Soyeon Park , Samiul Alam , Gavin Stoker , Kjersten Segura , Won Gyo Seo , Devin Young , Juhyeong Lee , Dae Han Sung
{"title":"基于复合材料的增材制造(CBAM):高通量热塑性复合材料的力学特性和城市空中交通应用演示","authors":"Soyeon Park , Samiul Alam , Gavin Stoker , Kjersten Segura , Won Gyo Seo , Devin Young , Juhyeong Lee , Dae Han Sung","doi":"10.1016/j.compositesb.2025.113035","DOIUrl":null,"url":null,"abstract":"<div><div>This study introduces Composite-Based Additive Manufacturing (CBAM), a novel laminate-based technique for fiber-reinforced thermoplastics, offering a promising alternative to conventional extrusion-based methods such as fused deposition modeling (FDM). CBAM consolidates thermoplastic micro-powders precisely patterned on fiber laminates with an automated system, enabling effective matrix impregnation and higher fiber volume fractions. Micro-X-ray computed tomography revealed that CBAM composites contain smaller, more uniformly distributed micropores, whereas FDM parts exhibit inter-filament macro-voids. The distinct microstructures from both processes along with printing directions lead to different mechanical performance. In tension, CBAM composites achieved Young's modulus of 10.0–11.4 GPa and strength of 119.4–121.1 MPa, significantly higher than FDM (4.2–8.1 GPa, 54.7–81.5 MPa), with reduced sensitivity to print orientation due to improved interlayer bonding. Flexural tests showed CBAM's modulus (8.1 GPa) and strength (103–106 MPa) remained consistent across orientations, again surpassing FDM, particularly for 45° flat specimens. In compression, CBAM exhibited lower strength (63.3 MPa at 0°, 54.4 MPa at 90°) than FDM (85.4–91.7 MPa), attributed to matrix-dominant properties. These results demonstrate that CBAM's improved tensile and flexural performance arises from the coupled effects of fiber orientation, volume fraction, and void morphology. To demonstrate application potential, a two-blade propeller was fabricated using CBAM with non-woven glass fiber and PA-12. Ten blades were produced within 3 h, meeting dimensional tolerances <1 mm—substantially faster than the 35–50 h typical of FDM. These establish CBAM as a rapid, precise, and structurally advantageous composite manufacturing technology for aerospace and advanced mobility applications.</div></div>","PeriodicalId":10660,"journal":{"name":"Composites Part B: Engineering","volume":"309 ","pages":"Article 113035"},"PeriodicalIF":14.2000,"publicationDate":"2025-09-15","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"Composite-Based Additive Manufacturing (CBAM): Mechanical characterization of high-throughput thermoplastic composites and demonstration for urban air mobility application\",\"authors\":\"Soyeon Park , Samiul Alam , Gavin Stoker , Kjersten Segura , Won Gyo Seo , Devin Young , Juhyeong Lee , Dae Han Sung\",\"doi\":\"10.1016/j.compositesb.2025.113035\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"<div><div>This study introduces Composite-Based Additive Manufacturing (CBAM), a novel laminate-based technique for fiber-reinforced thermoplastics, offering a promising alternative to conventional extrusion-based methods such as fused deposition modeling (FDM). CBAM consolidates thermoplastic micro-powders precisely patterned on fiber laminates with an automated system, enabling effective matrix impregnation and higher fiber volume fractions. Micro-X-ray computed tomography revealed that CBAM composites contain smaller, more uniformly distributed micropores, whereas FDM parts exhibit inter-filament macro-voids. The distinct microstructures from both processes along with printing directions lead to different mechanical performance. In tension, CBAM composites achieved Young's modulus of 10.0–11.4 GPa and strength of 119.4–121.1 MPa, significantly higher than FDM (4.2–8.1 GPa, 54.7–81.5 MPa), with reduced sensitivity to print orientation due to improved interlayer bonding. Flexural tests showed CBAM's modulus (8.1 GPa) and strength (103–106 MPa) remained consistent across orientations, again surpassing FDM, particularly for 45° flat specimens. In compression, CBAM exhibited lower strength (63.3 MPa at 0°, 54.4 MPa at 90°) than FDM (85.4–91.7 MPa), attributed to matrix-dominant properties. These results demonstrate that CBAM's improved tensile and flexural performance arises from the coupled effects of fiber orientation, volume fraction, and void morphology. To demonstrate application potential, a two-blade propeller was fabricated using CBAM with non-woven glass fiber and PA-12. Ten blades were produced within 3 h, meeting dimensional tolerances <1 mm—substantially faster than the 35–50 h typical of FDM. These establish CBAM as a rapid, precise, and structurally advantageous composite manufacturing technology for aerospace and advanced mobility applications.</div></div>\",\"PeriodicalId\":10660,\"journal\":{\"name\":\"Composites Part B: Engineering\",\"volume\":\"309 \",\"pages\":\"Article 113035\"},\"PeriodicalIF\":14.2000,\"publicationDate\":\"2025-09-15\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"Composites Part B: Engineering\",\"FirstCategoryId\":\"5\",\"ListUrlMain\":\"https://www.sciencedirect.com/science/article/pii/S1359836825009461\",\"RegionNum\":1,\"RegionCategory\":\"材料科学\",\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"Q1\",\"JCRName\":\"ENGINEERING, MULTIDISCIPLINARY\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"Composites Part B: Engineering","FirstCategoryId":"5","ListUrlMain":"https://www.sciencedirect.com/science/article/pii/S1359836825009461","RegionNum":1,"RegionCategory":"材料科学","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"Q1","JCRName":"ENGINEERING, MULTIDISCIPLINARY","Score":null,"Total":0}
Composite-Based Additive Manufacturing (CBAM): Mechanical characterization of high-throughput thermoplastic composites and demonstration for urban air mobility application
This study introduces Composite-Based Additive Manufacturing (CBAM), a novel laminate-based technique for fiber-reinforced thermoplastics, offering a promising alternative to conventional extrusion-based methods such as fused deposition modeling (FDM). CBAM consolidates thermoplastic micro-powders precisely patterned on fiber laminates with an automated system, enabling effective matrix impregnation and higher fiber volume fractions. Micro-X-ray computed tomography revealed that CBAM composites contain smaller, more uniformly distributed micropores, whereas FDM parts exhibit inter-filament macro-voids. The distinct microstructures from both processes along with printing directions lead to different mechanical performance. In tension, CBAM composites achieved Young's modulus of 10.0–11.4 GPa and strength of 119.4–121.1 MPa, significantly higher than FDM (4.2–8.1 GPa, 54.7–81.5 MPa), with reduced sensitivity to print orientation due to improved interlayer bonding. Flexural tests showed CBAM's modulus (8.1 GPa) and strength (103–106 MPa) remained consistent across orientations, again surpassing FDM, particularly for 45° flat specimens. In compression, CBAM exhibited lower strength (63.3 MPa at 0°, 54.4 MPa at 90°) than FDM (85.4–91.7 MPa), attributed to matrix-dominant properties. These results demonstrate that CBAM's improved tensile and flexural performance arises from the coupled effects of fiber orientation, volume fraction, and void morphology. To demonstrate application potential, a two-blade propeller was fabricated using CBAM with non-woven glass fiber and PA-12. Ten blades were produced within 3 h, meeting dimensional tolerances <1 mm—substantially faster than the 35–50 h typical of FDM. These establish CBAM as a rapid, precise, and structurally advantageous composite manufacturing technology for aerospace and advanced mobility applications.
期刊介绍:
Composites Part B: Engineering is a journal that publishes impactful research of high quality on composite materials. This research is supported by fundamental mechanics and materials science and engineering approaches. The targeted research can cover a wide range of length scales, ranging from nano to micro and meso, and even to the full product and structure level. The journal specifically focuses on engineering applications that involve high performance composites. These applications can range from low volume and high cost to high volume and low cost composite development.
The main goal of the journal is to provide a platform for the prompt publication of original and high quality research. The emphasis is on design, development, modeling, validation, and manufacturing of engineering details and concepts. The journal welcomes both basic research papers and proposals for review articles. Authors are encouraged to address challenges across various application areas. These areas include, but are not limited to, aerospace, automotive, and other surface transportation. The journal also covers energy-related applications, with a focus on renewable energy. Other application areas include infrastructure, off-shore and maritime projects, health care technology, and recreational products.