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dc.contributor.authorPIERRE, Laurent
dc.contributor.authorTEISSANDIER, Denis
dc.contributor.authorNADEAU, Jean-Pierre
dc.date.accessioned2021-05-14T09:58:10Z
dc.date.available2021-05-14T09:58:10Z
dc.date.created2010
dc.date.issued2010
dc.date.conference2010-10-20
dc.identifier.urihttps://oskar-bordeaux.fr/handle/20.500.12278/77933
dc.description.abstractEnThe performance of a turboshaft engine derives essentially from the performance of the turbine, which in turn is closely correlated with rotor/stator clearance at the blade tips. In this article we propose to define criteria for qualifying turbine architectures based on a geometric model which integrates variability due to the processes of obtaining parts, the assembly processes and the thermomechanical behaviour of the turbine. The geometric model proposed here integrates thermomechanical strains in 3D dimension-chains formalised by operations on polytopes (Minkowski sum and intersection).
dc.language.isoen
dc.subject.engeometric variability
dc.subject.entolerancing analysis
dc.subject.enthermomechanics
dc.subject.enperformance criteria
dc.title.enQualification of turbine architectures in a multiphysical approach: application to a turboshaft engine
dc.typeCommunication dans un congrès avec actes
dc.subject.halPhysique [physics]/Mécanique [physics]/Génie mécanique [physics.class-ph]
bordeaux.hal.laboratoriesInstitut de Mécanique et d’Ingénierie de Bordeaux (I2M) - UMR 5295*
bordeaux.institutionUniversité de Bordeaux
bordeaux.institutionBordeaux INP
bordeaux.institutionCNRS
bordeaux.institutionINRAE
bordeaux.institutionArts et Métiers
bordeaux.countryFR
bordeaux.title.proceeding9th International Conference of IDMME - Virtuazl Concept
bordeaux.conference.cityBordeaux
bordeaux.peerReviewedoui
hal.identifierhal-01094175
hal.version1
hal.origin.linkhttps://hal.archives-ouvertes.fr//hal-01094175v1
bordeaux.COinSctx_ver=Z39.88-2004&rft_val_fmt=info:ofi/fmt:kev:mtx:journal&rft.date=2010&rft.au=PIERRE,%20Laurent&TEISSANDIER,%20Denis&NADEAU,%20Jean-Pierre&rft.genre=proceeding


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