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Grant: Applied Research and Development Grants - Level 2

Cégep de Trois-Rivières

$75,000.00

Additive manufacturing assembly comparison

EF 2019-20

Résumé
Aeronautic parts with varying section thicknesses require extensive machining to produce and more often thannot, this is done using high value materials. This leads to high part production costs which in their final shapewould require significantly less material (high buy-to-fly ratio). Additive manufacturing (AM) brings newopportunities in design and manufacturing. One such opportunity comes from AM processes that can addmaterial on existing parts such as directed energy deposition, welding, thermal projection and brazing. Forexample, those processes allow the addition of metal on thin parts where thicker sections are required;therefore significantly reducing the amount of material required (thus decreasing the buy-to-fly ratio). Multipleconcerns arise from those processes regarding the production of aeronautic critical parts, such as themechanical properties of the bond, distortion and residual stress induced in the parts.From the technical and commercial points of view, the ability to add metal or modify sections of existing partsbrings the possibility to significantly reduce the amount of material machined, therefore decreasing thebuy-to-fly ratio, which is a constant objective in the aeronautic field where high value materials are used,particularly for titanium (Ti-6Al-4V) and nickel (Inconel 625) alloys.The purpose of this project is thus to evaluate the effects of the different additive manufacturing depositiontechnologies on the integrity of the bonds created, the distortion and the residual stresses induced by thethermal processes and to compare those characteristics to the economics of the process. This will provide theindustrial partners list of selection criteria when selecting which additive manufacturing assembly process touse.
Programme
Applied Research and Development Grants - Level 2
Emplacement
Quebec, Canada
Type de bénéficiaire
Academia
Type
Grant
Source
NSERC's Awards Data

Tel que publié

Application id
506344-2016
Name nom
Marin, Gheorghe
Department département
Centre de métallurgie du Québec
Organization id
17333
Institution établissement
Cégep de Trois-Rivières
Province en
Québec
Province fr
Québec
Country en
CANADA
Country fr
CANADA
Fiscal year exercice financier
2019
Competition year année de concours
2016
Award amount
75000
Program id
CARD2
Program name en
Applied Research and Development Grants - Level 2
Program name fr
Subventions de recherche et développement appliquée - niveau 2
Group en
RESEARCH PARTNERSHIPS
Group fr
PARTENARIATS DE RECHERCHE
Committee code
1561
Committee name en
Applied Research and Development Grants
Committee name fr
Subventions de recherche et développement appliquée
Area of application code
703
Area of application group en
Transportation systems and services
Area of application group fr
Services et systèmes de transport
Area of application en
Aerospace
Area of application fr
Aérospatial
Research subject code
2000
Research subject group en
Materials science and technology
Research subject group fr
Science et technologie des matériaux
Research subject en
Materials science and technology
Research subject fr
Science et technologie des matériaux
Installment
inst:2 - 2
Partie
2
Nb partie
2
Application title
Additive manufacturing assembly comparison
Keyword
NSERC
Application summary
Aeronautic parts with varying section thicknesses require extensive machining to produce and more often thannot, this is done using high value materials. This leads to high part production costs which in their final shapewould require significantly less material (high buy-to-fly ratio). Additive manufacturing (AM) brings newopportunities in design and manufacturing. One such opportunity comes from AM processes that can addmaterial on existing parts such as directed energy deposition, welding, thermal projection and brazing. Forexample, those processes allow the addition of metal on thin parts where thicker sections are required;therefore significantly reducing the amount of material required (thus decreasing the buy-to-fly ratio). Multipleconcerns arise from those processes regarding the production of aeronautic critical parts, such as themechanical properties of the bond, distortion and residual stress induced in the parts.From the technical and commercial points of view, the ability to add metal or modify sections of existing partsbrings the possibility to significantly reduce the amount of material machined, therefore decreasing thebuy-to-fly ratio, which is a constant objective in the aeronautic field where high value materials are used,particularly for titanium (Ti-6Al-4V) and nickel (Inconel 625) alloys.The purpose of this project is thus to evaluate the effects of the different additive manufacturing depositiontechnologies on the integrity of the bonds created, the distortion and the residual stresses induced by thethermal processes and to compare those characteristics to the economics of the process. This will provide theindustrial partners list of selection criteria when selecting which additive manufacturing assembly process touse.