Grant: Alliance Grants
Université de Sherbrooke
$154,000.00
Advanced motor & power systems (AMPS)
EF 2024-25
Résumé
Electric propulsion opens new possibilities for aircraft design that improves flight envelope, safety and efficiency by allowing multiple distributed propellers, redundancy, and hybridization of the energy source. However, the weight of the systems must be reduced to achieve these benefits. A key system that needs to be as light as possible is the electric motor system, independently from the source of electric power. During the last NSERC Alliance collaborative project, the academic and industrial team has developed a novel rotor architecture that doubles the tangential speed over current ultra-high-speed motor and a micro-channel air-cooled stator that eliminates the need for a liquid cooling system. These two new technologies enable tripling the power density of the power system (motor, inverter, gearbox and the cooling system) compared to a direct drive motor. In this context, the present project now aims at validating the key technologies of the motor and inverter to address the key challenges, namely (1) increasing winding filling factor, (2) increase rotor life, (3) reducing vibration, and (4) develop adapted power electronics. Successful results from this project will reduce uncertainties about the novel technologies sufficiently to launch a technology demonstration project at full scale dedicated to the development of an increased performance hybrid vertical take-off and landing aircraft. During the first ten years of commercialization of the technology, 158 kt of CO2 in Quebec, and 3 Mt worldwide, are expected to be avoided in the hard-to-decarbonize aeronautic sector. Finally, this project will train 8 highly qualified research engineers in the rapidly expanding field of electric powertrains, in particular in their capacity to develop novel technologies required to solve current and upcoming challenges and position Canada industry as a leader in the field.
Programme
Alliance Grants
Bénéficiaire
Emplacement
Quebec, Canada
Type de bénéficiaire
Academia
Type
Grant
Source
NSERC's Awards Data
Tel que publié
Application id
591852-2023
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
2024
Competition year année de concours
2023
Award amount
154000
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
2501
Research subject group en
Electrical and electronic engineering
Research subject group fr
Génie électrique et électronique
Research subject en
Power systems
Research subject fr
Réseaux électriques
Field of research list names en
Not available
Field of research list names fr
Non disponible
Socioeconomic objective list names en
Not available
Socioeconomic objective list names fr
Non disponible
Application title
Advanced motor & power systems (AMPS)
Keywords
direct air cooling stator; electric propulsion; floating magnet rotor; permanent magnet synchronous motors; power-dense electronics; ultra-high speed electric motor
Application summary
Electric propulsion opens new possibilities for aircraft design that improves flight envelope, safety and efficiency by allowing multiple distributed propellers, redundancy, and hybridization of the energy source. However, the weight of the systems must be reduced to achieve these benefits. A key system that needs to be as light as possible is the electric motor system, independently from the source of electric power. During the last NSERC Alliance collaborative project, the academic and industrial team has developed a novel rotor architecture that doubles the tangential speed over current ultra-high-speed motor and a micro-channel air-cooled stator that eliminates the need for a liquid cooling system. These two new technologies enable tripling the power density of the power system (motor, inverter, gearbox and the cooling system) compared to a direct drive motor. In this context, the present project now aims at validating the key technologies of the motor and inverter to address the key challenges, namely (1) increasing winding filling factor, (2) increase rotor life, (3) reducing vibration, and (4) develop adapted power electronics. Successful results from this project will reduce uncertainties about the novel technologies sufficiently to launch a technology demonstration project at full scale dedicated to the development of an increased performance hybrid vertical take-off and landing aircraft. During the first ten years of commercialization of the technology, 158 kt of CO2 in Quebec, and 3 Mt worldwide, are expected to be avoided in the hard-to-decarbonize aeronautic sector. Finally, this project will train 8 highly qualified research engineers in the rapidly expanding field of electric powertrains, in particular in their capacity to develop novel technologies required to solve current and upcoming challenges and position Canada industry as a leader in the field.