A system for distributing air to a plurality of aircraft zones includes an air mixer (22) including an air inlet plenum (26) and a manifold (24). The manifold including a plurality of sections (30) fluidly coupled to the plurality of aircraft zones. At least one thermoelectric device (40) is associated with said plurality of sections of said manifold. The at least one thermoelectric device is operable to condition air within said plurality of sections to a desired temperature corresponding to the plurality of aircraft zones.


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    Titel :

    AIR DISTRIBUTION MANIFOLD WITH INTEGRAL MULTIZONE THERMOELECTRIC TEC TRIM SYSTEM


    Weitere Titelangaben:

    LUFTVERTEILUNGSBLOCK MIT INTEGRIERTEM MEHRZONIGEM THERMOELEKTRISCHEM TEC TRIMMSYSTEM
    COLLECTEUR DE DISTRIBUTION D'AIR INTÉGRANT UN SYSTÈME THERMOÉLECTRIQUE TEC MULTIZONE


    Beteiligte:
    ARMY DONALD E (Autor:in)

    Erscheinungsdatum :

    24.07.2019


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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