Buoyancy Effect of Bristles for a Brush Seal with Disturbance-Suppressing HolesSource: Journal of Aerospace Engineering:;2024:;Volume ( 037 ):;issue: 006::page 04024073-1DOI: 10.1061/JAEEEZ.ASENG-5372Publisher: American Society of Civil Engineers
Abstract: Bristles in the first few rows float up from the rotor surface due to the radial airflow in the gap between the front plate and bristle pack, which directly affects seal performance and the service life of a brush seal. In this paper, firstly, two three-dimensional transient calculation models for a traditional brush seal (TBS) and a brush seal with disturbance-suppressing holes (DSBS) are established, respectively, based on the arbitrary Lagrange–Eulerian (ALE) method to study bristle deformation characteristics and leakage flow characteristics of the seals. Furthermore, effects of disturbance-suppressing (DS) hole structural parameters (i.e., height, diameter, and number of hole rows) were investigated to reveal the suppression mechanism of the DS holes on the buoyancy effect of bristles. The results showed that as soon as free ends of bristles at the first few rows moved along direction of the front plate in response to the radial airflow from the gap between front plate and bristle pack, a buoyancy effect of bristles occurred. The DSBS with DS holes set in the front plate of the TBS had a lower deformation of the bristles and a lower leakage amount of seal compared with that of TBS, indicating a good suppression to the buoyancy effect. With decreasing hole height and increasing hole diameter and number of hole rows, the suppression of bristle disturbance gradually increased due to decreases of the radial airflow and increases of torque acting on the bristles.
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contributor author | Dan Sun | |
contributor author | JiSheng Sun | |
contributor author | Huan Zhao | |
contributor author | Ze-Min Yang | |
contributor author | Haoyu Yin | |
contributor author | Wen-feng Xu | |
date accessioned | 2024-12-24T10:14:27Z | |
date available | 2024-12-24T10:14:27Z | |
date copyright | 11/1/2024 12:00:00 AM | |
date issued | 2024 | |
identifier other | JAEEEZ.ASENG-5372.pdf | |
identifier uri | http://yetl.yabesh.ir/yetl1/handle/yetl/4298553 | |
description abstract | Bristles in the first few rows float up from the rotor surface due to the radial airflow in the gap between the front plate and bristle pack, which directly affects seal performance and the service life of a brush seal. In this paper, firstly, two three-dimensional transient calculation models for a traditional brush seal (TBS) and a brush seal with disturbance-suppressing holes (DSBS) are established, respectively, based on the arbitrary Lagrange–Eulerian (ALE) method to study bristle deformation characteristics and leakage flow characteristics of the seals. Furthermore, effects of disturbance-suppressing (DS) hole structural parameters (i.e., height, diameter, and number of hole rows) were investigated to reveal the suppression mechanism of the DS holes on the buoyancy effect of bristles. The results showed that as soon as free ends of bristles at the first few rows moved along direction of the front plate in response to the radial airflow from the gap between front plate and bristle pack, a buoyancy effect of bristles occurred. The DSBS with DS holes set in the front plate of the TBS had a lower deformation of the bristles and a lower leakage amount of seal compared with that of TBS, indicating a good suppression to the buoyancy effect. With decreasing hole height and increasing hole diameter and number of hole rows, the suppression of bristle disturbance gradually increased due to decreases of the radial airflow and increases of torque acting on the bristles. | |
publisher | American Society of Civil Engineers | |
title | Buoyancy Effect of Bristles for a Brush Seal with Disturbance-Suppressing Holes | |
type | Journal Article | |
journal volume | 37 | |
journal issue | 6 | |
journal title | Journal of Aerospace Engineering | |
identifier doi | 10.1061/JAEEEZ.ASENG-5372 | |
journal fristpage | 04024073-1 | |
journal lastpage | 04024073-15 | |
page | 15 | |
tree | Journal of Aerospace Engineering:;2024:;Volume ( 037 ):;issue: 006 | |
contenttype | Fulltext |