Grant: Alliance Grants
Université de Sherbrooke
$92,958.00
Modeling and Validation of the Oil Control Ring Performance for a Orbiting Face-Sealing
EF 2021-22
Résumé
As ground transportation is slowly but surely being electrified, the air transportation industry is looking for solutions to reduce its carbon footprint. Unfortunately, batteries are too heavy to be viable for commercial flight and cheap, widely available bio-jet-fuel is still eluding. The best solution remains to increase engine efficiency to reduce fuel consumption as much as possible. Large gas turbines have reached impressive efficiency levels, but small gas turbines remains 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. One of the prime candidates for cleaner propulsion are the non-reciprocating combustion engines types that combine high efficiencies of volumetric engines while being well-known for their high power density. Unfortunately, these type of engine 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 leakage through the face-sealing Oil Control Rings (OCRs) can represent more than half of the oil consumption and is the first target to reduce total oil consumption as it can be drastically reduced from current values without a significant impact on engine durability. This proposed project aims at improving engine OCRs through detailed modeling and experimental validation. The UdeS and P&WC team will build upon previous OCR models by developing a novel numerical formulation of the hydrodynamic pressure generated tailored for the orbiting face-sealing OCR-housing interface required by this type of engines. The hydrodynamic pressure sub-model will then be integrated in a complete OCR simulation code that could be used to predict trends for oil leakage, friction and wear. In parallel, an experimental setup will be built to validate the model and OCR performance by measuring oil consumption and oil film thickness in a representative controlled environment.
Programme
Alliance Grants
Bénéficiaire
Emplacement
Quebec, Canada
Type de bénéficiaire
Academia
Type
Grant
Source
NSERC's Awards Data
Tel que publié
Application id
555815-2020
Name nom
Picard, Mathieu
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
2021
Competition year année de concours
2020
Award amount
92958
Program id
ALLRP
Program name en
Alliance Grants
Program name fr
Subventions Alliance
Group en
Research partnerships programs
Group fr
Programmes de partenariat
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
Installment
inst:2
Partie
1
Nb partie
3
Application title
Modeling and Validation of the Oil Control Ring Performance for a Orbiting Face-Sealing
Keyword
NSERC
Application summary
As ground transportation is slowly but surely being electrified, the air transportation industry is looking for solutions to reduce its carbon footprint. Unfortunately, batteries are too heavy to be viable for commercial flight and cheap, widely available bio-jet-fuel is still eluding. The best solution remains to increase engine efficiency to reduce fuel consumption as much as possible. Large gas turbines have reached impressive efficiency levels, but small gas turbines remains 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. One of the prime candidates for cleaner propulsion are the non-reciprocating combustion engines types that combine high efficiencies of volumetric engines while being well-known for their high power density. Unfortunately, these type of engine 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 leakage through the face-sealing Oil Control Rings (OCRs) can represent more than half of the oil consumption and is the first target to reduce total oil consumption as it can be drastically reduced from current values without a significant impact on engine durability. This proposed project aims at improving engine OCRs through detailed modeling and experimental validation. The UdeS and P&WC team will build upon previous OCR models by developing a novel numerical formulation of the hydrodynamic pressure generated tailored for the orbiting face-sealing OCR-housing interface required by this type of engines. The hydrodynamic pressure sub-model will then be integrated in a complete OCR simulation code that could be used to predict trends for oil leakage, friction and wear. In parallel, an experimental setup will be built to validate the model and OCR performance by measuring oil consumption and oil film thickness in a representative controlled environment.