Grant: Applied Research and Development Grants - Level 2
Cégep Edouard-Montpetit
$75,000.00
Non-destructive testing of landing gear parts made by additive manufacturing
FY 2020-21
Summary
In the aerospace industry, additive manufacturing (AM) is increasingly adopted for the production of critical parts as it allows for considerable gains in terms of weight, cost and engineering performance. However, its expansion is slowed down by the limited confidence in the process repeatability which is strongly linked to the lack of efficient non-destructive testing (NDT) to assess the quality of manufactured parts. NDT techniques need to be developed and optimized to address the challenging specificities of AM parts such as surface roughness, porosity, anisotropy and geometric complexities rendered possible by the process. The objective of this project, in partnership with Collins Aerospace, is to contribute to the development of advanced NDT techniques for the inspection of Ti-6Al-4V Titanium alloy landing gear parts obtained by powder bed fusion (PBF) and wire arc melting (WAM). Innovative ultrasound techniques will be developed and adapted to three families of parts defined by their geometric complexity. The developed techniques will then be validated on reference parts with simulated defects. The validated techniques will then lead to guidelines for inspection procedures for each family of parts.
Program
Applied Research and Development Grants - Level 2
Recipient
Location
Quebec, Canada
Recipient Type
Academia
Type
Grant
Source
NSERC's Awards Data
As published
Application id
549491-2019
Name nom
Désilets, Pascal
Department département
École nationale d'aérotechnique
Organization id
10335
Institution établissement
Cégep Edouard-Montpetit
Province en
Québec
Province fr
Québec
Country en
CANADA
Country fr
CANADA
Fiscal year exercice financier
2020
Competition year année de concours
2019
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 programs
Group fr
Programmes de partenariat
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
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:1 - 1
Partie
1
Nb partie
1
Application title
Non-destructive testing of landing gear parts made by additive manufacturing
Keyword
NSERC
Application summary
In the aerospace industry, additive manufacturing (AM) is increasingly adopted for the production of critical parts as it allows for considerable gains in terms of weight, cost and engineering performance. However, its expansion is slowed down by the limited confidence in the process repeatability which is strongly linked to the lack of efficient non-destructive testing (NDT) to assess the quality of manufactured parts. NDT techniques need to be developed and optimized to address the challenging specificities of AM parts such as surface roughness, porosity, anisotropy and geometric complexities rendered possible by the process. The objective of this project, in partnership with Collins Aerospace, is to contribute to the development of advanced NDT techniques for the inspection of Ti-6Al-4V Titanium alloy landing gear parts obtained by powder bed fusion (PBF) and wire arc melting (WAM). Innovative ultrasound techniques will be developed and adapted to three families of parts defined by their geometric complexity. The developed techniques will then be validated on reference parts with simulated defects. The validated techniques will then lead to guidelines for inspection procedures for each family of parts.