首页> 外国专利> Heat exchange circuit for air conditioning and cooling electronic equipment in aircraft, comprises heat exchangers, first and second heat transfer fluid loops and auxiliary tubes connecting the loops

Heat exchange circuit for air conditioning and cooling electronic equipment in aircraft, comprises heat exchangers, first and second heat transfer fluid loops and auxiliary tubes connecting the loops

机译:飞机空调和冷却电子设备的热交换回路,包括热交换器,第一和第二传热流体回路以及连接回路的辅助管

摘要

A heat exchange circuit for air conditioning in an aircraft, comprises heat exchangers (7) for cooling electronic equipment; first and second heat transfer fluid (HTF) loops (1, 2), each with HTF reservoir(s) (11, 21), pumps (12, 22), tubing and cooling devices (6, 13; 10, 23); and auxiliary tubes (40, 41; 42, 43) connecting the loops and containing auxiliary valve(s) (4, 5). A heat exchange circuit, using heat transfer fluid (HTF), for air conditioning in an aircraft, comprises: (A) heat exchangers (7) for cooling heat-generating electronic equipment; (B) first and second HTF loops (1, 2), each comprising HTF reservoir(s) (11, 21), pumps (12, 22) for supplying the HTF from the reservoirs into the loops, tubing for conveying HTF between the loops and heat exchangers to carry out heat exchange and cooling devices (6, 13; 10, 23) connected in series in the loops between the reservoirs and the heat exchangers; and (C) auxiliary tubes (40, 41; 42, 43) connecting the first and second loops and containing auxiliary valve(s) (4, 5) for allowing or preventing passage of at least part of the HTF between the two loops. Independent claims are included for: (1) a corresponding heat exchanging method, involving circulating HTF in the first and second loops (1, 2) between the reservoirs (11, 21) and heat exchanger (7) to cool the electronic equipment; cooling the HTF in the first loop using the cooling devices (6, 13; 10, 23); and connecting the two loops via the auxiliary tubes (40, 41; 42, 43); and (2) an aircraft air conditioning system, comprising at least one heat exchange circuit as above; an air circuit for providing conditioned air to pressurized zones of the aircraft from air extracted from the engines; and at least one air conditioning unit, having a turbine for conditioning air in the circuit and associated with a vapor cycle comprising a closed loop in which is refrigerant is circulated to cool the HTF in the loops (1, 2) of the heat exchange circuits.
机译:用于飞机中空调的热交换回路,包括用于冷却电子设备的热交换器(7);第一和第二传热流体(HTF)回路(1、2),每个回路都有HTF储罐(11、21),泵(12、22),管路和冷却装置(6、13、10、23);辅助管(40、41; 42、43)连接回路并包含辅助阀(4、5)。一种使用传热流体(HTF)进行飞机空调的热交换回路,包括:(A)热交换器(7),用于冷却发热的电子设备; (B)第一和第二HTF回路(1、2),每个回路均包括一个或多个HTF储液器(11、21),用于将HTF从储液器供应到回路中的泵(12、22),回路和热交换器,以执行在储罐和热交换器之间的回路中串联连接的热交换和冷却装置(6、13、10、23); (C)连接第一和第二回路并包含辅助阀(4、5)的辅助管(40、41; 42、43),用于允许或防止HTF的至少一部分在两个回路之间通过。包括以下独立权利要求:(1)相应的热交换方法,其涉及使HTF在储液罐(11、21)和热交换器(7)之间的第一回路和第二回路(1、2)中循环以冷却电子设备;使用冷却装置(6、13、10、23)在第一回路中冷却HTF;并通过辅助管(40、41; 42、43)连接两个回路。 (2)一种飞机空调系统,包括至少一个如上所述的热交换回路;空气回路,用于从发动机抽出的空气向飞机的加压区域提供调节空气;至少一个空调单元,其具有用于调节回路中的空气的涡轮机,并具有蒸气循环,该蒸气循环包括闭合回路,制冷剂在该闭合回路中循环以冷却热交换回路的回路(1、2)中的HTF。 。

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