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Mechanical system design and manufacturing process design of 500N Turbojet engine <br /> <br /> <br /> <br /> <br /> provide many engineering problem when the amount of the time and cost as well as limited design <br /> <br /> <br /> <br...

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Main Author: ANDISETIAWAN SUGIANTO (NIM : 13605034); Pembimbing : Dr-ing. M. Agoes Mulyadi; Dr. Firman Ha, ANUGRAH
Format: Final Project
Language:Indonesia
Online Access:https://digilib.itb.ac.id/gdl/view/14956
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Institution: Institut Teknologi Bandung
Language: Indonesia
id id-itb.:14956
spelling id-itb.:149562017-10-09T10:33:27Z#TITLE_ALTERNATIVE# ANDISETIAWAN SUGIANTO (NIM : 13605034); Pembimbing : Dr-ing. M. Agoes Mulyadi; Dr. Firman Ha, ANUGRAH Indonesia Final Project INSTITUT TEKNOLOGI BANDUNG https://digilib.itb.ac.id/gdl/view/14956 Mechanical system design and manufacturing process design of 500N Turbojet engine <br /> <br /> <br /> <br /> <br /> provide many engineering problem when the amount of the time and cost as well as limited design <br /> <br /> <br /> <br /> <br /> experience are considered. This research is to develop a small working engine with the limited <br /> <br /> <br /> <br /> <br /> manufacturing process uses for developing country. <br /> <br /> <br /> <br /> <br /> First step for building the engine is to calculate thermodynamics and propulsion <br /> <br /> <br /> <br /> <br /> aerodynamics based on the paper “The Design of Small Turbojet Engine for High Speed UAV” <br /> <br /> <br /> <br /> <br /> written by Dr. Firman Hartono from ITB. The second step is to obtain the type and rough dimension <br /> <br /> <br /> <br /> <br /> of compressor, combustion chamber, turbine, nozzle, and shaft system of the engine. Translating <br /> <br /> <br /> <br /> <br /> process from that theoretically designs type to the ready for production design, called “mechanical <br /> <br /> <br /> <br /> <br /> system design”, give some engineering consideration and unpredictable aerodynamics losses. For <br /> <br /> <br /> <br /> <br /> example, the design for the size and location of the bolt can influence aerodynamic stream at the <br /> <br /> <br /> <br /> <br /> compressor. So, we decide which a design that can give less unexpected loses and more simple <br /> <br /> <br /> <br /> <br /> manufacturing method for the components. <br /> <br /> <br /> <br /> <br /> Engine starting and idle running test have already done. The result shows that the idle <br /> <br /> <br /> <br /> <br /> condition of the engine is not achieved yet. Therefore, some further works are still needed. 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 Mechanical system design and manufacturing process design of 500N Turbojet engine <br /> <br /> <br /> <br /> <br /> provide many engineering problem when the amount of the time and cost as well as limited design <br /> <br /> <br /> <br /> <br /> experience are considered. This research is to develop a small working engine with the limited <br /> <br /> <br /> <br /> <br /> manufacturing process uses for developing country. <br /> <br /> <br /> <br /> <br /> First step for building the engine is to calculate thermodynamics and propulsion <br /> <br /> <br /> <br /> <br /> aerodynamics based on the paper “The Design of Small Turbojet Engine for High Speed UAV” <br /> <br /> <br /> <br /> <br /> written by Dr. Firman Hartono from ITB. The second step is to obtain the type and rough dimension <br /> <br /> <br /> <br /> <br /> of compressor, combustion chamber, turbine, nozzle, and shaft system of the engine. Translating <br /> <br /> <br /> <br /> <br /> process from that theoretically designs type to the ready for production design, called “mechanical <br /> <br /> <br /> <br /> <br /> system design”, give some engineering consideration and unpredictable aerodynamics losses. For <br /> <br /> <br /> <br /> <br /> example, the design for the size and location of the bolt can influence aerodynamic stream at the <br /> <br /> <br /> <br /> <br /> compressor. So, we decide which a design that can give less unexpected loses and more simple <br /> <br /> <br /> <br /> <br /> manufacturing method for the components. <br /> <br /> <br /> <br /> <br /> Engine starting and idle running test have already done. The result shows that the idle <br /> <br /> <br /> <br /> <br /> condition of the engine is not achieved yet. Therefore, some further works are still needed.
format Final Project
author ANDISETIAWAN SUGIANTO (NIM : 13605034); Pembimbing : Dr-ing. M. Agoes Mulyadi; Dr. Firman Ha, ANUGRAH
spellingShingle ANDISETIAWAN SUGIANTO (NIM : 13605034); Pembimbing : Dr-ing. M. Agoes Mulyadi; Dr. Firman Ha, ANUGRAH
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author_facet ANDISETIAWAN SUGIANTO (NIM : 13605034); Pembimbing : Dr-ing. M. Agoes Mulyadi; Dr. Firman Ha, ANUGRAH
author_sort ANDISETIAWAN SUGIANTO (NIM : 13605034); Pembimbing : Dr-ing. M. Agoes Mulyadi; Dr. Firman Ha, ANUGRAH
title #TITLE_ALTERNATIVE#
title_short #TITLE_ALTERNATIVE#
title_full #TITLE_ALTERNATIVE#
title_fullStr #TITLE_ALTERNATIVE#
title_full_unstemmed #TITLE_ALTERNATIVE#
title_sort #title_alternative#
url https://digilib.itb.ac.id/gdl/view/14956
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