Investigation of flame-assisted fuel cells integrated with an auxiliary power unit gas turbine

被引:15
作者
Ghotkar, Rhushikesh [1 ]
Milcarek, Ryan J. [1 ]
机构
[1] Arizona State Univ, Sch Engn Matter Transport & Energy, 501 E Tyler Mall, Tempe, AZ 85287 USA
关键词
Flame-assisted fuel cells; Solid oxide fuel cells; Two-stage combustion; Hybrid gas turbine; Jet fuel; Syngas production; HYBRID SYSTEM; AIRCRAFT; COMBUSTION; PROPANE; METHANE; EMISSIONS; ENGINE; STACK; HEAT; DFFC;
D O I
10.1016/j.energy.2020.117979
中图分类号
O414.1 [热力学];
学科分类号
摘要
Owing to several unsuccessful attempts of integrating dual chambered solid oxide fuel cell stack with the auxiliary power unit (APU) gas turbine, a novel concept for integration of flame-assisted fuel cells (FFC) with the gas turbine of an APU is presented in this paper. A complete analytical model of the FFC integrated hybrid system is presented. The FFC gas turbine hybrid system is predicted to be up to 30% more efficient at sea level and 16% more efficient at cruising altitudes compared to standard gas turbine cycle. A FFC is characterized experimentally with model combustion exhaust for fuel-rich combustion of JP-5. The fuel cell displayed 75% fuel utilization at the operating voltage of 0.5 V, which is higher than previous studies in this field. The analytically predicted reversible voltage shows good agreement with the open circuit voltage of the FFC experimental results. Analysis of temperature entropy and pressure volume diagrams of the proposed system shows that as the equivalence ratio increases the portion of the total FFC gas turbine hybrid power generated by gas turbine decreases. The breakeven distance and the complexity of the proposed FFC gas turbine hybrid is significantly lower than previous studies. (C) 2020 Elsevier Ltd. All rights reserved.
引用
收藏
页数:12
相关论文
共 47 条
  • [1] Solid oxide fuel cell/gas turbine hybrid system analysis for high-altitude long-endurance unmanned aerial vehicles
    Aguiar, P.
    Brett, D. J. L.
    Brandon, N. P.
    [J]. INTERNATIONAL JOURNAL OF HYDROGEN ENERGY, 2008, 33 (23) : 7214 - 7223
  • [2] [Anonymous], 2010, RIGHT CHOIC LARG AIR
  • [3] Characterization of Emissions from Liquid Fuel and Propane Open Burns
    Aurell, Johanna
    Hubble, David
    Gullett, Brian K.
    Holder, Amara
    Tabor, Dennis
    Washburn, Ephraim
    [J]. FIRE TECHNOLOGY, 2017, 53 (06) : 2023 - 2038
  • [4] System Architectures for Solid Oxide Fuel Cell-Based Auxiliary Power Units in Future Commercial Aircraft Applications
    Braun, R. J.
    Gummalla, M.
    Yamanis, J.
    [J]. JOURNAL OF FUEL CELL SCIENCE AND TECHNOLOGY, 2009, 6 (03): : 0310151 - 03101510
  • [5] Cao Y, 2017, APPL POWER ELECT CO, P1412, DOI 10.1109/APEC.2017.7930882
  • [6] The ignition, oxidation, and combustion of kerosene: A review of experimental and kinetic modeling
    Dagaut, P
    Cathonnet, M
    [J]. PROGRESS IN ENERGY AND COMBUSTION SCIENCE, 2006, 32 (01) : 48 - 92
  • [7] Solid oxide fuel cell hybrid system: A detailed review of an environmentally clean and efficient source of energy
    Damo, U. M.
    Ferrari, M. L.
    Turan, A.
    Massardo, A. F.
    [J]. ENERGY, 2019, 168 : 235 - 246
  • [8] An auxiliary power unit for advanced aircraft electric power systems
    Ebrahimi, Hadi
    Gatabi, Javad R.
    El-Kishky, Hassan
    [J]. ELECTRIC POWER SYSTEMS RESEARCH, 2015, 119 : 393 - 406
  • [9] SOFC-APU systems for aircraft: A review
    Fernandes, M. D.
    Andrade, S. T. de P.
    Bistritzki, V. N.
    Fonseca, R. M.
    Zacarias, L. G.
    Goncalves, H. N. C.
    de Castro, A. F.
    Domingues, R. Z.
    Matencio, T.
    [J]. INTERNATIONAL JOURNAL OF HYDROGEN ENERGY, 2018, 43 (33) : 16311 - 16333
  • [10] Greg H, 2007, AVIATION FUELS TECHN