液态氢
氮氧化物
汽车工程
涡轮机
环境科学
氢
燃气轮机
燃料效率
涡轮
能源消耗
工程类
航空航天工程
电气工程
化学
机械工程
燃烧
有机化学
作者
T. Dietl,J. Karger,K. Kaupe,A. Pfemeter,Phillip Weber,A. Zakrzewski,Andreas Strohmayer
摘要
Polaris is a liquid hydrogen turbo-electric transport aircraft which is designed to fulfill the NASA N 3 goals for entry into service in 2045. The main objective is to reduce the energy consumption by at least 60% compared to an A320 of 2005. Secondary objectives are the reduction of the NOX emissions by 80% and minimizing the noise emissions. The concept combines the synergies of a liquid hydrogen fuel system with a HTS power transmission and an intercooled gas turbine. By this a reduction of 62% in energy consumption and 80% lower NOx emissions are achieved at a comparable design mission.
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