Development of an electronic control unit for the T63 gas turbine

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dc.contributor.advisorYates, Andrewen_ZA
dc.contributor.advisorBurger, Victoren_ZA
dc.contributor.authorRobertson, Leanneen_ZA
dc.date.accessioned2014-11-05T03:50:49Z
dc.date.available2014-11-05T03:50:49Z
dc.date.issued2014en_ZA
dc.descriptionIncludes bibliographical references.en_ZA
dc.description.abstractFundamental research has been undertaken at the SASOL Advanced Fuels Laboratory to investigate the effects of the chemistry and physical properties of both conventional and synthetic jet fuels on threshold combustion. This research was undertaken using a purpose built low pressure continuous combustion test facility. Researchers at the laboratory now wish to examine these effects on an aviation gas turbine in service for which “off-map” scheduling of fuel to the engine would be required. A two phase project was thus proposed to develop this capability; the work of this thesis embodies Phase I of that project.en_ZA
dc.identifier.apacitationRobertson, L. (2014). <i>Development of an electronic control unit for the T63 gas turbine</i>. (Thesis). University of Cape Town ,Faculty of Engineering & the Built Environment ,Department of Mechanical Engineering. Retrieved from http://hdl.handle.net/11427/9145en_ZA
dc.identifier.chicagocitationRobertson, Leanne. <i>"Development of an electronic control unit for the T63 gas turbine."</i> Thesis., University of Cape Town ,Faculty of Engineering & the Built Environment ,Department of Mechanical Engineering, 2014. http://hdl.handle.net/11427/9145en_ZA
dc.identifier.citationRobertson, L. 2014. Development of an electronic control unit for the T63 gas turbine. University of Cape Town.en_ZA
dc.identifier.ris TY - Thesis / Dissertation AU - Robertson, Leanne AB - Fundamental research has been undertaken at the SASOL Advanced Fuels Laboratory to investigate the effects of the chemistry and physical properties of both conventional and synthetic jet fuels on threshold combustion. This research was undertaken using a purpose built low pressure continuous combustion test facility. Researchers at the laboratory now wish to examine these effects on an aviation gas turbine in service for which “off-map” scheduling of fuel to the engine would be required. A two phase project was thus proposed to develop this capability; the work of this thesis embodies Phase I of that project. DA - 2014 DB - OpenUCT DP - University of Cape Town LK - https://open.uct.ac.za PB - University of Cape Town PY - 2014 T1 - Development of an electronic control unit for the T63 gas turbine TI - Development of an electronic control unit for the T63 gas turbine UR - http://hdl.handle.net/11427/9145 ER - en_ZA
dc.identifier.urihttp://hdl.handle.net/11427/9145
dc.identifier.vancouvercitationRobertson L. Development of an electronic control unit for the T63 gas turbine. [Thesis]. University of Cape Town ,Faculty of Engineering & the Built Environment ,Department of Mechanical Engineering, 2014 [cited yyyy month dd]. Available from: http://hdl.handle.net/11427/9145en_ZA
dc.language.isoengen_ZA
dc.publisher.departmentDepartment of Mechanical Engineeringen_ZA
dc.publisher.facultyFaculty of Engineering and the Built Environment
dc.publisher.institutionUniversity of Cape Town
dc.subject.otherEngineeringen_ZA
dc.titleDevelopment of an electronic control unit for the T63 gas turbineen_ZA
dc.typeMaster Thesis
dc.type.qualificationlevelMasters
dc.type.qualificationnameMScen_ZA
uct.type.filetypeText
uct.type.filetypeImage
uct.type.publicationResearchen_ZA
uct.type.resourceThesisen_ZA
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