该文旨在确定渗灌渗水涂层成分的配比方案,制备出渗水性能良好的渗灌滴头。通过对所选用的蒙脱土MMT及聚丙烯酰胺PAM材料的结构和性能进行了分析和比较,设计制备工艺,制备渗灌滴头,在实验室内搭建了渗灌材料的实际渗水的试验平台;采用...该文旨在确定渗灌渗水涂层成分的配比方案,制备出渗水性能良好的渗灌滴头。通过对所选用的蒙脱土MMT及聚丙烯酰胺PAM材料的结构和性能进行了分析和比较,设计制备工艺,制备渗灌滴头,在实验室内搭建了渗灌材料的实际渗水的试验平台;采用拉伸强度试验对渗灌导水涂层材料与纤维结合性能进行研究,用电子显微镜对不同配比的渗灌导水材料的形貌进行了观察并对其微观结构和组成进行了分析,在不同环境条件下对渗灌材料的渗水自调节性进行分析。结果表明:PAM/MMT悬浮液的配比为0.20 g/50 m L(1∶250)时导水材料的成膜性较,涂层成膜性较好,分布较均匀。对于以1∶250聚丙烯酰胺和蒙脱石制备的的渗水材料,温度一定时,随着环境土壤含水率的逐渐增加,渗水速率逐渐降低,土壤含水率一定时,随着环境温度的增加,渗水速率逐渐下降。该研究为渗灌材料制备提供参考。展开更多
Abstract The continuously rotating detonation engine （CRDE） is a new concept of engines for air- craft and spacecraft. Quasi-stable continuously rotating detonation （CRD） can be observed in an annular combustion c...Abstract The continuously rotating detonation engine （CRDE） is a new concept of engines for air- craft and spacecraft. Quasi-stable continuously rotating detonation （CRD） can be observed in an annular combustion chamber, but the sustaining, stabilizing and adjusting mechanisms are not yet clear. To learn more deeply into the CRDE, experimental studies have been carried out to inves- tigate hydrogen-oxygen CRDE. Pressure histories are obtained during each shot, which show that stable CRD waves are generated in the combustor, when feeding pressures are higher than 0.5 MPa for fuel and oxidizer, respectively. Each shot can keep running as long as fresh gas feeding main- tains. Close-up of the pressure history shows the repeatability of pressure peaks and indicates the detonation velocity in hydrogen-oxygen CRD, which proves the success of forming a stable CRD in the annular chamber. Spectrum of the pressure history matches the close-up analysis and confirms the CRD. It also shows multi-wave phenomenon and affirms the fact that in this case a single detonation wave is rotating in the annulus. Moreover, oscillation phenomenon is found in pressure peaks and a self-adjusting mechanism is proposed to explain the phenomenon.展开更多
文摘该文旨在确定渗灌渗水涂层成分的配比方案,制备出渗水性能良好的渗灌滴头。通过对所选用的蒙脱土MMT及聚丙烯酰胺PAM材料的结构和性能进行了分析和比较,设计制备工艺,制备渗灌滴头,在实验室内搭建了渗灌材料的实际渗水的试验平台;采用拉伸强度试验对渗灌导水涂层材料与纤维结合性能进行研究,用电子显微镜对不同配比的渗灌导水材料的形貌进行了观察并对其微观结构和组成进行了分析,在不同环境条件下对渗灌材料的渗水自调节性进行分析。结果表明:PAM/MMT悬浮液的配比为0.20 g/50 m L(1∶250)时导水材料的成膜性较,涂层成膜性较好,分布较均匀。对于以1∶250聚丙烯酰胺和蒙脱石制备的的渗水材料,温度一定时,随着环境土壤含水率的逐渐增加,渗水速率逐渐降低,土壤含水率一定时,随着环境温度的增加,渗水速率逐渐下降。该研究为渗灌材料制备提供参考。
基金supported by the National Natural Science Foundation of China(No.91441110)
文摘Abstract The continuously rotating detonation engine （CRDE） is a new concept of engines for air- craft and spacecraft. Quasi-stable continuously rotating detonation （CRD） can be observed in an annular combustion chamber, but the sustaining, stabilizing and adjusting mechanisms are not yet clear. To learn more deeply into the CRDE, experimental studies have been carried out to inves- tigate hydrogen-oxygen CRDE. Pressure histories are obtained during each shot, which show that stable CRD waves are generated in the combustor, when feeding pressures are higher than 0.5 MPa for fuel and oxidizer, respectively. Each shot can keep running as long as fresh gas feeding main- tains. Close-up of the pressure history shows the repeatability of pressure peaks and indicates the detonation velocity in hydrogen-oxygen CRD, which proves the success of forming a stable CRD in the annular chamber. Spectrum of the pressure history matches the close-up analysis and confirms the CRD. It also shows multi-wave phenomenon and affirms the fact that in this case a single detonation wave is rotating in the annulus. Moreover, oscillation phenomenon is found in pressure peaks and a self-adjusting mechanism is proposed to explain the phenomenon.
