Surface integrity analysis of WEDMed specimen of Inconel 825 superalloy

WEDM has evolved as a well admired technique for machining of difficult to cut materials such as superalloys. WEDM produces intricate shape and profiles of superalloys by thermoelectric erosion process. But as the process is carried out at very high temperature, the formation of heat affected zone,...

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Main Authors: Pawan Kumar, Meenu Gupta, Vineet Kumar
Format: Article
Language:English
Published: Growing Science 2018-09-01
Series:International Journal of Data and Network Science
Subjects:
Online Access:http://www.growingscience.com/ijds/Vol2/ijdns_2018_7.pdf
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spelling doaj-52c07d7b18c4400583dede0905299a7c2020-11-25T01:37:07ZengGrowing ScienceInternational Journal of Data and Network Science2561-81482561-81562018-09-0123798810.5267/j.ijdns.2018.8.001Surface integrity analysis of WEDMed specimen of Inconel 825 superalloyPawan KumarMeenu GuptaVineet KumarWEDM has evolved as a well admired technique for machining of difficult to cut materials such as superalloys. WEDM produces intricate shape and profiles of superalloys by thermoelectric erosion process. But as the process is carried out at very high temperature, the formation of heat affected zone, microcracks, recast layer, porosity etc. resulted in decreased surface integrity of machined specimen and becomes a big problem in WEDM. Discharge energy is the most influencing param-eters that affect the surface integrity of WEDmed samples. In this study, Inconel 825, widely used in aerospace industry for making of combustor casing and turbine blades, was machined with WEDM under different discharge energy. The surface topography of the WEDMed specimen was carried cut by using SEM, XRD and EDX techniques. It was observed from the SEM micrograph that the machined surface includes cracks, pockmarks, craters, and pulled out material. The density and sice of craters increase with increase in discharge energy. Surface crack density of 0.0138 μm/μm2 and recast layer thickness of 34.62μm was obtained for the machined sample at high value of discharge energy while at low value surface crack density of 0.0016 μm/μm2 and recast layer thickness of 20.99μm was observed. EDX and XRD analysis of the specimen showed that an ap-preciable amount of elements viz. Fe (Ferrous), Cr (Chromium), Cu (Copper), Ni (Nickel) are mi-grated to the surface of the workpiece at high value of pulse on time. http://www.growingscience.com/ijds/Vol2/ijdns_2018_7.pdfWEDMInconel 825Surface crack densityMicrostructureRecast layer
collection DOAJ
language English
format Article
sources DOAJ
author Pawan Kumar
Meenu Gupta
Vineet Kumar
spellingShingle Pawan Kumar
Meenu Gupta
Vineet Kumar
Surface integrity analysis of WEDMed specimen of Inconel 825 superalloy
International Journal of Data and Network Science
WEDM
Inconel 825
Surface crack density
Microstructure
Recast layer
author_facet Pawan Kumar
Meenu Gupta
Vineet Kumar
author_sort Pawan Kumar
title Surface integrity analysis of WEDMed specimen of Inconel 825 superalloy
title_short Surface integrity analysis of WEDMed specimen of Inconel 825 superalloy
title_full Surface integrity analysis of WEDMed specimen of Inconel 825 superalloy
title_fullStr Surface integrity analysis of WEDMed specimen of Inconel 825 superalloy
title_full_unstemmed Surface integrity analysis of WEDMed specimen of Inconel 825 superalloy
title_sort surface integrity analysis of wedmed specimen of inconel 825 superalloy
publisher Growing Science
series International Journal of Data and Network Science
issn 2561-8148
2561-8156
publishDate 2018-09-01
description WEDM has evolved as a well admired technique for machining of difficult to cut materials such as superalloys. WEDM produces intricate shape and profiles of superalloys by thermoelectric erosion process. But as the process is carried out at very high temperature, the formation of heat affected zone, microcracks, recast layer, porosity etc. resulted in decreased surface integrity of machined specimen and becomes a big problem in WEDM. Discharge energy is the most influencing param-eters that affect the surface integrity of WEDmed samples. In this study, Inconel 825, widely used in aerospace industry for making of combustor casing and turbine blades, was machined with WEDM under different discharge energy. The surface topography of the WEDMed specimen was carried cut by using SEM, XRD and EDX techniques. It was observed from the SEM micrograph that the machined surface includes cracks, pockmarks, craters, and pulled out material. The density and sice of craters increase with increase in discharge energy. Surface crack density of 0.0138 μm/μm2 and recast layer thickness of 34.62μm was obtained for the machined sample at high value of discharge energy while at low value surface crack density of 0.0016 μm/μm2 and recast layer thickness of 20.99μm was observed. EDX and XRD analysis of the specimen showed that an ap-preciable amount of elements viz. Fe (Ferrous), Cr (Chromium), Cu (Copper), Ni (Nickel) are mi-grated to the surface of the workpiece at high value of pulse on time.
topic WEDM
Inconel 825
Surface crack density
Microstructure
Recast layer
url http://www.growingscience.com/ijds/Vol2/ijdns_2018_7.pdf
work_keys_str_mv AT pawankumar surfaceintegrityanalysisofwedmedspecimenofinconel825superalloy
AT meenugupta surfaceintegrityanalysisofwedmedspecimenofinconel825superalloy
AT vineetkumar surfaceintegrityanalysisofwedmedspecimenofinconel825superalloy
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