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Low pressure system component advancements Konstantinos G. Kyprianidis mission definitions. The sensitivity factors were combined with published infor- mation on the technologies developed under the umbrella of the VITAL project in order to assess the impact of failing to deliver expected year 2020 technology for the engine configurations in question. More specifically, the impact of failing to deliver specific component improvements has been successfully quantified, in terms of power plant noise and CO2 emissions and was discussed extensively. The study also increases confidence in the TERA2020 tool since the scenario of total failure (i.e. no progress achieved in any of the VITAL technology areas for the time period 2000 to 2020) results in a total CO2 penalty very close to the overall goals of the VITAL project predicted by industry. In the author’s opinion, all three engine configurations are optimal designs for the year 2020 and each has its own merits with respects to low technology risk and improved reliability, as well as reduced noise, CO2 and NOx emissions. Their commercial competitiveness will therefore largely depend on how the aviation market evolves in the years to come until 2020. Perhaps the most important aspect of this work is that the presented results essentially provide the means for making estimates of the relative merits of future technology investment; the relative importance of certain future aero engine research activities were highlighted for particular engine configurations. 5.5 Outlook Improvements in engine propulsive efficiency, as a way of reducing emissions from turbofan engines, have been discussed in this chapter in terms of specific thrust reduction. In the next chapter, TERA2020 will be used for addressing the need for higher engine thermal efficiency mainly by exploring benefits from the potential introduction of heat-exchanged cores in future aero engine designs. A thorough discussion on the main drivers that could support such initiatives will be presented. 128PDF Image | Multi-disciplinary conceptual design of future jet engine systems
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