An aircraft thermal management system comprising a high temperature loop and a low temperature loop. The high temperature loop is configured to manage a temperature of a fuel cell stack in a nacelle using a nacelle heat exchanger. The low temperature loop is configured to cool a number of heat loads in a nacelle using a heat capacity of liquid hydrogen.
FUEL CELL AIRCRAFT THERMAL MANAGEMENT SYSTEM
WÄRMEVERWALTUNGSSYSTEM FÜR EIN BRENNSTOFFZELLENFLUGZEUG
SYSTÈME DE GESTION THERMIQUE D'AÉRONEF À PILE À COMBUSTIBLE
19.02.2025
Patent
Elektronische Ressource
Englisch
Improving Aircraft Fuel-Thermal Management
SAE Technical Papers | 1993
|Integrated Aircraft Fuel Thermal Management
SAE Technical Papers | 1986
|