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Refrigerant Mixtures 制冷剂混合物
Pub Date : 2021-08-10 DOI: 10.5772/intechopen.99024
Selva Pandian Ebenezer
Evolution of refrigerants has a history since the introduction of air conditioning systems by Sir Willis Carrier. The first generation air conditioning systems used natural refrigerants like air, water, carbon dioxide etc. But the need of low temperature requirements in residential and industrial air conditioning systems has forced the air conditioning field to use chloro flouro carbon type refrigerants, which was introduced by Dupon in the previous century. Physical and chemical properties of CFC type refrigerants were very good and satisfactory and so it was used in almost all refrigeration and air conditioning systems. The main disadvantage of CFC type refrigerants is harming the ozone layer and contributing much to the global warming. This chapter reviews the use of CFC type and introducing alternate type of refrigerants.
自威利斯·开利爵士引进空调系统以来,制冷剂的发展已有一段历史。第一代空调系统使用天然制冷剂,如空气、水、二氧化碳等。但由于住宅和工业空调系统对低温的要求,空调领域不得不使用杜邦公司在上个世纪推出的氯氟碳型制冷剂。CFC型制冷剂具有良好的物理化学性能,几乎应用于所有的制冷和空调系统。氯氟烃制冷剂的主要缺点是破坏臭氧层,导致全球变暖。本章回顾了氯氟烃制冷剂的使用情况,并介绍了制冷剂的替代类型。
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引用次数: 0
Effect of Roughness Elements on the Evolution of Thermal Stratification in a Cryogenic Propellant Tank 粗糙度元素对低温推进剂储罐热分层演变的影响
Pub Date : 2021-07-27 DOI: 10.5772/intechopen.98404
S. Vishnu, B. T. Kuzhiveli
The cryogenic propulsion era started with the use of liquid rockets. These rocket engines use propellants in liquid form with reasonably high density, allowing reduced tank size with a high mass ratio. Cryogenic engines are designed for liquid fuels that have to be held in liquid form at cryogenic temperature and gas at normal temperatures. Since propellants are stored at their boiling temperature or subcooled condition, minimal heat infiltration itself causes thermal stratification and self-pressurization. Due to stratification, the state of propellant inside the tank varies, and it is essential to keep the propellant properties in a predefined state for restarting the cryogenic engine after the coast phase. The propellant’s condition at the inlet of the propellant feed system or turbo pump must fall within a narrow range. If the inlet temperature is above the cavitation value, cavitation will likely to happen to result in the probable destruction of the flight vehicle. The present work aims to find an effective method to reduce the stratification phenomenon in a cryogenic storage tank. From previous studies, it is observed that the shape of the inner wall surface of the storage tank plays an essential role in the development of the stratified layer. A CFD model is established to predict the rate of self-pressurization in a liquid hydrogen container. The Volume of Fluid (VOF) method is used to predict the liquid–vapor interface movement, and the Lee phase change model is adopted for evaporation and condensation calculations. A detailed study has been conducted on a cylindrical storage tank with an iso grid and rib structure. The development of the stratified layer in the presence of iso grid and ribs are entirely different. The buoyancy-driven free convection flow over iso grid structure result in velocity and temperature profile that differs significantly from a smooth wall case. The thermal boundary layer was always more significant for iso grid type obstruction, and these obstructions induces streamline deflection and recirculation zones, which enhances heat transfer to bulk liquid. A larger self-pressurization rate is observed for tanks with an iso grid structure. The presence of ribs results in the reduction of upward buoyancy flow near the tank surface, whereas streamline deflection and recirculation zones were also perceptible. As the number of ribs increases, it nullifies the effect of the formation of recirculation zones. Finally, a maximum reduction of 32.89% in the self-pressurization rate is achieved with the incorporation of the rib structure in the tank wall.
低温推进时代始于液体火箭的使用。这些火箭发动机使用的推进剂是密度相当高的液态推进剂,因此可以减小燃料箱的体积,同时具有较高的质量比。低温发动机是为液体燃料设计的,这些燃料在低温下必须保持液态,而在常温下则必须保持气态。由于推进剂是在沸腾温度或过冷状态下储存的,因此热量渗入极少本身就会导致热分层和自增压。由于分层,推进剂在贮箱内的状态会发生变化,因此必须将推进剂的特性保持在预定状态,以便在沿岸阶段结束后重新启动低温发动机。推进剂进料系统或涡轮泵入口处的推进剂状态必须在一个很小的范围内。如果入口温度高于气蚀值,就很可能发生气蚀,导致飞行器可能毁坏。本研究旨在寻找一种有效的方法来减少低温贮箱中的分层现象。根据以往的研究,储气罐内壁表面的形状对分层的形成起着至关重要的作用。本文建立了一个 CFD 模型来预测液氢容器中的自增压速率。采用流体体积(VOF)方法预测液体-蒸汽界面运动,并采用 Lee 相变模型进行蒸发和冷凝计算。对等网格和肋条结构的圆柱形储罐进行了详细研究。等网格和肋条结构下分层的发展完全不同。等网格结构上的浮力驱动自由对流导致速度和温度曲线与光滑壁面的情况大不相同。热边界层在等网格状障碍物中总是更为显著,这些障碍物导致流线偏转和再循环区,从而增强了向散装液体的热传递。等网格结构的储罐自压率更高。肋条的存在导致罐体表面附近向上的浮力流减少,同时也能感觉到流线偏转和再循环区。随着肋条数量的增加,形成再循环区的效果也会减弱。最后,在罐壁加入肋条结构后,自压率最大降低了 32.89%。
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引用次数: 0
Ultimate Compressive Strength of Steel Stiffened-Plate Structures Triggered by Brittle Fracture under Cryogenic Conditions 低温条件下脆性断裂引发的钢加筋板结构极限抗压强度
Pub Date : 2021-04-12 DOI: 10.5772/INTECHOPEN.97155
Dong Hun Lee, J. Paik, J. Ringsberg, P. Tan
This chapter presents a practical method to investigate the effects of brittle fracture on the ultimate compressive strength of steel stiffened-plate structures under cryogenic conditions. Computational models are developed to analyse the ultimate compressive strength of steel stiffened-plate structures, triggered by brittle fracture, under cryogenic condition. A phenomenological form of the material model for the high-strength steel at cryogenic condition is proposed, that takes into account the Bauschinger effect, and implemented into a nonlinear finite element solver (LS-DYNA). Comparison between computational predictions and experimental measurements is made for the ultimate compressive strength response of a full-scale steel stiffened-plate structure, showing a good agreement between them.
本章提出了一种研究低温条件下脆性断裂对钢加筋板结构极限抗压强度影响的实用方法。建立了低温条件下钢加筋板结构脆性断裂的极限抗压强度计算模型。提出了一种考虑鲍辛格效应的高强钢低温条件下材料模型的现象学形式,并将其实现到非线性有限元求解器(LS-DYNA)中。对全尺寸钢加筋板结构的极限抗压强度响应进行了计算预测与实验测量的比较,结果表明两者吻合较好。
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引用次数: 0
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Low-Temperature Technologies [Working Title]
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