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进口旋流方向对涡轮导叶全气膜冷却效率影响的数值研究
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作者 付仲议 余强 +2 位作者 赵丹 房兴龙 黄琦 《燃气涡轮试验与研究》 2024年第2期35-40,共6页
为了获取旋流条件下涡轮导叶的气膜冷却特性,采用数值模拟的方法分析了逆时针和顺时针旋流对燃气涡轮一级导叶全气膜冷却效率的影响,分别总结了导叶前缘、压力面和吸力面冷却效率的变化规律。结果表明:进口旋流方向对涡轮导叶气膜冷却... 为了获取旋流条件下涡轮导叶的气膜冷却特性,采用数值模拟的方法分析了逆时针和顺时针旋流对燃气涡轮一级导叶全气膜冷却效率的影响,分别总结了导叶前缘、压力面和吸力面冷却效率的变化规律。结果表明:进口旋流方向对涡轮导叶气膜冷却效率有明显影响,且不同区域的冷却效率受旋流方向的影响规律不同;叶片表面冷气受旋流影响而发生偏转。整体上看,导叶压力面的气膜冷却效率在旋流方向为逆时针条件下更高,前缘和吸力面的气膜冷却效率在旋流方向为顺时针条件下更高。 展开更多
关键词 航空发动机 旋流方向 涡轮导叶 气膜冷却 冷却效率
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喷嘴旋向对多喷嘴预混燃烧的影响 被引量:2
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作者 柳伟杰 葛冰 +2 位作者 田寅申 臧述升 翁史烈 《燃烧科学与技术》 EI CAS CSCD 北大核心 2016年第4期289-295,共7页
针对五喷嘴模型燃烧室采用层流小火焰模型进行数值模拟,讨论了中心喷嘴同向旋流和反向旋流对甲烷/空气多喷嘴预混燃烧的影响,模拟结果与实验结果吻合较好.数值模拟结果表明,多喷嘴预混火焰悬浮于喷嘴上方0.3,d处,多喷嘴气流相互掺混形... 针对五喷嘴模型燃烧室采用层流小火焰模型进行数值模拟,讨论了中心喷嘴同向旋流和反向旋流对甲烷/空气多喷嘴预混燃烧的影响,模拟结果与实验结果吻合较好.数值模拟结果表明,多喷嘴预混火焰悬浮于喷嘴上方0.3,d处,多喷嘴气流相互掺混形成了高度湍流的掺混区,在掺混区内发生强烈的燃烧化学反应.中心喷嘴同向旋流布置时,主回流区顺时针扭曲,流动最后发展为与单喷嘴类似的旋流流场结构;对于中心喷嘴反向布置,气流整体旋流偏转较小,掺混后喷嘴气流仍然保持着各自的旋流流动结构.此外,中心喷嘴的同向/反向布置对多喷嘴预混燃烧反应进程的影响不大. 展开更多
关键词 预混火焰 多喷嘴燃烧 旋流方向 反应进程变量 小火焰模型
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燃气透平进口旋流对热斑迁移及动叶热负荷影响的研究 被引量:3
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作者 刘兆方 王志多 丰镇平 《工程热物理学报》 EI CAS CSCD 北大核心 2016年第8期1641-1647,共7页
燃烧室出口旋流及热斑对下游透平叶栅气热特性产生显著影响,本文针对该现象,研究受不同方向和不同进口时序位置的旋流影响下的燃气透平内热斑迁移规律及动叶热负荷特性。结果表明:叶片压力面侧流速较低,流动方向较容易被改变,反向旋流... 燃烧室出口旋流及热斑对下游透平叶栅气热特性产生显著影响,本文针对该现象,研究受不同方向和不同进口时序位置的旋流影响下的燃气透平内热斑迁移规律及动叶热负荷特性。结果表明:叶片压力面侧流速较低,流动方向较容易被改变,反向旋流与通道涡的联合作用使热斑核心区向上端壁迁移,而正向旋流作用相反,但两种旋流均使热斑核心区径向范围减小,周向范围增大;旋转的动叶通道使进入的残余旋流因掺混而迅速削弱,对热斑高温流体的径向驱动能力减弱;当热斑与旋流正对流道中心时,并未受到静叶前缘的切割,形态保持相对稳定,且核心区的径向范围较大;进口旋流的存在削弱了进口时序位置的影响,旋流方向对热斑迁移及动叶热负荷的作用更为显著。 展开更多
关键词 热斑 旋流方向 时序位置 非定常流动 动叶热负荷
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On-Cam Operation of Counter-Rotating Type Hydroelectric Unit 被引量:1
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作者 Toshiaki Suzuki Toshiaki Kanemoto 《Journal of Energy and Power Engineering》 2013年第10期1966-1973,共8页
The counter-rotating type hydroelectric unit, which is composed of the axial flow type tandem runners and the peculiar generator with double rotational armatures, has been proposed. In the unit, the front and the rear... The counter-rotating type hydroelectric unit, which is composed of the axial flow type tandem runners and the peculiar generator with double rotational armatures, has been proposed. In the unit, the front and the rear runners counter-drive the inner and the outer armatures of the generator, respectively. Besides, the flow direction at the rear runner outlet must coincide with the direction at the front runner inlet, because the angular momentum change through the rear runner must coincides with that through the front runner. In this paper, the tandem runners work at on-cam conditions in keeping the induced frequency constant, to provide the hydroelectric unit for the power grid system. The output and the hydraulic efficiency are affected by the adjusting angles of the front and the rear blades. Both optimum angles giving the maximum output or efficiency were presented at the various discharge/head circumstances, accompanying with the turbine performances. 展开更多
关键词 Hydroelectric unit counter rotation tandem runners double rotational armatures on-cam.
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第四代DLE燃烧室流场特性研究
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作者 张亮 袁逸人 +1 位作者 虞江鹏 葛冰 《热能动力工程》 CAS CSCD 北大核心 2019年第10期34-41,105,共9页
参照西门子的第四代干式低污染(Dry Low Emissions,DLE)燃烧室,设计了模型燃烧室,通过激光粒子图像速度仪(Particle Image Velocimetry,PIV)测量技术,对燃烧室头部出口流场进行了实验研究,分析了头部结构变化和入口空气流量变化对流场... 参照西门子的第四代干式低污染(Dry Low Emissions,DLE)燃烧室,设计了模型燃烧室,通过激光粒子图像速度仪(Particle Image Velocimetry,PIV)测量技术,对燃烧室头部出口流场进行了实验研究,分析了头部结构变化和入口空气流量变化对流场特性的影响。研究结果表明:两个主旋流器的旋流方向组合对燃烧室头部出口的流场特性有着很大影响;预混室RPL (Rich-Pilot-Lean)段的流量变化主要影响旋流器中轴线附近的轴向回流速度;入口空气流量变化对流场的影响主要表现在速度值上,但对速度变化趋势没有太大的影响。 展开更多
关键词 干式低污染(DLE) 激光粒子图像速度仪(PIV) 流场特性 旋流方向
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An experimental study on the effects of relative rotation direction on the wake interferences among tandem wind turbines 被引量:5
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作者 YUAN Wei TIAN Wei +1 位作者 OZBAY Ahmet HU Hui 《Science China(Physics,Mechanics & Astronomy)》 SCIE EI CAS 2014年第5期935-949,共15页
An experimental study was conducted to investigate the effects of relative rotation direction on the wake interferences among two tandemwind turbines models.While the oncoming flow conditions were kept in constant dur... An experimental study was conducted to investigate the effects of relative rotation direction on the wake interferences among two tandemwind turbines models.While the oncoming flow conditions were kept in constant during the experiments,turbine power outputs,wind loads acting on the turbines,and wake characteristics behind the turbines were compared quantitatively with turbine models in either co-rotating or counter-rotating configuration.The measurement results reveal that the turbines in counter-rotating would harvest more wind energy from the same oncoming wind,compared with the co-rotating case.While the recovery of the streamwise velocity deficits in the wake flows was found to be almost identical with the turbines operated in either co-rotating or counter-rotating,the significant azimuthal velocity generated in the wake flow behind the upstream turbine is believed to be the reason why the counter-rotating turbines would have a better power production performance.Since the azimuthal flow velocity in the wake flow was found to decrease monotonically with the increasing downstream distance,the benefits of the counter-rotating configuration were found to decrease gradually as the spacing between the tandem turbines increases.While the counter-rotating downstream turbine was found to produce up to 20%more power compared with that of co-rotating configuration with the turbine spacing being about 0.7D,the advantage was found to become almost negligible when the turbine spacing becomes greater than 6.5D.It suggests that the counter-rotating configuration design would be more beneficial to turbines in onshore wind farms due to the smaller turbine spacing(i.e.,~3 rotor diameters for onshore wind farms vs.~7 rotor diameters for offshore wind farms in the prevailing wind direction),especially for those turbines sited over complex terrains with the turbine spacing only about 1–2 rotor diameters. 展开更多
关键词 wind energy wind turbine aerodynamics wind turbine wake interference complex vortex flows
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Active control of circular cylinder flow by affiliated rotating cylinders 被引量:3
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作者 WANG JianSheng XU YuanXin TIAN YongSheng 《Science China(Technological Sciences)》 SCIE EI CAS 2013年第5期1186-1197,共12页
This study puts forward an active control method for circular cylinder flow by placing two small affiliated rotating cylinders adjacent to the main cylinder, and their effects on the drag and lift forces acting on the... This study puts forward an active control method for circular cylinder flow by placing two small affiliated rotating cylinders adjacent to the main cylinder, and their effects on the drag and lift forces acting on the main cylinder as well as the heat trans- fer effectiveness are numerically investigated. According to the diameter of the main cylinder the Reynolds number is chosen as Re=200. The well-proven finite volume method is employed for the calculation. The code is validated by comparing the present computed results of flow passing an isolated rotating cylinder with those available from the literature. To describe the present control model, two parameters are defined: the rotation direction of the two small cylinders (including co-current rota- tion and counter-current rotation) and the dimensionless rotation rate a. In the simulation, the rotation rate a varies from 0 to 2.4. The results indicate that the optimum rotation direction of the subsidiary cylinders, which is beneficial to both drag reduc- tion and beat transfer enhancement, is the co-current rotating (the upper affiliated cylinder spins clockwise and the lower affili- ated cylinder spins counter-clockwise). We observe noticeable suppression of the vortex shedding and favorable reduction of the fluid forces acting on the main cylinder as the rotation rate increases. Besides, the pressure and viscous components of the drag force are analyzed. Energy balance between energy cost for activating the rotating cylinders and energy saving by the momentum injection is considered. In addition, the influence of the affiliated rotating cylinders on heat transfer is also investi- gated. The average Nusselt number is found to increase with the rotation rate. 展开更多
关键词 active control affiliated cylinders vortex suppression drag and lift forces Nusselt number
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