PRELIMINARY DESIGN OF GAS TURBINE WITH MULTI-SPOOL (CASE STUDY : M701F GAS TURBINE)

Energy transition is of particular concern to the Indonesian government at the moment. Until 2023, the increase in PLN's power generation capacity has been dominated by an increase in the capacity of PLTGU and PLTG. Until 2022, the total generating capacity of PLTU and PLTGU reached 32.4% of PL...

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Main Author: Syamsa Ramadan, Muhammad
Format: Final Project
Language:Indonesia
Online Access:https://digilib.itb.ac.id/gdl/view/87182
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Institution: Institut Teknologi Bandung
Language: Indonesia
id id-itb.:87182
spelling id-itb.:871822025-01-16T08:47:09ZPRELIMINARY DESIGN OF GAS TURBINE WITH MULTI-SPOOL (CASE STUDY : M701F GAS TURBINE) Syamsa Ramadan, Muhammad Indonesia Final Project Gas Turbine, Preliminary Design, Performance, mean-line design INSTITUT TEKNOLOGI BANDUNG https://digilib.itb.ac.id/gdl/view/87182 Energy transition is of particular concern to the Indonesian government at the moment. Until 2023, the increase in PLN's power generation capacity has been dominated by an increase in the capacity of PLTGU and PLTG. Until 2022, the total generating capacity of PLTU and PLTGU reached 32.4% of PLN's total generation. So that gas turbines can be said to be an important component in electricity generation in Indonesia for the present and the future. This study begins by conducting parametric analyses for single-spool and multi-spool gas turbines. The design of the compressor and turbine is done using the mean-line design method. The combustion chamber design is conducted using zero-dimensional analysis. The turbine in the multi-spool consists of a gas turbine generator and a power turbine as a power generator. The design calculation results were validated with gas turbine on the field. The calculation results of the multi-spool design are compared with the single-spool to determine the effect of configuration changes. The results showed a net power of 398.44 MW, thermal efficiency of 45.67%, heat rate of 8530 kJ/kWh, flue gas temperature of 894.20 K, flue gas mass flow rate of 748 kg/s, compressor pressure ratio of 21, combustion chamber volume of 2.10 m3. The multi spool configuration gave a decrease in turbine outlet diameter 0.41 m with the same performance as single-spool gas turbine. text
institution Institut Teknologi Bandung
building Institut Teknologi Bandung Library
continent Asia
country Indonesia
Indonesia
content_provider Institut Teknologi Bandung
collection Digital ITB
language Indonesia
description Energy transition is of particular concern to the Indonesian government at the moment. Until 2023, the increase in PLN's power generation capacity has been dominated by an increase in the capacity of PLTGU and PLTG. Until 2022, the total generating capacity of PLTU and PLTGU reached 32.4% of PLN's total generation. So that gas turbines can be said to be an important component in electricity generation in Indonesia for the present and the future. This study begins by conducting parametric analyses for single-spool and multi-spool gas turbines. The design of the compressor and turbine is done using the mean-line design method. The combustion chamber design is conducted using zero-dimensional analysis. The turbine in the multi-spool consists of a gas turbine generator and a power turbine as a power generator. The design calculation results were validated with gas turbine on the field. The calculation results of the multi-spool design are compared with the single-spool to determine the effect of configuration changes. The results showed a net power of 398.44 MW, thermal efficiency of 45.67%, heat rate of 8530 kJ/kWh, flue gas temperature of 894.20 K, flue gas mass flow rate of 748 kg/s, compressor pressure ratio of 21, combustion chamber volume of 2.10 m3. The multi spool configuration gave a decrease in turbine outlet diameter 0.41 m with the same performance as single-spool gas turbine.
format Final Project
author Syamsa Ramadan, Muhammad
spellingShingle Syamsa Ramadan, Muhammad
PRELIMINARY DESIGN OF GAS TURBINE WITH MULTI-SPOOL (CASE STUDY : M701F GAS TURBINE)
author_facet Syamsa Ramadan, Muhammad
author_sort Syamsa Ramadan, Muhammad
title PRELIMINARY DESIGN OF GAS TURBINE WITH MULTI-SPOOL (CASE STUDY : M701F GAS TURBINE)
title_short PRELIMINARY DESIGN OF GAS TURBINE WITH MULTI-SPOOL (CASE STUDY : M701F GAS TURBINE)
title_full PRELIMINARY DESIGN OF GAS TURBINE WITH MULTI-SPOOL (CASE STUDY : M701F GAS TURBINE)
title_fullStr PRELIMINARY DESIGN OF GAS TURBINE WITH MULTI-SPOOL (CASE STUDY : M701F GAS TURBINE)
title_full_unstemmed PRELIMINARY DESIGN OF GAS TURBINE WITH MULTI-SPOOL (CASE STUDY : M701F GAS TURBINE)
title_sort preliminary design of gas turbine with multi-spool (case study : m701f gas turbine)
url https://digilib.itb.ac.id/gdl/view/87182
_version_ 1822011306032496640