COOLING SYSTEM AND METHOD FOR COOLING DRINKING WATER IN AN AIRCRAFT
摘要
The invention discloses the multistage cooling of an aircraft electronic system (2) with at least one electronic component which delivers heat. The multistage feature results from the use of a plurality of circuits for transferring the waste heat. An internal coolant (14) circulating in a closed circuit which is thermally coupled to the electronic component carries heat from the at least one electronic component to a heat exchanger (6) which delivers the heat to an external coolant which flows and/or circulates from a source outside of the aircraft electronic system (2) through the heat exchanger (6) to a sink outside of the aircraft electronic system (2). The internal coolant flows from the heat exchanger (6) in the direction of the at least one electronic component and/or circulates in a closed circuit.
申请公布号
EP2081825(A1)
申请公布日期
2009.07.29
申请号
EP20070819875
申请日期
2007.11.20
申请人
AIRBUS DEUTSCHLAND GMBH
发明人
FREY, ANDREAS;KIRYAMAN, AHMET KAYIHAN;COLBERG, CARSTEN;SCHWEBKE, PETER;KERBER, MARKUS;DREYHAUPT, MICHAEL