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Grant: Collaborative Research and Development Grants

École Polytechnique de Montréal

$156,084.00

Advanced peening processes for the fatigue life improvement of aerospace components

EF 2019-20

Résumé
Shot peening consists in impacting a metal part with high velocity shots. The impacts plastically stretch the surface and induce a layer of compressive residual stresses and cold working. Under the right conditions, the process delivers components that can withstand 20 times more fatigue cycles than untreated parts. Nearly every metallic part of an aircraft is shot peened. High Temperature Shot Peening (HTSP) consists in carrying out conventional shot peening at elevated temperature. Authors have demonstrated that HTSP can deliver even further fatigue life improvement than shot peening. Vibratory Peening (VP) is a modified finishing process that induces similar benefits as shot peening but for a much better surface finish. The applicability of these two processes within an industrial context have yet to be demonstrated. This research will thoroughly investigate the effects of HTSP and VP on the fatigue lives of aerospace materials, namely: steel, titanium and aluminum. The research will involve manufacturing research HTSP and VP setups and thoroughly investigate their effects in terms of surface characteristics, residual stresses, hardness, microstructural changes and fatigue life. The work will be carried out by 10 B.Eng, 1 MSc and 4 PhD students over 4 years. The work will be carried out in collaboration with Polytechnique Montréal, Centre Technologique en Aérospatiale and Safran S.A. (in Canada and in France). This project has the potential to trigger significant innovation for the Canadian aerospace industry. First, HTSP has the potential to yield better fatigue life improvement than shot peening, which will yield to lighter and more durable Canadian aircraft. VP has the potential to also yield better fatigue life improvement than shot peening and also to combine two manufacturing processes into one: peening and surface finishing. These processes have therefore the potential to increase the competitiveness of our aerospace industry by producing lighter and more durable parts, as well as yielding cheaper and faster post-manufacturing processes. Moreover, lighter and more durable parts reduce the environmental imprint of air travel, which is beneficial for the environment.
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
518968-2017
Name nom
Lévesque, Martin
Department département
Génie mécanique
Organization id
64
Institution établissement
École Polytechnique de Montréal
Province en
Québec
Province fr
Québec
Country en
CANADA
Country fr
CANADA
Fiscal year exercice financier
2019
Competition year année de concours
2017
Award amount
156084
Program id
CRDPJ
Program name en
Collaborative Research and Development Grants
Program name fr
Subventions de recherche et développement coopérative
Group en
RESEARCH PARTNERSHIPS
Group fr
PARTENARIATS DE RECHERCHE
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
2108
Research subject group en
Mechanical engineering
Research subject group fr
Génie mécanique
Research subject en
Aerospace, aeronautical and automotive engineering
Research subject fr
Génie aérospatial, aéronautique et automobile
Installment
inst:2 - 2
Partie
2
Nb partie
2
Application title
Advanced peening processes for the fatigue life improvement of aerospace components
Keyword
NSERC
Application summary
Shot peening consists in impacting a metal part with high velocity shots. The impacts plastically stretch the surface and induce a layer of compressive residual stresses and cold working. Under the right conditions, the process delivers components that can withstand 20 times more fatigue cycles than untreated parts. Nearly every metallic part of an aircraft is shot peened. High Temperature Shot Peening (HTSP) consists in carrying out conventional shot peening at elevated temperature. Authors have demonstrated that HTSP can deliver even further fatigue life improvement than shot peening. Vibratory Peening (VP) is a modified finishing process that induces similar benefits as shot peening but for a much better surface finish. The applicability of these two processes within an industrial context have yet to be demonstrated. This research will thoroughly investigate the effects of HTSP and VP on the fatigue lives of aerospace materials, namely: steel, titanium and aluminum. The research will involve manufacturing research HTSP and VP setups and thoroughly investigate their effects in terms of surface characteristics, residual stresses, hardness, microstructural changes and fatigue life. The work will be carried out by 10 B.Eng, 1 MSc and 4 PhD students over 4 years. The work will be carried out in collaboration with Polytechnique Montréal, Centre Technologique en Aérospatiale and Safran S.A. (in Canada and in France). This project has the potential to trigger significant innovation for the Canadian aerospace industry. First, HTSP has the potential to yield better fatigue life improvement than shot peening, which will yield to lighter and more durable Canadian aircraft. VP has the potential to also yield better fatigue life improvement than shot peening and also to combine two manufacturing processes into one: peening and surface finishing. These processes have therefore the potential to increase the competitiveness of our aerospace industry by producing lighter and more durable parts, as well as yielding cheaper and faster post-manufacturing processes. Moreover, lighter and more durable parts reduce the environmental imprint of air travel, which is beneficial for the environment.