A climate control system (1), intended to be temporarily connected to at least one aircraft (2), when the aircraft is on the ground, with which handled air with at least one flexible conduit (23) is supplied to the aircraft's cabin from at least one air handling unit (3). The air handling unit (3) is comprised of at least one heating and cooling package (29) with which air to the cabin is heated or cooled and that the climate control system includes a transfer device (6) with which the air handling device may be moved in relation to the aircraft. The transfer device (6) is comprised of a telescopic boarding bridge (7). The climate control system (1) includes a subsystem for conveying heated or cooled fluid between the combined heating and cooling package (29) and a district heating network alternatively a network for district cooling, whose subsystem includes at least one flexible conduit (18) that includes at least one conduit for the input of fluid to the air handling unit and at least one conduit for return of fluid from the air handling unit.


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    Title :

    CLIMATE CONTROL SYSTEM FOR AIRCRAFT


    Contributors:

    Publication date :

    2016-01-07


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen



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