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.


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    Titel :

    TURBO-GENERATOR BASED BLEED AIR SYSTEM


    Beteiligte:

    Erscheinungsdatum :

    2018-05-17


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F02C Gasturbinenanlagen , GAS-TURBINE PLANTS



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