Climate Impact Reduction Potentials of Synthetic Kerosene and Green Hydrogen Powered Mid-Range Aircraft Concepts

被引:28
作者
Silberhorn, Daniel [1 ]
Dahlmann, Katrin [2 ]
Goertz, Alexander [3 ]
Linke, Florian [4 ]
Zanger, Jan [5 ]
Rauch, Bastian [5 ]
Methling, Torsten [5 ]
Janzer, Corina [5 ]
Hartmann, Johannes [1 ]
机构
[1] Deutsch Zentrum Luft & Raumfahrt, Inst Syst Architekturen Luftfahrt, D-21129 Hamburg, Germany
[2] Deutsch Zentrum Luft & Raumfahrt, Inst Phys Atmosphare, D-82234 Oberpfaffenhofen, Germany
[3] Deutsch Zentrum Luft & Raumfahrt, Inst Antriebstech, D-51147 Cologne, Germany
[4] Deutsch Zentrum Luft & Raumfahrt, Lufttransportsyst, D-21079 Hamburg, Germany
[5] Deutsch Zentrum Luft & Raumfahrt, Inst Verbrennungstech, D-70569 Stuttgart, Germany
来源
APPLIED SCIENCES-BASEL | 2022年 / 12卷 / 12期
关键词
aviation; climate impact assessment; liquid hydrogen; synthetic fuel; EMISSION; AVIATION;
D O I
10.3390/app12125950
中图分类号
O6 [化学];
学科分类号
0703 ;
摘要
One of aviation's major challenges for the upcoming decades is the reduction in its climate impact. As synthetic kerosene and green hydrogen are two promising candidates, their potentials in decreasing the climate impact is investigated for the mid-range segment. Evolutionary advancements for 2040 are applied, first with an conventional and second with an advanced low-NOx and low-soot combustion chamber. Experts and methods from all relevant disciplines are involved, starting from combustion, turbofan engine, overall aircraft design, fleet level, and climate impact assessment, allowing a sophisticated and holistic evaluation. The main takeaway is that both energy carriers have the potential to strongly reduce the fleet level climate impact by more than 75% compared with the reference. Applying a flight-level constraint of 290 and a cruise Mach number of 0.75, causing 5% higher average Direct Operating Costs (DOC), the reduction is even more than 85%. The main levers to achieve this are the advanced combustion chamber, an efficient contrail avoidance strategy, in this case a pure flight-level constraint, and the use of CO2 neutral energy carrier, in a descending priority order. Although vehicle efficiency gains only lead to rather low impact reduction, they are very important to compensate the increased costs of synthetic fuels or green hydrogen.
引用
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页数:25
相关论文
共 61 条
[1]  
Alder M., 2020, P AEROSPACE EUROPE C
[2]  
Becker R.G., 2011, P DEV GAS TURB PERF
[3]  
Beltramo MichaelN., 1977, Parametric study of transport aircraft systems cost and weight
[4]  
Boeing Commercial Airplanes, 2021, D6583256 BOEING COMM
[5]   Mitigating the contrail cirrus climate impact by reducing aircraft soot number emissions [J].
Burkhardt, Ulrike ;
Bock, Lisa ;
Bier, Andreas .
NPJ CLIMATE AND ATMOSPHERIC SCIENCE, 2018, 1
[6]   Process-based simulation of contrail cirrus in a global climate model [J].
Burkhardt, Ulrike ;
Kaercher, Bernd .
JOURNAL OF GEOPHYSICAL RESEARCH-ATMOSPHERES, 2009, 114
[7]  
Burschyk T., 2021, GERMAN AEROSPACE C D
[8]   Study of Prediction Methods for NOx Emission from Turbofan Engines [J].
Chandrasekaran, N. ;
Guha, Abhijit .
JOURNAL OF PROPULSION AND POWER, 2012, 28 (01) :170-180
[9]   Climate-Compatible Air Transport System-Climate Impact Mitigation Potential for Actual and Future Aircraft [J].
Dahlmann, Katrin ;
Koch, Alexander ;
Linke, Florian ;
Luehrs, Benjamin ;
Grewe, Volker ;
Otten, Tom ;
Seider, Doreen ;
Gollnick, Volker ;
Schumann, Ulrich .
AEROSPACE, 2016, 3 (04)
[10]  
Daniel Brewer G., 2017, Hydrogen aircraft technology, DOI DOI 10.1201/9780203751480