An Experimental Study of Contact Temperatures at Sealing Interface against Varying Shaft Surfaces

Increased temperatures at the sealing interface between the seal and shaft can reduce the working life of a seal through elastomer aging, swelling and increased friction. Degradation of the seal due to increased temperatures can cause pre-mature failure, wear and leakage. There is no such thing as a...

Full description

Bibliographic Details
Main Authors: Sarah Shabbir, Seamus D. Garvey, Sam M. Dakka, Benjamin C. Rothwell
Format: Article
Language:English
Published: MDPI AG 2021-01-01
Series:Coatings
Subjects:
Online Access:https://www.mdpi.com/2079-6412/11/2/156
id doaj-f415a22be7f140e8a579a465da40e490
record_format Article
spelling doaj-f415a22be7f140e8a579a465da40e4902021-01-30T00:04:41ZengMDPI AGCoatings2079-64122021-01-011115615610.3390/coatings11020156An Experimental Study of Contact Temperatures at Sealing Interface against Varying Shaft SurfacesSarah Shabbir0Seamus D. Garvey1Sam M. Dakka2Benjamin C. Rothwell3Institute of Aerospace Technology, University of Nottingham, Nottingham NG7 2TU, UKGas Turbine and Transmission Research Centre, Faculty of Engineering, University of Nottingham, Nottingham NG7 2TU, UKGas Turbine and Transmission Research Centre, Faculty of Engineering, University of Nottingham, Nottingham NG7 2TU, UKGas Turbine and Transmission Research Centre, Faculty of Engineering, University of Nottingham, Nottingham NG7 2TU, UKIncreased temperatures at the sealing interface between the seal and shaft can reduce the working life of a seal through elastomer aging, swelling and increased friction. Degradation of the seal due to increased temperatures can cause pre-mature failure, wear and leakage. There is no such thing as a perfect seal; each application has requirements to cater to the needs of each system. For radial oil seals in helicopter gearboxes, the contact temperatures at the sealing interface are a critical parameter to consider. In this manuscript, investigating the factors that influence the temperatures at the contact interface shed light on the operating parameters that cause an increase in contact temperatures. Four varying shaft coatings are tested against three seal spring loads for a range of sliding velocities between 5–25 ms<sup>−1</sup> to reproduce conditions of the gearbox. The study reveals an optimum seal spring of 12 oz, with a circumferential load of 3.34 N for lowest temperatures at the interface. Higher springs of 14 oz and lower springs of 8.5 oz both cause increased temperatures at the interface. Additionally, the need for surface coatings on the shaft is re-enforced through experimental evidence demonstrated by comparing temperatures reached between a plain stainless steel shaft and three surface coated shafts. Chrome plating shafts are undesirable due to the ‘polishing’ in effect they experience. The results of this study build on this by showing that chrome plated shafts have higher temperatures at the interface, aggravating any wear or polishing in of that surface. Contact temperatures with Tungsten carbide and Chrome oxide coatings remain within the expected temperature rise. Lastly, microscopically ‘rougher’ surfaces result in increased temperatures in contrast to surface coatings within the specified range of roughness as provided by DIN 3760/61/ISO 6194.https://www.mdpi.com/2079-6412/11/2/156radial-lip oil sealssealing interfacesleevessurface coatinggarter spring pre-loadhelicopter gearbox
collection DOAJ
language English
format Article
sources DOAJ
author Sarah Shabbir
Seamus D. Garvey
Sam M. Dakka
Benjamin C. Rothwell
spellingShingle Sarah Shabbir
Seamus D. Garvey
Sam M. Dakka
Benjamin C. Rothwell
An Experimental Study of Contact Temperatures at Sealing Interface against Varying Shaft Surfaces
Coatings
radial-lip oil seals
sealing interface
sleeves
surface coating
garter spring pre-load
helicopter gearbox
author_facet Sarah Shabbir
Seamus D. Garvey
Sam M. Dakka
Benjamin C. Rothwell
author_sort Sarah Shabbir
title An Experimental Study of Contact Temperatures at Sealing Interface against Varying Shaft Surfaces
title_short An Experimental Study of Contact Temperatures at Sealing Interface against Varying Shaft Surfaces
title_full An Experimental Study of Contact Temperatures at Sealing Interface against Varying Shaft Surfaces
title_fullStr An Experimental Study of Contact Temperatures at Sealing Interface against Varying Shaft Surfaces
title_full_unstemmed An Experimental Study of Contact Temperatures at Sealing Interface against Varying Shaft Surfaces
title_sort experimental study of contact temperatures at sealing interface against varying shaft surfaces
publisher MDPI AG
series Coatings
issn 2079-6412
publishDate 2021-01-01
description Increased temperatures at the sealing interface between the seal and shaft can reduce the working life of a seal through elastomer aging, swelling and increased friction. Degradation of the seal due to increased temperatures can cause pre-mature failure, wear and leakage. There is no such thing as a perfect seal; each application has requirements to cater to the needs of each system. For radial oil seals in helicopter gearboxes, the contact temperatures at the sealing interface are a critical parameter to consider. In this manuscript, investigating the factors that influence the temperatures at the contact interface shed light on the operating parameters that cause an increase in contact temperatures. Four varying shaft coatings are tested against three seal spring loads for a range of sliding velocities between 5–25 ms<sup>−1</sup> to reproduce conditions of the gearbox. The study reveals an optimum seal spring of 12 oz, with a circumferential load of 3.34 N for lowest temperatures at the interface. Higher springs of 14 oz and lower springs of 8.5 oz both cause increased temperatures at the interface. Additionally, the need for surface coatings on the shaft is re-enforced through experimental evidence demonstrated by comparing temperatures reached between a plain stainless steel shaft and three surface coated shafts. Chrome plating shafts are undesirable due to the ‘polishing’ in effect they experience. The results of this study build on this by showing that chrome plated shafts have higher temperatures at the interface, aggravating any wear or polishing in of that surface. Contact temperatures with Tungsten carbide and Chrome oxide coatings remain within the expected temperature rise. Lastly, microscopically ‘rougher’ surfaces result in increased temperatures in contrast to surface coatings within the specified range of roughness as provided by DIN 3760/61/ISO 6194.
topic radial-lip oil seals
sealing interface
sleeves
surface coating
garter spring pre-load
helicopter gearbox
url https://www.mdpi.com/2079-6412/11/2/156
work_keys_str_mv AT sarahshabbir anexperimentalstudyofcontacttemperaturesatsealinginterfaceagainstvaryingshaftsurfaces
AT seamusdgarvey anexperimentalstudyofcontacttemperaturesatsealinginterfaceagainstvaryingshaftsurfaces
AT sammdakka anexperimentalstudyofcontacttemperaturesatsealinginterfaceagainstvaryingshaftsurfaces
AT benjamincrothwell anexperimentalstudyofcontacttemperaturesatsealinginterfaceagainstvaryingshaftsurfaces
AT sarahshabbir experimentalstudyofcontacttemperaturesatsealinginterfaceagainstvaryingshaftsurfaces
AT seamusdgarvey experimentalstudyofcontacttemperaturesatsealinginterfaceagainstvaryingshaftsurfaces
AT sammdakka experimentalstudyofcontacttemperaturesatsealinginterfaceagainstvaryingshaftsurfaces
AT benjamincrothwell experimentalstudyofcontacttemperaturesatsealinginterfaceagainstvaryingshaftsurfaces
_version_ 1724318451895369728