Journal of large-scale research facilities, 2, A66 (2016) http://dx.doi.org/10.17815/jlsrf-2-125 Published: 18.04.2016 EVo: Net Shape RTM Production Line Deutsches Zentrum für Luft- und Raumfahrt e.V., Institut für Faserverbundleichtbau und Adaptronik, Zentrum für Leichtbauproduktionstechnologie * Instrument Scientists: - Sven Torstrick, Deutsches Zentrum für Luft- und Raumfahrt e.V. (DLR), Zentrum für Leichtbaupro- duktionstechnologie (ZLP), phone: +49 531 295-3707, email: Sven.Torstrick@dlr.de - Dr.-Ing. Felix Kruse, Deutsches Zentrum für Luft- und Raumfahrt e.V. (DLR), Zentrum für Leicht- bauproduktionstechnologie (ZLP), phone: +49 531 295-3700, email: felix.kruse@dlr.de - Prof. Dr.-Ing. Martin Wiedemann, Deutsches Zentrum für Luft- und Raumfahrt e.V. (DLR), Institut für Faserverbundleichtbau und Adaptronik (FA), phone: +49 531 295-2300, email: martin.wiedemann@dlr.de Abstract: EVo research platform is operated by the Center for Lightweight-Production-Technology of the German Aerospace Center in Stade. Its objective is technology demonstration of a fully automated RTM (Resin Transfer Molding) production line for composite parts in large quantities. Process steps include cutting and ply handling, draping, stacking, hot-forming, preform-trimming to net shape, resin injection, curing and demolding. 1 Introduction In order to increase fuel e�ciency, the development of light and innovative structural components in the aerospace industry is at all times a fundamental aim which is pushed by the use of �ber reinforced plas- tics. The demand for a holistic approach in the �elds of composites also drives the German Aerospace Center’s (DLR) Institute of Composite Structures and Adaptive Systems. The institute closed the gap between basic research and industrial application by opening the Center for Lightweight Production Technology (ZLP) in Stade and Augsburg in the year 2010. Its thematic priority is the development of optimized, reliable, productive and, hence, also cost e�ective production processes. The focus is not only on production of large scale part geometries, but also on technologies that allow large production rates for smaller parts, such as typical frames of aircraft fuselages or automotive parts. Project EVo (Endkonturnahe Volumenbauteile – net shaped parts in large quantities) addressed this approach and launched an automated production line for RTM-parts. *Cite article as: DLR-FA & DLR-ZLP. (2016). EVo: Net Shape RTM Production Line. Journal of large-scale research facilities, 2, A66. http://dx.doi.org/10.17815/jlsrf-2-125 1 http://jlsrf.org/ http://dx.doi.org/10.17815/jlsrf-2-125 http://dx.doi.org/10.17815/jlsrf-2-125 https://creativecommons.org/licenses/by/4.0/ Journal of large-scale research facilities, 2, A66 (2016) http://dx.doi.org/10.17815/jlsrf-2-125 2 EVo - plant concept In order to achieve a fully automated production of complex composite parts in high rates, an RTM (Resin Transfer Molding) process most suitable with respect to cycle times and cost. Before the actual RTM-process – mainly consisting of resin injection into a closed mold and curing at high temperatures – can take place, the so called preform has to be produced. Preforms are consolidated stacks of carbon fabrics that already roughly have the 3D shape of the �nished part. State of the art is production of oversized parts that get machined, inspected and edge sealed as post processes. EVo’s approach is to eliminate post processing such as edge sealing and instead perform net shape trimming and quality inspection in line. Trimming preforms to net shape before injection has some advantages compared to post processing. Tool abrasion can be minimized due to waiving the grinding of a cured composite part, micro-fractures can be avoided and a more robust injection is realized because the preform �ts in the mold’s cavity more precisely, thereby a pre running of the resin around the preform’s edges can be avoided, having a lower risk of dry spots. For a precise trimming, though, it must be ensured that the preforms geometry is very close to that of the cured part, because e.g. in case of a further compaction inside the RTM-mold, the preform’s edges will no longer be net shaped, but somewhat distorted. To prevent that, both draping and hotforming have to be performed very accurate. Since the target part has a curved pro�le geometry, all layers must be draped one by one, because otherwise wrinkles and ondulations might occur at the inner layers. EVo’s in-situ-NDI detects defects in �ber angle orientation by an eddy current measurement and analyses the preform’s net shape by means of a laser scan. The degree of shear deformation during draping and hotforming can be examined by an “Argus” optical measurement. Figure 1: CAD-overview of EVo - research platform. 3 Sub processes In the following the main sub processes and used machinery is described in main segments of ply preparation, preforming and RTM. 2 http://dx.doi.org/10.17815/jlsrf-2-125 https://creativecommons.org/licenses/by/4.0/ http://dx.doi.org/10.17815/jlsrf-2-125 Journal of large-scale research facilities, 2, A66 (2016) 3.1 Ply preparation NCF (non crimped fabrics) or woven carbon fabrics on rolls get inserted into the process line on mag- azine racks of 3 rolls each. Up to 6 di�erent materials can be processed into one part. Material rolls get transferred towards an uncoiling unit and fed towards a cutter. All plies are cut out of the material and stored inside drawers. Thus it is not necessary to exchange rolls because of a part layup that contains di�erent material in each layer. Individual plies then are picked out of the drawer-storage and placed on a transfer table. Technical data: • material storage with exchangeable magazines for 2x3 rolls of 100“ max. width • automatic roll transfer to cutter • Zünd-Cutter (3200mm x 2700mm) with variable tools for cutting, punching, grinding, plotting • ply-storage with automated drawers, pick and place portal-robot Figure 2: Cutter, storage and ply handling. 3.2 Preforming EVo’s preforming segment contains the process steps draping, hot forming and trimming to net shape as well as preform handling and robotic quality inspection. Figure 3: Preforming segment. 3 http://dx.doi.org/10.17815/jlsrf-2-125 https://creativecommons.org/licenses/by/4.0/ Journal of large-scale research facilities, 2, A66 (2016) http://dx.doi.org/10.17815/jlsrf-2-125 3.2.1 Pick and drape Plies on the transfer table are detected by a camera that forwards the actual position on the table as an o�set to the draping robots picking-program. The robot drapes the ply onto a vacuum assisted preforming-mold and stacks a sub preform. Once the sub preform stacking is completed, it is transferred to the consolidation-mold. A DLSR-camera linked to an “Argus”-optical measurement system evaluates the draping itself by analyzing the ply’s deformation and is also mounted on the robots head. Single plies are locally �xed be electric binder activation. Technical data draping robot: • Reis- RV240-180 on linear axis • VITRONIC - optical detection of ply positioning • FASTcurve - o�ine programming • �exible, active draping-gripper • ARGUS - optical drape analysis • local electric binder activation Figure 4: Robot with draping-gripper and mold. 3.2.2 Hot forming Sub preforms as well as the complete preform are consolidated during the hotforming process. A mem- brane applies vacuum and additional air pressure to the preform while IR-rays melt the textile’s binder particles. The result is a sti� preform. Technical data hotforming: • Bürkle Membrane Press • hotforming / consolidation of subpreforms • IR- heating • 2m x 2,5 m • vacuum and additionally 4 bar air pressure • automatic membrane feeding 4 http://dx.doi.org/10.17815/jlsrf-2-125 https://creativecommons.org/licenses/by/4.0/ http://dx.doi.org/10.17815/jlsrf-2-125 Journal of large-scale research facilities, 2, A66 (2016) Figure 5: Hot forming. 3.2.3 Preform handling / NDI As a quality gate, an eddy current measurement detects the local �ber angle orientation throughout 5-6 layers in depth. While measuring every sub preform after each hotforming step, the �ber orientation of every layer can be visualized. The preform afterwards is transferred to net shape trimming. Technical Data Handling / NDI - Robot • wall mounted Reis RVL130 on linear axis • FASTcurve - o�ine programming • Eddy-Cus - �bre angle measurement • preforminsertion and partdemolding with vacuum grippers • automatic cleaning and sealing of RTM-mold (coming soon) • Schunk quick-change system Figure 6: Eddy current measurement. 5 http://dx.doi.org/10.17815/jlsrf-2-125 https://creativecommons.org/licenses/by/4.0/ Journal of large-scale research facilities, 2, A66 (2016) http://dx.doi.org/10.17815/jlsrf-2-125 3.2.4 Trimming to net shape A high accuracy portal robot equipped with an ultrasonic knife trims the preform’s edges into net shape. After the residue is collected by a needle gripper, a laser scans the preform’s topology to determine its thickness Technical data trimming robot • Reis portal robot RLP16 • FASTcurve – o�ine programming • EM-Systeme – ultrasonic knife • Renishaw – referencing system • laser – topology scan • laserready safety housing • vacuum assisted mold Figure 7: Net shape trimming (left) and laser scan (right). 3.3 RTM RTM processes for aerospace applications usually mean cycle times of 4 hours and more. The mold must be prepared with seals and release agent, the preform has to be positioned, the mold is closed and heated up with a pre-de�ned ramp, then held for a given time before and during injection. After injection the mold is heated up to curing temperature and hours later cooled down under de�ned conditions. Both, heating times and curing time are the major bottlenecks for the achievable cycle times in an RTM- process. In order to cut these times to a minimum, EVo’s RTM-section uses transportable core molds and �xed shell molds that contain heating circuits. Using transportable molds, an isothermal process can be realized. Outside the press, in a lifting station, the hot mold is opened and a robot prepares the mold and inserts the preform. It is then transferred into the press for injection. Once the resin has reached a certain degree of cure, the still closed mold is transported to a curing oven. Thus, the press occupancy time can be reduced from 4-5 hours to only 30-40 minutes. Technical data RTM unit • injection Unit (1K / 2K, 60 bar max. auto coupling) • press (500t, 2m x 2,5m press table) • water-based mold heating (200°C max) • RTM mold (�xed shell-mold, movable core-mold) • ultrasonic sensors for curing • curing oven (pyrometer controlled, camera, 2 mold-slots) 6 http://dx.doi.org/10.17815/jlsrf-2-125 https://creativecommons.org/licenses/by/4.0/ http://dx.doi.org/10.17815/jlsrf-2-125 Journal of large-scale research facilities, 2, A66 (2016) Figure 8: RTM-section containing transport system, opening station, press and cure oven (f.l.t.r.). Figure 9: Two-component injection unit with automated docking system. References Grohmann, F., Y. und Zacharias. (2014). Electrical resistsnce heating - a method for binder activation in CFRP processing? In ECCM16 - 16th European Conference on Composite Materials. Sevilla, Spain. (22. - 26. June 2014) Heuer, H., Schulze, M., Pooch, M., Gäbler, S., Nocke, A., Bardl, G., . . . Petrenz, S. (2015). Re- view on quality assurance along the {CFRP} value chain – non-destructive testing of fabrics, pre- forms and {CFRP} by {HF} radio wave techniques. Composites Part B: Engineering, 77, 494 - 501. http://dx.doi.org/10.1016/j.compositesb.2015.03.022 Hindersmann, A. and Exner, W. and Liebers, N. and Opitz, M. and Torstrick, S. and Ucan, H. (2012). Forschungsplattform für endkonturnahe Faserverbund-Bauteile im automatisierten Ferti- gungsprozess. In Deutscher Luft- und Raumfahrtkongress 2012. Braunschweig, Deutschland. (Docu- mentID: 281289) 7 http://dx.doi.org/10.17815/jlsrf-2-125 http://dx.doi.org/10.1016/j.compositesb.2015.03.022 https://creativecommons.org/licenses/by/4.0/ Introduction EVo - plant concept Sub processes Ply preparation Preforming Pick and drape Hot forming Preform handling / NDI Trimming to net shape RTM