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Exit-flow velocity survey of two single-tangential-inlet vaneless turbine volutes

机译:两个单切入口无叶涡轮蜗壳的出口流速调查

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摘要

The most cited analytical technique for designing turbine volutes is to assume the throughflow is free from torque, although for this assumption to hold, the volute walls must lie near what would be streamlines in an unbounded free vortex-plus-sink flow. The single tangential inlet design, with inlet offset decreased and diameter increased to attain the weak exit swirl required by high specific speed turbines, deviates from such a shape, and the volute's internal geometry is no longer torque-free. It is desired to know the actual time-averaged flow leaving such a volute, so that a rotor can be designed to compliment it.For two existing single tangential inlet volutes, time-averaged radial and tangential velocity and static pressure measurements of exit flow have been obtained on a cylindrical cut plane through the radial-inflow section using a three-port yawmeter in air. The Reynolds numbers based on inlet pipe mean conditions, around 10~5, are well into the fully-turbulent regime and on the order of comparable water turbines.A comprehensive map of time-averaged exit flow of both volutes is presented. The integrated values of gross angular momentum flux change and total pressure loss coefficient are tabulated. Circumferential variation of flowrate and swirl strength highlight unexpected differences in outlet flow between the two volute designs. Results are presented alongside corresponding numerical results from the commercial package Fluent (Fluent, Inc., Lebanon, NH, USA) using Reynolds stress, k-ω, and inviscid flow models.In both volutes, measured gross exit angular momentum flux was more than 1.7 times what the zero-torque assumption would predict when blindly applied to the volute as a whole. This discrepancy is attributed to significant turning near the volute's inlet region leading to an updated view of what an appropriate control volume is when applying the zero-torque assumption. Additionally, variation of both radial and tangential velocity in both the circumferential and axial directions on the order of 15% of the mean value reveal that volute swirl characterization by a single measurement would have a significant associated uncertainty.
机译:设计涡轮机蜗壳时,最常引用的分析技术是假设通流没有扭矩,尽管要保持这一假设,蜗壳壁必须位于无边的自由涡旋加沉流中的流线附近。单切向进气口设计偏离了这种形状,进气口偏移减小了,直径增大了,以达到高比转速涡轮机所需的弱出口涡流,并且蜗壳的内部几何形状不再无扭矩。希望知道离开这种蜗壳的实际时间平均流量,以便可以设计转子来对其进行补充。对于两个现有的单切向入口蜗壳,出口流量的时间平均径向和切向速度以及静压力测量值使用三端口偏航仪在空气中通过径向流入部分在圆柱剖切面上获得λ。雷诺数基于进水管平均工况,大约在10〜5之间,完全进入了湍流状态,并且处于可比水轮机的水平。给出了两个蜗壳的时间平均出口流量的综合图。将总角动量通量变化和总压力损失系数的积分值制成表格。流量和旋流强度的周向变化突出表明了这两种蜗壳设计之间出口流量的意外差异。结果与商业软件包Fluent(Fluent,Inc.,Lebanon,NH,USA)的相应数值结果一起使用雷诺应力,k-ω和无粘性流模型给出。在两个蜗壳中,测得的总出口角动量通量均大于盲目地应用于整个蜗壳时,零扭矩假设的预测值的1.7倍。这种差异归因于蜗壳入口区域附近的明显转向,从而导致在应用零扭矩假设时适当控制体积的最新视图。另外,沿圆周方向和轴向方向的径向速度和切线速度的变化都在平均值的15%左右,这表明通过单次测量来表征蜗壳涡旋将具有显着的相关不确定性。

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