A system is provided for cooling at least one heat producing device in an aircraft that includes, but is not limited to at least one coolant circuit. A coolant absorbs heat from the heat producing device and dissipates heat, by way of a heat dissipation device, to the surroundings of the aircraft. A temperature spreading device reduces the temperature of the coolant in a feed line of the coolant circuit and increases the heat dissipation temperature of the heat dissipation device relative to the temperature of the coolant in a return line of the coolant circuit. In this manner ram air ducts that are commonly used in the state of the art or systems that consume pre-cooled air can be avoided, which in particular when the aircraft is situated on the ground on hot days can render avionics cooling or the like difficult.
SYSTEM UND VERFAHREN ZUM KÜHLEN MINDESTENS EINER WÄRME ERZEUGENDEN EINRICHTUNG IN EINEM FLUGZEUG
SYSTEM AND METHOD FOR COOLING AT LEAST ONE HEAT-PRODUCING DEVICE IN AN AIRCRAFT
SYSTÈME ET PROCÉDÉ DE REFROIDISSEMENT D'AU MOINS UN DISPOSITIF PRODUISANT DE LA CHALEUR DANS UN AVION
2015-11-04
Patent
Electronic Resource
German
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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