DESIGN STUDY OF GAS TURBINE-BASED AIRCRAFT ENGINE EXHAUST GAS EMISSION MEASUREMENT SYSTEM

The aviation sector in Indonesia, a vital sector of Indonesia's economic growth and national connectivity, faces challenges related to significant greenhouse gas emissions, particularly carbon dioxide (CO2). The Indonesian government, through the Ministry of Energy and Mineral Resources, has se...

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Main Author: Raynary Fabian, Oktavio
Format: Final Project
Language:Indonesia
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Online Access:https://digilib.itb.ac.id/gdl/view/86355
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Institution: Institut Teknologi Bandung
Language: Indonesia
id id-itb.:86355
spelling id-itb.:863552024-09-17T16:48:09ZDESIGN STUDY OF GAS TURBINE-BASED AIRCRAFT ENGINE EXHAUST GAS EMISSION MEASUREMENT SYSTEM Raynary Fabian, Oktavio Teknik (Rekayasa, enjinering dan kegiatan berkaitan) Indonesia Final Project Bioavtur, Emissions, Exhaust Gas, Aircraft, Regulation, Measurement Systems INSTITUT TEKNOLOGI BANDUNG https://digilib.itb.ac.id/gdl/view/86355 The aviation sector in Indonesia, a vital sector of Indonesia's economic growth and national connectivity, faces challenges related to significant greenhouse gas emissions, particularly carbon dioxide (CO2). The Indonesian government, through the Ministry of Energy and Mineral Resources, has set a target to develop bioavtur with a 5% biofuel content by 2025. This regulation follows the international regulations of the International Civil Aviation Organization (ICAO) and the Environmental Protection Agency (EPA). These regulations set emission standards for pollutants such as particulate matter (PM) and nitrogen oxides (NOx) for aircraft engines. This research focuses on the design of an aircraft emission measurement system, based on the requirements and objectives of the regulations. Key questions involved identifying parameters and methods for measuring aircraft emission gases and evaluating the performance comparison of the current measurement system with existing regulations. The result of this study is the identification of important parameters for measuring aircraft exhaust emissions, namely smoke, hydrocarbons (HC), carbon monoxide (CO), nitrogen oxides (NOx), non-volatile particulate matter mass (nvPM mass), and non-volatile particulate matter number (nvPM number). The six parameters are measured using 3 different test methods. These methods are smoke testing to measure smoke emissions, gas emissions testing to measure HC, CO, and NOx, and nvPM testing to measure nvPM mass and nvPM number. Based on the review, only 2 of the 3 recommended testing methods are gas emission testing and nvPM testing. The recommended measurement system for gas emission testing is the MEXA-1700 because it uses three different methods depending on the gas emissions being measured. The recommended measurement systems for nvPM testing are AVL Micro Soot Sensor 2, AVL CPC and CPC 3750-10 due to their compliance with regulations. For now, it is necessary to search for data on these measurement systems to ensure that the measurement tools can be used for aircraft exhaust emission testing. 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
topic Teknik (Rekayasa, enjinering dan kegiatan berkaitan)
spellingShingle Teknik (Rekayasa, enjinering dan kegiatan berkaitan)
Raynary Fabian, Oktavio
DESIGN STUDY OF GAS TURBINE-BASED AIRCRAFT ENGINE EXHAUST GAS EMISSION MEASUREMENT SYSTEM
description The aviation sector in Indonesia, a vital sector of Indonesia's economic growth and national connectivity, faces challenges related to significant greenhouse gas emissions, particularly carbon dioxide (CO2). The Indonesian government, through the Ministry of Energy and Mineral Resources, has set a target to develop bioavtur with a 5% biofuel content by 2025. This regulation follows the international regulations of the International Civil Aviation Organization (ICAO) and the Environmental Protection Agency (EPA). These regulations set emission standards for pollutants such as particulate matter (PM) and nitrogen oxides (NOx) for aircraft engines. This research focuses on the design of an aircraft emission measurement system, based on the requirements and objectives of the regulations. Key questions involved identifying parameters and methods for measuring aircraft emission gases and evaluating the performance comparison of the current measurement system with existing regulations. The result of this study is the identification of important parameters for measuring aircraft exhaust emissions, namely smoke, hydrocarbons (HC), carbon monoxide (CO), nitrogen oxides (NOx), non-volatile particulate matter mass (nvPM mass), and non-volatile particulate matter number (nvPM number). The six parameters are measured using 3 different test methods. These methods are smoke testing to measure smoke emissions, gas emissions testing to measure HC, CO, and NOx, and nvPM testing to measure nvPM mass and nvPM number. Based on the review, only 2 of the 3 recommended testing methods are gas emission testing and nvPM testing. The recommended measurement system for gas emission testing is the MEXA-1700 because it uses three different methods depending on the gas emissions being measured. The recommended measurement systems for nvPM testing are AVL Micro Soot Sensor 2, AVL CPC and CPC 3750-10 due to their compliance with regulations. For now, it is necessary to search for data on these measurement systems to ensure that the measurement tools can be used for aircraft exhaust emission testing.
format Final Project
author Raynary Fabian, Oktavio
author_facet Raynary Fabian, Oktavio
author_sort Raynary Fabian, Oktavio
title DESIGN STUDY OF GAS TURBINE-BASED AIRCRAFT ENGINE EXHAUST GAS EMISSION MEASUREMENT SYSTEM
title_short DESIGN STUDY OF GAS TURBINE-BASED AIRCRAFT ENGINE EXHAUST GAS EMISSION MEASUREMENT SYSTEM
title_full DESIGN STUDY OF GAS TURBINE-BASED AIRCRAFT ENGINE EXHAUST GAS EMISSION MEASUREMENT SYSTEM
title_fullStr DESIGN STUDY OF GAS TURBINE-BASED AIRCRAFT ENGINE EXHAUST GAS EMISSION MEASUREMENT SYSTEM
title_full_unstemmed DESIGN STUDY OF GAS TURBINE-BASED AIRCRAFT ENGINE EXHAUST GAS EMISSION MEASUREMENT SYSTEM
title_sort design study of gas turbine-based aircraft engine exhaust gas emission measurement system
url https://digilib.itb.ac.id/gdl/view/86355
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