A power system includes a liquid hydrogen fuel source including a fuel tank (14) containing a volume of hydrogen fuel (12). The fuel tank includes two or more vacuum insulation layers (52), and a liquid insulation material (54) positioned between the two or more vacuum insulation layers. A first power generator (22a) located fluidly downstream of the hydrogen fuel source. The first power generator utilizes a flow of hydrogen fuel from the volume of hydrogen fuel to generate electrical or mechanical power.
AUXILLARY POWER GENERATION AND COOLING SYSTEMS ON LIQUID HYDROGEN FUELED AIRCRAFT
HILFSSTROMERZEUGUNGS- UND KÜHLSYSTEME AN MIT FLÜSSIGEM WASSERSTOFF ANGETRIEBENEN FLUGZEUGEN
SYSTÈMES DE PRODUCTION D'ÉNERGIE AUXILIAIRE ET DE REFROIDISSEMENT SUR AÉRONEF ALIMENTÉ EN HYDROGÈNE LIQUIDE
21.02.2024
Patent
Elektronische Ressource
Englisch
Auxiliary power generation and cooling systems on liquid hydrogen fueled aircraft
Europäisches Patentamt | 2024
|Auxiliary power generation and cooling systems on liquid hydrogen fueled aircraft
Europäisches Patentamt | 2023
|HEAT EXCHANGER COOLING SYSTEMS AND AUXILIARY POWER GENERATION ON LIQUID HYDROGEN-FUELED AIRCRAFTS
Europäisches Patentamt | 2024
|INTEGRATED SUPPORT STRUCTURE FOR AN AIRCRAFT ENGINE AND ITS AUXILLARY COMPONENTS
Europäisches Patentamt | 2019
|