Zero-Gravity Test Results For Ultrasonic Sensing of Air-Liquid Interface in a Vortex Separator

Computer Science – Sound

Scientific paper

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Ultrasonics, Quantum Acoustics, And Physical Effects Of Sound

Scientific paper

An ultrasonic pulse-echo method for detecting the location of the air-liquid interface of a air-liquid vortex in microgravity was tested. A vortex was established in near-zero gravity conditions in hydraulically-stirred phase separator. A single ultrasonic transducer located about mid-plane of the vortex was used to sense the thickness of the layer of liquid inside the phase separator and local to the ultrasonic transducer. Comparison was made between the sensed liquid layer thickness and an ideal right circular liquid annulus calculated from the know liquid inventory in the phase separator. The absolute error between the sensed and ideal annulus thicknesses was found to be in the neighborhood of 0.1 inches for the full operational range of the separator.

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