Difference between revisions of "Test Data AC6-15"

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=Vortex ropes in draft tube of a laboratory Kaplan hydro turbine at low load=
 
=Vortex ropes in draft tube of a laboratory Kaplan hydro turbine at low load=
 
==Application Area 6: Turbomachinery Internal Flow==
 
==Application Area 6: Turbomachinery Internal Flow==

Revision as of 11:29, 27 November 2018

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Vortex ropes in draft tube of a laboratory Kaplan hydro turbine at low load

Application Area 6: Turbomachinery Internal Flow

Application Challenge AC6-15

Test Data

Description of Experiment

The experiments were performed in an open aerodynamic test rig (Fig. 1a). Air supply into the draft tube model was provided by a vortex air blower MT 08-M1S-7.5 with a maximum flow rate Qmax=550 m3/h and pressure excess of ?P=0.4 bar. The air flowrate was controlled by an ultrasonic flowmeter "IRVIS-Ultra" and frequency converter of the blower with feedback. For capturing the LDA signal the air flow was seeded with tracers produced by a standard-type generator of the paraffin oil aerosol with a mean particle diameter of 1-3 ?m.

Figure 1 provides a photo and a sketch of the experimental turbine model. The airflow with tracers was supplied to an axisymmetric chamber through six radial inlet channels. To suppress the influence of turning the radial inflow into axial flow and to align the airflow entering the guide vanes, two honeycombs and a profiled nozzle were applied. Air flows through the cascade of blades and enters the draft tube cone. The draft-tube model and a pair of blade rows "guide vanes - runner" were manufactured using a 3D printing technology. Servo drive SPSh10-3410 ensured precise setting of the rotation frequency of the runner in the range from 0 to 3000 min-1. The control of the experiment was ensured by a computer. Using the original software it was possible to maintain the present flow regime with an accuracy of 1.5% and 0.5% for the flowrate and the runner rotation frequency respectively.

The experiments included the measurements of the velocity fields in the conical part of the draft tube using a two-component LDA system LAD-06i, whereas pressure pulsations were recorded by acoustic sensors mounted on the cone walls (Fig. 2). The pressure fluctuations were recorded using a Bruel&Kjaer analyzer and a sound-level meter Type 2250 complemented by a microphone Type 4189 with high output characteristics, a frequency range of 6.3 Hz - 20 kHz, a dynamic range 14.6 - 146 dB and a sensitivity of 50 mV/Pa. The microphone head was set half-way along the draft tube cone mounted flush with the wall (45 mm below the swirler), Fig. 2.



Contributed by: A. Minakov [1,2], D. Platonov [1,2], I. Litvinov [2], S. Shtork [2], K. Hanjalić [3] — 

[1] Institute of Thermophysics SB RAS, Novosibirsk, Russia,

[2] Siberian Federal University, Krasnoyarsk, Russia,

[3] Delft University of Technology, Chem. Eng. Dept., Holland.

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