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Turbocharger Based Thrust Generating Device /

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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


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