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contributor authorMehta, Naitik J.
contributor authorChilds, Dara W.
date accessioned2017-05-09T01:07:18Z
date available2017-05-09T01:07:18Z
date issued2014
identifier issn1528-8919
identifier othergtp_136_01_012501.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/154619
description abstractMeasured results are presented to compare rotordynamic coefficients and leakage of a slantedtooth labyrinth seal and a straighttooth labyrinth seal. Both seals had identical pitch, depth, and number of teeth. The teeth inclination angle of the teeth on the slantedtooth labyrinth was 65 deg from the normal axis. Experiments were carried out at an inlet pressure of 70 bara (1015 psia), pressure ratios of 0.4, 0.5, and 0.6, rotor speeds of 10.2, 15.35, and 20.2 krpm, and a radial clearance of 0.2 mm (8 mils). One zero and two positive inlet preswirl ratios were used. The results show only minute difference in the rotordynamic coefficients between the two seals. The slantedtooth labyrinth seal consistently leaked approximately 10% less at all conditions. Predictions were made using a one control volume bulkflow model (1CVM) which was developed for a straighttooth labyrinth seal design. 1CVM underpredicted the rotordynamic coefficients and the leakage.
publisherThe American Society of Mechanical Engineers (ASME)
titleMeasured Comparison of Leakage and Rotordynamic Characteristics for a Slanted Tooth and a Straight Tooth Labyrinth Seal
typeJournal Paper
journal volume136
journal issue1
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.4025267
journal fristpage12501
journal lastpage12501
identifier eissn0742-4795
treeJournal of Engineering for Gas Turbines and Power:;2014:;volume( 136 ):;issue: 001
contenttypeFulltext


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