Airbus Deutschland Gmbh

Airbus Operations Gmbh

Matthias Witschke

Thomas Scherer

Ahmet Kayihan Kiryaman

Ozan Uluc

Wolfgang Ebigt

Carsten Colberg

Marco Mundt

Peter Detjen

Kayihan Ahmet Kiryaman

A system for cooling items of freight on board an aircraft includes a refrigerating device and also a cooling station to which cooling energy generated by the refrigerating device is supplied by a refrigerant medium. The cooling station is capable of being connected to a freight compartment of the aircraft or to a freight container on board the aircraft, in order to lead the cooling energy supplied to the cooling station away into the freight compartment or into the freight container. A freight container for receiving items of freight designated for transportation on board an aircraft is capable of being connected to a cooling station of a system for cooling items of freight on board an aircraft, so that the cooling energy supplied to the cooling station is capable of being led away into the freight container.

Cooling system and freight container

A cooling system for the cooling of heat producing devices in an aircraft is designed with a central cold producing device, at least one cold consumer and a cold conveyance system which connects the cold producing device and the cold consumer. With this cooling system, the cold conveyance system has at least one cooling circuit which supplies a cooled cold carrier medium from the cold producing device to at least one cold consumer and brings the cold carrier medium back to the cold producing device, so that at least one cold consumer is supplied with the cold produced in the cold producing device.

Cooling system for the cooling of heat-producing devices in an aircraft

A dispenser of cooled or heated liquid which in one embodiment is a server cart for an aircraft. To avoid the need for a pump, the reservoir has a cooling or heating heat exchanger that helically coils around the main reservoir, which cools from the top down or heats from the bottom up, forming a counter current. The reservoir is connected to at least two conduits, one near the cooler top of the reservoir and one near the relatively warmer bottom of the reservoir. The two conduits connect to one another at a distance from the reservoir forming a dispensing passage, thereby allowing fluid to constantly circulate through the dispensing passage due to difference in the specific gravity in the fluid caused by the temperature difference. The elimination of the pump device is especially desirable for weight sensitive environments such as an aircraft.

Device for providing a cooled or heated liquid onboard an aircraft

In a cooling system () for cooling heat-generating installations () in an aircraft, with a refrigerating installation (), at least one refrigeration consumer () and a refrigeration transport system () connecting the refrigerating installation () and the refrigeration consumer (), it is provided that the refrigerating installation () comprises at least one refrigeration machine () which covers the maximum refrigeration requirement of the at least one refrigeration consumer () and in that the at least one refrigeration consumer () is supplied with cold generated in the refrigerating installation () via a refrigerating agent circulating in the refrigeration transport system ().

Cooling system for cooling heat-generating installations and for maintaining the temperature of closed-off areas at below cabin temperature in an aircraft

Growing community of inventors

Hamburg, Germany

Matthias Witschke