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Grant: Strategic Projects Supplemental Competition

Université de Sherbrooke

$99,999.00

A low cost / high power density engine for hybrid fuel cell drive trains

EF 2007-08

Résumé
The proposed research will study a new, high risk/high reward, engine technology for hybrid fuel cell power trains that could significantly reduce the cost of fuel cells powered vehicles. A hybrid fuel cell system using the proposed engine would have costs of ~22$/kW compared to the actual costs of full fuel cell systems of ~73$/kW. Moreover, system weight and size would be about 3 times lower (from 163kg to 50kg and 114L to 31L), further improving fuel economy and easing vehicle design.The engine technology proposed here is based on a rotary ramjet engine configuration using rim rotors (patent pending). It uses a unidirectional carbon-fiber rim rotor to reach supersonic rim speeds of up to Mach 3. Rotational power comes from supersonic thrusters (ramjets) placed inside the rim rotor. Power is extracted via an electrical generator or a reduction gearbox. Preliminary theoretical analysis of this engine running on hydrogen shows very high power densities (10kW/kg vs 1.6kW/kg for high power piston engines), acceptable energy conversion efficiencies (10-30%), and low production costs (~$500). The engine has multi-fuel capabilities and can operate on any kind of gaseous or liquid fuels. The research aims to demonstrate the feasibility of the proposed technology. This will be done by showing that a ramjet designed for the rim-rotor configuration can produce thrust and by showing that a representative rim-rotor engine can achieve the required rim speeds of Mach 3. The ramjet demonstration will be addressed with a stationary ramjet test bed to measure the flow properties, visualize the flow fields, and measure the net thrust of a representative rim-rotor ramjet (with combustion). The rim-rotor demonstration will be addressed by measuring the bursting speed of an optimal rim-rotor rotary ramjet engine made with proper high strenghtcarbon fiber materials (without combustion).
Programme
Strategic Projects Supplemental Competition
Emplacement
Quebec, Canada
Type de bénéficiaire
Academia
Type
Grant
Source
NSERC's Awards Data

Tel que publié

Application id
356878-2007
Name nom
Plante, JeanSébastien
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
2007
Competition year année de concours
2007
Award amount
99999
Program id
STPSC
Program name en
Strategic Projects Supplemental Competition
Program name fr
Projets stratégiques compétition supplémentaire
Group en
Research partnerships programs
Group fr
Programmes de partenariat
Committee code
1065
Committee name en
Strategic Projects Selection Panel - Energy 1
Committee name fr
Comité de sélection des projets stratégiques - Énergie 1
Area of application code
303
Area of application group en
Energy resources
Area of application group fr
Ressources d'énergie
Area of application en
Alternative energy resources
Area of application fr
Autres ressources d'énergie
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
Partie
1
Nb partie
2
Application title
A low cost / high power density engine for hybrid fuel cell drive trains
Keyword
NA
Application summary
The proposed research will study a new, high risk/high reward, engine technology for hybrid fuel cell power trains that could significantly reduce the cost of fuel cells powered vehicles. A hybrid fuel cell system using the proposed engine would have costs of ~22$/kW compared to the actual costs of full fuel cell systems of ~73$/kW. Moreover, system weight and size would be about 3 times lower (from 163kg to 50kg and 114L to 31L), further improving fuel economy and easing vehicle design.The engine technology proposed here is based on a rotary ramjet engine configuration using rim rotors (patent pending). It uses a unidirectional carbon-fiber rim rotor to reach supersonic rim speeds of up to Mach 3. Rotational power comes from supersonic thrusters (ramjets) placed inside the rim rotor. Power is extracted via an electrical generator or a reduction gearbox. Preliminary theoretical analysis of this engine running on hydrogen shows very high power densities (10kW/kg vs 1.6kW/kg for high power piston engines), acceptable energy conversion efficiencies (10-30%), and low production costs (~$500). The engine has multi-fuel capabilities and can operate on any kind of gaseous or liquid fuels. The research aims to demonstrate the feasibility of the proposed technology. This will be done by showing that a ramjet designed for the rim-rotor configuration can produce thrust and by showing that a representative rim-rotor engine can achieve the required rim speeds of Mach 3. The ramjet demonstration will be addressed with a stationary ramjet test bed to measure the flow properties, visualize the flow fields, and measure the net thrust of a representative rim-rotor ramjet (with combustion). The rim-rotor demonstration will be addressed by measuring the bursting speed of an optimal rim-rotor rotary ramjet engine made with proper high strenghtcarbon fiber materials (without combustion).