A climate control system is intended to be temporarily connected externally to an aircraft when the aircraft is on the ground. The system directs air through flexible conduits from an external independent air handling unit to the aircraft. The system may include a transfer device with which the air handling device may be moved in relation to the aircraft. The transfer device may be an element of a telescopic boarding bridge. The system includes systems for conveying heated or cooled fluid from a distant source to the air handling unit.


    Access

    Download


    Export, share and cite



    Title :

    External systems for aircraft climate control


    Contributors:

    Publication date :

    2019-06-18


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



    EXTERNAL AIRCRAFT GROUND CONTROL

    WARPINSKI MATTHEW / LAMKIN ANDREW FANNON / BUSTER DUKE | European Patent Office | 2016

    Free access

    External aircraft ground control

    WARPINSKI MATTHEW / LAMKIN ANDREW FANNON / BUSTER DUKE | European Patent Office | 2018

    Free access

    CLIMATE CONTROL SYSTEM FOR AIRCRAFT

    TENGMAN ANDERS | European Patent Office | 2016

    Free access

    Aircraft External Weight and Balance Systems

    Ogilvie, G. K. | British Library Conference Proceedings | 2005


    CLIMATE CONTROL SYSTEM FOR AIRCRAFT

    TENGMAN ANDERS | European Patent Office | 2017

    Free access