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MANUFACTURING REQUIREMENTS IN DESIGN: THE RTM PROCESS IN AERONAUTICS

hal.structure.identifierUniversité Sciences et Technologies - Bordeaux 1 [UB]
dc.contributor.authorMOUTON, Serge
hal.structure.identifierUniversité Sciences et Technologies - Bordeaux 1 [UB]
dc.contributor.authorTEISSANDIER, Denis
dc.contributor.authorSEBASTIAN, Patrick
IDREF: 11385692X
dc.contributor.authorNADEAU, Jean-Pierre
dc.date.accessioned2021-05-14T10:02:10Z
dc.date.available2021-05-14T10:02:10Z
dc.date.issued2008
dc.date.conference2008-07
dc.identifier.urihttps://oskar-bordeaux.fr/handle/20.500.12278/78277
dc.description.abstractEnA sub-unit of an aeronautical structure (fuselage, fin, wing, etc.) consists of a set of components fixed rigidly together. One of today's major industrial challenges is to produce these sub-units out of composite materials in order to increase the level of integration and reduce and cost. This article describes a procedure to assist in the industrialisation of aeronautical components produced from composite materials in a design for manufacturing context. In a multi-expertise approach, the problem of optimising integration is combined with the feasibility of injection for the Resin Transfer Molding process. This approach then takes into account admissible manufacturing deviations, defined from a classification of the structure parts. The limits set for admissible deviations guarantee the mechanical behaviour of the assembled component and the requirements of the assembly as a whole. Finally, an industrialisation solutions space is defined. A constraint satisfaction problem solver is used to carry out this research with a spar from a horizontal plane in an aircraft used to illustrate the procedure.
dc.language.isoen
dc.source.title9th international conference on flow processes in composite materials. FPCM-9 [Multimédia multisupport] : 8-10 July, 2008
dc.subject.enResin Transfer Molding (RTM)
dc.subject.enassembly
dc.subject.enresidual stresses
dc.subject.enindustrialisation
dc.subject.enstrain
dc.subject.engeometric specification for non-rigid parts
dc.subject.enConstraint Satisfaction Problem (CSP) solver
dc.title.enMANUFACTURING REQUIREMENTS IN DESIGN: THE RTM PROCESS IN AERONAUTICS
dc.typeCommunication dans un congrès avec actes
dc.subject.halSciences de l'ingénieur [physics]/Matériaux
dc.subject.halSciences de l'ingénieur [physics]/Mécanique [physics.med-ph]
dc.subject.halSciences de l'ingénieur [physics]/Mécanique [physics.med-ph]/Génie mécanique [physics.class-ph]
dc.subject.halPhysique [physics]/Mécanique [physics]/Génie mécanique [physics.class-ph]
bordeaux.page8p.
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.countryCA
bordeaux.title.proceeding9th international conference on flow processes in composite materials. FPCM-9 [Multimédia multisupport] : 8-10 July, 2008
bordeaux.peerReviewedoui
hal.identifierhal-00971367
hal.version1
hal.origin.linkhttps://hal.archives-ouvertes.fr//hal-00971367v1
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