Detail publikace
Labyrinth seal design for space applications
POUZAR, J. KOŠŤÁL, D. WESTERBERG, L. NYBERG, E. KŘUPKA, I.
Anglický název
Labyrinth seal design for space applications
Typ
článek v časopise ve Web of Science, Jimp
Jazyk
en
Originální abstrakt
Labyrinth seals, extensively used in space applications, serve to prevent the loss of liquid lubricants and shield satellite subsystems from contamination. These seals are essential for the reliable functioning of bearings and for protecting satellite subsystems from contamination. This study compares analytical predictions of lubricant loss against experimental measurements and computer simulations to optimize labyrinth seal configurations. Analytical models tend to overestimate mass loss by 5-8 times compared to experimental data, indicating limited reliability for complex seal geometries. Simulations using MolFlow+ and COMSOL Multiphysics align closely with experimental results, providing accurate mass loss predictions. Key findings highlight that labyrinth length, width, and surface roughness are critical factors in minimizing evaporative mass loss. Notably, stepped labyrinth seals with relief grooves and optimized step positioning effectively reduce molecular beaming effects and improve sealing performance compared to straight geometries. Effective sealing not only reduces mission failures but also helps to minimize space debris, thereby promoting safer satellite missions.
Anglický abstrakt
Labyrinth seals, extensively used in space applications, serve to prevent the loss of liquid lubricants and shield satellite subsystems from contamination. These seals are essential for the reliable functioning of bearings and for protecting satellite subsystems from contamination. This study compares analytical predictions of lubricant loss against experimental measurements and computer simulations to optimize labyrinth seal configurations. Analytical models tend to overestimate mass loss by 5-8 times compared to experimental data, indicating limited reliability for complex seal geometries. Simulations using MolFlow+ and COMSOL Multiphysics align closely with experimental results, providing accurate mass loss predictions. Key findings highlight that labyrinth length, width, and surface roughness are critical factors in minimizing evaporative mass loss. Notably, stepped labyrinth seals with relief grooves and optimized step positioning effectively reduce molecular beaming effects and improve sealing performance compared to straight geometries. Effective sealing not only reduces mission failures but also helps to minimize space debris, thereby promoting safer satellite missions.
Klíčová slova anglicky
Vacuum evaporation; Molecular flow; Labyrinth seals; Contamination; Liquid lubricants; Space tribology
Vydáno
14.02.2025
Nakladatel
Elsevier
Místo
OXFORD
ISSN
0042-207X
Ročník
232
Číslo
2
Strany od–do
1–10
Počet stran
10
BIBTEX
@article{BUT197164,
author="Josef {Pouzar} and David {Košťál} and Lars-Göran {Westerberg} and Erik {Nyberg} and Ivan {Křupka},
title="Labyrinth seal design for space applications",
year="2025",
volume="232",
number="2",
month="February",
pages="1--10",
publisher="Elsevier",
address="OXFORD",
issn="0042-207X"
}