公开(公告)号：US20100044016A1

公开(公告)日：2010-02-25

申请号：US12514731

申请日：2007-11-20

申请人： Andreas Frey ,  Ahmet Kayihan Kiryaman ,  Markus Kerber ,  Michael Dreyhaupt ,  Carsten Colberg ,  Peter Schwebke

发明人： Andreas Frey ,  Ahmet Kayihan Kiryaman ,  Markus Kerber ,  Michael Dreyhaupt ,  Carsten Colberg ,  Peter Schwebke

IPC分类号： F28D15/00

CPC分类号： H05K7/20845 ,  B64D13/06 ,  B64D2013/0614 ,  H05K7/20127 ,  H05K7/20218 ,  H05K7/20872 ,  Y02T50/44 ,  Y02T50/56

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.

摘要翻译： 本发明公开了一种具有至少一个传递热量的电子部件的飞行器电子系统（2）的多级冷却。 多级特征是由于使用多个用于传送废热的电路。 在热耦合到电子部件的闭合回路中循环的内部冷却剂（14）将热量从至少一个电子部件运送到热交换器（6），热交换器将热量传递到外部冷却剂，所述外部冷却剂从 飞机电子系统（2）外部通过热交换器（6）到飞机电子系统（2）外的水槽的源。 内部冷却剂沿着至少一个电子部件的方向从热交换器（6）流动和/或在闭合回路中循环。

公开(公告)号：US20090126900A1

公开(公告)日：2009-05-21

申请号：US10584779

申请日：2004-12-30

申请人： Thomas Scherer ,  Mathias Witschke ,  Carsten Colberg

发明人： Thomas Scherer ,  Mathias Witschke ,  Carsten Colberg

IPC分类号： B60H1/32

CPC分类号： F25D17/02 ,  B64D11/04 ,  B64D13/06 ,  B64D2013/0629 ,  Y02T50/56

摘要： A cooling system (10) for the cooling of heat producing devices (44, 46, 48) in an aircraft is designed with a central cold producing device (12), at least one cold consumer (44, 46, 48) and a cold conveyance system (14) which connects the cold producing device (12) and the cold consumer (44, 46, 48). With this cooling system, the cold conveyance system (14) has at least one cooling circuit which supplies a cooled cold carrier medium from the cold producing device (12) to at least one cold consumer (44, 46, 48) and brings this back to the cold producing device (12), so that at least one cold consumer (44, 46, 48) is supplied with the cold produced in the cold producing device (12) by means of the cold carrier medium circulating in the cooling circuit.

摘要翻译： 用于冷却飞行器中的发热装置（44,46,48）的冷却系统（10）设计有中央冷产生装置（12），至少一个冷消耗装置（44,46,48）和冷 输送系统（14），其连接冷产生装置（12）和冷消费者（44,46,48）。 通过该冷却系统，冷输送系统（14）具有至少一个冷却回路，该冷却回路将冷却的冷载体介质从冷产生装置（12）提供给至少一个冷消耗器（44,46,48），并将其返回 通过在冷却回路中循环的冷载体介质，向冷产生装置（12）提供至少一个冷消耗装置（44,46,48），冷冷生产装置（12）产生的冷。