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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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Assessment of core technologies and concepts Konstantinos G. Kyprianidis significantly lower. This is a consequence of the ICAO LTO NOx legislative limits being quite strict for low OPR engines, while providing a better LTO NOx allowance for high OPR engines. Despite the generally low OPR, cruise NOx may still remain an important con- cern for an intercooled recuperated configuration, if lean-burn combustion tech- nology is not introduced. During cruise, the need for high heat exchange levels in the recuperator results in high combustor inlet temperatures and low AFR values; designing a conventional RQL technology combustor for such conditions could still prove a challenging task. To this extent, the intercooled recuperated concept essentially lends itself to lean-burn combustion technology. Due to the variable geometry LPT, the primary zone temperature during cruise will not be so far away from the take-off value when compared to conventional engine designs. It can therefore prove easier to balance the combustor primary zone design to achieve both low NOx and CO emissions at cruise conditions, as well as retain low NOx levels at high power conditions such as take-off. Substitut- ing the RQL combustor with a lean-burn design, can reduce NOx emissions but the effect would be less profound compared to lean-burn combustion technology coupled with high OPR cycles. Similarly, introducing a variable geometry LPT in an intercooled core with lean- burn combustion technology can improve LTO NOx and the margin from the ICAO CAEP/6 certification limit by nearly 10%, at a given level of cruise NOx. This involves running the intercooled core approximately 60 [K] hotter during cruise in order to achieve the same thrust levels. The reduction in LTO NOx levels is mainly the result of bringing the primary zone temperature during cruise closer to the take-off value; the latter results in the lean-burn combustor design - balanced for NOx and CO at cruise - retaining acceptable NOx levels at high power conditions such as ICAO 100% FN. Running the engine hotter at cruise also improves SFC by nearly 1%. It is worth noting that the effect of elevated cruise temperatures on HPT life, and consecutively on engine time between overhaul and maintenance costs is not profound, for the temperature increase proposed. The main reason behind this is that HPT life is dominated by the time spent at take-off and climb, with cruise effects being of secondary order due to the significantly lower operating temperatures encountered. Moreover, modulating T41 to remain constant at the higher cruise thrust range (i.e. flat temperature profile), could actually prove 148

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