Grant: Collaborative Research and Development Grants
Université du Québec à Chicoutimi
$41,158.00
Low power de-icing systems for light weight helicopters
EF 2019-20
Résumé
Rotorcraft is vulnerable to rotor-blade in-flight icing. As so far only large helicopter may have rotor blades de-iced by means of high-energy electro-thermal systems, whereas small helicopter is lacking in the electrical power required to run them. That is why Bell Helicopter Textron, a manufacturer of small rotorcraft, realized at University of Quebec at Chicoutimi (UQAC) between 2006 and 2014 two CRSNG-CRIAQ projects, in which three approaches were evaluated in simulated icing tests and demonstrated practical for rotorcraft application. These were then recommended for further investigation at higher TRL: as energy-wise technologies, low-ice-adhesion coatings and piezoelectric actuators, and as solution avoiding slips rings the low-weight mast-mounted generator (MMG). The project consists of developing in laboratory up to TRL level 5, the three technologies previously demonstrated feasible at TRL 3, or a combination thereof: ice-phobic coatings poised to reduce ice adhesion, but requiring high erosion resistance (Objective 1), efficient piezoelectric system equipped with resistant piezo-elements to ensure a durable anti-icing blade protection (Objective 2); and for MMG technology a wireless system for efficiently controlling the rotor blade heating (Objective 3). The project includes two fundamental works : the development of a new software for modelling the heat transfer on rotorcraft blades during de-icing (objective 4) and the continuation of the previous work on a physic-based model elaborated on ice adhesion (objective 5). The grant proposal will involve three Canadian industrial partners, Bell Helicopter Textron Canada, MagChem Inc. Canada, and Iders Canada; and four institutional partners: Anti-Icing Materials Laboratory of UQAC, National Research Council Aerospace, Ecole Polytechnique de Montreal and Ecole de Technologie Superieure. Three graduate students, two Ph. D. and a Master degree, will be involved in Objectives 2, 3 and 4. Given the present state of knowledge and scientific advancement, the full development of a durable ice-phobic coating or/and a reliable piezo-equipped system will constitute a breakdown, which will profit to all Canadian partners.
Programme
Collaborative Research and Development Grants
Bénéficiaire
Emplacement
Quebec, Canada
Type de bénéficiaire
Academia
Type
Grant
Source
NSERC's Awards Data
Tel que publié
Application id
478088-2014
Name nom
Volat, Christophe
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
2019
Competition year année de concours
2014
Award amount
41158
Program id
CRDPJ
Program name en
Collaborative Research and Development Grants
Program name fr
Subventions de recherche et développement coopérative
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:3 - 3
Partie
3
Nb partie
3
Application title
Low power de-icing systems for light weight helicopters
Keyword
NSERC
Application summary
Rotorcraft is vulnerable to rotor-blade in-flight icing. As so far only large helicopter may have rotor blades de-iced by means of high-energy electro-thermal systems, whereas small helicopter is lacking in the electrical power required to run them. That is why Bell Helicopter Textron, a manufacturer of small rotorcraft, realized at University of Quebec at Chicoutimi (UQAC) between 2006 and 2014 two CRSNG-CRIAQ projects, in which three approaches were evaluated in simulated icing tests and demonstrated practical for rotorcraft application. These were then recommended for further investigation at higher TRL: as energy-wise technologies, low-ice-adhesion coatings and piezoelectric actuators, and as solution avoiding slips rings the low-weight mast-mounted generator (MMG). The project consists of developing in laboratory up to TRL level 5, the three technologies previously demonstrated feasible at TRL 3, or a combination thereof: ice-phobic coatings poised to reduce ice adhesion, but requiring high erosion resistance (Objective 1), efficient piezoelectric system equipped with resistant piezo-elements to ensure a durable anti-icing blade protection (Objective 2); and for MMG technology a wireless system for efficiently controlling the rotor blade heating (Objective 3). The project includes two fundamental works : the development of a new software for modelling the heat transfer on rotorcraft blades during de-icing (objective 4) and the continuation of the previous work on a physic-based model elaborated on ice adhesion (objective 5). The grant proposal will involve three Canadian industrial partners, Bell Helicopter Textron Canada, MagChem Inc. Canada, and Iders Canada; and four institutional partners: Anti-Icing Materials Laboratory of UQAC, National Research Council Aerospace, Ecole Polytechnique de Montreal and Ecole de Technologie Superieure. Three graduate students, two Ph. D. and a Master degree, will be involved in Objectives 2, 3 and 4. Given the present state of knowledge and scientific advancement, the full development of a durable ice-phobic coating or/and a reliable piezo-equipped system will constitute a breakdown, which will profit to all Canadian partners.