An environmental control system includes a refrigerant circuit (102) with a pump segment (156) and an evaporator segment (150), an evaporator (144) arranged along the evaporator segment and in fluid communication with of the refrigerant circuit, and a coolant circuit (104). The coolant circuit extends through the evaporator and is thermally coupled to refrigerant circuit by the evaporator, the coolant circuit including a first segment and a second segment arranged in parallel with one another to transfer heat from a first zone to a first portion of liquid coolant traversing the coolant circuit and transfer additional heat from a second zone to a second portion of coolant traversing the coolant circuit. Aircraft and environmental control systems are also described.


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    Title :

    AIRCRAFT MULTI-ZONE ENVIRONMENTAL CONTROL SYSTEMS


    Additional title:

    FLUGZEUG-MEHRZONEN-KLIMAREGELUNGSSYSTEME
    SYSTÈMES DE CONTRÔLE ENVIRONNEMENTAL MULTIZONE D'AÉRONEF


    Contributors:

    Publication date :

    2023-01-25


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



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