Grant: CCI Applied Research and Development Grants
Cégep Édouard-Montpetit
$40,000.00
Ultrasonic testing of aircraft engine components made by additive manufacturing.
EF 2024-25
Résumé
The aerospace industry is increasingly adopting additive manufacturing (AM) as a more eco-friendly and economical fabrication method due to its potential to reduce aircraft weight, fuel consumption, and raw material usage compared to traditional machining methods. However, for AM to be applied to critical aircraft components, it is essential to develop and validate non-destructive testing (NDT) methods that ensure the structural integrity of these parts.
This project is a collaboration between the Centre Technologique en Aérospatiale (CTA) and Pratt & Whitney Canada, aiming to adapt and evaluate advanced ultrasonic NDT methods to inspect an aircraft engine part under development by Pratt & Whitney Canada. The first phase of the project involves the identification of the characteristics of defects that may be produced during the fabrication process, such as their shape, size, orientation and position within the part. This information will direct the fabrication of AM samples, incorporating artificial defects with relevant characteristics that accurately reflect the flaws anticipated in the production process. Meanwhile, numerical simulations will be carried out to understand the ultrasound propagation within the part and simulate the interaction between the acoustic waves and defects. Subsequently, using the simulation results, the performance of various ultrasonic phased array imaging methods, including the Total Focusing Method (TFM), phase coherence imaging (PCI), and pulse-echo phased-array technique, will be evaluated and adapted. In addition, the "signature method," a novel approach developed at CTA for identifying defective parts by analyzing their acoustic signature, will also be evaluated. Finally, the simulation results will be validated experimentally using the UT methods and the samples produced with artificial defects. The minimal defect size detectable for each defect type and NDT method employed will be determined and communicated to the partner alongside considerations for implementing such inspection methods in production.
Programme
CCI Applied Research and Development Grants
Bénéficiaire
Emplacement
Quebec, Canada
Type de bénéficiaire
Academia
Type
Grant
Source
NSERC's Awards Data
Tel que publié
Application id
CCARD-2023-00638
Name nom
Désilets, Pascal
Department département
Direction Générale - Cégep Édouard-Montpetit
Organization id
10335
Institution établissement
Cégep Édouard-Montpetit
Province en
Québec
Province fr
Québec
Country en
CANADA
Country fr
CANADA
Fiscal year exercice financier
2024
Competition year année de concours
2023
Award amount
40000
Program id
CCARD
Program name en
CCI Applied Research and Development Grants
Program name fr
ICC Subventions de recherche et développement appliquée
Group en
RESEARCH PARTNERSHIPS
Group fr
PARTENARIATS DE RECHERCHE
Committee code
nan
Area of application code
9999
Area of application group en
Not available
Area of application group fr
Non disponible
Area of application en
Not available
Area of application fr
Non disponible
Research subject code
9999
Research subject group en
Not available
Research subject group fr
Non disponible
Research subject en
Not available
Research subject fr
Non disponible
Field of research list codes
RDF1030401
Field of research list names en
Acoustics and acoustical devices and waves
Field of research list names fr
Acoustique et appareils acoustiques et les ondes
Socioeconomic objective list names en
Not available
Socioeconomic objective list names fr
Non disponible
Application title
Ultrasonic testing of aircraft engine components made by additive manufacturing.
Keywords
Ultrasound; Additive manufacturing; Non-destructive testing; Titanium alloys; Inspection; Numerical simulation; Data analysis; Imaging algorithms
Application summary
The aerospace industry is increasingly adopting additive manufacturing (AM) as a more eco-friendly and economical fabrication method due to its potential to reduce aircraft weight, fuel consumption, and raw material usage compared to traditional machining methods. However, for AM to be applied to critical aircraft components, it is essential to develop and validate non-destructive testing (NDT) methods that ensure the structural integrity of these parts.
This project is a collaboration between the Centre Technologique en Aérospatiale (CTA) and Pratt & Whitney Canada, aiming to adapt and evaluate advanced ultrasonic NDT methods to inspect an aircraft engine part under development by Pratt & Whitney Canada. The first phase of the project involves the identification of the characteristics of defects that may be produced during the fabrication process, such as their shape, size, orientation and position within the part. This information will direct the fabrication of AM samples, incorporating artificial defects with relevant characteristics that accurately reflect the flaws anticipated in the production process. Meanwhile, numerical simulations will be carried out to understand the ultrasound propagation within the part and simulate the interaction between the acoustic waves and defects. Subsequently, using the simulation results, the performance of various ultrasonic phased array imaging methods, including the Total Focusing Method (TFM), phase coherence imaging (PCI), and pulse-echo phased-array technique, will be evaluated and adapted. In addition, the "signature method," a novel approach developed at CTA for identifying defective parts by analyzing their acoustic signature, will also be evaluated. Finally, the simulation results will be validated experimentally using the UT methods and the samples produced with artificial defects. The minimal defect size detectable for each defect type and NDT method employed will be determined and communicated to the partner alongside considerations for implementing such inspection methods in production.