An environmental control system, ECS (30), for an aircraft includes a primary heat exchanger (36), a compressor (42) including an inlet (44) fluidically connected to the primary heat exchanger (36), a turbine (50) operatively connected to the compressor (42), and a cryogenic fluid heat exchanger (65) fluidically connected to the primary heat exchanger (36).
CRYOGENIC FLUID HEAT EXCHANGER SYSTEM FOR AN AIRCRAFT ENVIRONMENTAL CONTROL SYSTEM (ECS)
WÄRMETAUSCHERSYSTEM FÜR KRYOGENES FLUID FÜR EIN UMGEBUNGSSTEUERUNGSSYSTEM (ECS) EINES FLUGZEUGS
SYSTÈME D'ÉCHANGEUR DE CHALEUR À FLUIDE CRYOGÉNIQUE POUR UN SYSTÈME DE CONTRÔLE ENVIRONNEMENTAL D'AÉRONEF (ECS)
2023-03-15
Patent
Electronic Resource
English
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
CRYOGENIC FLUID HEAT EXCHANGER SYSTEM FOR AN AIRCRAFT ENVIRONMENTAL CONTROL SYSTEM (ECS)
European Patent Office | 2023
|Heat Exchanger Fouling Detection in Aircraft Environmental Control Systems
SAE Technical Papers | 2012
|