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New Hydrophilic, Composite Membranes for Air Removal from Water Coolant Systems

机译:新的亲水性,复合膜,用于空气冷却剂系统的空气去除

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Liquid coolants are commonly used as thermal transport media to increase efficiency and flexibility in aerospace vehicle design. The introduction of gas bubbles into the coolant can have negative consequences, including: loss of centrifugal pump prime, irregular sensor readings, and blockage of coolant flow to remote systems. One solution to mitigate these problems is the development of a passive gas removal device, or gas trap, installed in the flight cooling system. In this study, a new hydrophilic, composite membrane has been developed for passage of the coolant fluid and retention of gas bubbles. The trapped bubbles are subsequently vented from the system by a thin, hydrophobic, microporous membrane. The original design for this work employed a homogeneous membrane that was susceptible to fouling and pore plugging. Spare gas traps of this variety have degraded during storage, and recreation of the membranes has been complicated due to problems with polymer duplication and property variations in the final membranes. In this work, replacements have been developed based on deposition of a hydrophilic polymer on the bore-side of a porous polyethylene (PE) tube. The tube provides excellent chemical and mechanical stability, and the hydrophilic layer provides for retention of gas bubbles due to elevated bubble pressure. Preliminary results have shown that intimate contact is required between the deposited layer and the substrate to overcome surface energy differences that reduce good adhesion. This has been accomplished by presoaking the membrane tube in the solvent to raise its surface energy. Polymer solutions of various concentrations have been used to promote penetration of the polymer layer into the porous substrate and to control separation layer thickness. The resulting composite membranes have shown repeatable decrease in nitrogen permeability, which is indicative of a decrease in membrane pore size. Studies with water permeation have yielded similar results. We have observed some swelling of the added polymer layer, which causes a slight decrease in membrane pore size, and should result in improved bubble retention. Preliminary studies have also been performed on gas retention in flowing systems. Initial results have been promising, with negligible gas permeation for the coated membranes compared to 100% gas permeation in the uncoated tube.
机译:液体冷却剂通常用作热传输介质,以提高航空航天车辆设计中的效率和灵活性。将气泡引入冷却剂可以具有负面后果,包括:离心泵源的损失,不规则的传感器读数和对远程系统的冷却剂流阻塞。减轻这些问题的一种解决方案是在飞行冷却系统中开发被动气体去除装置或气体陷阱。在该研究中,已经开发了一种新的亲水性复合膜,用于通过冷却剂流体通过并保持气泡。随后通过薄的疏水性的微孔膜从系统中排出捕获的气泡。这项工作的原始设计采用均匀的膜,易受污垢和孔隙堵塞的影响。这种品种的备用汽油疏水阀在储存期间降解,并且由于最终膜的聚合物重复和性能变化的问题,膜的娱乐已经复杂化。在这项工作中,已经基于在多孔聚乙烯(PE)管的孔侧上的亲水聚合物的沉积来开发替代品。该管提供优异的化学和机械稳定性,并且亲水层由于升高的气泡压力而提供气泡的保留。初步结果表明,在沉积的层和基材之间需要紧密接触,以克服降低良好粘附性的表面能差。这是通过预设溶剂中的膜管来实现的,以提高其表面能。已经使用各种浓度的聚合物溶液促进聚合物层渗透到多孔基材中并控制分离层厚度。所得复合膜已显示氮气渗透性的可重复降低,这表明膜孔径的降低。水渗透的研究产生了类似的结果。我们已经观察到添加的聚合物层的一些溶胀,这导致膜孔径略微降低,并且应导致改善的气泡保留。还对流动系统的气体保留进行了初步研究。初始结果一直很有前途,具有可忽略的涂覆膜的气体渗透与未涂覆的管中的100%气体渗透相比。

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