An aircraft is provided including an environmental control system (ECS) having a first ECS pack and a second ECS pack. A duct couples the first ECS pack to the second ECS pack. The duct includes a first bypass conduit configured to form a bypass around a first primary heat exchanger of the first ECS pack. A second bypass conduit configured to form a bypass around a second primary heat exchanger of the second ECS pack. The duct includes a crossover conduit extending between the first bypass conduit and the second bypass conduit. The duct includes a plurality of valves for selectively controlling a flow between the first bypass conduit and the second bypass conduit.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Primary heat exchanger crossover bypass manifold


    Beteiligte:

    Erscheinungsdatum :

    23.01.2018


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



    HEAT EXCHANGER MANIFOLD

    STRZALKA BOGUSLAW / TARNOWSKI ADRIAN | Europäisches Patentamt | 2022

    Freier Zugriff

    HEAT EXCHANGER AND BYPASS VALVE USED IN HEAT EXCHANGER

    CHOI JI HOON / JANG JUN-IL / LEE WONTAEK et al. | Europäisches Patentamt | 2023

    Freier Zugriff

    ROTATING HEAT EXCHANGER/BYPASS COMBO

    HAUGSTETTER CHRISTOPH | Europäisches Patentamt | 2019

    Freier Zugriff

    Heat exchanger and bypass valve used in heat exchanger

    CHOI JI-HOON / JANG JUN-IL / LEE WON-TAEK et al. | Europäisches Patentamt | 2024

    Freier Zugriff

    ROTATING HEAT EXCHANGER/BYPASS COMBO

    HAUGSTETTER CHRISTOPH | Europäisches Patentamt | 2021

    Freier Zugriff