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Assessing selected technologies and operational strategies for improving the environmental performance of future aircraft

机译:评估选定的技术和运营战略,以改善未来飞机的环境性能

摘要

The aviation industry is expected to grow at a rate of 4-5% in the next 20 years. Such a growth rate may have important impacts on local air quality, climate change and community noise. This work assesses selected technologies and operational procedures aimed at improving the environmental performance of future airplanes. Two different studies are presented: estimating turbine durability benefits from jet engine water injection and evaluating improvements in fuel burn and operating costs from using advanced technology, high bypass ratio engines and varying the design cruise speed. Water injection in commercial airplane engine combustors lowers operating temperatures and can lead to significant reductions in NO, and soot emissions, potentially improving engine hot section life. With increasing fuel prices and possible introduction of emissions trading in the future, fuel burn may become a more critical aircraft design driver. Increasing engine bypass ratio and lowering cruise speed can lead to reduced fuel consumption. The dominant mechanisms of failure in turbine blades are low cycle fatigue, creep and oxidation. The Universal Slopes method is used to evaluate possible fatigue life benefits from water injection for three representative blade materials.
机译:未来20年,航空业预计将以4-5%的速度增长。这样的增长率可能会对当地的空气质量,气候变化和社区噪音产生重要影响。这项工作评估了旨在改善未来飞机的环境性能的选定技术和操作程序。提出了两项​​不同的研究:估算喷气发动机喷水带来的涡轮机耐用性收益,以及评估通过使用先进技术,高旁通比发动机和改变设计巡航速度而改善的燃油消耗和运行成本。商用飞机发动机燃烧室中的注水可降低运行温度,并能显着减少NO和烟尘排放,从而有可能延长发动机热区的寿命。随着燃油价格的上涨以及未来可能引入的排放交易,燃油消耗可能会成为飞机设计中更为关键的因素。增加发动机旁通比和降低巡航速度可以减少燃油消耗。涡轮叶片失效的主要机理是低循环疲劳,蠕变和氧化。通用坡度方法用于评估三种代表性叶片材料注水带来的疲劳寿命收益。

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