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Process-Structure-Property Relationships in Selective Laser Melting of Aerospace Alloys

dc.contributor.advisorElbestawi, M. A.
dc.contributor.advisorVeldhuis, Stephen
dc.contributor.authorYakout, Mostafa
dc.contributor.departmentMechanical Engineeringen_US
dc.date.accessioned2019-04-15T18:26:06Z
dc.date.available2019-04-15T18:26:06Z
dc.date.issued2019
dc.description.abstractMetal additive manufacturing can be used for producing complex and functional components in the aerospace industry. This thesis deals with the process-structure-property relationships in selective laser melting of three aerospace alloys: Invar 36, stainless steel 316L, and Ti-6Al-4V. These alloys are weldable but hard to machine, which make them good candidates for the selective laser melting process. Invar 36 has a very low coefficient of thermal expansion because of its nickel concentration of 36% and stainless steel 316L contains 16-18% chromium that gives the alloy a corrosion resistance property. Ti-6Al-4V offers high strength-to-weight ratio, high biocompatibility, and outstanding corrosion resistance. Any changes in the chemical composition of these materials could affect their performance during application. In this thesis, a full factorial design of experiments is formulated to study a wide range of laser process parameters. The bulk density, tensile mechanical properties, fractography, microstructure, material composition, material phases, coefficient of thermal expansion, magnetic dipole moments, and residual stresses of the parts produced are experimentally investigated. An optimum process window has been suggested for each material based on experimental work. The thermal cycle, residual stresses, and part distortions are examined using a thermo-mechanical finite element model. The model predicts the residual stress and part distortion after build plate removal. The thesis introduces two laser energy densities for each material: brittle-ductile transition energy density, ET, and critical laser energy density, EC. Below the brittle-ductile transition energy density, the parts exhibited void formation, low density, and brittle fracture. Above the critical energy density, the parts showed vaporization of some alloying elements that have low boiling temperatures. Additionally, real-time measurements were taken using a pyrometer and a high-speed camera during the selective laser melting process. The trends found in the numerical results agree with those found experimentally.en_US
dc.description.degreeDoctor of Philosophy (PhD)en_US
dc.description.degreetypeThesisen_US
dc.identifier.urihttp://hdl.handle.net/11375/24243
dc.language.isoenen_US
dc.subjectSelective Laser Meltingen_US
dc.subjectAdditive Manufacturingen_US
dc.subjectAerospace Industryen_US
dc.subjectSolidificationen_US
dc.subjectAdvanced Manufacturingen_US
dc.subjectTi-6Al-4Ven_US
dc.subjectInvar 36en_US
dc.subjectStainless Steel 316Len_US
dc.titleProcess-Structure-Property Relationships in Selective Laser Melting of Aerospace Alloysen_US
dc.typeThesisen_US

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