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) (50) is in fluid communication with one or more of the engines (12) 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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    Title :

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


    Additional title:

    SYNTHETISIERTES NIEDERDRUCK-ZAPFLUFTSCHEMA FÜR EIN FLUGZEUGZAPFLUFTNETZWERK
    SCHÉMA D'AIR DE PURGE BASSE PRESSION SYNTHÉTISÉ POUR RÉSEAU D'AIR DE PURGE D'AÉRONEF


    Contributors:

    Publication date :

    2024-07-24


    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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