Modelling and simulation of the Water Enhanced Turbofan concept

dc.contributor.authorHerbertsson, Filip
dc.contributor.departmentChalmers tekniska högskola / Institutionen för mekanik och maritima vetenskapersv
dc.contributor.departmentChalmers University of Technology / Department of Mechanics and Maritime Sciencesen
dc.contributor.examinerGrönstedt, Tomas
dc.contributor.supervisorGrönstedt, Tomas
dc.date.accessioned2024-06-10T12:09:26Z
dc.date.available2024-06-10T12:09:26Z
dc.date.issued2024
dc.date.submitted
dc.description.abstractThe aviation industry needs to reduce its climate impact. The Water Enhanced Turbofan (WET) is a new engine technology that could reduce the climate impact from aviation with regards to carbon dioxide (CO2 ) emissions, nitrogen oxides (NOx ) emissions and contrail formation. In the WET cycle, water is injected into the combustion chamber, which lowers the formation of NOx -gases. The water also increases the thermodynamic efficiency of the turbines, and is collected through a set of heat exchangers so that it can be pumped back into the combustion chamber. If more water is collected than what was injected, the exhaust stream will contain less water that has the potential to produce contrails. In this work, a WET cycle engine and the components it consists from are modeled, based on a reference engine from previous Chalmers research and the most recent WET cycle concept from MTU Aero Engines. The concept engine is analysed through selected cycle design parameters, as well as through generalized geometric parameters (GGP) of the heat exchangers. The design point is optimized with respect to specific fuel consumption (SFC), and the benefits of the water injection are analysed. It is estimated that, by careful selection of cycle parameters, CO2 -emissions can be reduced by more than 7% and NOx -emissions can be reduced by more than 85%. This is in fair agreement with the benefits that MTU Aero Engines predicts. Limiting factors include the weights of the WET cycle components, the size of the engine as well as the temperature that the low pressure turbine (LPT) can handle. It is proposed that, in order to obtain further benefits, other cycle parameters should be analysed such as the overall pressure ratio (OPR) and the amount of cooling flow. Further, to remove the limit of LPT temperature, the LPT could be cooled by air from the compressor stages.
dc.identifier.coursecodeMMSX30
dc.identifier.urihttp://hdl.handle.net/20.500.12380/307742
dc.language.isoeng
dc.setspec.uppsokTechnology
dc.subjectWater Enhanced Turbofan
dc.subjectCO2 emissions
dc.subjectNOx emissions
dc.subjectcycle optimization
dc.subjectGESTPAN
dc.subjectmodelling
dc.subjectsimulation
dc.titleModelling and simulation of the Water Enhanced Turbofan concept
dc.type.degreeExamensarbete för masterexamensv
dc.type.degreeMaster's Thesisen
dc.type.uppsokH
local.programmeMobility engineering (MPMOB), MSc
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