An aircraft includes an electrical system having at least one cooled electrical component. The at least one cooled electrical component is a low grade heat source. The aircraft further includes a cooling system with a coolant loop passing through the at least one cooled electrical component and through a first adsorption cooler. The first adsorption cooler is configured to cool coolant in the cooling loop using an adsorption process.
ADSORPTION BASED AIRCRAFT COOLANT SYSTEM
2025-07-31
Patent
Electronic Resource
English
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
COOLANT TANK, COOLANT CONDUCTING SYSTEM, AND MOTOR VEHICLE
European Patent Office | 2024
|SAE | 2002