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MANUFACTURING REQUIREMENTS IN DESIGN: THE RTM PROCESS IN AERONAUTICS
hal.structure.identifier | Université Sciences et Technologies - Bordeaux 1 [UB] | |
dc.contributor.author | MOUTON, Serge | |
hal.structure.identifier | Université Sciences et Technologies - Bordeaux 1 [UB] | |
dc.contributor.author | TEISSANDIER, Denis | |
dc.contributor.author | SEBASTIAN, Patrick
IDREF: 11385692X | |
dc.contributor.author | NADEAU, Jean-Pierre | |
dc.date.accessioned | 2021-05-14T10:02:10Z | |
dc.date.available | 2021-05-14T10:02:10Z | |
dc.date.issued | 2008 | |
dc.date.conference | 2008-07 | |
dc.identifier.uri | https://oskar-bordeaux.fr/handle/20.500.12278/78277 | |
dc.description.abstractEn | A 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.iso | en | |
dc.source.title | 9th international conference on flow processes in composite materials. FPCM-9 [Multimédia multisupport] : 8-10 July, 2008 | |
dc.subject.en | Resin Transfer Molding (RTM) | |
dc.subject.en | assembly | |
dc.subject.en | residual stresses | |
dc.subject.en | industrialisation | |
dc.subject.en | strain | |
dc.subject.en | geometric specification for non-rigid parts | |
dc.subject.en | Constraint Satisfaction Problem (CSP) solver | |
dc.title.en | MANUFACTURING REQUIREMENTS IN DESIGN: THE RTM PROCESS IN AERONAUTICS | |
dc.type | Communication dans un congrès avec actes | |
dc.subject.hal | Sciences de l'ingénieur [physics]/Matériaux | |
dc.subject.hal | Sciences de l'ingénieur [physics]/Mécanique [physics.med-ph] | |
dc.subject.hal | Sciences de l'ingénieur [physics]/Mécanique [physics.med-ph]/Génie mécanique [physics.class-ph] | |
dc.subject.hal | Physique [physics]/Mécanique [physics]/Génie mécanique [physics.class-ph] | |
bordeaux.page | 8p. | |
bordeaux.hal.laboratories | Institut de Mécanique et d’Ingénierie de Bordeaux (I2M) - UMR 5295 | * |
bordeaux.institution | Université de Bordeaux | |
bordeaux.institution | Bordeaux INP | |
bordeaux.institution | CNRS | |
bordeaux.institution | INRAE | |
bordeaux.institution | Arts et Métiers | |
bordeaux.country | CA | |
bordeaux.title.proceeding | 9th international conference on flow processes in composite materials. FPCM-9 [Multimédia multisupport] : 8-10 July, 2008 | |
bordeaux.peerReviewed | oui | |
hal.identifier | hal-00971367 | |
hal.version | 1 | |
hal.origin.link | https://hal.archives-ouvertes.fr//hal-00971367v1 | |
bordeaux.COinS | ctx_ver=Z39.88-2004&rft_val_fmt=info:ofi/fmt:kev:mtx:journal&rft.btitle=9th%20international%20conference%20on%20flow%20processes%20in%20composite%20materials.%20FPCM-9%20%5BMultim%C3%A9dia%20multisupport%5D%20:%208-10%20July,%202008&rft.date=2008&rft.spage=8p.&rft.epage=8p.&rft.au=MOUTON,%20Serge&TEISSANDIER,%20Denis&SEBASTIAN,%20Patrick&NADEAU,%20Jean-Pierre&rft.genre=proceeding |
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