An investigation into engineered thermoplastic polymer composite filament for through thickness reinforcement of laminated carbon fibre composites.

Lead Research Organisation: University of Ulster
Department Name: School of Engineering

Abstract

Laminated composites from dry carbon fibre preforms are increasingly being used to produce primary structures in several industries. However, the poor performance in the out-of-plane (through the thickness) direction, and delamination has been a cause of concern, requiring the careful analysis of load paths to limit out-of plane stress. Furthermore, this has a limiting effect on the design freedom for composite components and could challenge the use of composites for future aerodynamic or structural concepts. Several 'first-generation' methods have been proposed to improve out-of-plane performance including z-pinning, selective interlayers and hybrids, protective layers or resin toughening; one method that is becoming increasingly successful is to reinforce composites with a fibre that connects the layers together running from the upper to lower surface of the laminate. This method shows potential but has been limited by the lack of suitable materials available for through-thickness reinforcement where we have hitherto been limited to carbon fibre, glass, basalt, Aramid or other polymeric fibres. Also, there is a limited understanding of the mechanisms involved in out-of-plane rate-dependent response of composite materials. This proposal aims to develop a new understanding of through-thickness reinforcement and to research a method to produce composites with a through-thickness response which is designer defined. This will be done by placing a 'second-generation' manufactured yarn with optimised properties in the through-thickness direction, thereby enabling the design of optimum Ez (laminate through-thickness Young's modulus) for a given loading scenario. The new yarn will be made by compounding extrusion of a thermoplastic monofilament reinforced with carbon fibres of specified length, optimising material and process parameters, and using these yarns as through-thickness reinforcement in carbon fibre/epoxy laminates. The performance will be characterised and a predictive analytical elastic stiffness model will be developed. Also, the visco-elastic properties of the new through thickness yarn will be related to the transverse impact performance of the laminated composite. These subjects have not been previously researched and if successful, the results could be transformative and generate global impact for UK composites research and industry. In the future the research will benefit aerospace companies; with the proposed enhanced out-of-plane performance they could potentially design a pressurised blended wing, composite lug arrangement, stringer to skin interface and run-out, buckling critical locations, high impact locations, etc.

Planned Impact

This project will potentially benefit many users of composite materials as structural load carrying elements, or as blast-protection products. In the future, the research will directly benefit UK aerospace companies; with the proposed enhanced out-of-plane performance they could potentially design a composite lug arrangement, stringer to skin interface and run-out, buckling critical locations, high impact locations, etc. The enhanced properties mean that the knock-down factors applied to the design such as barley viable impact damage (BVID) will be reduced. Also, initial research has shown that notch sensitivity and stress concentration caused by open-holes is reduced. Currently, the overall structural weight of an aircraft is increased by over 10% to allow for these factors. By developing new materials and understanding, the designers will be able to reduce this conservatism, reduce weight of the airframe and therefore, fuel burn. This will have a greater environmental impact with reduction in greenhouse gas. Furthermore, new ultra-efficient aircraft designs such as the Boeing X-48C Blended Wing Body Research Aircraft (Environmentally Responsible Aviation project) might not be feasible with existing composite laminates due to the large out-of-plane stresses the composite pressurised blended wing would experience. This research therefore, is vital for the UK at this time. These new aircraft will reduce community noise, fuel burn and nitrogen oxides (NOx) emissions. These aircraft might enter service by 2025.
The UK is currently well positioned to benefit economically from these new technologies through the supply chain. A UKTI (UK Trade & Investment) and BIS market report completed in April 2010 and published in 2011 entitled 'UK Composites Supply Chain Scoping Study - Key Findings' estimated that there were 1,500 companies in the UK composites sector producing added value of around £1.1 billion. The UK aerospace industry represents 17% of global market and is the2nd largest globally. The first generation laminated composite primary structures are now flying, so there is an urgent need to develop new performance and a move away from the current 2D design strategies. This could be realised in the medium term during a re-engineering of the existing aircraft in search of fuel efficiency (5 years) or on the next generation aircraft (10 years). This project however will aid development of composites structure capability in sectors other than aerospace. With the proposed new through thickness yarn and preforming methods, the automotive industry could increase deposition rates of composite materials, therefore reducing manufacturing costs. Through the proposed Pathways to impact, the information generated in this project will also be disseminated to the marine industry through an existing KTP, the renewables sector through a Marie Curie programme, and could influence existing DSTL research undertaken at University of Ulster.

Publications

10 25 50
 
Description To date we have produced and characterised a range of (including high temperature) polymer yarns which have been used to stitch carbon fibre laminates together to provide through thickness reinforcement and improve delamination resistance. In addition we have also researched and produced multi-filament yarns. The yarns have been sent to Institut für Flugzeugbau for tufting trials and will then be tested at Ulster University and in collaboration with other research centres.
Exploitation Route We are currently working on 2 comference papers and will develop 2 Journal papers. The developed yarns will be supplied to other research programmes such as the ICONIC EU H2020 programme. ICONIC is a multinational Marie Sklodowska-Curie Innovative Training Network (ITN) funded by the European Union's Horizon 2020 programme.
Sectors Aerospace, Defence and Marine,Leisure Activities, including Sports, Recreation and Tourism,Transport

URL https://www.researchgate.net/project/Novel-stitching-yarn-to-improve-the-interlaminar-mechanical-properties-of-fibre-reinforced-polymer-composites
 
Description Axis Composites Ltd and Bombardier Aerospace are currently using some of the stitching material produced in the grant to trial for further work. Other automotive companies have also expressed an interest in the potential.
First Year Of Impact 2015
Sector Aerospace, Defence and Marine,Energy,Transport
Impact Types Economic

 
Description DEL PhD
Amount £30,000 (GBP)
Organisation Government of Northern Ireland 
Department Department for Employment and Learning Northern Ireland (DELNI)
Sector Public
Country United Kingdom
Start 10/2016 
End 10/2019
 
Description EU Marie Curie
Amount € 2,500,000 (EUR)
Funding ID FP7 - 612531 
Organisation Marie Sklodowska-Curie Actions 
Sector Academic/University
Country Global
Start 02/2014 
End 01/2018
 
Description NIACE Complex Preforming
Amount £100,000 (GBP)
Organisation Invest Northern Ireland 
Sector Public
Country United Kingdom
Start 10/2015 
End 04/2017
 
Description RESEARCH FELLOWSHIP SCHEME
Amount £59,000 (GBP)
Organisation Ulster University 
Sector Academic/University
Country United Kingdom
Start 01/2015 
End 12/2017
 
Description The Future Composites Manufacturing Hub
Amount £49,942 (GBP)
Organisation Engineering and Physical Sciences Research Council (EPSRC) 
Sector Academic/University
Country United Kingdom
Start 04/2019 
End 11/2019
 
Description Athlone Institute of Technology 
Organisation Athlone Institute of Technology
Country Ireland 
Sector Academic/University 
PI Contribution Ulster University visited Athlone Institute of Technology and worked with them on extrusion trials. The yarns were supplied to Ulster for stitching and weaving trials.
Collaborator Contribution Athlone Institute of Technology let us use their Eurotech single screw extruder with fibre spinning set-up.
Impact A paper will be published soon.
Start Year 2016
 
Description Bombardier Aerospace 
Organisation Bombardier Inc.
Country Canada 
Sector Private 
PI Contribution We supplied tufted preforms using a range of our materials developed during the process. We will also test these plaques and share the data with Bombardier.
Collaborator Contribution Bombardier have used their RTI process to infuse further test plaques for this project.
Impact None to date but will be presented in the next year.
Start Year 2017
 
Description Institut für Flugzeugbau - Faserverbundtechnologie 
Organisation University of Stuttgart
Department Institute of Aircraft Design
Country Germany 
Sector Academic/University 
PI Contribution Ulster University manufactured a range of stitching yarns and sent them to Institut für Flugzeugbau . At the Institut für Flugzeugbau the yarns were used to tuft carbon fibre preforms which will be tested soon.
Collaborator Contribution Ulster provided the polymer yarns and Carbon Fibre. Institut für Flugzeugbau provided in-kind tufting of the preforms.
Impact 2 members from Ulster visited Institut für Flugzeugbau and further collaboration is expected.
Start Year 2017