Conceptual Flutter Analysis of Labyrinth Seals Using Analytical Models—Part II: Physical InterpretationSource: Journal of Turbomachinery:;2018:;volume 140:;issue 012::page 121007DOI: 10.1115/1.4041377Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: The dimensionless model presented in part I of the corresponding paper to describe the flutter onset of two-fin rotating seals is exploited to extract valuable engineering trends with the design parameters. The analytical expression for the nondimensional work-per-cycle depends on three dimensionless parameters of which two of them are new. These parameters are simple but interrelate the effect of the pressure ratio, the height, and length of the interfin geometry, the seal clearance, the nodal diameter (ND), the fluid swirl velocity, the vibration frequency, and the torsion center location in a compact and intricate manner. It is shown that nonrelated physical parameters can actually have an equivalent impact on seal stability. It is concluded that the pressure ratio can be stabilizing or destabilizing depending on the case, whereas the swirl of the flow is always destabilizing. Finally, a simple method to extend the model to multiple interfin cavities, neglecting the unsteady interaction among them, is described.
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contributor author | Vega, Almudena | |
contributor author | Corral, Roque | |
date accessioned | 2019-02-28T11:09:58Z | |
date available | 2019-02-28T11:09:58Z | |
date copyright | 10/18/2018 12:00:00 AM | |
date issued | 2018 | |
identifier issn | 0889-504X | |
identifier other | turbo_140_12_121007.pdf | |
identifier uri | http://yetl.yabesh.ir/yetl1/handle/yetl/4253373 | |
description abstract | The dimensionless model presented in part I of the corresponding paper to describe the flutter onset of two-fin rotating seals is exploited to extract valuable engineering trends with the design parameters. The analytical expression for the nondimensional work-per-cycle depends on three dimensionless parameters of which two of them are new. These parameters are simple but interrelate the effect of the pressure ratio, the height, and length of the interfin geometry, the seal clearance, the nodal diameter (ND), the fluid swirl velocity, the vibration frequency, and the torsion center location in a compact and intricate manner. It is shown that nonrelated physical parameters can actually have an equivalent impact on seal stability. It is concluded that the pressure ratio can be stabilizing or destabilizing depending on the case, whereas the swirl of the flow is always destabilizing. Finally, a simple method to extend the model to multiple interfin cavities, neglecting the unsteady interaction among them, is described. | |
publisher | The American Society of Mechanical Engineers (ASME) | |
title | Conceptual Flutter Analysis of Labyrinth Seals Using Analytical Models—Part II: Physical Interpretation | |
type | Journal Paper | |
journal volume | 140 | |
journal issue | 12 | |
journal title | Journal of Turbomachinery | |
identifier doi | 10.1115/1.4041377 | |
journal fristpage | 121007 | |
journal lastpage | 121007-8 | |
tree | Journal of Turbomachinery:;2018:;volume 140:;issue 012 | |
contenttype | Fulltext |