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dc.contributor.advisorTian Tian.en_US
dc.contributor.authorPicard, Mathieuen_US
dc.contributor.otherMassachusetts Institute of Technology. Department of Mechanical Engineering.en_US
dc.date.accessioned2014-12-08T18:54:04Z
dc.date.available2014-12-08T18:54:04Z
dc.date.copyright2014en_US
dc.date.issued2014en_US
dc.identifier.urihttp://hdl.handle.net/1721.1/92169
dc.descriptionThesis: Ph. D., Massachusetts Institute of Technology, Department of Mechanical Engineering, 2014.en_US
dc.descriptionCataloged from PDF version of thesis.en_US
dc.descriptionIncludes bibliographical references (pages 341-344).en_US
dc.description.abstractRotary engines offer higher power density, fewer parts and lower vibrations than conventional reciprocating piston engines. However, rotary engines are more difficult to seal because of the rotor shape which leads to higher gas leakage and oil consumption resulting in lower efficiency and higher emissions. In order to address this problem, this thesis presents a set of multiscale models to assess rotary engine performances by estimating gas leakage, oil consumption, wear and friction. An oil seal multiscale model is developed to estimate internal oil consumption guided by oil transport visualization experiments carried using a laser-induced fluorescence technique. A finite element beam model is used to predict the clearance between the oil seals and the side housing for each crank angle in the cycle. From seal-housing clearance, oil transport through the oil seals is calculated using a control volume approach. The main mechanism leading to internal oil consumption is outward scraping of the oil seals due to a lack in conformability of the seals to the distorted side housing, especially next to the intake and exhaust ports. A set of multiscale models are developed for the performance of the apex and side seals. The models are formulated to couple gas flow to the dynamics and deformation of the seals while accurately describing the interfaces between the seals and their profile and groove. The models are used to predict apex and side seal behavior and understand the mechanisms leading to gas leakage. The main leakage mechanisms identified are leakage through (1) the corner seal clearance, (2) the spark plug holes, (3) the flanks of the seals at high speed, and (4) the side piece corner for the apex seals and at the ends of the side seals. The apex seal model shows good agreement with experiments, especially for the pressure in the apex seal groove. It is the first time such comprehensive models are developed for rotary engines and they will be valuable tools to help design more efficient and environment-friendly rotary engines.en_US
dc.description.statementofresponsibilityby Mathieu Picard.en_US
dc.format.extent357 pagesen_US
dc.language.isoengen_US
dc.publisherMassachusetts Institute of Technologyen_US
dc.rightsM.I.T. theses are protected by copyright. They may be viewed from this source for any purpose, but reproduction or distribution in any format is prohibited without written permission. See provided URL for inquiries about permission.en_US
dc.rights.urihttp://dspace.mit.edu/handle/1721.1/7582en_US
dc.subjectMechanical Engineering.en_US
dc.titleDevelopment of multiscale models for the performance of the gas and oil seals in rotary enginesen_US
dc.typeThesisen_US
dc.description.degreePh. D.en_US
dc.contributor.departmentMassachusetts Institute of Technology. Department of Mechanical Engineering
dc.identifier.oclc897134064en_US


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