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contributor authorYan, Xin
contributor authorDai, Xinbo
date accessioned2022-02-06T05:32:15Z
date available2022-02-06T05:32:15Z
date copyright10/4/2021 12:00:00 AM
date issued2021
identifier issn0742-4795
identifier othergtp_143_12_121001.pdf
identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4278237
description abstractThe wear behaviors of the rectangular labyrinth seal fin against high-speed rotor were experimentally investigated on the incursion test rig. The material losses, worn geometries, frictional temperature distributions, and contact forces of labyrinth fin in rubbing events were measured at three incursion rates, three final incursion depths and two rotor sliding velocities. The morphologies of the worn labyrinth fin tips were magnified to reveal the wear mechanisms in rubbing events. The transient temperatures and contact forces were detailed to analyze the thermal–mechanical interactions between two contacting parts. The results show that the material loss percentage in the labyrinth fin is higher at the early stage of rubbing process, accounting for 18% mass loss of the worn region, than at final stage. The material loss is decreased with increasing the incursion rate. The incursion rate and final incursion depth have pronounced effects on the mushroom region extensions and curlings. The friction coefficient is fluctuated significantly in the high sliding velocity and low incursion rate conditions, and the averaged value of friction coefficient is about 0.1–0.125 among all experiments. The temperature at labyrinth fin tip is increased with increasing the final incursion depth, incursion rate, and sliding velocity. However, the temperature at fin tip is not increased further as it reaches about 1200 °C. The heat convection from hot fin to ambient plays an important role in worn geometries and transient temperature distributions at fin tip.
publisherThe American Society of Mechanical Engineers (ASME)
titleExperimental Investigation on Wear Behavior of Rectangular Labyrinth Fin Against High-Speed Rotor
typeJournal Paper
journal volume143
journal issue12
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.4051991
journal fristpage0121001-1
journal lastpage0121001-16
page16
treeJournal of Engineering for Gas Turbines and Power:;2021:;volume( 143 ):;issue: 012
contenttypeFulltext


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