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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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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 |
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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 />
<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 #TITLE_ALTERNATIVE# |
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 |
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url |
https://digilib.itb.ac.id/gdl/view/14956 |
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1820737356371591168 |