An aircraft propulsion system includes a gas turbine engine; an environmental control system (ECS); and a bleed flowpath from the gas turbine engine through the ECS. A turbine is along the bleed flowpath and a propulsion fan is mechanically coupled to the turbine to be driven by the turbine.
Environmental control systems
2024-02-27
Patent
Electronic Resource
English
NTRS | 1961
NTRS | 1982
|NTRS | 1982
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