Feasibility analysis of a new thermal insulation concept of cryogenic fuel tanks for hydrogen fuel cell powered commercial aircraft

被引:17
|
作者
Monkam, Linus Kameni [1 ,3 ]
Schweinitz, Arne Graf von [1 ,3 ]
Friedrichs, Jens [2 ,3 ]
Gao, Xin [1 ,3 ]
机构
[1] Tech Univ Carolo Wilhelmina Braunschweig, Inst Energy & Proc Syst Engn InES, Braunschweig, Germany
[2] Tech Univ Carolo Wilhelmina Braunschweig, Inst Flugantriebe & Stromungsmaschinen IFAS, Braunschweig, Germany
[3] Cluster Excellence SE 2 Asustainable & Energy Effi, Braunschweig, Germany
关键词
Cryogenic hydrogen; Onboard storage; Heat insulation; Thermal design; Aviation;
D O I
10.1016/j.ijhydene.2022.07.069
中图分类号
O64 [物理化学(理论化学)、化学物理学];
学科分类号
070304 ; 081704 ;
摘要
Of cryogenic liquid hydrogen tanks for future airliners, their volumetric and gravimetric efficiencies, their robustness and their environmental adaptability are all strengthened via a novel thermal insulation concept proposed in this work.A conventional cryogenic tank is insulated either purely by a layer/layers of Polyurethane (PU) foam or by a vacuum-based multilayer insulation (MLI). In the new concept, an extra layer is inserted into the PU foam. The intermediate layer can be filled with liquid nitrogen while on the ground or with ambient air during flight.By this new design, analysis shows an approximate 33% volumetric saving compared to PU insulation. Furthermore, a 6-fold amount of passive heat input during cruise flight is easily achieved compared to the rest two concepts. This showcases an increased robustness against possible failure of the tank's active heating system, and the potential for significant parasitic power loss reduction.(c) 2022 Hydrogen Energy Publications LLC. Published by Elsevier Ltd. All rights reserved.
引用
收藏
页码:31395 / 31408
页数:14
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