An environmental control system (ECS) for a multi-engine aircraft includes a controller configured to switch the ECS between a plurality of operating modes. The plurality of operating modes includes a first operating mode configured to receive bleed air from each engine of the aircraft in a first environmental condition, wherein the pressure of the bleed air is about equal from each engine. The plurality of operating modes includes a second operating mode configured to receive bleed air from at least one engine of the aircraft in a second environmental condition, wherein the pressure of the bleed air is different between at least two engines.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    ENVIRONMENTAL COOLING SYSTEMS FOR AIRCRAFT


    Beteiligte:
    SABNIS JAYANT (Autor:in) / BRUNO LOUIS J (Autor:in)

    Erscheinungsdatum :

    2016-11-17


    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



    Environmental cooling systems for aircraft

    SABNIS JAYANT / BRUNO LOUIS J | Europäisches Patentamt | 2020

    Freier Zugriff

    ENVIRONMENTAL COOLING SYSTEMS FOR AIRCRAFT

    SABNIS JAYANT / BRUNO LOUIS J | Europäisches Patentamt | 2020

    Freier Zugriff

    ENVIRONMENTAL COOLING SYSTEMS FOR AIRCRAFT

    SABNIS JAYANT / BRUNO LOUIS J | Europäisches Patentamt | 2019

    Freier Zugriff

    Environmental cooling systems for aircraft

    SABNIS JAYANT / BRUNO LOUIS J | Europäisches Patentamt | 2019

    Freier Zugriff

    Aircraft environmental systems

    Neese, Bill | SLUB | 1999