Numerical analysis of brush seal hysteresis based on orthogonal test method

Abstract By the finite element analysis software ABAQUS, utilizing General Contact and Contact damping algorithm, the brush seal hysteresis numerical model with pressure differential considered was established. The hysteresis was quantified by the hysteresis energy, and the hysteresis energy and maximum stress are obtained by numerical calculations. An orthogonal test was conducted to study the effects of bristle diameter, bristle cant angle, fence height, bristle length, upstream and downstream differential pressure, and rotor radial displacement on the hysteresis and maximum stress of the brush seal. Results show that the primary and secondary orders of parameters affecting hysteresis are: rotor radial displacement, bristle diameter, upstream and down-stream differential pressure, bristle cant angle, bristle length, and fence height. The primary and secondary orders of parameters affecting maximum stress are: upstream and downstream differential pressure, fence height, bristle cant angle, bristle diameter, bristle length, and rotor radial displacement. Finally, based on the numerical results, a fitted correlation was developed. Comprehensive effects of the six parameters on both performances were analyzed, and structural design optimization methods focusing on single performance and comprehensive performance were proposed, providing references for the design of brush seals in practical engineering applications.

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Publication Details

Journal
International Journal of Turbo and Jet Engines
Published
2024-11-21
DOI
https://doi.org/10.1515/tjj-2024-0078
Primary Topic
Tribology and Lubrication Engineering
Type
article
Field-Weighted Citation Impact
0.00

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article

Numerical analysis of brush seal hysteresis based on orthogonal test method

Yuchi Kang, Sharon Kao‐Walter, Yuanlun Wang, Furen Xiao
International Journal of Turbo and Jet Engines
Tribology and Lubrication Engineering
article

Numerical analysis of brush seal hysteresis based on orthogonal test method

Yuchi Kang, Sharon Kao‐Walter, Yuanlun Wang, Furen Xiao
article en

Abstract

Abstract By the finite element analysis software ABAQUS, utilizing General Contact and Contact damping algorithm, the brush seal hysteresis numerical model with pressure differential considered was established. The hysteresis was quantified by the hysteresis energy, and the hysteresis energy and maximum stress are obtained by numerical calculations. An orthogonal test was conducted to study the effects of bristle diameter, bristle cant angle, fence height, bristle length, upstream and downstream differential pressure, and rotor radial displacement on the hysteresis and maximum stress of the brush seal. Results show that the primary and secondary orders of parameters affecting hysteresis are: rotor radial displacement, bristle diameter, upstream and down-stream differential pressure, bristle cant angle, bristle length, and fence height. The primary and secondary orders of parameters affecting maximum stress are: upstream and downstream differential pressure, fence height, bristle cant angle, bristle diameter, bristle length, and rotor radial displacement. Finally, based on the numerical results, a fitted correlation was developed. Comprehensive effects of the six parameters on both performances were analyzed, and structural design optimization methods focusing on single performance and comprehensive performance were proposed, providing references for the design of brush seals in practical engineering applications.

International Journal of Turbo and Jet EnginesVol. 42(2)
Kunming University of Science and Technology (CN), Yunnan Machinery Research and Design Institute (CN), Blekinge Institute of Technology (SE)
Kunming University of Science and Technology
Affordable and clean energy
Openalex Percentile: Top 79%
Tribology and Lubrication Engineering
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Numerical analysis of brush seal hysteresis based on orthogonal test method — Yuchi Kang, Sharon Kao‐Walter, et al. · International Journal of Turbo and Jet Engines (2024) | TGRS Research Map | TGRS