NASA NTRS · 19970024778
Upstream Swirl Effects on the Flow Inside a Labyrinth Seal
Abstract
The flow field inside a seven cavity tooth on rotor labyrinth seal was measured using a 3D laser Doppler anemometer system. The seal was operated at a Reynolds number of 24,000 and a Taylor number of 6,600 using water as the working fluid. Swirl vanes were placed upstream of the seal to produce positive, negative, and no preswirl. It was found that the axial and radial velocities were minimally effected. The tangential velocity, both in the clearance region and the seal cavities on the rotor, were greatly altered by the preswirl. By applying negative preswirl, the tangential velocity was suppressed, even in the seventh cavity. The turbulence levels decreased as the preswirl varied from negative to positive.
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Morrison, Gerald L., Johnson, Mark C.. 1997-05-01. Upstream Swirl Effects on the Flow Inside a Labyrinth Seal. https://ntrs.nasa.gov/citations/19970024778
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