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Grant: Collaborative Research and Development Grants

University of British Columbia

$136,800.00

Design and technology development of optimized composite aircraft structures using knowledge based iterations

EF 2016-17

Résumé
This project addresses design, development and manufacture of a challenging aircraft geometry, the knife edged 3D closeout structure. This geometry has difficult to fabricate key features with technology gaps, and has been selected for its high technical and economic benefit potential. The research partners will collaborate to resolve its key technology gaps, generate knowledge and create innovative solutions.The project will define baseline metrics using Boeing 737MAX 'similar to' products and will focus on improvements to cost, weight and manufacturing cycle time. An aggregate improvement of 25-50% is targeted. The knowledge generated, and experience gained during the design, tooling and manufacturing optimization processes will provide for competitive advantages. These advantages will manifest themselves as cost reductions, quality improvements and enable fabrication cycle time reductions though application of lean design and lean manufacturing.The overall research project involves six industrial partners, one research consortium, two research organizations and two academic institutions. The grant applied for here is to support the activities of one of the academic partners: The Composites Research Network (CRN) at The University of British Columbia. CRN's role in the overall project is to lead development of simulation methods and best practices, assessment and documentation of design and manufacturing best practices developed during the project. CRN will also identify technical gaps in existing scientific knowledge and document the findings in the Knowledge in Practice Centre hosted by CRN. This project will further the knowledge, experience and capability of advanced composite design, development and manufacturing in Canadian industry. Outcomes will be industrial competitive advantages, best practices documents and Highly Qualified Personnel (HQP).
Programme
Collaborative Research and Development Grants
Emplacement
British Columbia, Canada
Type de bénéficiaire
Academia
Type
Grant
Source
NSERC's Awards Data

Tel que publié

Application id
491744-2015
Name nom
Fernlund, Goran
Department département
Materials Engineering
Organization id
2
Institution établissement
University of British Columbia
Province en
British Columbia
Province fr
Colombie-Britannique
Country en
CANADA
Country fr
CANADA
Fiscal year exercice financier
2016
Competition year année de concours
2015
Award amount
136800
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
1702
Research subject group en
Design and manufacturing
Research subject group fr
Conception et fabrication
Research subject en
Advanced manufacturing
Research subject fr
Méthodes de fabrication avancées
Partie
1 & 2
Nb partie
2
Application title
Design and technology development of optimized composite aircraft structures using knowledge based iterations
Keyword
NSERC
Application summary
This project addresses design, development and manufacture of a challenging aircraft geometry, the knife edged 3D closeout structure. This geometry has difficult to fabricate key features with technology gaps, and has been selected for its high technical and economic benefit potential. The research partners will collaborate to resolve its key technology gaps, generate knowledge and create innovative solutions.The project will define baseline metrics using Boeing 737MAX 'similar to' products and will focus on improvements to cost, weight and manufacturing cycle time. An aggregate improvement of 25-50% is targeted. The knowledge generated, and experience gained during the design, tooling and manufacturing optimization processes will provide for competitive advantages. These advantages will manifest themselves as cost reductions, quality improvements and enable fabrication cycle time reductions though application of lean design and lean manufacturing.The overall research project involves six industrial partners, one research consortium, two research organizations and two academic institutions. The grant applied for here is to support the activities of one of the academic partners: The Composites Research Network (CRN) at The University of British Columbia. CRN's role in the overall project is to lead development of simulation methods and best practices, assessment and documentation of design and manufacturing best practices developed during the project. CRN will also identify technical gaps in existing scientific knowledge and document the findings in the Knowledge in Practice Centre hosted by CRN. This project will further the knowledge, experience and capability of advanced composite design, development and manufacturing in Canadian industry. Outcomes will be industrial competitive advantages, best practices documents and Highly Qualified Personnel (HQP).