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contributor authorSaim Dinc
contributor authorGayle Goetze
contributor authorChristopher Wolfe
contributor authorMark Florin
contributor authorJohn Maupin
contributor authorMehmet Demiroglu
contributor authorNorman Turnquist
contributor authorJames Hopkins
contributor authorJason Mortzheim
date accessioned2017-05-09T00:09:02Z
date available2017-05-09T00:09:02Z
date copyrightApril, 2002
date issued2002
identifier issn0889-504X
identifier otherJOTUEI-28695#293_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/127649
description abstractAdvanced seals have been applied to numerous turbine machines over the last decade to improve the performance and output. Industrial experiences have shown that significant benefits can be attained if the seals are designed and applied properly. On the other hand, penalties can be expected if brush seals are not designed correctly. In recent years, attempts have been made to apply brush seals to more challenging locations with high speed (>400 m/s), high temperature (>650 °C), and discontinuous contact surfaces, such as blade tips in a turbine. Various failure modes of a brush seal can be activated under these conditions. It becomes crucial to understand the physical behavior of a brush seal under the operating conditions, and to be capable of quantifying seal life and performance as functions of both operating parameters and seal design parameters. Design criteria are required for different failure modes such as stress, fatigue, creep, wear, oxidation etc. This paper illustrates some of the most important brush seal design criteria and the trade-off of different design approaches.
publisherThe American Society of Mechanical Engineers (ASME)
titleFundamental Design Issues of Brush Seals for Industrial Applications
typeJournal Paper
journal volume124
journal issue2
journal titleJournal of Turbomachinery
identifier doi10.1115/1.1451847
journal fristpage293
journal lastpage300
identifier eissn1528-8900
keywordsDesign
keywordsFlow (Dynamics)
keywordsTurbines
keywordsRotors AND Engines
treeJournal of Turbomachinery:;2002:;volume( 124 ):;issue: 002
contenttypeFulltext


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