Grant: Alliance Grants
École de technologie supérieure
$93,000.00
An Aerodynamic-Acoustic Design of an Electrical and Shrouded Tail Rotor
EF 2022-23
Résumé
Aerospace industry innovations targets reduction of fuel consumption and noise emission. Electrical power-by-wire enabled technology address these challenges yielding lighter designs, increased operation flexibility and cost reduction. With electric motors having variable rotational speed, constraints in design and optimization strategies for rotor and propellers can be released. In addition to conventional aircraft and rotorcraft, new concepts arise in the urban air mobility or autonomous air delivery markets that will respond to urban missions such as emergency medical service, traffic and safety monitoring, passenger transportation. Noise annoyance during manoeuvre and local community noise concerns around heliports have to be addressed early by manufacturers. This research project is intended to take on the challenge with the development of aerodynamic-aeroacoustic coupled optimization methods for the design of quieter rotor and propellers. The objective of the partnership with École de technologie supérieure de Montréal, McGill University, and Université de Sherbrooke and the Canadian industrial companies Bell Textron Canada and Optis Engineering is to develop a coupled aerodynamic-aeroacoustic optimization framework for an electrical distributed anti-torque (EDAT) system to equip future Bell helicopters produced in Canada. Seven research students will be committed to apply state-of-the-art multi-disciplinary optimization methodologies and fill knowledge gaps in aeroacoustics of rotating machines. Thanks to the high-fidelity simulations and experimental approaches that will be conducted on a single shrouded fan representative of the EDAT system, this research will provide accurate validation and calibration data for the noise predictions. With this initiative, the most advanced optimization technique will be coupled with fast and accurate aeroacoustic models in a unique manner. In addition to maintaining and improving the competitiveness of the Canadian Aerospace industry in a world-wide market, the highly qualified personnel involved in the proposed research project will be valuable assets for the Canadian industry: aware of communities noise annoyance and skilled to tackle it.
Programme
Alliance Grants
Bénéficiaire
Emplacement
Quebec, Canada
Type de bénéficiaire
Academia
Type
Grant
Source
NSERC's Awards Data
Tel que publié
Application id
570863-2021
Name nom
Sanjose, Marlene M
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
2022
Competition year année de concours
2021
Award amount
93000
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
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
Installment
inst:2
Partie
1
Nb partie
2
Application title
An Aerodynamic-Acoustic Design of an Electrical and Shrouded Tail Rotor
Application summary
Aerospace industry innovations targets reduction of fuel consumption and noise emission. Electrical power-by-wire enabled technology address these challenges yielding lighter designs, increased operation flexibility and cost reduction. With electric motors having variable rotational speed, constraints in design and optimization strategies for rotor and propellers can be released. In addition to conventional aircraft and rotorcraft, new concepts arise in the urban air mobility or autonomous air delivery markets that will respond to urban missions such as emergency medical service, traffic and safety monitoring, passenger transportation. Noise annoyance during manoeuvre and local community noise concerns around heliports have to be addressed early by manufacturers. This research project is intended to take on the challenge with the development of aerodynamic-aeroacoustic coupled optimization methods for the design of quieter rotor and propellers. The objective of the partnership with École de technologie supérieure de Montréal, McGill University, and Université de Sherbrooke and the Canadian industrial companies Bell Textron Canada and Optis Engineering is to develop a coupled aerodynamic-aeroacoustic optimization framework for an electrical distributed anti-torque (EDAT) system to equip future Bell helicopters produced in Canada. Seven research students will be committed to apply state-of-the-art multi-disciplinary optimization methodologies and fill knowledge gaps in aeroacoustics of rotating machines. Thanks to the high-fidelity simulations and experimental approaches that will be conducted on a single shrouded fan representative of the EDAT system, this research will provide accurate validation and calibration data for the noise predictions. With this initiative, the most advanced optimization technique will be coupled with fast and accurate aeroacoustic models in a unique manner. In addition to maintaining and improving the competitiveness of the Canadian Aerospace industry in a world-wide market, the highly qualified personnel involved in the proposed research project will be valuable assets for the Canadian industry: aware of communities noise annoyance and skilled to tackle it.