Please use this identifier to cite or link to this item: http://bura.brunel.ac.uk/handle/2438/24360
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dc.contributor.authorBlanco, E-
dc.contributor.authorOmairey, SL-
dc.contributor.authorLuque, R-
dc.contributor.authorBarrientos, JM-
dc.contributor.authorFerrera, E-
dc.contributor.authorKazilas, M-
dc.date.accessioned2022-03-28T15:38:11Z-
dc.date.available2022-03-28T15:38:11Z-
dc.date.issued2022-02-15-
dc.identifier.citationBlanco, E. et al. (2022) ‘Jig-less end-effector system for automating exhausting composite fuselage assembly tasks’, IOP Conference Series: Materials Science and Engineering. 1226 (1), 012005, pp. 1-8. doi:10.1088/1757-899x/1226/1/012005.en_US
dc.identifier.issn1757-8981-
dc.identifier.urihttps://bura.brunel.ac.uk/handle/2438/24360-
dc.descriptionCollections: Brunel Composite Centre-
dc.description.abstractCopyright © the author(s) 2022. In this study, the jig-less end-effector system developed to assemble components of a full-scale multifunctional integrated composite thermoplastic lower fuselage section is tested and validated. To offset the environmental impact of higher volume of air transport, the aviation industry wants to design lighter and more environmentally friendly aircraft. To achieve this, there is a need to exploit novel materials and technologies. Advanced thermoplastic composites provide an excellent material option thanks to their weldability, low density, low overall production cost, improved fracture toughness and recyclability. However, to fully appreciate their capabilities and benefits, new manufacturing approaches and techniques are needed. Hence, projects such as TCTool, "innovative tooling, end-effector development and industrialisation for welding of thermoplastic components", aim to develop innovative tooling and end-effector systems for the assembly of a multifunctional thermoplastic fuselage. This study presents the development, operation, and testing of the jig-less end-effector system used in the TCTool project for picking, placing, and temporary welding and fixing fuselage's clips and stringers.en_US
dc.description.sponsorshipClean Sky 2 Joint Undertaking under the European Union's Horizon 2020 research and innovation program under grant agreement No. 865131 for TCTool Project, and has been partially funded by the projet “5R – Cervera Network in robotic technologies for intelligent manufacturing”, contract number CER-20211007, under “Centros Tecnológicos de Excelencia Cervera” (founded by “The Centre for the Development of Industrial Technology (CDTI)”).en_US
dc.format.extent1 - 8-
dc.format.mediumPrint-Electronic-
dc.language.isoenen_US
dc.publisherIOP Publishingen_US
dc.rightsCopyright © the author(s) 2022. Content from this work may be used under the terms of the Creative Commons Attribution 3.0 licence. Any further distribution of this work must maintain attribution of the author(s) and the title of the work, journal citation and DOI. Published under licence by IOP Publishing.-
dc.rights.urihttps://creativecommons.org/licenses/by/3.0-
dc.subjectthermoplasticen_US
dc.subjectcompositesen_US
dc.subjectaerospaceen_US
dc.subjectautomationen_US
dc.subjectend-effectoren_US
dc.subjectmanufacturingen_US
dc.titleJig-less end-effector system for automating exhausting composite fuselage assembly tasksen_US
dc.typeConference Paperen_US
dc.identifier.doihttps://doi.org/10.1088/1757-899x/1226/1/012005-
dc.relation.isPartOfIOP Conference Series: Materials Science and Engineering-
pubs.issue1-
pubs.publication-statusPublished-
pubs.volume1226-
dc.identifier.eissn1757-899X-
dc.rights.holderThe author(s)-
Appears in Collections:Dept of Mechanical and Aerospace Engineering Research Papers

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