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contributor authorGervas Franceschini
contributor authorTerry V. Jones
contributor authorDavid R. H. Gillespie
date accessioned2017-05-09T00:41:20Z
date available2017-05-09T00:41:20Z
date copyrightOctober, 2010
date issued2010
identifier issn0889-504X
identifier otherJOTUEI-28766#041004_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/144963
description abstractBrush seals are used to provide flow resistance between rotating and stationary components in gas turbines. Compliant filament seals, such as brush seals, exhibit a phenomenon called blow-down, where the filaments deflect toward the rotor surface when a differential pressure is applied across the seal. This phenomenon is desirable as it enables seal contact to be maintained during rotor contractions and eccentric excursions. This paper describes an aerodynamic mechanism, which can cause the blow-down of bristles. Importantly it shows that distortion of the bristle pack is not necessary to achieve blow-down. Experimental and computational investigations of a large scale model representative of a section of a brush seal are also reported. The measured and predicted detailed pressure distributions thus obtained are used to validate the model of blow-down presented.
publisherThe American Society of Mechanical Engineers (ASME)
titleImproved Understanding of Blow-Down in Filament Seals
typeJournal Paper
journal volume132
journal issue4
journal titleJournal of Turbomachinery
identifier doi10.1115/1.3213552
journal fristpage41004
identifier eissn1528-8900
keywordsForce
keywordsPressure
keywordsFlow (Dynamics)
keywordsComputer simulation
keywordsMomentum
keywordsMechanisms
keywordsStrips
keywordsRotors
keywordsClearances (Engineering) AND Wind tunnels
treeJournal of Turbomachinery:;2010:;volume( 132 ):;issue: 004
contenttypeFulltext


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