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Average velocity measurements in six automotive torque converters: Part 1 - pump measurements

机译:六个汽车液力变矩器的平均速度测量:第1部分-泵测量

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摘要

The internal flow fields of three automotive Plexiglas torque converter pumps with two different turbines were examined. A laser velocimeter was utilized to measure the velocity flow field at the pump mid- and exit planes in the six different geometry combinations; the stator was the same for all combinations. The pump geometries differed only by the exit blade angle while the turbine geometries differed only by the inlet blade angle. The torque converter was operated at three different turbine/pump rotational speed ratios: 0.065 (near stall), 0.600, and 0.800 (near coupling point). For all geometries at the mid-plane, at low speed ratios the velocities are slightly higher near the suction surface but for the highest speed ratio a strong reverse flow is seen near the suction surface; at high speed ratios velocities were high near the shell. At the exit plane the flow is non-uniform in the blade-to-blade direction at all speed ratios. Velocities were fairly uniform in the core-to-shell direction at all speed ratios. Furthermore, through flow velocity non-uniformity became more pronounced as the speed ratio increased. Variations in turbine inlet blade angle minimally altered the pump mid- and exit plane velocities. Variations in the pump exit blade angle had no effects on the pump mid-plane velocity fields but did, however, significantly affect the exit plane flow fields. In particular, core-to-shell direction through flow velocity non-uniformity decreased with a corresponding decrease in pump exit blade angle while through flow velocity non-uniformity in the suction-to-pressure direction increased. The pump exit plane slip factors improved as the pump exit blade angle decreased. A counter-clockwise circulatory secondary flow pat tern at the pump mid-plane was observed for all geometries and, conversely, clockwise circulatory secondary flow patterns at the pump exit plane were recorded. Resulting vorticities were found to depend on geometries and speed ratios.
机译:检查了具有两个不同涡轮机的三个汽车Plexiglas变矩器泵的内部流场。激光测速仪用于测量六种不同几何形状组合中泵中和出口平面处的速度流场。所有组合的定子都相同。泵的几何形状仅因出口叶片角而异,而涡轮的几何形状仅因入口叶片角而异。变矩器以三种不同的涡轮/泵转速比运行:0.065(接近失速),0.600和0.800(接近耦合点)。对于中平面上的所有几何形状,在低速比时,吸力表面附近的速度略高,但对于最高速比,在吸力表面附近会看到强烈的逆流;在高速比下,壳附近的速度很高。在出口平面,在所有速比下,流量在叶片到叶片方向上都是不均匀的。在所有速比下,速度在芯壳方向上都相当均匀。此外,随着速度比的增加,贯穿流速的不均匀性变得更加明显。涡轮进口叶片角度的变化最小程度地改变了泵的中平面和出口平面速度。泵出口叶片角度的变化对泵中平面速度场没有影响,但是确实影响出口平面流场。特别地,随着流速的不均匀性,芯壳方向随着泵出口叶片角的减小而减小,而沿吸气压力方向的流速不均匀性增大。随着泵出口叶片角度减小,泵出口平面滑移系数提高。对于所有几何形状,均观察到泵中平面处的逆时针循环二次流模式,反之,则记录了泵出口平面处的顺时针循环二次流模式。发现产生的涡度取决于几何形状和速比。

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