Numerical and experimental investigation of influencing factors on blow-down effect in brush seal
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Le résumé fourni par la source
Brush seal experiences blow-down effect during operation, which accelerates bristle wear and directly shortens their operational lifespan. A theoretical model for blow-down effect in brush seal was established, along with a three dimensional transient numerical model based on Arbitrary Lagrange-Euler (ALE) method for fluid-structure interaction. A visible experimental device for bristle deformation was designed, and radial deformation was experimentally recorded. After verifying the numerical model's accuracy, axial, radial, and cross-sectional deformation characteristics of bristles were investigated, respectively. Radial blow-down displacement was quantitatively analyzed, and effects of different factors on this displacement were compared. Mechanisms inducing blow-down effect were specifically examined. Results showed that inherent circumferential inclination angle of bristles and radial pressure gradient within bristle pack region formed inducing conditions for blow-down effect. Moreover, normal compressive force and tangential friction between bristles caused deformation, which subsequently influenced blow-down effect. While blow-down effect reduced leakage, it increased frictional wear between bristle tips and rotor surface. Increasing circumferential tilt angle of bristles was found to mitigate blow-down effect. Additionally, blow-down effect manifested as non-steady deformation accompanied by bristle disturbance. Radial blow-down displacement increased with rising pressure ratio (up to 18.5%) but decreased with larger circumferential tilt angles (reduction up to 27%).
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Le contrôle bibliographique ouvert
DOI retrouvé dans Crossref DOI retrouvé ; titre concordant.
- Titre Crossref
- Numerical and experimental investigation of influencing factors on blow-down effect in brush seal
- Date Crossref
- 06/09/2025
- Éditeur
- GPPS
- Type
- proceedings-article
Ce recoupement confirme des métadonnées liées au DOI. Il ne confirme ni la méthode ni les conclusions de l’étude, et il ne compte pas comme une seconde source scientifique indépendante.
Où se fait cette recherche
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Liaoning University pays non établi dans la noticeUniversité ou école supérieure
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Shenyang Aerospace University Liaoning Key Lab of Advanced Test Technology for Aerospace Propulsion System pays non établi dans la noticeUniversité ou école supérieure
Liaoning University et Liaoning Key Lab of Advanced Test Technology for Aerospace Propulsion System — Shenyang Aerospace University.
Une affiliation ne permet pas de déduire la nationalité d’un auteur.