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Multi-disciplinary conceptual design of future jet engine systems

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Multi-disciplinary conceptual design of future jet engine systems ( multi-disciplinary-conceptual-design-future-jet-engine-syste )

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Introduction Konstantinos G. Kyprianidis 7. Quantify potential benefits from the introduction of novel lean-burn com- bustion technology, as developed under the NEWAC project, coupled with future novel aero engine designs. 1.4 Thesis overview The main contents of this thesis have been organised in the following chapters: • In Chapter 2, the developed aero engine conceptual design framework is presented. • InChapter3,developmentscarriedoutbytheauthoronindividualTERA2020 modules are discussed. • In Chapter 4, the impact of fluid modelling uncertainty on performance calculations and emissions predictions at aircraft system level is assessed. Accuracy limitations in assessing novel engine core concepts as imposed by current practice in thermo-fluid modelling are identified. • In Chapter 5, the potential benefits from various low pressure spool com- ponent advancements are presented, and the impact of failing to deliver specific component technologies is quantified, in terms of power plant noise and CO2 emissions. • In Chapter 6, an assessment of various novel engine core technologies and concepts coupled with lean-burn combustion concepts is presented. • In Chapter 7, various aspects are presented of an intercooled core and con- ventional core turbofan engine optimisation procedure using TERA2020. A back-to-back comparison between the two engine configurations is per- formed and fuel optimal designs for year 2020 entry into service are pro- posed. • In Chapter 8, overall conclusions are drawn from the work carried out and recommendations for future work are made. Additional information to support the work carried out for this project is pre- sented in the following appendices: 6

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