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Additives to Prevent Filamentous Coke Formation in Endothermic Heat Exchangers

机译:防止吸热热交换器中丝状焦形成的添加剂

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Aircraft that travel at hypersonic speeds must use fuel to cool the ramjet/scramjet propulsion system. Both sensible heating and endothermic reactions can be used to provide the required heat sink; however, in the process the fuel temperature can reach 650 deg C (1200 deg F). When fuel reaches these temperatures, carbonaceous deposits (coke) form on the walls of the heat exchangers. These deposits can inhibit fuel flow and reduce transfer across the heat exchanger surface. Coke foramtion is a complicated process and deposits are known to form by at least three different mechanisms: an oxidative mechanism involving dissolved oxygen in the fuel (1,2) a gas phase mechanism in which high molecula weight hydrocarbons are formed from the products of thermal cracking reactions (condendation mechanism) (3,4,5,6), and finally a reaction between the fuel and metals in the flow path walls, which produces carbon filaments (7,8,9). Although methods currently are avaiable for controlling the oxidative and condensation pathways (1,2,5,10), a practical means to control the filamentous mechanism, which is the dominant coke formation mechanism under these conditions, has not yet been identified.
机译:以超音速飞行的飞机必须使用燃料冷却冲压喷气发动机/超燃冲压发动机的推进系统。显热和吸热反应均可用于提供所需的散热器。但是,在此过程中,燃料温度可以达到650摄氏度(1200华氏度)。当燃料达到这些温度时,在热交换器壁上会形成碳质沉积物(焦炭)。这些沉积物会抑制燃料流动,并减少整个热交换器表面的传递。焦炭的形成是一个复杂的过程,并且已知通过至少三种不同的机理形成沉积物:一种涉及在燃料中溶解氧的氧化机理(1,2),一种气相机理,其中由热产物形成高分子量的碳氢化合物。裂解反应(屈服机理)(3、4、5、6),最后是燃料与流道壁中的金属之间的反应,从而产生碳丝(7、8、9)。尽管目前有控制氧化和冷凝途径的方法(1,2,5,10),但尚未发现控制丝状机理的实用手段,而丝状机理是这些条件下主要的焦炭形成机理。

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