A system for an aircraft (100) includes an engine bleed source (251) of a gas turbine engine (20). The system also includes a means for chilling an engine bleed air flow (252) from the engine bleed source (251) to produce a chilled working fluid. The system further includes a means for providing the chilled working fluid for an aircraft use.
CRYOGENIC COOLING SYSTEM FOR AN AIRCRAFT
KRYOGENES KÜHLSYSTEM FÜR EIN FLUGZEUG
SYSTÈME DE REFROIDISSEMENT CRYOGÉNIQUE POUR AÉRONEF
2024-04-24
Patent
Electronic Resource
English
IPC: | F25J LIQUEFACTION, SOLIDIFICATION, OR SEPARATION OF GASES OR GASEOUS MIXTURES BY PRESSURE AND COLD TREATMENT , Verflüssigen, Verfestigen oder Trennen von Gasen oder Gasgemischen durch Druck- und Kältebehandlung / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F02C Gasturbinenanlagen , GAS-TURBINE PLANTS |