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The cooling system to expel heat from a heat source located in the interior of an aircraft, and.Method for the discharge of heat from a heat source disposed within a plane

机译:用于从位于飞机内部的热源排出热量的冷却系统以及用于从位于飞机内部的热源释放热量的方法

摘要

"Refrigeration system to expel heat from a heat source located in the interior of an aircraft.Method for the discharge of heat from a heat source disposed in the interior of an aircraft.A refrigeration system to expel heat from a heat source (30) located in the interior of an aircraft to a reducer of heat (322).A piping system (10) sealed with respect to the surrounding atmosphere.Which is thermally coupled with a heat input section (14) with the heat source (38) and with a section of heat output (22) with the reducer heat (32).And that preferably has an essentially adiabatic transport section (21), it is proposed that the piping system (10) is filled with a heat transport medium (12).When he takes heat from the heat source (38) in the entry of heat (14) is undergoing a transition from the liquid phase to the gas phase.Then flows to the heat output section (22) and here, when the discharge of heat to the heat sink (32).Condenses again again and flows back to the heat input section (14).
机译:制冷系统,用于从位于飞机内部的热源排出热量。从布置在飞机内部的热源释放热量的方法。制冷系统,用于从热源释放热量(30)位于飞机内部的热量减少装置(322)。相对于周围大气密封的管道系统(10),其中热源(38)和热输入段(14)与热输入段(14)热耦合。提出了一种具有一部分热量输出(22)和还原剂热量(32)的方案。并且优选具有基本上绝热的输送段(21),建议在管道系统(10)中填充传热介质(12)。当他从热源(38)吸收热量时,热量(14)进入从液相到气相的转变,然后流到热输出部分(22),在此当热量再次流入散热器(32)。再次凝结并回流到热量输入部分(14 )。

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