An aircraft propulsion system (20) includes a gas turbine engine; an environmental control system (ECS) (22); and a bleed flowpath (600) from the gas turbine engine through the ECS (22). A turbine (28) is along the bleed flowpath (600) and a propulsion fan (26) is mechanically coupled to the turbine (28) to be driven by the turbine (28).
ENVIRONMENTAL CONTROL SYSTEMS
KLIMAREGELUNGSSYSTEME
SYSTÈMES DE COMMANDE ENVIRONNEMENTALE
2023-08-23
Patent
Elektronische Ressource
Englisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
NTRS | 1961
NTRS | 1982
|NTRS | 1982
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