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斜向角度对涡轮轮缘密封性能的影响
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作者 白涛 张晶辉 +2 位作者 吝琳 王淼儿 李怡 《兵器装备工程学报》 CAS CSCD 北大核心 2022年第11期246-251,共6页
为了研究斜向角度对轮缘密封性能影响,对3个带有不同斜向角度的涡轮轮缘密封装置进行数值模拟。研究表明:不同斜向角度的盘腔装置内燃气入侵主要发生在靠近转子一侧;随着斜向角度增大,燃气入侵在周向和径向上都加深,从而使得封严效率下... 为了研究斜向角度对轮缘密封性能影响,对3个带有不同斜向角度的涡轮轮缘密封装置进行数值模拟。研究表明:不同斜向角度的盘腔装置内燃气入侵主要发生在靠近转子一侧;随着斜向角度增大,燃气入侵在周向和径向上都加深,从而使得封严效率下降,当斜向角度增加30°,最大可使得封严效率下降44%;随着斜向角度增大,由燃气入侵和封严出流诱导产生的封严间隙涡会增强,并且会促进转子下游通道涡的发展,从而使得转子叶片负荷能力降低。 展开更多
关键词 斜向角度 轮缘密封 涡轮 燃气入侵 封严效率
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郑州地铁某盾构区间隧道不同斜向交角下穿施工对铁路的影响研究 被引量:15
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作者 杜明芳 满景奇 +1 位作者 易领兵 朱东东 《现代隧道技术》 EI CSCD 北大核心 2020年第S01期466-472,共7页
为研究盾构隧道斜向下穿施工对铁路产生的影响,文章采用Midas/GTS数值分析方法对郑州地铁某盾构区间下穿陇海铁路施工进行有限元模拟;将计算得到的竖向和横向变形结果与实际监测结果进行对比,以验证模拟的合理性;针对5种不同形式的交叉... 为研究盾构隧道斜向下穿施工对铁路产生的影响,文章采用Midas/GTS数值分析方法对郑州地铁某盾构区间下穿陇海铁路施工进行有限元模拟;将计算得到的竖向和横向变形结果与实际监测结果进行对比,以验证模拟的合理性;针对5种不同形式的交叉工况(夹角18°,36°,54°,72°,90°),探讨和分析了盾构下穿施工对既有铁路的影响。结果表明:数值模拟的结果与实际变化趋势基本一致,变形的差异保持在10%以内,且都在控制要求内;交叉角度不同对路轨的变形有着很大影响,路轨的变形量和影响范围随交叉角度的减小而增大,尤其在角度小于54°时的变化更为明显;在实际的小夹角下穿施工时应给予一定的重视。 展开更多
关键词 地铁隧道 盾构 铁路 斜向角度 下穿施工 监测变形
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Wing load investigation of the plunge-diving locomotion of a gannet Morus inspired submersible aircraft 被引量:12
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作者 LIANG JianHong YAO GuoCai +4 位作者 WANG TianMiao YANG XingBang ZHAO WenDi SONG Gang ZHANG YuCheng 《Science China(Technological Sciences)》 SCIE EI CAS 2014年第2期390-402,共13页
In this paper,we studied the wing root pivot joint’s radial load of a submersible airplane which imitates the locomotion of gannet’s Morus plunge-diving,by implementing a test device name Mimic-Gannet.The housing of... In this paper,we studied the wing root pivot joint’s radial load of a submersible airplane which imitates the locomotion of gannet’s Morus plunge-diving,by implementing a test device name Mimic-Gannet.The housing of the device was designed by mimicking the morphology of a living gannet,and the folding wings were realized by the mechanism of variable swept back wing.Then,the radial loads of the wing root were obtained under the conditions of different dropping heights,different sweptback angles and different water-entry inclination angles(i.e.,the angle between the longitudinal body axis and the water surface),and the relationships between the peak radial load and the above three parameters were analyzed and discussed respectively.In the studied areas,the minimum peak radial load of the pivot joint is 50.93 N,while the maximum reaches up to1135.00 N.The largest peak load would be generated for the situation of vertical water entry and zero wing sweptback angle.And it is of great significance to choose the three parameters properly to reduce the pivot joint’s radial load,i.e.,larger wing sweptback angle,smaller dropping height and water-entry inclination angle.It is also concluded that the peak radial load on the wing root is closely linear with the water-entry dropping height and the wing sweptback angle with a significant correlation.Eventually,the relationship between the wing load and the dropping height,water-entry inclination angle or wing sweptback angle,could be used to calculate the wing load about plunge-diving of a submersible aircraft,and the conclusions reveal the wing load characteristic of the gannet’s plunge process for the biologists. 展开更多
关键词 submersible aircraft mimic gannet water entry plunge diving sweptback wing load investigation
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