Mechanical Properties and Flame Resistance of ۳D-printed Coextruded Continuous Carbon Fiber Reinforced Polycarbonate
محل انتشار: ماهنامه بین المللی مهندسی، دوره: 38، شماره: 8
سال انتشار: 1404
نوع سند: مقاله ژورنالی
زبان: انگلیسی
مشاهده: 92
فایل این مقاله در 15 صفحه با فرمت PDF قابل دریافت می باشد
- صدور گواهی نمایه سازی
- من نویسنده این مقاله هستم
استخراج به نرم افزارهای پژوهشی:
شناسه ملی سند علمی:
JR_IJE-38-8_019
تاریخ نمایه سازی: 21 اسفند 1403
چکیده مقاله:
The active development of modern additive manufacturing technologies, namely continuous fiber extrusion based on fused deposition modeling (FDM), shows their significant potential for the creation of advanced materials based on fibrous polymer composites. These materials are widely used in the aviation industry, but their use as aircraft components is limited by the need to meet a number of requirements. One of such requirements is flame resistance. For such applications, it is of the utmost importance that a polymer composite is considered to be compliant with the type certificate prior to its integration. This research paper presents the results of a study that ۳D-printed a continuously reinforced polymer composite with a polycarbonate matrix, with enhanced mechanical properties, and conducted flame resistance tests to demonstrate the feasibility of the printed materials in aviation applications. The study encompassed a series of interfacial shear strength, tensile strength, and flame resistance tests. The study presents a detailed characterization of the ۳D-printed composite using ASTM D۶۳۸-۱۰, ASTM D۶۳۵-۲۲, optical microscopy, and pull-out tests of a single towpreg immersed in the matrix. The use of continuous carbon fiber coextrusion allowed for a fourfold increase in the tensile strength of the material (۲۳۹.۲۹ MPa) in comparison to unreinforced polycarbonate (۵۴.۹۲ MPa). The findings of the investigation into the flame resistance of printed continuously-reinforced polycarbonate indicate that the composite exhibited a burning time of less than ۳۰ seconds following each flame application. Furthermore, the total burning time of a series of five samples after double flame application did not exceed ۲۵۰ seconds, with an average of ۵۶ seconds. The results obtained led to the conclusion that printed continuously reinforced polycarbonate is a viable material for its use in aircraft design. As to further support the use of the presented printing technology, the frame of an unmanned aerial vehicle was manufactured from continuously reinforced polycarbonate.
کلیدواژه ها:
Additive Manufacturing ، ۳D Printing ، fused deposition modeling ، Coextrusion ، Continuous Carbon Fiber ، polycarbonate ، Carbon fiber reinforced polymer ، Mechanical properties ، flame resistance
نویسندگان
A. Sotov
Peter the Great St. Petersburg Polytechnic University, St. Petersburg, ۱۹۵۲۵۱, Russia
A. Abdrakhmanova
Peter the Great St. Petersburg Polytechnic University, St. Petersburg, ۱۹۵۲۵۱, Russia
A. Zaytsev
Peter the Great St. Petersburg Polytechnic University, St. Petersburg, ۱۹۵۲۵۱, Russia
E. Zhuchenko
Mechanical Engineering, Materials and Transport, Peter the Great St. Petersburg Polytechnic University, Russia
A. Popovich
Peter the Great St. Petersburg Polytechnic University, St. Petersburg, ۱۹۵۲۵۱, Russia
مراجع و منابع این مقاله:
لیست زیر مراجع و منابع استفاده شده در این مقاله را نمایش می دهد. این مراجع به صورت کاملا ماشینی و بر اساس هوش مصنوعی استخراج شده اند و لذا ممکن است دارای اشکالاتی باشند که به مرور زمان دقت استخراج این محتوا افزایش می یابد. مراجعی که مقالات مربوط به آنها در سیویلیکا نمایه شده و پیدا شده اند، به خود مقاله لینک شده اند :