The effect of EDM wire cutting on the fatigue properties of 4340 steel.

Electric discharge machining (EDM) is a metal removal process that has seen increasing use in the recent years. EDM is replacing the use of conventional machining in certain applications due to its ability to machine conductive materials of any hardness into highly complex shapes. One such applicati...

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Main Author: Yeo, Wei Hsien Yvonne
Format: Article in Journal/Newspaper
Language:unknown
Published: University of Canterbury. Mechanical Engineering 1999
Subjects:
Online Access:https://dx.doi.org/10.26021/1416
https://ir.canterbury.ac.nz/handle/10092/6630
id ftdatacite:10.26021/1416
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spelling ftdatacite:10.26021/1416 2023-05-15T13:54:50+02:00 The effect of EDM wire cutting on the fatigue properties of 4340 steel. Yeo, Wei Hsien Yvonne 1999 https://dx.doi.org/10.26021/1416 https://ir.canterbury.ac.nz/handle/10092/6630 unknown University of Canterbury. Mechanical Engineering Copyright Wei Hsien Yvonne Yeo https://canterbury.libguides.com/rights/theses CreativeWork article 1999 ftdatacite https://doi.org/10.26021/1416 2021-11-05T12:55:41Z Electric discharge machining (EDM) is a metal removal process that has seen increasing use in the recent years. EDM is replacing the use of conventional machining in certain applications due to its ability to machine conductive materials of any hardness into highly complex shapes. One such application is the manufacture of structural components for skis used by Antarctica-bound Hercules aircraft. As fatigue properties are important for structural components used in the aeronautical industry, the effect of EDM on fatigue properties is significant. Literature indicates that EDM causes degradation in fatigue properties; however, there is insufficient information relating EDM wire cutting (EDWC) (the process to be used) to fatigue. Results indicate that EDWC is greatly detrimental to fatigue properties. Fatigue limits of EDWC specimens are reduced from approximately 900MPa (ground specimens) to 300MPa. Numerous cracks in the surface and sub-surface of the specimens, together with a surface roughness of 3μm Ra, indicate that surface topography contributes to the reduction in fatigue limit. A phase change in the surface layer and the presence of a residual tensile stress are also possible contributing factors. The effect of shot peening after EDWC is also investigated, as there is little information on this subject. Shot peening after the EDWC process has returned the fatigue limit to its initial value, and in some cases has even increased it (1000MPa). This result is attributed to the introduction of residual compressive stresses in the surface. The use of EDWC alone to manufacture the aircraft structural components is not practical. By adding the shot peening process after EDWC, the manufacturing process can become a viable alternative to conventional machining. Article in Journal/Newspaper Antarc* Antarctica DataCite Metadata Store (German National Library of Science and Technology) Hercules ENVELOPE(161.450,161.450,-77.483,-77.483)
institution Open Polar
collection DataCite Metadata Store (German National Library of Science and Technology)
op_collection_id ftdatacite
language unknown
description Electric discharge machining (EDM) is a metal removal process that has seen increasing use in the recent years. EDM is replacing the use of conventional machining in certain applications due to its ability to machine conductive materials of any hardness into highly complex shapes. One such application is the manufacture of structural components for skis used by Antarctica-bound Hercules aircraft. As fatigue properties are important for structural components used in the aeronautical industry, the effect of EDM on fatigue properties is significant. Literature indicates that EDM causes degradation in fatigue properties; however, there is insufficient information relating EDM wire cutting (EDWC) (the process to be used) to fatigue. Results indicate that EDWC is greatly detrimental to fatigue properties. Fatigue limits of EDWC specimens are reduced from approximately 900MPa (ground specimens) to 300MPa. Numerous cracks in the surface and sub-surface of the specimens, together with a surface roughness of 3μm Ra, indicate that surface topography contributes to the reduction in fatigue limit. A phase change in the surface layer and the presence of a residual tensile stress are also possible contributing factors. The effect of shot peening after EDWC is also investigated, as there is little information on this subject. Shot peening after the EDWC process has returned the fatigue limit to its initial value, and in some cases has even increased it (1000MPa). This result is attributed to the introduction of residual compressive stresses in the surface. The use of EDWC alone to manufacture the aircraft structural components is not practical. By adding the shot peening process after EDWC, the manufacturing process can become a viable alternative to conventional machining.
format Article in Journal/Newspaper
author Yeo, Wei Hsien Yvonne
spellingShingle Yeo, Wei Hsien Yvonne
The effect of EDM wire cutting on the fatigue properties of 4340 steel.
author_facet Yeo, Wei Hsien Yvonne
author_sort Yeo, Wei Hsien Yvonne
title The effect of EDM wire cutting on the fatigue properties of 4340 steel.
title_short The effect of EDM wire cutting on the fatigue properties of 4340 steel.
title_full The effect of EDM wire cutting on the fatigue properties of 4340 steel.
title_fullStr The effect of EDM wire cutting on the fatigue properties of 4340 steel.
title_full_unstemmed The effect of EDM wire cutting on the fatigue properties of 4340 steel.
title_sort effect of edm wire cutting on the fatigue properties of 4340 steel.
publisher University of Canterbury. Mechanical Engineering
publishDate 1999
url https://dx.doi.org/10.26021/1416
https://ir.canterbury.ac.nz/handle/10092/6630
long_lat ENVELOPE(161.450,161.450,-77.483,-77.483)
geographic Hercules
geographic_facet Hercules
genre Antarc*
Antarctica
genre_facet Antarc*
Antarctica
op_rights Copyright Wei Hsien Yvonne Yeo
https://canterbury.libguides.com/rights/theses
op_doi https://doi.org/10.26021/1416
_version_ 1766260971860393984