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Grant: Alliance Grants

Université du Québec à Chicoutimi

$200,000.00

Aircraft Representative Testing in Icing Conditions of Cutting-edge Anti-icing Technologies

EF 2024-25

Résumé
This project aims to establish two world-unique experimental facilities to advance knowledge on in-flight icing issues, develop highly sophisticated ice protection systems to support future air mobility, and advance predictive numerical methods. The first installation involves a full-scale tail rotor placed in a cold chamber capable of simulating hovering flight in icy conditions. Fully instrumented to study rotor performance and operate de-icing systems, the test rig will generate experimental data and serve in the development of a novel ice protection technology. The second installation consists of an aircraft engine fan set up in an icing wind tunnel to investigate critical in-flight icing scenarios. This setup will produce experimental data and support the development of predictive models for ice accumulation and shedding. This project will foster the next generation of scientists in this cutting-edge field by enabling the graduation of two master's and doctoral students (4 in total), as well as the training of a postdoctoral researcher. For Bell Textron Canada, this setup will be crucial for developing low-energy consumption ice protection systems for its future lightweight rotorcraft. For Pratt & Whitney, the experimental data will enhance understanding of mechanical loads caused by ice and improve numerical simulation capabilities. This will directly support the future development of lighter, high-efficiency aircraft engines.
Programme
Alliance Grants
Emplacement
Quebec, Canada
Type de bénéficiaire
Academia
Type
Grant
Source
NSERC's Awards Data

Tel que publié

Application id
590793-2023
Name nom
Momen, Gelareh G
Department département
Sciences appliquées
Organization id
52
Institution établissement
Université du Québec à Chicoutimi
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
200000
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
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
Aircraft Representative Testing in Icing Conditions of Cutting-edge Anti-icing Technologies
Keywords
experimental methods; finite elements; ice protection systems; ice shedding; icing of engines; icing of rotors; in-flight icing; modeling of ice accretion; stochastic methods
Application summary
This project aims to establish two world-unique experimental facilities to advance knowledge on in-flight icing issues, develop highly sophisticated ice protection systems to support future air mobility, and advance predictive numerical methods. The first installation involves a full-scale tail rotor placed in a cold chamber capable of simulating hovering flight in icy conditions. Fully instrumented to study rotor performance and operate de-icing systems, the test rig will generate experimental data and serve in the development of a novel ice protection technology. The second installation consists of an aircraft engine fan set up in an icing wind tunnel to investigate critical in-flight icing scenarios. This setup will produce experimental data and support the development of predictive models for ice accumulation and shedding. This project will foster the next generation of scientists in this cutting-edge field by enabling the graduation of two master's and doctoral students (4 in total), as well as the training of a postdoctoral researcher. For Bell Textron Canada, this setup will be crucial for developing low-energy consumption ice protection systems for its future lightweight rotorcraft. For Pratt & Whitney, the experimental data will enhance understanding of mechanical loads caused by ice and improve numerical simulation capabilities. This will directly support the future development of lighter, high-efficiency aircraft engines.