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Grant: Collaborative Research and Development Grants

École de technologie supérieure

$80,000.00

Brazing process optimisation for structural aerospace applications

EF 2015-16

Résumé
Brazing is a relatively low cost joining process used in many applications by the aerospace industry. However,some of the critical parameters to ensure braze joint reliability are still to be determined. Pratt & WhitneyCanada (PWC) and Turbomeca Canada (TMC) use many brazing pastes for stainless steels and Nickel basedsuperalloys for non-structural applications and reapers. Sometime, the braze reproducibility and success inpost-brazing testing is not consistent. More understanding of the wetting behaviour combined with thecharacterisation of the industrial brazing process is required. Achieving reproducibility and reliability, togetherwith understanding of all aspects related to braze metal wetting behaviour as well as microstructure-mechanicalproperty relationship is the first goal for this research. This includes surface tension characterization, liquidbraze wetting behaviour, fluidity of filler metal, brazing gap and diffusion into the parent metal in order to ensure successful brazing for gas turbine components. Moreover, brasing of titanium alloys is a new andrelevant domain to investigate in the framework of turbine applications. The other objective will be todetermine the potential of brazing alloys to carry structural loading during operation of gas turbine engines. Infact, such a versatile joining process (as it is possible to assemble dissimilar alloys easily) could replacewelding processes that result in major component distortion and affects the dimensional tolerances of machinedparts.
Programme
Collaborative Research and Development Grants
Emplacement
Quebec, Canada
Type de bénéficiaire
Academia
Type
Grant
Source
NSERC's Awards Data

Tel que publié

Application id
411485-2010
Name nom
Bocher, Philippe
Department département
Génie mécanique
Organization id
53
Institution établissement
École de technologie supérieure
Province en
Québec
Province fr
Québec
Country en
CANADA
Country fr
CANADA
Fiscal year exercice financier
2015
Competition year année de concours
2010
Award amount
80000
Program id
CRDPJ
Program name en
Collaborative Research and Development Grants
Program name fr
Subventions de recherche et développement coopérative
Group en
Research partnerships programs
Group fr
Programmes de partenariat
Committee code
96
Committee name en
RPP Internal Decision Cttee
Committee name fr
Cté de décision interne - PPR
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
2002
Research subject group en
Materials science and technology
Research subject group fr
Science et technologie des matériaux
Research subject en
Materials processing
Research subject fr
Transformation des matériaux
Partie
5
Nb partie
5
Application title
Brazing process optimisation for structural aerospace applications
Keyword
NSERC
Application summary
Brazing is a relatively low cost joining process used in many applications by the aerospace industry. However,some of the critical parameters to ensure braze joint reliability are still to be determined. Pratt & WhitneyCanada (PWC) and Turbomeca Canada (TMC) use many brazing pastes for stainless steels and Nickel basedsuperalloys for non-structural applications and reapers. Sometime, the braze reproducibility and success inpost-brazing testing is not consistent. More understanding of the wetting behaviour combined with thecharacterisation of the industrial brazing process is required. Achieving reproducibility and reliability, togetherwith understanding of all aspects related to braze metal wetting behaviour as well as microstructure-mechanicalproperty relationship is the first goal for this research. This includes surface tension characterization, liquidbraze wetting behaviour, fluidity of filler metal, brazing gap and diffusion into the parent metal in order to ensure successful brazing for gas turbine components. Moreover, brasing of titanium alloys is a new andrelevant domain to investigate in the framework of turbine applications. The other objective will be todetermine the potential of brazing alloys to carry structural loading during operation of gas turbine engines. Infact, such a versatile joining process (as it is possible to assemble dissimilar alloys easily) could replacewelding processes that result in major component distortion and affects the dimensional tolerances of machinedparts.