M. Horn, L. Langer, S. Dietrich, G. Schlick, C. Seidel, G. Reinhart
{"title":"Cross-Contaminations in Powder Bed Fusion: Influence of Copper Alloy Particles in Nickel-Base Alloy Feedstock on Part Quality","authors":"M. Horn, L. Langer, S. Dietrich, G. Schlick, C. Seidel, G. Reinhart","doi":"10.2139/ssrn.3724208","DOIUrl":null,"url":null,"abstract":"When two or more different metal powders are processed on a single additive manufacturing (AM) machine, cross-contaminations can occur. This is particularly relevant to the consecutive processing of different materials on a powder bed fusion (PBF) machine through material changes as well as simultaneous processing of different materials via multi-material PBF. However, uncertainty about tolerable foreign particle percentages in metal powder feedstock limits the applicability of material changes and multi-material PBF. Two alloys which are of particular relevance to the aerospace industry are nickel-base alloy 2.4668 and copper alloy CW106C. In multi-material applications, 2.4668 mainly serves as a structural, load-bearing material. Therefore, this study investigates the influence of defined quantities of copper alloy particles in nickel-base alloy feedstock on metallurgical structure and static tensile strength. Foreign particle inclusions were dissolved in the matrix material and formed a solid solution. No material deteriorations were observed for contamination levels up to 20 particle percent (part.%). Etching revealed a nonhomogeneous solid solution with Cu-rich areas. Contamination levels up to two particle part.% CW106C in 2.4668 showed no influence on ultimate tensile strength and a limited influence on fracture elongation. At five part.% contamination, both properties deteriorated and inferior material qualities were observed. Fractography showed a similar fracture behavior for all of the contamination levels examined. Implications for the aerospace industry by the material combination examined are made on the basis of the results presented.","PeriodicalId":151146,"journal":{"name":"TransportRN: Air Transportation Systems (Topic)","volume":"23 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2020-11-03","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"4","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"TransportRN: Air Transportation Systems (Topic)","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.2139/ssrn.3724208","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
引用次数: 4
Abstract
When two or more different metal powders are processed on a single additive manufacturing (AM) machine, cross-contaminations can occur. This is particularly relevant to the consecutive processing of different materials on a powder bed fusion (PBF) machine through material changes as well as simultaneous processing of different materials via multi-material PBF. However, uncertainty about tolerable foreign particle percentages in metal powder feedstock limits the applicability of material changes and multi-material PBF. Two alloys which are of particular relevance to the aerospace industry are nickel-base alloy 2.4668 and copper alloy CW106C. In multi-material applications, 2.4668 mainly serves as a structural, load-bearing material. Therefore, this study investigates the influence of defined quantities of copper alloy particles in nickel-base alloy feedstock on metallurgical structure and static tensile strength. Foreign particle inclusions were dissolved in the matrix material and formed a solid solution. No material deteriorations were observed for contamination levels up to 20 particle percent (part.%). Etching revealed a nonhomogeneous solid solution with Cu-rich areas. Contamination levels up to two particle part.% CW106C in 2.4668 showed no influence on ultimate tensile strength and a limited influence on fracture elongation. At five part.% contamination, both properties deteriorated and inferior material qualities were observed. Fractography showed a similar fracture behavior for all of the contamination levels examined. Implications for the aerospace industry by the material combination examined are made on the basis of the results presented.