Advanced Continuous Tow Shearing in 3D (ACTS3D): Advanced fibre placement technology for manufacturing defect-free complex 3D composite structures

Lead Research Organisation: University of Bristol
Department Name: Aerospace Engineering

Abstract

The aerospace industry is the key sector for growth of the UK economy. The potential market share of the UK, which is specialised in the most complicated and high tech aircraft parts, is estimated to be around $600 billion. This enormous market demand was also driven by the environmental issue, which requires the lightweight composite aircraft structures to meet the future CO2 emission regulations.
The automated fibre placement (AFP) process is the core technology that underpins the UK's aerospace industry. This process can lay up carbon fibre tape (or tow) materials on a three dimensional mould surface using a robotic or a computer-controlled gantry machine at high speed, which is mainly used in the aerospace industry to manufacture composite structural components such as fuselages, wings, and spars. The AFP machine's capability of feeding individual tows at different speeds enables steering the fibres within the tows along curved paths, and such fibre steering allows for manufacturing composite structures with complex geometry as well as realising ultra-high structural efficiency beyond the limit of the conventional straight fibre lay-up design. However, it has a few fundamental limitations in fibre steering to produce complex composite components. First, since the AFP machine steers the fibres by bending the tow tape, fibre-buckling defects are always generated. Second, it needs to frequently cut the tows when laying up on a doubly-curved surface that cannot be perfectly tessellated with the finite width tows, which also creates defects such as fibre discontinuity and resin pockets. Such process-induced defects are a critical barrier that reduces the production speed and complicates the design process in the aerospace industry. Furthermore, as the shape of the composite components becomes more complex, the minimisation of such defects in fibre steering process is getting more important.
This project aims to develop a new game-changing fibre placement technology that can produce defect-free doubly-curved composite components, based on fundamental understanding of the impregnation and deformation characteristics of tow materials. The new head mechanism to be developed will be capable of producing variable width tows on-the-fly to cover tessellated sections of a complex 3D surface without gaps. The scientific knowledge on tow-level deformation characteristics will be integrated with an advanced head mechanisms as well as a new head control algorithm in order to realise the buckling free fibre steering using the continuous tow shearing mechanism on complex 3D surfaces. Finally, a prototype head will be tested on a robotic platform programmed using the developed head control algorithm, and the lay-up quality and accuracy will be evaluated using various inspection methods. This establishes a proof-of-concept manufacturing process for complex 3D composite components.
Although the industry is making various attempts to solve the quality problems by modifying the process parameters or the tow material, there are no existing AFP technologies that can either steer the tow without defects or control the tow width. The successful development of this unique and disruptive AFP process will provide the UK aerospace industry with a fundamental solution to the quality problems that they are facing, which enable the UK to be at the forefront of next-generation automated composites manufacturing technology.

Planned Impact

The new AFP process to be developed will be a unique and disruptive automated composites manufacturing technology, which enables manufacturing defect-free complex composite components by using a completely different working mechanism from the current technologies. This game-changing technology will benefit the following groups in different aspects.
1) UK's leadership in automated composites manufacturing
Although the UK has the largest market share in European aerospace industry and is well-known for specialised manufacturing capability of most complicated aircraft parts, the industry is highly dependent on foreign manufacturing technologies in automated composites manufacturing. Especially, the UK aerospace industry is investing multi-million pounds for purchasing the AFP machines from abroad. However, they are still struggling to reduce the defect rate in manufacturing complex composite parts. Without paradigm shift in modern AFP technology, they will face more problems, as more complex components will be required in near future.
The ACTS technology to be developed will deliver great impact to the aerospace industry in many aspects. Its unique capability of steering fibre paths on a doubly curved surface without fibre wrinkling and tow gaps will enable the aerospace industry (e.g. Airbus, BAE Systems, Rolls-Royce) to significantly improve the quality of complex composite components such as wing skins, fuselage panels, spars, and fan blades. Furthermore, such capability will also allow for improving structural efficiency of composite aerostructures through shape and fibre path optimisation. The reduced defect rates will lead to increasing the production rate by simplifying the design process.
2) Industrial research facilitators
Although the AFP technology is essential to the key composites manufacturing process of the UK aerospace industry, there are no UK-based AFP machine manufacturers. The national composites centre (NCC) is a great alternative development route to maximise the national benefit. The new AFP technology to be developed in this project will be transferred to the NCC through their technology pull-through mechanism, in order to establish a manufacturing demonstration cell at the NCC. The NCC could provide the end-users with excellent opportunities to try the ACTS technology for their future products in a de-risking environment. This will attract more international partners to the NCC to exploit various other applications of this advanced AFP technology.
3) Academics working in the field of composites
The AFP process-induced defects are the most critical issues to the researchers working in the field of composites design and optimisation. The ACTS technology will enable them to explore more challenging concepts with wider design flexibility without concerns about the process-induced defects. Furthermore, its completely different working mechanism will motivate the manufacturing researchers to think outside the box escaping from the conventional paradigm in the AFP related research. The ACTS will also derive various research topics on non-conventional mechanical behaviours of fibre steered composites in terms of failure, damage tolerance, vibration, and dimensional stability. Many interdisciplinary researches with other international research groups can be created for the application of this new technology so that the students and researchers can take the opportunities to participate in development process of this cutting-edge technology. The trained students and researchers will contribute to encouraging university and industrial people to understand the new technology and its application to different fields of industries. Their expertise will underpin the value-added manufacturing and knowledge economy that directly benefits the UK. Furthermore, by publishing the research outcomes in high-quality international journals, the UK academia will be able to take the lead in composites manufacturing field.

Publications

10 25 50
 
Description In this work, the world's first defect-free fibre steering process using variable width tows on a complex 3D geometry was experimentally demonstrated, which was achieved by further advancing the continuous tow shearing (CTS) technology through the development and integration of the on-the-fly tow width control (TWiC) mechanism and the new head control algorithm.
The Continuous Tow Shearing (CTS) technology is a world's first automated fibre placement (AFP) process that can steer carbon fibre tapes without generating defects. The potential of this CTS process has been successfully demonstrated for flat fibre-steered panels, however a significant further technical development needs to be made for 3D complex shapes. A special robot end-effector that can steer and deposit carbon fibre tapes on a mould surface is used, and the robot's movement is the key in achieving high fibre steering quality. For 2D fibre steering, the robot movement is straightforward compared to conventional processes. However, for 3D fibre steering, the movement should be completely different from the conventional way of controlling the robot movement.
In this project, the 3D deformation characteristics of the carbon tape material was investigated and a new robot control algorithm to achieve defect-free fibre steering on complex 3D surfaces was developed, which is not possible with any existing AFP machines. The key research element was to characterise the deformation of the carbon fibre tape in 3D and find an optimal way to controlling the deformation boundary. The material characterisation study found that the tape could be modelled as a strip comprising elements of 4 bar links, and by detecting the orientation of the bars, the trajectory and orientation of the robot head as well as the trajectories of the tape edges could be predicted. A special material test fixture was developed and used for studying 2D deformation behaviour of two different carbon fibre tape materials. Through extensive material testing with various processing conditions, it was found that various factors can affect the material's shearing quality: production quality of the tape, processing temperature, shearing rate, and fibre tension.
An improved CTS prototype head with Tow Width Control (TWiC) capability has been successfully developed through this project and implemented in the Advanced CTS process and used in combination with a novel head control algorithm. The developed head was mounted on an industrial robot and the hardware and software interfaces between the robot controller and the head controller were established. Through a series of fibre-steering process on a doubly-curved complex shape, the developed head control algorithm was successfully demonstrated. The result experimentally proved that 3D-CTS can produce high-quality 3D composite parts without defects. And, 3D fibre-steering was also possible while resolving one of the most critical problems in AFP layups. Furthermore, we also successfully demonstrate that composite parts with complex 3D surfaces, which was impossible to produce without gaps or overlaps, can be produced through ACTS-3D process (Advanced CTS) with tow width control capability. The TWiC allowed for perfectly tessellate a complex doubly-curved surface using variable width tapes.
Exploitation Route The study on the deformation characteristics of carbon fibre tape materials will be extremely useful to other research groups who are focusing on the simulation of the current automated fibre placement process. Since there has been no suitable characterisation method, people have been using the properties of large pre-impregnated carbon fibre sheets, which might not be enough to simulate complicated 'fibre-steering' process. For other research groups working on automated composites manufacturing could get useful ideas about what the most important material parameters are as well as how important the movement of the robot is for achieving high-quality AFP process. The layup quality inspection method is also novel, which could be a great reference for people who are doing similar research. Furthermore, the new manufacturing capability (i.e. tow width control, 3D CTS) will inspire researchers working on composites design optimisation by allowing them to explore the design space that has never been explored in the past due to the limitation of the current AFP technology.
Sectors Aerospace

Defence and Marine

Manufacturing

including Industrial Biotechology

 
Description The current automated fibre placement processes face a significant challenge due to process-induced defects, hindering the production of high-quality composite aerospace parts at a low cost. The ACTS3D technology developed in this research shows promising potential in overcoming such defect issues. It enables the creation of high-performance composite structures, embraced by fibre-steered design, with highly complex geometries that were not manufacturable using any existing automated fibre placement technologies without defects. Layup tests on a complex doubly-curved surface successfully showcased the advantages of the three key features of the ACTS3D technology. A conformable compaction shoe mechanism and a novel 3D head control algorithm, developed within this project, realised Continuous Tow Shearing on a 3D shape, resulting in a 3D fibre-steered preform without overlaps/gaps and wrinkling. Additionally, the inline tow width control mechanism integrated into the head enabled defect-free fibre steering on surfaces that cannot be tessellated using finite-width tapes, significantly broadening the design possibilities for fibre-steered high-performance composite structures. This technology paves the way for manufacturing 3D complex composite components vital in the aerospace industry, such as fan blades, wing skins, and spars, without defects. Its introduction will streamline the design process by eliminating the need to account for defect-induced effects on mechanical properties during the design phase. Furthermore, it will foster wider adoption of non-conventional composite designs, particularly fibre-steered designs, in both industry and academia.
Sector Aerospace, Defence and Marine,Manufacturing, including Industrial Biotechology
Impact Types Societal

Economic

 
Description Advanced continuous tow shearing process for manufacturing defect-free complex composite parts
Amount £40,000 (GBP)
Funding ID 2096016 
Organisation Engineering and Physical Sciences Research Council (EPSRC) 
Sector Public
Country United Kingdom
Start 08/2018 
End 03/2023
 
Description ABB robotics 
Organisation ABB Group
Country Switzerland 
Sector Private 
PI Contribution Technical presentations in the advisor board meetings, exploring collaboration opportunities
Collaborator Contribution Discount of a robot training course, ad-hoc technical support
Impact N/A
Start Year 2019
 
Description Airbus - UoB 
Organisation Airbus Group
Department Airbus Operations
Country United Kingdom 
Sector Private 
PI Contribution Technical presentation at the advisory board meeting, enhancing their understanding of the new tow termination technology and its advantage against conventional methods
Collaborator Contribution Attendance of the advisory board meetings, provision of technical information about potential applications
Impact N/A
Start Year 2017
 
Description BAE Systems 
Organisation BAE Systems
Country United Kingdom 
Sector Academic/University 
PI Contribution Technical presentations in the advisor board meetings, exploring collaboration opportunities, enhancing their understanding of the new technology and its advantages
Collaborator Contribution Attendance of the advisory board meetings, technical discussions
Impact N/A
Start Year 2017
 
Description National Composites Centre 
Organisation National Composites Centre (NCC)
Country United Kingdom 
Sector Private 
PI Contribution Technical presentations in the advisor board meetings, exploring collaboration opportunities, enhancing their understanding of the new technology and its advantages
Collaborator Contribution Attendance of the advisory board meetings
Impact N/A
Start Year 2017
 
Description IP discussion meeting with iCOMAT 
Form Of Engagement Activity A formal working group, expert panel or dialogue
Part Of Official Scheme? No
Geographic Reach Local
Primary Audience Industry/Business
Results and Impact UoB team visited iCOMAT and some of the project outcomes were discussed with their engineers and company directors to see if there is any IP that can be commercialised. An NDA between the UoB and the company was made before the meeting. In the meeting, they appreciated the outstanding 3D layup quality based on a novel 3D head control algorithm and there were in-depth discussions on the detail of the process and its industrial potential. But they concluded that it would be rather difficult to protect it for commercial use. It was a great opportunity to share the knowledge and experience with the company and motivate the team members by the positive feedback from the company.
Year(s) Of Engagement Activity 2022
 
Description Presentation in a technical workshop jointly organised by the PI and Embraer SA 
Form Of Engagement Activity A talk or presentation
Part Of Official Scheme? No
Geographic Reach International
Primary Audience Professional Practitioners
Results and Impact The technical workshop focused on aeroelastic tailoring design, drawing attendance from 27 participants including academics, researchers, and industry professionals from various international universities, research organizations, and companies. The Principal Investigator (PI) introduced the Advanced Continuous Tow Shearing in 3D developed in this project. The presentation garnered positive feedback from the audience, primarily composed of professionals specialising in design, simulation, and optimisation. It offered a comprehensive insight into the novel manufacturing process, showcasing its potential to enable aeroelastic tailoring through defect-free fibre steering technology. This presentation inspired attendees to broaden their design horizons and consider the manufacturability of their innovative designs.
Year(s) Of Engagement Activity 2023