*Labyrinth seal is one of the most popular non-contact annular seals that used in centrifugal compressors to improve machine efficiency by reducing the secondary flow leakage. Reducing the radial clearance* *C~r~ can effectively decrease the seal’s leakage and therefore increase the machine efficiency. However, reducing* *C~r~ can also introduce undesired effects on the machine’s vibration behaviors. This paper experimentally studies the impact of reducing* *C~r~ on the leakage and rotordynamic coefficients of a 16-tooth see-through labyrinth seal under wet-gas conditions. The test seal’s inner diameter is 89.256 mm. Two rotors with different diameters are used to obtain two radial clearances (0.102 mm and 0.178 mm). Tests are carried out at a supply pressure of 62 bars, three speeds from 10krpm to 20 krpm, three pressure ratios from 0.21 to 0.46, and six inlet liquid volume fractions (LVFs) from zero to 15%. The test fluid is a mixture comprised of air and silicon oil. Test results show that, for all pure-air and mainly-air conditions, decreasing* *C~r~ decreases (as expected) the test seal’s leakage mass flow rate. For all test cases,* *direct dynamic stiffness K~Ω~ is negative, producing a negative centering force on the associated rotor.* *For inlet LVF≤8%, the effects of decreasing C~r~ on K~Ω~* *are negligible. When inlet LVF=12% and 15%, decreasing C~r~ increases K~Ω~ (decreases the magnitude). In other words, when inlet LVF=12% and 15%, decreasing C~r~ reduces the test seal’s negative centering force on the rotor, and would increase the critical speeds of the rotor.* *The value of the effective damping C~eff~ near 0.5ω represents the seal’s capability to suppress the rotor’s potential whirling motion at about 0.5ω. For all pure-air and mainly-air conditions, decreasing C~r~ generally increases the* *C~eff~ value near 0.5ω; i.e., decreasing C~r~ improves the test seal’s stabilizing capability against the rotor’s potential whirling motion at about 0.5ω.*


Effects of Clearance on the Performance of a Labyrinth Seal Under Wet-Gas Conditions

Division / Sponsor:
International Gas Turbine Institute (IGTI)

Paper Proceedings: https://asmedigitalcollection.asme.org/GT/GT2020/volume/84058

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