Please use this identifier to cite or link to this item: https://apo.ansto.gov.au/dspace/handle/10238/10438
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dc.contributor.authorHoye, N-
dc.contributor.authorLi, H-
dc.contributor.authorCuiuri, D-
dc.contributor.authorParadowska, AM-
dc.date.accessioned2021-02-25T03:11:23Z-
dc.date.available2021-02-25T03:11:23Z-
dc.date.issued2013-12-02-
dc.identifier.citationHoye, N., Li, H., Cuiuri, D., & Paradowska, A. M. (2013). Residual stresses in titanium aerospace components formed via additive manufacture. Paper presented at the 11th AINSE-ANBUG Neutron Scattering Symposium (AANSS), Sydney, 2 - 3 December 2013 (p.51)en_US
dc.identifier.urihttps://apo.ansto.gov.au/dspace/handle/10238/10438-
dc.descriptionNot available online. Conference Handbook held by ANSTO Library at DDC 539.758/15en_US
dc.description.abstractAdditive manufacturing (AM) using arc-wire based metal deposition has been suggested as one method to reduce the costs associated with production of titanium components, particularly within the aerospace sector. In the present study gas tungsten arc welding (GTAW) with automated wire addition was used to additively manufacture (AM) a representative thin-walled aerospace component from Ti-6AI-4V in a layer-wise manner. Residual strains, and hence stresses, were analysed quantitatively using neutron diffraction techniques on the KOWARI strain scanner at the OPAL research facility operated by the Australian Nuclear Science and Technology Organisation (ANSTO). Results showed that residual strains within such an AM sample could be measured with relative ease using the neutron diffraction method. Residual stress levels were found to be greatest in the longitudinal direction and concentrated at the interface between the base plate and deposited wall. Difficulties in measurement of lattice strains in some discrete locations were ascribed to the formation of the formation of localised texturing where α-Ti laths form in aligned colonies within prior β-Ti grain boundaries upon cooling. Observations of microstructure reveal 'basket-weave' morphology typical of welds in Ti-6AI-4V. Microhardness measurements show a drop in hardness in the top region of the deposit, indicating a dependence on thermal cycling from sequential welds. Time-of-flight neutron diffraction has been proposed to analyse stresses in both the α-Ti and β-Ti phases simultaneously as well as inter-granular strains. This study forms part of a wider investigation into the suitability of arc-wire based deposition techniques for the additive manufacture of titanium components.en_US
dc.language.isoenen_US
dc.publisherAustralian Institute of Nuclear Science and Engineering (AINSE)en_US
dc.subjectAerospace industryen_US
dc.subjectANSTOen_US
dc.subjectComputer-aided manufacturingen_US
dc.subjectOPAL Reactoren_US
dc.subjectMaterials testingen_US
dc.subjectNeutron diffractionen_US
dc.subjectResidual stressesen_US
dc.subjectStrain gagesen_US
dc.titleResidual stresses in titanium aerospace components formed via additive manufactureen_US
dc.typeConference Abstracten_US
dc.date.statistics2021-02-25-
Appears in Collections:Conference Publications

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