Abstract: 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.

Abstract: 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).