Grant: Alliance Grants
Université de Sherbrooke
$107,863.00
Experimental investigations for improvement of oil control for an orbiting sealing application
FY 2024-25
Summary
The most promising path to decarbonize commercial flights are synthetic fuels and carbon offsets. In both cases, the fuel costs will increase significantly, making improvement in engine efficiency paramount in reaching an economically viable solution. Large gas turbines have reached impressive efficiency levels, but small gas turbines remain relatively inefficient due to limited combustion temperatures combined to high viscous and tip losses. In order to achieve radical reduction in fuel consumptions, manufacturers are forced to revisit alternative engine configurations with a new perspective. Prime candidates for cleaner propulsion are the non-reciprocating combustion engines that combine high efficiencies of volumetric engines while being well-known for their high power density. Unfortunately, these engines are also well-known for their oil consumption that needs to be reduced before they are used for aerospace applications in order to meet customer perceptions, weight and forthcoming emission regulations. The first targets are to address leakage through the face-sealing Oil Control Rings (OCRs) and injected oil spilling away from the gas seals as they can be drastically reduced from current values without a significant impact on engine durability. This proposed project aims at reducing oil consumption through the development of improved OCRs and injection strategy. The team will: (1) measure the impedance of the OCRs and their embedded O-ring to update the model and guide the design of new OCRs, (2) use the current experimental setup that measures the effect of secondary motion on oil consumption to test the performance of the new OCR designs, and (3) build a new rig to observe oil injection to the gas seals and test new strategies for directing oil to the running surfaces. The results will reduce direct hydrocarbon emissions, contribute to enabling engines that will reduce CO2 emissions and strengthen Canadian industry leadership in advanced propulsion.
Program
Alliance Grants
Recipient
Location
Quebec, Canada
Recipient Type
Academia
Type
Grant
Source
NSERC's Awards Data
As published
Application id
586043-2023
Name nom
Picard, Mathieu M
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
2024
Competition year année de concours
2023
Award amount
107863
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
Experimental investigations for improvement of oil control for an orbiting sealing application
Keywords
cleaner engines; experimental validation; oil control rings; oil injection; reduced emissions; reduced oil consumption; rotary engine
Application summary
The most promising path to decarbonize commercial flights are synthetic fuels and carbon offsets. In both cases, the fuel costs will increase significantly, making improvement in engine efficiency paramount in reaching an economically viable solution. Large gas turbines have reached impressive efficiency levels, but small gas turbines remain relatively inefficient due to limited combustion temperatures combined to high viscous and tip losses. In order to achieve radical reduction in fuel consumptions, manufacturers are forced to revisit alternative engine configurations with a new perspective. Prime candidates for cleaner propulsion are the non-reciprocating combustion engines that combine high efficiencies of volumetric engines while being well-known for their high power density. Unfortunately, these engines are also well-known for their oil consumption that needs to be reduced before they are used for aerospace applications in order to meet customer perceptions, weight and forthcoming emission regulations. The first targets are to address leakage through the face-sealing Oil Control Rings (OCRs) and injected oil spilling away from the gas seals as they can be drastically reduced from current values without a significant impact on engine durability. This proposed project aims at reducing oil consumption through the development of improved OCRs and injection strategy. The team will: (1) measure the impedance of the OCRs and their embedded O-ring to update the model and guide the design of new OCRs, (2) use the current experimental setup that measures the effect of secondary motion on oil consumption to test the performance of the new OCR designs, and (3) build a new rig to observe oil injection to the gas seals and test new strategies for directing oil to the running surfaces. The results will reduce direct hydrocarbon emissions, contribute to enabling engines that will reduce CO2 emissions and strengthen Canadian industry leadership in advanced propulsion.