Grant: Strategic Projects - Group
Université de Sherbrooke
$165,906.00
A low cost / high power density gas turbine concept based on rotary ramjets
FY 2014-15
Summary
Developing clean mechanical power sources is strategic for developed countries to remain competitive in the years to come due to a constantly growing environmental pressure and stringent emissions regulations. This research develops a new type of gas turbine based on rotary ramjets for motive and stationary power systems. Compared to conventional gas turbines, the proposed engine, named the R4E (Rim-Rotor Rotary Ramjet Engine), promises potential for up to ten times the power density, similar efficiencies, low NOx emissions, and low costs. Such advantages could make this engine design a breakthrough technology for future gas turbines. Designing functional rotary ramjet engines requires pushing the limit of material strength and known combustion physics with combustion taking place in centrifugal acceleration fields of more than half a million « g's ». A first research initiative, funded from an NSERC Strategic Grant, developed the necessary fundamental understanding to get rotary ramjet engines to work and lead to very promising results proving the concept feasibility and even demonstrating positive blade power.This new proposal builds on these exciting results and continues the development of the R4E toward the demonstration of an engine prototype that can provide positive brake power continuously. At this stage of development, problematics of heat management, optimal aerothermodynamic design, windage loss reductions as well as system integration will be studied. The work is done in collaboration with the National Research Council Canada, Composites Atlantic, Hydrogenics, Pratt and Whitney Canada, and Cognitek Canada. The outcomes of the research are a new engine design and derived technologies that can be used by Canadian industries as well as highly qualified personnel in the clean power generation sector.
Program
Strategic Projects - Group
Recipient
Location
Quebec, Canada
Recipient Type
Academia
Type
Grant
Source
NSERC's Awards Data
As published
Application id
430667-2012
Name nom
Plante, JeanSebastien
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
2014
Competition year année de concours
2012
Award amount
165906
Program id
STPGP
Program name en
Strategic Projects - Group
Program name fr
Projets stratégiques - De groupe
Group en
Research partnerships programs
Group fr
Programmes de partenariat
Committee code
1571
Committee name en
Strategic Projects Selection Panel - Energy
Committee name fr
Comité de sélection des projets stratégiques - Énergie
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
Partie
3
Nb partie
3
Application title
A low cost / high power density gas turbine concept based on rotary ramjets
Keyword
NSERC
Application summary
Developing clean mechanical power sources is strategic for developed countries to remain competitive in the years to come due to a constantly growing environmental pressure and stringent emissions regulations. This research develops a new type of gas turbine based on rotary ramjets for motive and stationary power systems. Compared to conventional gas turbines, the proposed engine, named the R4E (Rim-Rotor Rotary Ramjet Engine), promises potential for up to ten times the power density, similar efficiencies, low NOx emissions, and low costs. Such advantages could make this engine design a breakthrough technology for future gas turbines. Designing functional rotary ramjet engines requires pushing the limit of material strength and known combustion physics with combustion taking place in centrifugal acceleration fields of more than half a million « g's ». A first research initiative, funded from an NSERC Strategic Grant, developed the necessary fundamental understanding to get rotary ramjet engines to work and lead to very promising results proving the concept feasibility and even demonstrating positive blade power.This new proposal builds on these exciting results and continues the development of the R4E toward the demonstration of an engine prototype that can provide positive brake power continuously. At this stage of development, problematics of heat management, optimal aerothermodynamic design, windage loss reductions as well as system integration will be studied. The work is done in collaboration with the National Research Council Canada, Composites Atlantic, Hydrogenics, Pratt and Whitney Canada, and Cognitek Canada. The outcomes of the research are a new engine design and derived technologies that can be used by Canadian industries as well as highly qualified personnel in the clean power generation sector.