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Grant: Alliance Grants

Université de Sherbrooke

$300,000.00

Clean-fuel Efficient Rim-rotor Architecture MICroturbogenerator (CERAMIC)

EF 2022-23

Résumé
Hybrid-electric propulsion requires clean and highly efficient new power sources to drastically exceed battery energy density and offset the additional cost of carbon neutral fuels such as hydrogen and synfuel. Exonetik Turbo's turbogenerator, created in partnership with Université de Sherbrooke, has the potential to almost double the efficiency of current small gas turbines and operate at near-zero emissions by the reliable integration of ceramic blades in an inside-out configuration. The technology feasibility was successfully demonstrated with a 100h-test of a proof-of-concept turbine prototype during the previous NSERC/CRIAQ project. Following this proof of concept, this proposed project aims at developing the critical technologies of the hot section (combustor and turbine) to operate the engine for thousands of hours with targeted performance. In particular, the team will develop and integrate in a turbogenerator: a creep-free retaining system for the blades in the hub, an insulated low-cooling carbon-polyimide structural shroud and an ultra-low-NOx highly recuperated micromix combustor, three of the critical components identified in the previous project. Success of this project will validate the technologies in a simulated environment through their integration in a complete, viable, closer-to-market prototype. Following this project, product development and commercialization with partners will lead to highly qualified jobs in the aeronautics sector here in Quebec. Once on the market, the turbogenerator is projected to save 12 megatonnes of CO2 during its first ten years of deployment in Canada only, with worldwide potential several times greater.
Programme
Alliance Grants
Emplacement
Quebec, Canada
Type de bénéficiaire
Academia
Type
Grant
Source
NSERC's Awards Data

Tel que publié

Application id
572241-2022
Name nom
Picard, Mathieu M
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
2022
Competition year année de concours
2022
Award amount
300000
Program id
ALLRP
Program name en
Alliance Grants
Program name fr
Subventions Alliance
Group en
RESEARCH PARTNERSHIPS
Group fr
PARTENARIATS DE RECHERCHE
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
2100
Research subject group en
Mechanical engineering
Research subject group fr
Génie mécanique
Research subject en
Mechanical engineering
Research subject fr
Génie mécanique
Installment
inst:1
Partie
1
Nb partie
1
Application title
Clean-fuel Efficient Rim-rotor Architecture MICroturbogenerator (CERAMIC)
Application summary
Hybrid-electric propulsion requires clean and highly efficient new power sources to drastically exceed battery energy density and offset the additional cost of carbon neutral fuels such as hydrogen and synfuel. Exonetik Turbo's turbogenerator, created in partnership with Université de Sherbrooke, has the potential to almost double the efficiency of current small gas turbines and operate at near-zero emissions by the reliable integration of ceramic blades in an inside-out configuration. The technology feasibility was successfully demonstrated with a 100h-test of a proof-of-concept turbine prototype during the previous NSERC/CRIAQ project. Following this proof of concept, this proposed project aims at developing the critical technologies of the hot section (combustor and turbine) to operate the engine for thousands of hours with targeted performance. In particular, the team will develop and integrate in a turbogenerator: a creep-free retaining system for the blades in the hub, an insulated low-cooling carbon-polyimide structural shroud and an ultra-low-NOx highly recuperated micromix combustor, three of the critical components identified in the previous project. Success of this project will validate the technologies in a simulated environment through their integration in a complete, viable, closer-to-market prototype. Following this project, product development and commercialization with partners will lead to highly qualified jobs in the aeronautics sector here in Quebec. Once on the market, the turbogenerator is projected to save 12 megatonnes of CO2 during its first ten years of deployment in Canada only, with worldwide potential several times greater.