An aircraft includes one or more engines configured to generate high-pressure bleed air and low-pressure bleed air. An aircraft environmental control system (ECS) is in fluid communication with one or more of the engines to receive the high-pressure bleed air and the low-pressure bleed air. The ECS calculates a synthesized low-pressure value associated with the low-pressure bleed air while still providing bleed air using the high pressure bleed air. The ECS further switches from the high pressure bleed air to the low-bleed pressure air through the ECS while blocking flow of the high-pressure bleed air through the ECS based on the synthesized low-pressure value.


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    Titel :

    SYNTHESIZED LOW-PRESSURE BLEED AIR SCHEME FOR AIRCRAFT BLEED AIR NETWORK


    Beteiligte:
    KAMENETZ JEFFRY K (Autor:in) / KLINE ERIN G (Autor:in) / ERNST JEFFREY (Autor:in) / SCHRODER BRUCE R (Autor:in) / DEROY KEVIN R (Autor:in) / VESSELLA VINCE (Autor:in) / MCGRATH DARRAGH (Autor:in) / FAGNANI ADAM (Autor:in) / LABRECQUE MICHEL (Autor:in)

    Erscheinungsdatum :

    26.09.2019


    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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