Automated manufacture of 3D reinforced aerospace composite structures

Purpose - The purpose of this paper is to focus on exploring an innovative combination of cutting-edge technologies to be implemented within automated processes for composite parts manufacturing. The objective is the design of a production route for components with tailored fibre orientation and ply...

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Veröffentlicht in:International journal of structural integrity 2012-01, Vol.3 (1), p.22-40
Hauptverfasser: Dell'Anno, Giuseppe, Partridge, Ivana, Cartié, Denis, Hamlyn, Alexandre, Chehura, Edmon, James, Stephen, Tatam, Ralph
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container_end_page 40
container_issue 1
container_start_page 22
container_title International journal of structural integrity
container_volume 3
creator Dell'Anno, Giuseppe
Partridge, Ivana
Cartié, Denis
Hamlyn, Alexandre
Chehura, Edmon
James, Stephen
Tatam, Ralph
description Purpose - The purpose of this paper is to focus on exploring an innovative combination of cutting-edge technologies to be implemented within automated processes for composite parts manufacturing. The objective is the design of a production route for components with tailored fibre orientation and ply lay-up, with improved damage tolerance thanks to through-the-thickness reinforcement and integrated health monitoring systems based on optical fibres technology. This study is part of the FP7 project ADVITAC.Design methodology approach - The proposed technologies are described in detail and their compatibility and potential for integration are discussed.A set up for on-line monitoring of infusion and curing processes of carbon epoxy laminates preformed by dry fibre placement technology is proposed, and a preliminary study of their mechanical performance is presented. The possibility of reinforcing through-the-thickness preforms manufactured with dry slit tapes automatically laid-up and consolidated by laser heating is investigated.Findings - Improved knowledge was obtained of interaction compatibility between the discussed technologies and scope for application.Research limitations implications - The paper reports the technical potential and practical feasibility of the proposed integrated production process. Limited quantitative evaluations on the materials performance are provided. The analysis of the technologies involved represents the early outcome of the ongoing ADVITAC project.Practical implications - This study contributes to the identification of a new generation of composite architecture which allows production cost and weight savings while retaining the level of quality suitable for demanding structural applications, with particular relevance to the aerospace field.Originality value - This paper investigates for the first time the practical possibility of designing a single automated process involving dry fibre placement, tufting and optical fibre sensor monitoring for the production of complex composite components.
doi_str_mv 10.1108/17579861211209975
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source Emerald Journals; Standard: Emerald eJournal Premier Collection
subjects Aerospace engineering
Automation
Composite materials
Costs
Crack initiation
Manufacturing
Optics
Robotics
Robots
Sensors
title Automated manufacture of 3D reinforced aerospace composite structures
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