A Mixed-Elastohydrodynamic Lubrication Model of a Capped-T-Ring Seal with a Sectioned Multi-Material Film Thickness in Landing Gear Shock Absorber Applications

Numerical investigations of capped T-ring (CTR) seals performance in reciprocating motion for landing gear shock absorber applications are presented. A lubrication model using the Elastohydrodynamic lubrication theory and deformation mechanics is developed in a multi-material contact zone, and a pro...

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Main Authors: Aaron Feria Alanis, Ahmed A. Sheikh Al-Shabab, Antonis F. Antoniadis, Panagiotis Tsoutsanis, Martin Skote
Format: Article
Language:English
Published: MDPI AG 2024-11-01
Series:Fluids
Subjects:
Online Access:https://www.mdpi.com/2311-5521/9/12/271
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author Aaron Feria Alanis
Ahmed A. Sheikh Al-Shabab
Antonis F. Antoniadis
Panagiotis Tsoutsanis
Martin Skote
author_facet Aaron Feria Alanis
Ahmed A. Sheikh Al-Shabab
Antonis F. Antoniadis
Panagiotis Tsoutsanis
Martin Skote
author_sort Aaron Feria Alanis
collection DOAJ
description Numerical investigations of capped T-ring (CTR) seals performance in reciprocating motion for landing gear shock absorber applications are presented. A lubrication model using the Elastohydrodynamic lubrication theory and deformation mechanics is developed in a multi-material contact zone, and a procedure for coupling fluid and deformation mechanics is introduced. By conducting Finite Element Method (FEM) simulations, the static contact pressure is obtained, which subsequently is used within the model developed herein consisting of a modified Reynolds equation and an asperity contact model, to calculate the fluid film pressure, and the deformation of the fluid channel is determined using an elastic deformation model applied to a multi-component multi-mechanical property channel. These computational results are used for estimations of the seal leakage and friction under various conditions. In addition, the influence of asperity orientation is compared with other parameters, such as sealing pressure and piston velocity. A correlation between asperity orientation and leakage was found, and a general trend of reduced leakage with longitudinally oriented asperities was established.
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institution DOAJ
issn 2311-5521
language English
publishDate 2024-11-01
publisher MDPI AG
record_format Article
series Fluids
spelling doaj-art-3ad8dddefd92470d93bb248edaa1bcd52025-08-20T02:56:06ZengMDPI AGFluids2311-55212024-11-0191227110.3390/fluids9120271A Mixed-Elastohydrodynamic Lubrication Model of a Capped-T-Ring Seal with a Sectioned Multi-Material Film Thickness in Landing Gear Shock Absorber ApplicationsAaron Feria Alanis0Ahmed A. Sheikh Al-Shabab1Antonis F. Antoniadis2Panagiotis Tsoutsanis3Martin Skote4Faculty of Engineering and Applied Sciences, Cranfield University, Cranfield MK43 0AL, UKFaculty of Engineering and Applied Sciences, Cranfield University, Cranfield MK43 0AL, UKFaculty of Engineering and Applied Sciences, Cranfield University, Cranfield MK43 0AL, UKFaculty of Engineering and Applied Sciences, Cranfield University, Cranfield MK43 0AL, UKFaculty of Engineering and Applied Sciences, Cranfield University, Cranfield MK43 0AL, UKNumerical investigations of capped T-ring (CTR) seals performance in reciprocating motion for landing gear shock absorber applications are presented. A lubrication model using the Elastohydrodynamic lubrication theory and deformation mechanics is developed in a multi-material contact zone, and a procedure for coupling fluid and deformation mechanics is introduced. By conducting Finite Element Method (FEM) simulations, the static contact pressure is obtained, which subsequently is used within the model developed herein consisting of a modified Reynolds equation and an asperity contact model, to calculate the fluid film pressure, and the deformation of the fluid channel is determined using an elastic deformation model applied to a multi-component multi-mechanical property channel. These computational results are used for estimations of the seal leakage and friction under various conditions. In addition, the influence of asperity orientation is compared with other parameters, such as sealing pressure and piston velocity. A correlation between asperity orientation and leakage was found, and a general trend of reduced leakage with longitudinally oriented asperities was established.https://www.mdpi.com/2311-5521/9/12/271mixed-elastohydrodynamic lubricationcapped T-ring sealreciprocating seallanding gears
spellingShingle Aaron Feria Alanis
Ahmed A. Sheikh Al-Shabab
Antonis F. Antoniadis
Panagiotis Tsoutsanis
Martin Skote
A Mixed-Elastohydrodynamic Lubrication Model of a Capped-T-Ring Seal with a Sectioned Multi-Material Film Thickness in Landing Gear Shock Absorber Applications
Fluids
mixed-elastohydrodynamic lubrication
capped T-ring seal
reciprocating seal
landing gears
title A Mixed-Elastohydrodynamic Lubrication Model of a Capped-T-Ring Seal with a Sectioned Multi-Material Film Thickness in Landing Gear Shock Absorber Applications
title_full A Mixed-Elastohydrodynamic Lubrication Model of a Capped-T-Ring Seal with a Sectioned Multi-Material Film Thickness in Landing Gear Shock Absorber Applications
title_fullStr A Mixed-Elastohydrodynamic Lubrication Model of a Capped-T-Ring Seal with a Sectioned Multi-Material Film Thickness in Landing Gear Shock Absorber Applications
title_full_unstemmed A Mixed-Elastohydrodynamic Lubrication Model of a Capped-T-Ring Seal with a Sectioned Multi-Material Film Thickness in Landing Gear Shock Absorber Applications
title_short A Mixed-Elastohydrodynamic Lubrication Model of a Capped-T-Ring Seal with a Sectioned Multi-Material Film Thickness in Landing Gear Shock Absorber Applications
title_sort mixed elastohydrodynamic lubrication model of a capped t ring seal with a sectioned multi material film thickness in landing gear shock absorber applications
topic mixed-elastohydrodynamic lubrication
capped T-ring seal
reciprocating seal
landing gears
url https://www.mdpi.com/2311-5521/9/12/271
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