3 Documents Claim Missing Document
Claim Missing Document
Check
Articles

Found 3 Documents
Search

 1 
Rancang Bangun Ignition System Untuk Turbocharger Gas Turbine Engine dengan Inducer Diameter 1,75 Inch M. Zuhal Fachri A; Wira Gauthama; Zulham Hidayat
Langit Biru: Jurnal Ilmiah Aviasi Vol 14 No 02 (2021): Langit Biru: Jurnal Ilmiah Aviasi
Publisher : Politeknik Penerbangan Indonesia Curug

Show Abstract | Download Original | Original Source | Check in Google Scholar | DOI: 10.54147/langitbiru.v14i02.405

Abstract

Turbocharger adalah sebuah kompresor sentrifugal yang mendapat daya dari turbin yang sumber tenaganya berasal dari gas buang mesin. Pada perancangan ini turbocharger digunakan sebagai pengganti dari fungsi compressor dan turbine. Target dalam perancangan ignition system ini adalah dapat menghasilkan percikan api yang kuat sehingga mampu membakar bahan bakar yang masuk kedalam ruang bakar. Dari hasil pehitungan, didapatkan bahwa energi yang diperlukan untuk membakar 0,013 kg/s gas LPG sebesar 0,164 kW dan energi yang dihasilkan dari rancang bangun ignition system sebesar 326,286 kW. Dari hasil perhitungan maka rancang bangun ignition system yang penulis rancang dapat memenuhi energi untuk membakar 0,0013 kg/s gas LPG. Pada proses uji coba turbocharger gas turbine engine didapatkan bahwa engine dapat menyala secara continuous.
Rancang Bangun Ignition System Untuk Turbocharger Gas Turbine Engine dengan Inducer Diameter 1,75 Inch M. Zuhal Fachri A; Wira Gauthama; Zulham Hidayat
Langit Biru: Jurnal Ilmiah Aviasi Vol 14 No 02 (2021): Langit Biru: Jurnal Ilmiah Aviasi
Publisher : Politeknik Penerbangan Indonesia Curug

Show Abstract | Download Original | Original Source | Check in Google Scholar | DOI: 10.54147/langitbiru.v14i02.405

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.
Rancang Bangun Ignition System Untuk Turbocharger Gas Turbine Engine dengan Inducer Diameter 1,75 Inch M. Zuhal Fachri A; Wira Gauthama; Zulham Hidayat
Langit Biru: Jurnal Ilmiah Aviasi Vol 14 No 02 (2021): Langit Biru: Jurnal Ilmiah Aviasi
Publisher : Politeknik Penerbangan Indonesia Curug

Show Abstract | Download Original | Original Source | Check in Google Scholar | DOI: 10.54147/langitbiru.v14i02.405

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.
Co-Authors Wira Gauthama Zulham Hidayat