An engine bleed air system providing air to an aircraft system includes a port for extracting high pressure bleed air from an engine and a turbo-generator having a turbine and a generator. The generator is driven by rotation of the turbine. A bleed passage fluidly couples the port and an inlet of the turbo-generator. An outlet passage fluidly coupling an outlet of the turbo-generator and the aircraft system.
TURBO-GENERATOR BASED BLEED AIR SYSTEM
2018-05-17
Patent
Elektronische Ressource
Englisch
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