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Title: Laser velocimeter measurements in the pump of an automotive torque converter. Part 2: Unsteady measurements

Journal Article · · Journal of Turbomachinery
DOI:https://doi.org/10.1115/1.2836704· OSTI ID:287468
; ;  [1]
  1. Univ. of Virginia, Charlottesville, VA (United States)

The unsteady velocity field found in the pump of an automotive torque converter was measured using laser velocimetry. Velocities in the inlet, mid-, and exit planes of the pump were investigated at two significantly different operating conditions: turbine/pump rotational speed ratios of 0.065 and 0.800. A data organization method was developed to visualize the three-dimensional, periodic unsteady velocity field in the rotating frame. For this method, the acquired data are assumed to be periodic at synchronous and blade interaction frequencies. Two shaft encoders were employed to obtain the instantaneous angular position of the torque converter pump and turbine at the instant of laser velocimeter data acquisition. By proper registration of the data, visualizing the transient interaction effects between the stator and the pump, and between the pump and the turbine, was possible. Results showed strong cyclic velocity fluctuations in the pump inlet plane as a function of the relative stator-pump position. Typical percent periodic fluctuations in the through flow velocity were 70% of the average through flow velocity. The upstream propagation influence of the turbine on the pump exit plane flow field was seen to be smaller. Percent periodic fluctuations of the through flow velocity were typically 30%. The effect of the stator and turbine on the midplane flow field was seen to be negligible. The incidence angle at the pump inlet fluctuated by 27 and 14 deg. for the 0.065 and 0.800 speed ratios, respectively. Typical slip factors at the exit were 0.965 and fluctuated by less than 1%.

Sponsoring Organization:
USDOE
OSTI ID:
287468
Report Number(s):
CONF-940626-; ISSN 0889-504X; TRN: IM9639%%56
Journal Information:
Journal of Turbomachinery, Vol. 118, Issue 3; Conference: 39. international gas turbine and aeroengine congress and exposition, The Hague (Netherlands), 13-16 Jun 1994; Other Information: PBD: Jul 1996
Country of Publication:
United States
Language:
English

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