Thank you for visiting nature.com. You are using a browser version with limited support for CSS. To obtain the best experience, we recommend you use a more up to date browser (or turn off compatibility mode in Internet Explorer). In the meantime, to ensure continued support, we are displaying the site without styles and JavaScript.
Scientific Reports volume 6, Article number: 23058 (2016 ) Cite this article
We have developed a method for the three-dimensional (3D) printing of continuous fiber-reinforced thermoplastics based on fused-deposition modeling. The technique enables direct 3D fabrication without the use of molds and may become the standard next-generation composite fabrication methodology. A thermoplastic filament and continuous fibers were separately supplied to the 3D printer and the fibers were impregnated with the filament within the heated nozzle of the printer immediately before printing. Polylactic acid was used as the matrix while carbon fibers, or twisted yarns of natural jute fibers, were used as the reinforcements. The thermoplastics reinforced with unidirectional jute fibers were examples of plant-sourced composites; those reinforced with unidirectional carbon fiber showed mechanical properties superior to those of both the jute-reinforced and unreinforced thermoplastics. Continuous fiber reinforcement improved the tensile strength of the printed composites relative to the values shown by conventional 3D-printed polymer-based composites.
Three-dimensional (3D) printing1,2,3 or additive manufacturing4,5,6 enables the fabrication of near-net-shaped complex 3D parts without expensive molds or tools in short periods of time, based on 3D computer-aided design (CAD) data. 3D printing is expected to revolutionize the manufacturing of components. While several 3D printing systems are available4,6, printing based on fused-deposition modeling (FDM) using thermoplastics7,8,9 is particularly widespread because of the simplicity and potential applicability of the method. However, the mechanical properties of products fabricated by conventional FDM 3D printing are inherently poor because of the thermoplastic resins10,11 used, although the optimization of processing parameters, such as the lamination direction and laminate thickness, has been investigated for improving the mechanical properties of thermoplastic resin parts12. 3D printing has primarily been used for trial products or toys, without application to the manufacture of structural components for aerospace or automotive products. Broadening the applicability of 3D printing to obtain mechanically strong components for aerospace and automotive structures is a major goal of industrial fabrication.
Carbon-fiber composites show good mechanical performance because they incorporate the attributes of carbon fibers, which show high strength and stiffness, with those of polymer resins or metals. Fiber-reinforced thermoplastic (FRTP) composites can be applied in passenger automobiles to achieve high recyclability and load-bearing capability13. “Green” composites, based on natural fibers derived from plants and biodegradable resins, are in high demand to meet regulatory requirements of recyclability14,15,16. However, the conventional fabrication methods for composites require expensive facilities and equipment, such as autoclaves and complex rigid molds, hindering the wide application of composites.
The 3D printing of composite materials with enhanced mechanical properties is under extensive exploration17,18,19,20,21. Various reinforcements, such as carbon black22, reinforcing platelets20 and short fibers including chopped carbon fibers23, polymer fibrils24, carbon nanotubes25,26 and glass fibers27 have been used. In most such studies, the additives were mixed into thermoplastic filaments prior to being loaded into the printer, where the mixture replaced the conventional thermoplastic filament. However, some 3D printers use two printer heads for fabricating composites28. These composites usually show poor mechanical properties compared to composites manufactured by conventional methods, because composites reinforced with short fibers or particles are mechanically inferior to composites reinforced with continuous fibers29,30,31. Some 3D-printed composites are fabricated to achieve specific functionalities outside of mechanical behavior, such as high electric conductivities22,26, low coefficients of thermal expansion and high thermal conductivities32.
To improve the mechanical properties of 3D-printed composites, a printer capable of fabricating continuous fiber-reinforced plastics is much in demand. One 3D printer using a plastic filament impregnated with carbon fibers has been developed33. However, in this process, the resin-fiber combination is predetermined; the selection of any other resin or reinforcing fibers for 3D printing is impossible. If the 3D printing of continuous FRTP of varied materials becomes possible, significant weight-saving can be achieved by optimizing the fiber direction in the printed components. In addition to applications in the automotive and aerospace industries, the technology would be well-suited to manufacture a wide variety of custom products in small quantities, such as load-bearing composite orthopedic implants34 and prosthetic limbs35,36 in the healthcare industry. Realizing the 3D printing of composites could supplant the conventional laborious manufacturing of composites, thus becoming the next-generation standard of composite fabrication (or “Composites 2.0”).
This study investigates the 3D printing of continuous FRTP, which combines fibers and resin in a nozzle based on FDM printing. We refer to composites obtained by direct digital manufacturing (DDM) as Composites 2.0 (as mentioned above) and those obtained by conventional manufacturing as Composites 1.0. A fiber-reinforced plastic obtained by Composites 2.0 technology would be a fully structurally optimized material, with the fiber direction and volume fraction precisely controlled at every location in the composite material. As proofs of concept, we have used straight tows of carbon fibers or twisted yarns of jute fibers as reinforcements in a matrix resin of polylactic acid (PLA). The carbon fiber composites demonstrate excellent mechanical properties, while the jute fiber composites are examples of plant-sourced composites37,38. The test specimens were printed along the longitudinal direction, parallel to the direction of fiber alignment. The mechanical properties of the 3D-printed continuous fiber composites were measured by tensile testing and compared with the performance of neat PLA resin.
Figure 1(a) shows a schematic of the 3D printer head used for the production of continuous FRTP composites by in-nozzle impregnation. The thermoplastic resin filament and reinforcing fibers, i.e., the carbon fiber tow or twisted jute-fiber yarn (Fig. 1(b)), are separately supplied to the printer head. The reinforcing fibers are heated using a nichrome wire before entering the nozzle, to enhance the permeation of the fiber bundles with thermoplastic resin; the heat diffuses to the resin and decreases the viscosity of the PLA. The resin filament is transferred using drive gears and a stepping motor, while the reinforcing fibers are directly supplied to the nozzle. No additional devices are required for feeding the reinforcing fibers, because the fibers are automatically supplied to the head by the movement of the resin filament. The resin filament is melted by the heater inside the printer head, consolidating the reinforcing fibers and the resin in the heated section. The resin-reinforced fibers are extruded from the nozzle and laminated onto a hot table for the layer-by-layer fabrication of solid components. Fig. 1(c) shows the 3D printing process for manufacturing continuous carbon fiber-reinforced composites.
(a) Schematic of the 3D printer head used to produce continuous FRTPs using in-nozzle impregnation based on FDM. (b) Continuous fiber reinforcements used for 3D printing. (c) Photograph of the 3D printing of a CFRTP.
The 3D printer for obtaining continuous-fiber composites was developed by modifying the printer head of the commercially available FDM 3D printer Blade-1 printer with a preheating system. This modified printer was used to print carbon fiber-reinforced thermoplastics (CFRTPs), as shown in supplementary Fig. 1. A modified FlashForge printer was used to print jute fiber-reinforced thermoplastic (JFRTP) green composites (no preheating was used for the JFRTPs to prevent the degradation of the jute fibers). Unmodified PLA was also printed using the Blade-1 printer, as a comparison to measure the mechanical enhancement achieved by reinforcing the resin with continuous fibers. In the Blade-1 printer, the printer head moves along the x and z directions, whereas the hot table moves in the y direction to enable 3D fabrication. The diameter of the resin filament is 1.85 mm, exceeding the 1.4 mm diameter of the nozzle. Hence, the molten resin inside the nozzle is pushed out from the solid resin; the pressure facilitates the impregnation of molten resin into the fiber bundles in the nozzle. Since a large nozzle diameter was used in this pilot study to prevent clogging of the reinforcing fibers, the layer resolution was relatively low.
The PLA filament and carbon or jute fiber bundles were heated to 210 °C in the nozzle, while the temperature of the hot table was set to 80 °C. For CFRTPs and JFRTPs, the fiber/filament feeding speed and nozzle head speed were 100 mm/min and 60 mm/min, respectively. The difference in feeding speeds for the carbon and jute fibers prevented fiber stacking, which depended on the fiber type, within the nozzle. The fiber volume fraction (vf) of the FRTPs was determined by the supplied amounts of reinforcing fibers and an optical examination of the cross-section of the extruded filament, measured by scanning electron microscopy. The vf of CFRTP and JFRTP was 6.6% and 6.1%, respectively. The jute fiber had a density of 1.46 g/cm3 39.
Figure 2(a,b) show the obtained printed CFRTP and JFRTP specimens. Figure 2 (c,d) show an overview and a magnification of a cross-section of a printed CFRTP part, confirming that the PLA resin has impregnated the fiber bundles. The cross-sectional areas of the printed composites are elliptical, despite the circular nozzle, because the filaments are compressed against the hot tables during printing.
3D-printed (a) CFRTP and (b) dumbbell-shaped JFRTP tensile test specimens. (c) Cross-section and (d) magnified cross-section of the CFRTP specimen.
The continuous FRTP tensile test specimens were 3D-printed according to the JIS K 7162 standards40. For the CFRTPs, the test specimens were sliced from rectangular frames (see supplementary Fig. 2), while dumbbell-shaped JFRTP specimens were fabricated with a traversable CAD path. The ply created by this path was layered in the z-direction four times for a total specimen thickness of ~4 mm. The carbon or jute fibers were aligned along the longitudinal direction, which was chosen as the loading direction and no fibers were aligned in the transverse (y) or thickness (z) directions in the gage region of the tensile test specimens. Therefore, the mechanical properties of the tensile specimen are orthotropic and maximized along the loading direction. Aligning the reinforcing fibers with the transverse and thickness directions would also be possible; however, the aspect of alignment is beyond the scope of this study and related experiments are not presented here. Neat PLA tensile specimens were also fabricated to demonstrate the reinforcing effect achieved by the continuous carbon or jute fibers. Four specimens each of PLA, CFRTP and JFRTP were used for the tensile tests.
Figure 3 shows the stress-strain curves of PLA, CFRTP and JFRTP. In the CFRTP specimen, the stress linearly increases before fracture occurs. A stress drop is observed in some specimens before failure. The stress-strain curve of JFRTP shows non-linearity; the tangential modulus decreases with increasing strain. No stress drop is observed before failure. The average values and standard deviation of the tensile modulus, tensile strength and tensile strain-to-failure for the different specimens are shown in Fig. 4 (see supplementary Table 1 for a listing of the values). The tensile modulus and strength of 3D-printed CFRTP are 19.5 (±2.08) GPa and 185.2 (±24.6) MPa, respectively, which are 599% and 435% of those of the PLA specimen. Therefore, the mechanical properties are highly improved by 3D printing the PLA with continuous carbon fiber. The tensile strain-to-failure of CFRTP is decreased to 0.95 (±0.0873)% from the value of 1.45 (±0.0945)% shown by the PLA specimens, because of the low strain-to-failure characteristics of the carbon fibers. We also tested the samples by three-point bending; the flexural strength was 133 MPa, flexural modulus was 5.93 GPa and flexural strain-to-failure was 4.09%. However, because the fibers were distributed non-uniformly in the cross-section of the specimen, these flexural properties should be understood as reference values.
Stress-strain curves of PLA, unidirectional CFRTP and unidirectional JFRTP specimens fabricated by 3D printing.
(a) Tensile modulus, (b) tensile strength and (c) tensile strain-to-failure of specimens fabricated by 3D printing.
The tensile strength of JFRTP is not improved significantly compared to that of CFRTP. For JFRTP, the tensile modulus and strength are 5.11 (±0.41) GPa and 57.1 (±5.33) MPa, corresponding to 157% and 134% of those shown by the PLA specimen, respectively. The tensile modulus of JFRTP is obtained from the tensile strain in the range of 0.05% to 0.25%, based on the JIS K 7162 standard, although the tangential modulus decreases with increased stress above this strain range. The decrease in tangential modulus and the lack of improvement in the tensile strength can be attributed to the degradation of fiber-resin interactions with increased applied stress.
While the mechanical property and volume fraction of the fiber reinforcement affected the properties of the FRPT, the composite properties are also affected by the configuration of the twisted yarn reinforcement41,42,43. In the 3D printing method employed, no tension was applied to the jute fiber when the yarn was fed to the nozzle. This led to a non-uniform configuration of the twisted jute yarn fibers, which may have created weak points in the printed filament. When using a twisted yarn as reinforcement, an appropriate tension and torsional moment must be applied to the yarn during 3D printing, which would assist the uniform molding of the FRTP.
Figure 5(a,b) show the fracture surface and cross-sections, respectively, obtained by scanning electron microscopy (SEM) after the tensile testing of the CFRTP specimen, while Fig. 5 (c) shows the fracture surface of the JFRTP specimen. For comparison, an image of the fracture surface of the PLA specimen is shown in the supplementary Fig. 3. In both the CFRTP and JFRTP specimens, fiber pullout attributed to fracture is observed both macroscopically and microscopically. This indicates that the adhesion between the fibers and the thermoplastic resin is insufficient; hence, treatment of the fiber surfaces is required to achieve further enhancement in mechanical properties. Poor adhesion between thermoplastic resin and reinforcing fibers is common in the development of FRTPs. Voids are observed between filaments in the CFRTP sample because the molten CFRTP filament, once ejected from the nozzle, becomes laminated and assumes an elliptical shape. Voids between filaments are also common in FDM-type 3D printing44,45. In the future, similar candidate 3D printed composites should be modeled by numerical simulation to predict mechanical strength, but the fiber bundle distribution and void existence may require special consideration.
Fracture of a unidirectional continuous FRTP fabricated by 3D printing.
Fiber pullout due to tensile fracture observed as an (a) overview and (b) scanning electron microscopy image of the CFRTP specimen. (c) Fiber pullout in the JFRTP specimen.
Figure 6 shows the Young’s modulus and strength values obtained in the present study (indicated as continuous-fiber composites) and the values shown by conventional polymer-based 3D-printed samples reported in the literature, including samples fabricated using commercially available 3D printers and those reinforced by FDM using nano-clay platelets21, short carbon fibers23 and carbon nanotubes25. The continuous carbon-fiber composites fabricated in the present study show superior Young’s moduli and strengths compared with materials fabricated using commercially available 3D printers, whether these are operated by selective laser sintering, stereolithography, or FDM. Further, the Young’s moduli of composites from this study exceed those shown by composites obtained by FDM, with the exception of composites fabricated by FDM using nanoclay platelets as reinforcements21, because in this specific case, the resin used was epoxy, which exhibits high mechanical properties. As the fiber volume fraction of the printed composites in the present study is low and the Young’s modulus can be improved by increasing the fiber volume fraction, the performance of our composites could be improved. The carbon composites used in aerospace structures typically have fiber volume fractions of ~67%. We estimate the upper limit of fiber volume fraction in FDM 3D printing to be ~40–50%, because of the necessity of running fibers through the printer nozzle. The strength of the composites from this study was approximately twice that of the composites fabricated by FDM. Hence, the process we propose to fabricate continuous fiber composites expands the applicability of 3D printing to the manufacture of load-bearing components, which cannot be realized by conventional 3D printing.
Young’s moduli and strengths of continuous carbon-fiber composites fabricated in the present study compared with composites fabricated by FDM21,23,25 and using commercially available 3D printers, such as SLS48, SLA48 and FDM49.
Commercially available PLA filament (Hotproceed, 1.75 mm diameter) was used as the matrix material. Polyacrylonitrile (PAN)-based carbon fibers (T800S-10E, Toray) and twisted jute natural plant fibers46 were used as continuous reinforcements. For the carbon fibers, several thousand filaments were extracted from the straight 24000 filaments and supplied to the printer head. The carbon fibers were used as-is with epoxy sizing. The mechanical properties of the carbon fibers and jute fibers are shown in supplementary Table 147. For the jute fibers, a single strand of yarn was extracted from the twisted 500-Tex double yarn. No surface treatment was performed after purchasing.
The FDM Blade-1 3D printer, produced by Hotproceed, Japan, was modified for printing CFRTP, while the FlashForge printer, produced by Zhejiang FlashForge 3D Technology, China, was modified for printing JFRTP.
Quasistatic tensile tests were performed on the CFRTP, JFRTP and PLA specimens using a universal tester (AG-IS 150 kN, Shimadzu) at a crosshead speed of 1.0 mm/min. A strain gage was attached to the specimen surface to measure strain. The specimen configuration was rectangular with PLA end tabs for the CFRTP, while the JFRTP and PLA specimens were dumbbell-shaped without end tabs. The shoulder portions of the specimen were clamped directly by the wedge grips of the tester and a tensile load was applied uniaxially to the specimen. We tested four specimens each of CFRTP, JFRTP and PLA.
How to cite this article: Matsuzaki, R. et al. Three-dimensional printing of continuous-fiber composites by in-nozzle impregnation. Sci. Rep. 6, 23058; doi: 10.1038/srep23058 (2016).
Yan, X. & Gu, P. A review of rapid prototyping technologies and systems. Computer-Aided Design 28, 307–318 (1996).
Berman, B. 3-D printing: The new industrial revolution. Business Horizons 55, 155–162 (2012).
Rengier, F. et al. 3D printing based on imaging data: review of medical applications. Int J Comput Assist Radiol Surg 5, 335–341 (2010).
Wong, K. V. & Hernandez, A. A Review of Additive Manufacturing. ISRN Mechanical Engineering 2012, 1–10 (2012).
Huang, S. H., Liu, P., Mokasdar, A. & Hou, L. Additive manufacturing and its societal impact: a literature review. The International Journal of Advanced Manufacturing Technology 67, 1191–1203 (2012).
Guo, N. & Leu, M. C. Additive manufacturing: technology, applications and research needs. Frontiers of Mechanical Engineering 8, 215–243 (2013).
Grimm, T. Fused deposition modelling: a technology evaluation. Time-Compression Technologies 11, 1–6 (2003).
Jones, R. et al. RepRap- the replicating rapid prototyper. Robotica 29, 177–191 (2011).
Kelly, J. F. & Hood-Daniel, P. Printing in Plastic: Buid your own 3D printer. Apress (2011).
Lee, C. S., Kim, S. G., Kim, H. J. & Ahn, S. H. Measurement of anisotropic compressive strength of rapid prototyping parts. Journal of Materials Processing Technology 187–188, 627–630 (2007).
Bagsik, A. & Schöppner, V. Mechanical properties of fused deposition modeling parts manufactured with ultem*9085. In Proceedings of 69th Annual Technical Conference of the Society of Plastics Engineers (ANTEC’11), 2, 1294–1298 (2011).
Panda, S. K. Optimization of Fused Deposition Modelling (FDM) Process Parameters Using Bacterial Foraging Technique. Intelligent Information Management 01, 89–97 (2009).
Ning, H., Janowski, G. M., Vaidya, U. K. & Husman, G. Thermoplastic sandwich structure design and manufacturing for the body panel of mass transit vehicle. Composite Structures 80, 82–91 (2007).
Marsh, G. Next step for automotive materials. Materials Today 6, 36–43 (2003).
Netravali, A. N. & Chabba, S. Composites get greener. Materials Today 6, 22–29 (2003).
Holbery, J. & Houston, D. Natural-fiber-reinforced polymer composites in automotive applications. JOM 58, 80–86 (2006).
Kumar, S. & Kruth, J.-P. Composites by rapid prototyping technology. Materials & Design 31, 850–856 (2010).
Bakarich, S. E., Gorkin, R. 3rd, in het Panhuis, M. & Spinks, G. M. Three-dimensional printing fiber reinforced hydrogel composites. ACS applied materials & interfaces 6, 15998–16006 (2014).
Suwanprateeb, J., Sanngam, R., Suvannapruk, W. & Panyathanmaporn, T. Mechanical and in vitro performance of apatite-wollastonite glass ceramic reinforced hydroxyapatite composite fabricated by 3D-printing. J Mater Sci Mater Med 20, 1281–1289 (2009).
Dimas, L. S. & Buehler, M. J. Modeling and additive manufacturing of bio-inspired composites with tunable fracture mechanical properties. Soft Matter 10, 4436–4442 (2014).
CAS ADS Article Google Scholar
Compton, B. G. & Lewis, J. A. 3D-printing of lightweight cellular composites. Adv Mater 26, 5930–5935 (2014).
Leigh, S. J., Bradley, R. J., Purssell, C. P., Billson, D. R. & Hutchins, D. A. A simple, low-cost conductive composite material for 3D printing of electronic sensors. PLoS One 7, e49365 (2012).
CAS ADS Article Google Scholar
Tekinalp, H. L. et al. Highly oriented carbon fiber–polymer composites via additive manufacturing. Compos Sci Technol 105, 144–150 (2014).
Gray, IV, R. W., Baird, D. G. & Bohn, J. H. Thermoplastic composites reinforced with long fiber thermotropic liquid crystalline polymers for fused deposition modeling. Polym Compos 19, 383–394 (1998).
Shofner, M. L., Lozano, K., Rodriguez-Macias, F. J. & Barrera, E. V. Nanofiber-reinforced polymers prepared by fused deposition modeling. Journal of Applied Polymer Science 89, 3081–3090 (2003).
Pidcock, G. C. & in het Panhuis, M. Extrusion Printing of Flexible Electrically Conducting Carbon Nanotube Networks. Advanced Functional Materials 22, 4790–4800 (2012).
Zhong, W., Li, F., Zhang, Z., Song, L. & Li, Z. Short fiber reinforced composites for fused deposition modeling. Materials Science and Engineering A 301, 125–130 (2001).
Scheithauer, U., Bergner, A., Schwarzer, E., Richter, H.-J. & Moritz, T. Studies on thermoplastic 3D printing of steel–zirconia composites. Journal of Materials Research 29, 1931–1940 (2014).
CAS ADS Article Google Scholar
Hsueh, C.-H. Young’s modulus of unidirectional discontinous-fibre composites. Compos Sci Technol 60, 2671–2680 (2000).
III. CLT, Liang E. Stiffness predictions for unidirectional short-fiber composites: Review and evaluation. Compos Sci Technol 59, 655–671 (1999).
Hine, P. J., Lusti, H. R. & Gusev, A. A. Numerical simulation of the effects of volume fraction, aspect ratio and fibre length distribution on the elastic and thermoelastic properties of short fibre composites. Compos Sci Technol 62, 1445–1453 (2002).
Love, L. J. et al. The importance of carbon fiber to polymer additive manufacturing. Journal of Materials Research 29, 1893–1898 (2014).
CAS ADS Article Google Scholar
MarkForged, https://markforged.com, accessed: April 2015.
Evans, S. L. & Gregson, P. J. Composite technology in load-bearing orthopaedic implants. Biomaterials 19, 1329–1342 (1998).
Ramakrishna, S., Mayer, J., Wintermantel, E. & Leong, K. W. Biomedical applications of polymer-composite materials: a review. Compos Sci Technol 61, 1189–1224 (2001).
Scholz, M. S. et al. The use of composite materials in modern orthopaedic medicine and prosthetic devices: A review. Compos Sci Technol 71, 1791–1803 (2011).
La Mantia, F. P. & Morreale, M. Green composites: A brief review. Compos A 42, 579–588 (2011).
Plackett, D., Løgstrup Andersen, T., Batsberg Pedersen, W. & Nielsen, L. Biodegradable composites based on l-polylactide and jute fibres. Compos Sci Technol 63, 1287–1296 (2003).
Beukers, A. & Hinte, E. V. Lightness: The Inevitable Renaissance of Minimum Energy Structures. NAI Publishers (2013).
Japanese Industrial Standards Committee. JIS K7162 Plastics–Determination of tensile properties–Part 2: Test conditions for moulding and extrusion plastics. In: JIS Handbook Plastic I. 409–413 (Japanese Industrial Standards Committee, 2011).
Shah, D. U., Schubel, P. J. & Clifford, M. J. Modelling the effect of yarn twist on the tensile strength of unidirectional plant fibre composites. J Compos Mater 47, 425–436 (2013).
Rask, M. & Madsen, B. Twisting of fibres in yarns for natural fibre composites. In Proceedings of 18th International Conference on Composite Materials, M15-14 (2011).
Ma, H. & Luo, Y. The effect of fiber twist on the mechanical properties of natural fiber reinforced composites. In Proceedings of 18th International Conference on Composite Materials, M03-03 (2011).
Huang, B. & Singamneni, S. Raster angle mechanics in fused deposition modelling. J Compos Mater 49, 363–383 (2014).
Ahn, S. H., Montero, M., Odell, D., Roundy, S. & Wright, P. K. Anisotropic material properties of fused deposition modeling ABS. Rapid Prototyping Journal 8, 248–257 (2002).
Handicraft Manufacturer Gosyo Co., Ltd, http://www.rakuten.ne.jp/gold/gosyo/, accessed: August 9 2015.
Toray Technical Data sheet, T800S data sheet, http://www.toraycfa.com/pdfs/T800SDataSheet.pdf, accessed: August 10 2015.
Production 3D Printer Materials | Production 3D Printing Materials - 3dsystems.com, http://www.3dsystems.com/materials/production, accessed: August 10 2015.
FDM. Thermoplastics Material Overview | Stratasys, http://www.stratasys.com/materials/fdm/, accessed: August 10 2015.
We acknowledge the funding provided by the Ministry of Economy, Trade and Industry of Japan through the Supporting Industries program.
Matsuzaki Ryosuke and Ueda Masahito contributed equally to this work.
Tokyo University of Science, 2641 Yamazaki, Noda, 278-8510, Chiba, Japan
Ryosuke Matsuzaki, Keisuke Horiguchi & Taishi Nakamura
Nihon University, 1-8-14 Kanda-surugadai, Chiyoda, 101-8308, Tokyo, Japan
Masahito Ueda, Masaki Namiki, Tae-Kun Jeong & Hirosuke Asahara
Tokyo Institute of Technology, 2-12-1 O-okayama, Meguro, 152-8551, Tokyo, Japan
Japan Aerospace Exploration Agency, 6-13-1 Osawa, Mitaka, 181-0015, Tokyo, Japan
You can also search for this author in PubMed Google Scholar
You can also search for this author in PubMed Google Scholar
You can also search for this author in PubMed Google Scholar
You can also search for this author in PubMed Google Scholar
You can also search for this author in PubMed Google Scholar
You can also search for this author in PubMed Google Scholar
You can also search for this author in PubMed Google Scholar
You can also search for this author in PubMed Google Scholar
You can also search for this author in PubMed Google Scholar
R.M., M.U., A.T. and Y.H. conceived the idea. M.N., T.K.J., H.A., K.H. and T.N. performed the experiments. R.M. and M.U. co-wrote the manuscript. All authors discussed the results and commented on the manuscript.
The authors declare no competing financial interests.
This work is licensed under a Creative Commons Attribution 4.0 International License. The images or other third party material in this article are included in the article’s Creative Commons license, unless indicated otherwise in the credit line; if the material is not included under the Creative Commons license, users will need to obtain permission from the license holder to reproduce the material. To view a copy of this license, visit http://creativecommons.org/licenses/by/4.0/
Matsuzaki, R., Ueda, M., Namiki, M. et al. Three-dimensional printing of continuous-fiber composites by in-nozzle impregnation. Sci Rep 6, 23058 (2016). https://doi.org/10.1038/srep23058
DOI: https://doi.org/10.1038/srep23058
Anyone you share the following link with will be able to read this content:
Sorry, a shareable link is not currently available for this article.
Provided by the Springer Nature SharedIt content-sharing initiative
The International Journal of Advanced Manufacturing Technology (2022)
Journal of Mechanical Science and Technology (2022)
The International Journal of Advanced Manufacturing Technology (2022)
By submitting a comment you agree to abide by our Terms and Community Guidelines. If you find something abusive or that does not comply with our terms or guidelines please flag it as inappropriate.
Scientific Reports (Sci Rep) ISSN 2045-2322 (online)
Sign up for the Nature Briefing newsletter — what matters in science, free to your inbox daily.