An aircraft includes an electrical system (30) having at least one cooled electrical component (40). The at least one cooled electrical component is a low grade heat source. The aircraft further includes a cooling system with a coolant loop (100) passing through the at least one cooled electrical component and through a first adsorption cooler (50). The first adsorption cooler is configured to cool coolant in the cooling loop using an adsorption process.
ADSORPTION BASED AIRCRAFT COOLANT SYSTEM
ADSORPTIONSBASIERTES FLUGZEUGKÜHLSYSTEM
SYSTÈME DE REFROIDISSEMENT D'AÉRONEF À BASE D'ADSORPTION
2025-08-06
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 | 2004