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.
CLIMATE CONTROL SYSTEM FOR AIRCRAFT
KLIMAREGELUNGSSYSTEM FÜR FLUGZEUGE
SYSTÈME DE RÉGULATION THERMIQUE POUR AÉRONEF
2017-08-16
Patent
Electronic Resource
English
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 |
Individual and collective climate control in aircraft cabins
Online Contents | 2006
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