dc.contributor.author |
Muhammad Ahmad Ali, Salman Zahid ,Mohammad Khubaib Mujahid,Mohammad Hashir Ijaz |
|
dc.date.accessioned |
2024-06-06T10:25:23Z |
|
dc.date.available |
2024-06-06T10:25:23Z |
|
dc.date.issued |
2024 |
|
dc.identifier.other |
336386,342176,347036,308076 |
|
dc.identifier.uri |
http://10.250.8.41:8080/xmlui/handle/123456789/43847 |
|
dc.description |
Supervisor : Dr Asad Javed |
en_US |
dc.description.abstract |
This project aims to repurpose standard turbochargers into thrust-generating
devices by integrating them with a combustion chamber and nozzle. The
concept involves utilizing the compressed air generated by the turbocharger's
compressor section to produce thrust through controlled combustion. By
directing the resulting gases to the turbine segment of the turbocharger and
then through a specifically designed nozzle, thrust is generated.
The primary objective is to showcase the versatility of turbochargers beyond
their conventional role of enhancing engine performance. This modification
demonstrates their potential to power diverse propulsion systems, opening up
new avenues for creative engineering solutions. By harnessing the energy of
compressed air in a controlled combustion process, this project seeks to
explore alternative methods of propulsion, moving beyond traditional internal
combustion engines.
The integration of a combustion chamber and nozzle with the turbocharger
offers a novel approach to propulsion system design. It highlights the
adaptability of turbocharger technology and its potential applications across
various engineering domains. This initiative not only explores innovative
propulsion techniques but also encourages creativity in engineering solutions.
Through this project, turbochargers are transformed into dynamic components
capable of driving different mechanisms forward, particularly suited for
applications requiring low thrust, such as unmanned aerial vehicles (UAVs).
By repurposing turbochargers in this manner, the project not only
demonstrates their adaptability but also addresses the specific needs of UAVs
and similar devices. |
en_US |
dc.language.iso |
en |
en_US |
dc.publisher |
School of Mechanical & Manufacturing Engineering (SMME) , NUST |
en_US |
dc.relation.ispartofseries |
SMME-FY329; |
|
dc.title |
Turbocharger Based Thrust Generating Device / |
en_US |
dc.type |
Thesis |
en_US |