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Conform连续挤压双进多出生产挤压铜产品的实践 被引量:1
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作者 鄢明 吴予才 何剑辉 《中国有色冶金》 北大核心 2007年第5期52-55,共4页
采用双进四出方式,解决了单轮槽Conform连续挤压法难以生产小截面型材的问题。通过除氧化层和防扭绞实现了双根进料;通过一模多孔,设置分流刀和模支撑实现了多根出料,从而降低了挤压比,减少了溢料,提高了腔体等寿命。
关键词 双进四出连续挤压 组合腔体 除氧化层装置 防扭绞装置 防粘结装置 分流刀
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A comparative analysis of 3D flow fields between straight and bowed blades in a steam turbine
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作者 M.HASSANVAND 王仲奇 王松涛 《Journal of Harbin Institute of Technology(New Series)》 EI CAS 2004年第6期588-592,共5页
A commercial Navier-Stokes flow solver has been employed for simulating steady subsonic flow characteristics and analyzing the comparative features of flow fields between straight and bowed blades applied to the stato... A commercial Navier-Stokes flow solver has been employed for simulating steady subsonic flow characteristics and analyzing the comparative features of flow fields between straight and bowed blades applied to the stator of a high pressure steam turbine. For comparison, we have studied the effects of bowed blades on the wakes of stator trailing edge and horse shoe vortex in the rotor. It was found that the position of wakes for bowed blades is shifted toward the blade suction side. Also, we have discussed and compared the entropy generation and energy loss caused by dissipation mechanism within the boundary layers on the hub and shroud; and temperature gradient in meridional plane. 展开更多
关键词 bowed blade STATOR WAKE VORTEX entropy generation
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Corner Separations around a NACA65 Blade in a Decelerating Flow (Experimental Investigations by Five-Hole Probe and PIV) 被引量:1
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作者 Yoichi Kinoue Ryutaro Ohhira +1 位作者 Norimasa Shiomi Toshiaki Setoguchi 《Journal of Thermal Science》 SCIE EI CAS CSCD 2013年第1期23-28,共6页
In order to examine the fundamental characteristics of corner separation in a decelerating cascade flow,the experimental apparatus was made and separations around a NACA65 blade in a decelerating channel flow were exa... In order to examine the fundamental characteristics of corner separation in a decelerating cascade flow,the experimental apparatus was made and separations around a NACA65 blade in a decelerating channel flow were examined.Two-dimensional calculations show that the NACA65 cascade flow that has 45 deg.of turning,1.24 of solidity and 17 deg.of stagger angle is equivalent to the channel flow that has 14 deg.of stagger angle in terms of pitchwise blade force.Experimental investigation by five-hole probe shows that the accumulations of low energy fluid can be seen around the corner part and the overturning flow due to the secondary flow exists.And,as the periodicity of the blade wake in a pitchwise direction is comparably good,the wake of this channel flow is similar to the wake of the cascade flow for two pitch portion.PIV measurement results shows that a vortex pattern can be seen in the momentary streamline on the suction surface of the blade and in the averaged streamline on the perpendicular to both the suction surface and the endwall. 展开更多
关键词 corner separation NACA65 blade decelerating channel flow five-hole probe PIV
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