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.
CHILLED WORKING FLUID GENERATION AND SEPARATION FOR AN AIRCRAFT
ERZEUGUNG UND TRENNUNG GEKÜHLTER ARBEITSFLUIDE FÜR EIN FLUGZEUG
GÉNÉRATION ET SÉPARATION DE FLUIDE DE TRAVAIL RÉFRIGÉRÉ POUR UN AÉRONEF
2023-02-15
Patent
Electronic Resource
English
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F02C Gasturbinenanlagen , GAS-TURBINE PLANTS / 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 |
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