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Grant: Collaborative Research and Development Grants

École de technologie supérieure

$140,000.00

Propulsion system integration and optimisation

EF 2017-18

Résumé
The gas turbine engine has envolved rapidly to provide a reliable and efficient business solution for global transportation. The engine design process is clearly a large contributor to this evolution. This process is highly iterative, multidisciplinary and complex in nature. The success of an engine depends on a carefully balanced design that best exploits the interactions between numerous traditional engineering disciplines such as aerodynamics and structures as well as lifecycle analysis of cost, manufacturability, serviceability and supportability. Pratt & Whitney Canada (P&WC) is the world leader in the design and manufacturing of small aero-engines. P&WC typically designs and develops 10-15 engines per years, which has resulted in a record 50 new engines certified over the past ten years. To continue this and to address new market requirements, advanced design and engine module design studies could reach 30 to 50 per years. The proposed program aims to deploy a fully automated and integrated P&WC Turbine System Optimizer ""TSO"" that is capable of finding the optimal balance between aerodynamic performance, cooling flows, durability, cost and weight in order to achieve the best product performance. The resulting ""TSO"" is expected to produce better-integrated results, while providing a step reduction in engine design elapsed time. A simplified version will be made available to universities in order to provide students with knowledge of trade-off between engine performance, weight and cost. The proposed program draws motivation from the vision at École de technologie supérieure (ETS), whose aim is to strengthen its expertise in propulsion systems through a strategic industrial partnership with P&WC in order to develop a new generation of engineers with greater knowledge in optimization and integration of the entire powerplant and aircraft system.
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
488703-2015
Name nom
Moustapha, SaidHany
Department département
Génie mécanique
Organization id
53
Institution établissement
École de technologie supérieure
Province en
Québec
Province fr
Québec
Country en
CANADA
Country fr
CANADA
Fiscal year exercice financier
2017
Competition year année de concours
2015
Award amount
140000
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
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
2
Nb partie
3
Application title
Propulsion system integration and optimisation
Keyword
NSERC
Application summary
The gas turbine engine has envolved rapidly to provide a reliable and efficient business solution for global transportation. The engine design process is clearly a large contributor to this evolution. This process is highly iterative, multidisciplinary and complex in nature. The success of an engine depends on a carefully balanced design that best exploits the interactions between numerous traditional engineering disciplines such as aerodynamics and structures as well as lifecycle analysis of cost, manufacturability, serviceability and supportability. Pratt & Whitney Canada (P&WC) is the world leader in the design and manufacturing of small aero-engines. P&WC typically designs and develops 10-15 engines per years, which has resulted in a record 50 new engines certified over the past ten years. To continue this and to address new market requirements, advanced design and engine module design studies could reach 30 to 50 per years. The proposed program aims to deploy a fully automated and integrated P&WC Turbine System Optimizer ""TSO"" that is capable of finding the optimal balance between aerodynamic performance, cooling flows, durability, cost and weight in order to achieve the best product performance. The resulting ""TSO"" is expected to produce better-integrated results, while providing a step reduction in engine design elapsed time. A simplified version will be made available to universities in order to provide students with knowledge of trade-off between engine performance, weight and cost. The proposed program draws motivation from the vision at École de technologie supérieure (ETS), whose aim is to strengthen its expertise in propulsion systems through a strategic industrial partnership with P&WC in order to develop a new generation of engineers with greater knowledge in optimization and integration of the entire powerplant and aircraft system.