An intercooled cooling system (100) for a gas turbine engine (20) includes cooling stages (110,115) in fluid communication with an air stream (275) utilized for cooling. A first cooling stage (110) is fluidly coupled to a bleed port (145,165) of the gas turbine engine (20) to receive and cool bleed air with the air stream (275) to produce a cool bleed air. The intercooled cooling system (100) includes a pump (105) fluidly coupled to the first cooling stage (110) to receive and increase a pressure of the cool bleed air to produce a pressurized cool bleed air. A second cooling stage (115) is fluidly coupled to the pump (105) to receive and cool the pressurized cool bleed air to produce an intercooled cooling air. The intercooled cooling system includes an air cycle machine (190) in fluid communication to outputs of the cooling stages (110,115) to selectively receive the cool bleed air or the intercooled cooling air.


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    Titel :

    INTERCOOLED COOLED COOLING INTEGRATED AIR CYCLE MACHINE


    Weitere Titelangaben:

    ZWISCHENGEKÜHLTE GEKÜHLTE KÜHLUNGSINTEGRIERTE LUFTKREISLAUFMASCHINE
    MACHINE À CYCLE D'AIR INTÉGRÉ REFROIDIE PAR REFROIDISSEMENT INTERMÉDIAIRE


    Beteiligte:
    STAUBACH JOSEPH B (Autor:in) / SNAPE NATHAN (Autor:in)

    Erscheinungsdatum :

    04.11.2020


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    F02K JET-PROPULSION PLANTS , Strahltriebwerke / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F02C Gasturbinenanlagen , GAS-TURBINE PLANTS



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