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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。
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公开(公告)号：US08438865B2
公开(公告)日：2013-05-14
申请号：US12514742
申请日：2007-11-20
申请人： Andreas Frey , Ahmet Kayihan Kiryaman , Carsten Colberg , Peter Schwebke , Markus Kerber , Michael Dreyhaupt
发明人： Andreas Frey , Ahmet Kayihan Kiryaman , Carsten Colberg , Peter Schwebke , Markus Kerber , Michael Dreyhaupt
CPC分类号： H05K7/20845 , B64D13/06 , B64D2013/0614 , H05K7/20127 , H05K7/20218 , H05K7/20872 , Y02T50/44 , Y02T50/56
摘要： A cooling system (10) for cooling an aircraft device (12) comprises an evaporator (14, 16, 18) for receiving a fluid (F) which is to be evaporated, a first adsorber (24) which contains a medium (28) for the adsorption of the fluid (F) which is evaporated in the evaporator (14, 16, 18), as well as a second adsorber (26) which contains a medium for the adsorption of the fluid (F) which is evaporated in the evaporator (14, 16, 18). A control system (22) is adapted to establish or to interrupt a fluid connection between the evaporator (14, 16, 18) and the first and/or the second adsorber(s) (24, 26).
摘要翻译： 用于冷却航空器装置（12）的冷却系统（10）包括用于接收待蒸发的流体（F）的蒸发器（14,16,18），包含介质（28）的第一吸附器（24） 用于吸附在蒸发器（14,16,18）中蒸发的流体（F）以及第二吸附器（26），所述第二吸附器包含吸附流体（F）的介质，所述介质在所述蒸发器 蒸发器（14,16,18）。 控制系统（22）适于建立或中断蒸发器（14,16,18）与第一和/或第二吸附器（24,26）之间的流体连接。
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公开(公告)号：US20100051237A1
公开(公告)日：2010-03-04
申请号：US12514742
申请日：2007-11-20
申请人： Andreas Frey , Ahmet Kayihan Kiryaman , Carsten Colberg , Peter Schwebke , Markus Kerber , Michael Dreyhaupt
发明人： Andreas Frey , Ahmet Kayihan Kiryaman , Carsten Colberg , Peter Schwebke , Markus Kerber , Michael Dreyhaupt
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： A cooling system (10) for cooling an aircraft device (12) comprises an evaporator (14, 16, 18) for receiving a fluid (F) which is to be evaporated, a first adsorber (24) which contains a medium (28) for the adsorption of the fluid (F) which is evaporated in the evaporator (14, 16, 18), as well as a second adsorber (26) which contains a medium for the adsorption of the fluid (F) which is evaporated in the evaporator (14, 16, 18). A control system (22) is adapted to establish or to interrupt a fluid connection between the evaporator (14, 16, 18) and the first and/or the second adsorber(s) (24, 26).
摘要翻译： 用于冷却航空器装置（12）的冷却系统（10）包括用于接收待蒸发的流体（F）的蒸发器（14,16,18），包含介质（28）的第一吸附器（24） 用于吸附在蒸发器（14,16,18）中蒸发的流体（F）以及第二吸附器（26），所述第二吸附器包含吸附流体（F）的介质，所述介质在所述蒸发器 蒸发器（14,16,18）。 控制系统（22）适于建立或中断蒸发器（14,16,18）与第一和/或第二吸附器（24,26）之间的流体连接。
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