An environmental control system is provided. The environmental control system may receive pressurized air from a single supply line. A pressure regulating turbomachine may be located within the supply line. A motor-generator 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 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.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Single stage engine bleed


    Beteiligte:
    RONAN MICHAEL (Autor:in)

    Erscheinungsdatum :

    2018-09-11


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    F04D Strömungsarbeitsmaschinen , NON-POSITIVE-DISPLACEMENT PUMPS / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F02C Gasturbinenanlagen , GAS-TURBINE PLANTS



    SINGLE STAGE ENGINE BLEED

    RONAN MICHAEL | Europäisches Patentamt | 2019

    Freier Zugriff

    SINGLE STAGE ENGINE BLEED

    RONAN MICHAEL | Europäisches Patentamt | 2016

    Freier Zugriff

    SINGLE STAGE ENGINE BLEED

    RONAN MICHAEL | Europäisches Patentamt | 2019

    Freier Zugriff

    Engine bleed system with multi-tap bleed array

    SCHWARZ FREDERICK M | Europäisches Patentamt | 2020

    Freier Zugriff

    ENGINE BLEED SYSTEM WITH MULTI-TAP BLEED ARRAY

    SCHWARZ FREDERICK M | Europäisches Patentamt | 2023

    Freier Zugriff