A COMPARISON OF SOLID OXIDE FUEL CELL DESIGNS AS ENERGY SOURCE FOR THE ALL-ELECTRIC AIRCRAFT

机译：固体氧化物燃料电池设计作为全电飞机能源的比较

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The development of new aircraft system architectures for the so-called all-electric aircraft results in a highly increased electrical power demand from the systems. This electrical power can be provided by generators which convert engine shaft power into electrical power, and auxiliary power units on ground with engines off. Fuel cell systems may be an engine-independent alternative to this combination. Different system designs and alternative integration modes are presented in this paper and linked to their impact on aircraft performance. While the assessment of fuel cells on system level has been the object of many studies, the focus of this paper is the performance evaluation on aircraft level.

机译：用于所谓的全电动飞机的新飞机系统架构的发展导致系统的电力需求大大增加。可以通过将发动机轴功率转换为电能的发电机以及在关闭发动机的情况下将辅助动力装置接地来提供此电能。燃料电池系统可以是该组合的独立于发动机的替代方案。本文介绍了不同的系统设计和替代集成模式，并将它们与对飞机性能的影响联系在一起。尽管在系统级别上对燃料电池的评估一直是许多研究的目标，但本文的重点是在飞机级别上的性能评估。

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来源
《Congress of the International Council of the Aeronautical Sciences; 20060903-08; Hamburg(DE)》|2006年|P.3463-3472|共10页
会议地点 Hamburg(DE)
作者
N.Bundschuh; J.Dollmayer; U.B.Carl;
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作者单位

DLR e.V., Institute of Technical Thermodynamics;

TTI GmbH TGU Visimbel, Germany;

Institute of Aircraft Systems Engineering, Hamburg University of Technology (TUHH), Germany;

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会议组织
原文格式 PDF
正文语种 eng
中图分类航空;
关键词
fuel cell; aircraft systems; fuel consumption;

机译：燃料电池;飞机系统;燃料消耗;

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1. Fuel mass penalty due to generators and fuel cells as energy source of the all-electric aircraft [J] . Jürgen Dollmayer, Nicola Bundschuh, Udo B. Carl Aerospace science and technology . 2006,第8期

机译：由于发电机和燃料电池作为全电动飞机的能源而导致的燃油质量损失
2. Comparison between conventional design and cathode gas recirculation design of a direct-syngas solid oxide fuel cell–gas turbine hybrid systems part II: Effect of temperature difference at the fuel cell stack [J] . Vahid Azami, Mortaza Yari International Journal of Renewable Energy Development . 2018,第3期

机译：直接合成气固体氧化物燃料电池-燃气轮机混合系统的常规设计和阴极气体再循环设计的比较第二部分：燃料电池堆上的温差的影响
3. On the Decentralized Energy Management Strategy for the All-Electric APU of Future More Electric Aircraft Composed of Multiple Fuel Cells and Supercapacitors [J] . Chen Jie, Song Qingchao, Yin Sihao, IEEE Transactions on Industrial Electronics . 2020,第8期

机译：关于多种燃料电池和超级电路组成的未来更多电气飞机的分散能源管理策略
4. A COMPARISON OF SOLID OXIDE FUEL CELL DESIGNS AS ENERGY SOURCE FOR THE ALL-ELECTRIC AIRCRAFT [C] . N.Bundschuh, J.Dollmayer, U.B.Carl Congress of the International Council of the Aeronautical Sciences . 2006

机译：固体氧化物燃料电池设计与全电机的能源相比
5. Numeric Design and Performance Analysis of Solid Oxide Fuel Cell -- Gas Turbine Hybrids on Aircraft. [D] . Hovakimyan, Gevorg. 2014

机译：飞机上固体氧化物燃料电池-燃气轮机混合动力的数值设计和性能分析。
6. Rational Design of a Water‐Storable Hierarchical Architecture Decorated with Amorphous Barium Oxide and Nickel Nanoparticles as a Solid Oxide Fuel Cell Anode with Excellent Sulfur Tolerance [O] . Yufei Song, Wei Wang, Lei Ge, 2017

机译：以非晶态氧化钡和镍纳米粒子作为耐硫性优异的固体氧化物燃料电池阳极的蓄水分层结构的合理设计
7. Design improvements of micro-tubular solid oxide fuel cells for unmanned aircraft applications [O] . Howe Katie Sarah 2014

机译：用于无人驾驶飞机应用的微管状固体氧化物燃料电池的设计改进
8. Enhanced Power Stability for Proton Conducting Solid Oxides Fuel Cells. Calculated energy barriers for proton diffusion in Y-doped BaZrO3. Potential electrode materials for application in proton ceramic fuel cells. [R] . 2005

机译：提高质子传导固体氧化物燃料电池的功率稳定性。计算Y掺杂BaZrO3中质子扩散的能垒。用于质子陶瓷燃料电池的潜在电极材料。

A COMPARISON OF SOLID OXIDE FUEL CELL DESIGNS AS ENERGY SOURCE FOR THE ALL-ELECTRIC AIRCRAFT

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