Title
Surface machining condition and fatigue life on Inconel 718Author
xmlui.dri2xhtml.METS-1.0.item-contributorOtherinstitution
Tecnun Ceit-IK4ITP Aero
Version
http://purl.org/coar/version/c_970fb48d4fbd8a85
Rights
© 2018 The AuthorsAccess
http://purl.org/coar/access_right/c_abf2Publisher’s version
https://doi.org/10.1016/j.prostr.2018.12.339Published at
Procedia Structural Integrity Vol. 13. Pp. 1609-1614. Elsevier, 2018Publisher
ElsevierKeywords
Machining
Surface Condition
Fatigue
High Temperature ... [+]
Surface Condition
Fatigue
High Temperature ... [+]
Machining
Surface Condition
Fatigue
High Temperature
Inconel 718 [-]
Surface Condition
Fatigue
High Temperature
Inconel 718 [-]
Abstract
Life assessment of components working in aero-engines at elevated temperatures is critical. Machining has a serious effect on these nickel-based alloys, for example in turbine discs, affecting their l ... [+]
Life assessment of components working in aero-engines at elevated temperatures is critical. Machining has a serious effect on these nickel-based alloys, for example in turbine discs, affecting their life in service. Machining (turning, broaching…) modifies surface roughness, thickness of the affected substrate layer (including the effect of possible broken carbides) and residual stress distribution near the component surface. On top of that, it is possible to shot-peen or not the component, which again modifies its surface integrity. The aim of this work is to discern among the effect of the different parameter: roughness, damage and residual stresses on fatigue performance and optimum machining conditions. [-]
xmlui.dri2xhtml.METS-1.0.item-sponsorship
Comisión europeaxmlui.dri2xhtml.METS-1.0.item-projectID
info:eu-repo/grantAgreement/EC/7th Framework Programme/604999/EU/Engine Module Validators/ENOVALCollections
The following license files are associated with this item: