An environmental control system (200) is provided. The environmental control system may receive pressurized air from a single supply line (220). A pressure regulating turbomachine (230) may be located within the supply line. A motor-generator (232) may be coupled to the pressure regulating turbomachine. In response to a pressure in the supply line being less than a desired pressure in the environmental control system, the motor-generator (232) may supply energy to the pressure regulating turbomachine, causing the pressure regulating turbomachine to function as a compressor. In response to a pressure in the supply line being greater than a desired pressure in the environmental control system, the pressure regulating turbomachine may function as a turbine and supply energy to the motor-generator.


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    Title :

    SINGLE STAGE ENGINE BLEED


    Additional title:

    EINSTUFIGE ZAPFLUFTENTNAHME
    PRÉLÈVEMENT RÉACTEUR À UN SEUL ÉTAGE


    Contributors:

    Publication date :

    2019-01-02


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



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