Grant: Collaborative Research and Development Grants
Université de Sherbrooke
$175,464.00
Characterization of guided wave propagation in aircraft structures
EF 2012-13
Résumé
Structural health monitoring (SHM) is a major area of interest for the aerospace community, especially considering aging aircraft where the growing maintenance costs estimated to $10,4 billion worldwide annually. The 5 to 10 years goal of the industry is to deploy SHM systems which will 1) meet the in-service inspection requirements with sensors permanently installed on the structure and 2) provide economic benefits compared to the baseline inspection methods. Strategies using guided wave propagation have been proposed for embedded monitoring of airframe structures. However, wave propagation and interaction with defects in complex structures is addressed in the literature only for specific and limited number of components and types of defects. For example, interaction with cracks in metallic joints and debonding in composite joints has been investigated to some extent. The objective of this knowledge-gap based research is to provide the industry with an extended knowledge base for a variety of basic aircraft structures, or standards, from which the guided wave propagation and interaction with defects for other specific structures could be inferred from. The knowledge base will contain parameters such as the type of modes propagating in the structures or interacting with defects, the attenuation of the waves, the spatial pattern of the waves and the dispersion curves. The specific objectives of the project are: 1) develop a standard process to characterize guided wave propagation, 2) develop a knowledge base of guided wave characteristics for a variety of common aircraft structures, 3) develop a knowledge base of guided wave interaction mechanisms with damage for a variety of common aircraft structures and 4) propose SHM design criteria for guided waves in aircraft structures. Such a knowledge base would allow industrial partners to optimize sensing configuration and minimize development time, by reducing required testing for validation and qualification of SHM applications for damage monitoring.
Programme
Collaborative Research and Development Grants
Bénéficiaire
Emplacement
Quebec, Canada
Type de bénéficiaire
Academia
Type
Grant
Source
NSERC's Awards Data
Tel que publié
Application id
421842-2011
Name nom
Masson, Patrice
Department département
Génie mécanique
Organization id
68
Institution établissement
Université de Sherbrooke
Province en
Québec
Province fr
Québec
Country en
CANADA
Country fr
CANADA
Fiscal year exercice financier
2012
Competition year année de concours
2011
Award amount
175464
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
141
Committee name en
University/Industry
Committee name fr
Universités/industrie
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
Partie
1
Nb partie
3
Application title
Characterization of guided wave propagation in aircraft structures
Keyword
NSERC
Application summary
Structural health monitoring (SHM) is a major area of interest for the aerospace community, especially considering aging aircraft where the growing maintenance costs estimated to $10,4 billion worldwide annually. The 5 to 10 years goal of the industry is to deploy SHM systems which will 1) meet the in-service inspection requirements with sensors permanently installed on the structure and 2) provide economic benefits compared to the baseline inspection methods. Strategies using guided wave propagation have been proposed for embedded monitoring of airframe structures. However, wave propagation and interaction with defects in complex structures is addressed in the literature only for specific and limited number of components and types of defects. For example, interaction with cracks in metallic joints and debonding in composite joints has been investigated to some extent. The objective of this knowledge-gap based research is to provide the industry with an extended knowledge base for a variety of basic aircraft structures, or standards, from which the guided wave propagation and interaction with defects for other specific structures could be inferred from. The knowledge base will contain parameters such as the type of modes propagating in the structures or interacting with defects, the attenuation of the waves, the spatial pattern of the waves and the dispersion curves. The specific objectives of the project are: 1) develop a standard process to characterize guided wave propagation, 2) develop a knowledge base of guided wave characteristics for a variety of common aircraft structures, 3) develop a knowledge base of guided wave interaction mechanisms with damage for a variety of common aircraft structures and 4) propose SHM design criteria for guided waves in aircraft structures. Such a knowledge base would allow industrial partners to optimize sensing configuration and minimize development time, by reducing required testing for validation and qualification of SHM applications for damage monitoring.