Open Access Article
Zhe
Chen
a,
Wenjia
Wang
b,
Tongtong
Wang
c,
Sean
Tang
a,
Sabin
Gautam
d,
Nilay
Saha
e,
Piumi
Samarawickrama
d,
So Tie
Tjeng
c,
Eric G.
Eddings
*b and
Maohong
Fan
*fg
aDepartment of Energy & Petroleum Engineering, University of Wyoming, Laramie, WY 82071, USA
bDepartment of Chemical Engineering, University of Utah, Salt Lake City, UT 84112, USA. E-mail: eric.eddings@chemeng.utah.edu
cDepartment of Chemical and Biomedical Engineering, University of Wyoming, Laramie, WY 82071, USA
dDepartment of Physics and Astronomy, University of Wyoming, Laramie, WY 82071, USA
eDepartment of Chemistry, University of Wyoming, Laramie, WY 82071, USA
fCollege of Engineering and Physical Sciences, and School of Energy Resources, University of Wyoming, Laramie, WY 82071, USA. E-mail: mfan@uwyo.edu
gCollege of Engineering, Georgia Institute of Technology, Atlanta, GA 30332, USA
First published on 3rd October 2025
Carbon fibers (CFs) are valuable in applications such as aircraft, automobiles, wind turbines, and energy storage devices. However, the production cost of CFs is high due to the use of conventional precursor polyacrylonitrile, and an affordable substitute is imperative. For the first time, this work combined cheap coal and waste plastic material to fabricate CFs. Currently, conventional disposal methods for waste plastics lack sustainability and profitability. Despite its unpopularity as an energy source, coal can serve as a feedstock for chemicals and materials. High-density polyethylene (HDPE), a commonly used plastic, was hydrogenolyzed into a plastic-derived liquid (PDL). PDL served as an effective solvent during mild solvolysis liquefaction of coal, and the acquired coal–plastic liquid was modified into mesophase coal–plastic liquids (MCPLs). MCPLs were melt-spun and heat-treated into CFs through different heat treatment conditions. The diameters of the CFs were 8.2–45.8 μm, and the Young's modulus and tensile strength were 75–759 GPa and 0.54–4.03 GPa, respectively. The CFs belong to the categories of general-purpose and high-performance CFs. The high-performance CFs (diameter: 8.2 μm, Young's modulus: 759 GPa, and tensile strength: 4.03 GPa) are comparable to commercial and laboratory CFs whose precursors are coal–tar pitch featuring low coal-to-pitch yield, or coal liquefied by conventional, costly solvents. Analysis shows the PDL enhances hydrogen transfer, stabilizes radicals, and promotes mesophase development during thermal treatment. The mechanisms valorizing coal and plastics simultaneously to high-performance CFs are proposed. This work demonstrates a novel and sustainable valorization pathway for waste plastics and coals. Future work will explore industrial-scale plant design, techno-economic analysis, and life-cycle assessment to quantify the economic and environmental impacts.
Keywords: Environmentally unfriendly polyacrylonitrile; Valorization of waste plastic and coal; Low CO2-emission; High-performance carbon fiber.
Fortunately, liquefied coal emerged as a viable low-cost CF precursor. Liquefied coal has an approximately 85% yield from fresh CFs to CFs due to its high carbon content, which is the primary reason for its lower production cost.6,7,10 Its high content of polyaromatic hydrocarbons (PAHs) promotes the formation of graphitic structures during heat treatment. Additionally, melt-spinning of liquefied coal is a more economical and faster technique than solution spinning of PAN.11 Coal can be liquefied by pyrolysis; the liquid product, called coal tar, is the precursor of general-purpose CFs. By further pyrolysis, coal tar can be modified into coal tar pitch, a mesophase precursor of high-performance carbon fibers (CFs).12–14 The yield of coal tar from coal pyrolysis is only between 5% and 25%,15,16 with metallurgical coke being the main product. Another technique, called direct coal liquefaction, can achieve a liquid yield of up to 90%.17 The method is dissolving the coal and heating it under H2. However, direct coal liquefaction requires catalysts, temperatures up to 450 °C, and H2 pressures up to 20 MPa.18 To tackle these issues, mild solvolysis liquefaction is utilized. It features lower temperature and lower H2 pressure, no catalysts,19,20 and lower capital cost. Mild solvolysis liquefaction also avoids excessive cracking,19,20 reducing the yield of volatiles. A techno-economic analysis showed that with direct coal liquefaction and mild solvolysis liquefaction-generated precursors, CFs cost $9.5–10.63 per kg,6,7 only half that of PAN-based CFs.
Like direct coal liquefaction, mild solvolysis liquefaction involves four steps: 1) slurry (coal and solvent mixture) preparation, 2) liquefaction, 3) separation, and 4) solvent recycling.21 Step 2 is hydrogenation, which heats the slurry under an H2 atmosphere. Step 3 involves refining, distillation, extraction, and other processes to separate the products. Step 4 recovers the solvent for reuse in step 1. The solvent not only diffuses coal molecules but also donates and shuttles hydrogen. Pure solvents, such as tetralin and anthracene, are used in academic research. Industrial solvents are typically middle or heavy liquefaction products from step 3, containing 2–4 ring PAHs, hydro-PAHs, and paraffins.21,22 Donor solvents like tetralin have a hydrogen bound to an α carbon (Hα), a naphthenic or aliphatic carbon adjacent to an aromatic ring. These Hα represent a primary hydrogen source. PAHs only have aromatic hydrogen (Har),23,24 and are less effective donors. Numerous researchers have liquefied coal by mild solvolysis liquefaction and fabricated CFs.25–29 Their mechanical performance varies significantly due to differences in feedstock and fabrication conditions. The Young's modulus ranged from 30 to 800 GPa, and tensile strength ranged from 0.9 to 4 GPa, comparable to commercial Mitsubishi and Nippon products.30,31 The disadvantage of mild solvolysis liquefaction is that to make the slurry pumpable, the solvent–coal mass ratio is typically 1–3,32,33 and over half of the mild solvolysis liquefaction products are recycled instead of valorized.
This inefficiency can be overcome by introducing a low-cost solvent that does not require recycling. Plastic-derived liquid (PDL), a byproduct of plastic decomposition, is a promising candidate. After mild solvolysis liquefaction, the recovered PDL can be used as consumer products or feedstocks in other processes. Recycling is not necessary due to the vast supply of waste plastics and the added value of the PDL. There has been significant growth in the production of plastics and the generation of waste plastics. In 1950, the world produced only 2 million tons (mt) of plastics, reaching 460 mt in 2019.34 From 1950 to 2015, 6.3 billion tons (bt) of waste plastics had been generated.35 By 2035, the cumulative weight of waste plastics would be equal to the fish in the ocean.35,36 The current disposal methods lack sustainability. Mechanically recycled plastics often deteriorate in quality; landfills, incineration, and mismanagement can release contaminants.37,38 Combustion of plastics, like coal, emits CO2, whose capture39 and utilization40 entail high costs. One approach to addressing these issues is to upgrade plastics into value-added products through various methods that break down plastic molecules into hydrogen (H2), monomers, oils, and waxes, which can be used as fuels or chemicals.38,41–45 PDL contains aliphatics and aromatics, and its similarity to mild solvolysis liquefaction solvent makes PDL a potential solvent. The high hydrogen content of plastics can be inherited by PDL, which reduces the cost of H2. The above solvent–coal mass ratio is feasible given the low price of waste plastics, ranging from $0.04 to $0.34 per kg.46 So far, few researchers have adopted PDL as a mild solvolysis liquefaction solvent.47 More publications, including those co-liquefying plastic–coal mixtures,48–50 utilized solvents that need recycling in a commercial process.
Although 1) PDL has the potential to function as a non-recycling mild solvolysis liquefaction solvent and 2) coal can be liquefied by mild solvolysis liquefaction and fabricated into CFs, no researchers have integrated both. According to the studies6,7 mentioned above and the economic feasibility of plastic waste, combining 1) and 2) presents a potential cost-effective process to produce CFs. Although a detailed techno-economic analysis is required to prove cost-effectiveness, this work demonstrates technical feasibility, the process is shown in Fig. 1. High-density polyethylene (HDPE) was hydrogenolyzed into a PDL, successfully serving as a mild solvolysis liquefaction solvent to liquefy an Utah low-bituminous coal into a coal–plastic liquid. Our mild solvolysis liquefaction process was conducted at 400 °C and an initial H2 pressure of 6 MPa. Compared to direct coal liquefaction, a significantly lower pressure allows thinner walls of reactors and tubing. A lower temperature reduces energy consumption, and the absence of catalysts also simplifies the reactor and operation. All these significantly reduce the cost of direct coal liquefaction. A coal–plastic liquid was upgraded into several mesophase coal–plastic liquids (MCPLs) under different upgrading conditions. These MCPLs were fabricated into CFs, and the diameters of CFs ranged from 8.2 to 45.8 μm. The Young's modulus was between 75 and 759 GPa, and the tensile strength was between 0.54 and 4.03 GPa. The CFs qualified as general-purpose CF and high-performance CF, comparable to those of CFs in publications that used pure solvents, as well as commercial CFs. This work establishes a scalable method to convert waste plastics and low-rank coal into carbon fibers by integrating plastic-derived liquids as hydrogen-rich solvents in mild solvolysis liquefaction. We identified a new approach to eliminate waste plastic pollution and valorize inexpensive coal and plastic feedstocks into value-added CFs. This research has significant implications for environmental sustainability.
:
1. This ratio was selected to simulate industrial process whose ratios are from 1
:
1 to 1
:
3, and also because this ratio was proven effective in our previous work.51 Higher ratios (e.g., 1
:
0.5) increase viscosity, complicating handling, while lower ratios (e.g., 1
:
5) waste energy on excess solvent heating. Therefore, in this work other ratios were not tested, allowing a full focus on subsequent carbon fiber fabrication. From coal to liquid, tetralin and PDL led to yield of 63.4 ± 0.9% and 62.1 ± 4.3% respectively. This confirms that PDL matches tetralin in liquefaction efficiency, leading to more liquid than coal pyrolysis. MCPLs were prepared by heat-treating coal–plastic liquid under N2 (essentially a pyrolysis) at different temperatures and soaking times. The weight change during stabilization of fresh CFs was simulated by TGA using MCPLs, and the results are shown in Fig. 2. The change in weight as the temperature rises can indicate oxidation reactions. At ∼150 °C, all samples exhibited mass gain due to oxygen intake. Maximum weight occurred between 300 and 340 °C, followed by combustion. Complete weight loss by 550 °C confirms zero ash content. TGA curves will help identify the optimal stabilization temperature in section 2.3.
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| Fig. 2 TGA curves of MCPL1–3. Inset: Detail from 100–450 °C (method: under airflow, ramped at 0.5 °C min−1 from room temperature to 600 °C, and held at 600 °C for 2 h). | ||
The upgrading conditions and properties of MCPLs is summarized in Table 1. From MCPL1 to MCPL3, the yield of MCPLs decreased because thermal upgrading vaporized light components. The softening point, quinoline insolubility, and mesophase content increased due to polymerization52 and the stacking of molecules. The trends of these properties were consistent with upgrading conditions shown in Table 1, suggesting the changes were due to increasing thermal severity. MCTL (mesophase coal–tetralin liquid) was prepared using the same method as coal–plastic liquid, but with tetralin as the solvent instead of PDL. It was then thermally upgraded under the same conditions as MCPL3 for comparison. MCTL's softening point exceeded 350 °C, above melt-spinning limits, and it also features higher quinoline insolubility and lower mesophase content than MCPL3. Spinnable coal or petroleum-derived precursors require a softening point between 230–280 °C,53 low quinoline insoluble, no ash, and a narrow molecular weight distribution.53,54 PDL exhibited more favorable melt-spinning properties than tetralin, which can be attributed to the distribution of functional groups in PDL and tetralin, as indicated by 1H NMR (Table S2). To reveal the detailed mechanisms, more experiments are needed, which is not the scope of this work.
| MCPL | Condition | Yield | SP (°C) | QI | MP | Ash | d o (mm) | T (°C) | P (kPa) | v (m min−1) |
|---|---|---|---|---|---|---|---|---|---|---|
| Yield = (wt of MCPL)/(wt of coal–plastic liquid) × 100%, cited from Wang, et al.,51 the yield of MCPL1 was acquired from communication with Dr. Wang. For MCTL, yield = (wt of MCTL)/(wt of coal–tetralin liquid) × 100%. Condition: the temperature and soaking time when thermally upgrading coal–plastic liquid to MCPL. SP: softening point; QI: quinoline insoluble; MP: mesophase content. Detailed method for measuring these values can be found in the SI. do: orifice diameter of the spinneret; T: spinning temperature; p: extrusion pressure over standard atmosphere (101 kPa); v: linear velocity of drum collector. | ||||||||||
| MCPL1 | 380 °C, 6 h | 28.5% | 238 | 32% | 0% | 0 | 0.2 | 350 | 452 | 134 |
| MCPL2 | 410 °C, 3 h | 25.1% | 289 | 48% | 42% | 0 | 0.2 | 390 | 118 | 267 |
| MCPL3 | 425 °C, 3 h | 22.7% | 302 | 63% | 85% | 0 | 0.3 | 360 | 601 | 267 |
| MCTL | 425 °C, 3 h | 31.9% | >350 | 79% | 79% | 0 | — | — | — | — |
Molecular weight distribution was indicated by the distribution of mass-to-charge ratio (m/z). The results are presented as MALDI-TOF/TOF spectra shown in Fig. 3. MCPLs can be divided based on mass-to-charge ratio (m/z) as monomers (<388 Da), dimers (388–645 Da), trimers (645–890 Da), and tetramers (890–1120 Da).55,56 From MCPL1 to MCPL3, the tails of MALDI-TOF-MS spectra are more obvious, and the singular peak at 243 Da disappeared on MCPL3. This suggested that small molecules disappeared and larger molecules emerged as the upgrading gained thermal severity. From the lowest recorded m/z (40 Da) to 1120 Da, the average m/z of MCPL1, MCPL2, and MCPL3 are 636, 643 and 650 Da, respectively. Their polydispersity indices were 1.14, 1.13, and 1.12, showing a similar distribution breadth. From MCPL1 to MCPL3, the trend of average m/z is consistent with that of softening point, quinoline insoluble, and mesophase content shown in Table 1. More thorough upgrading led to the polymerization of aromatics in the coal–plastic liquid, thereby increasing the molecular weight of MCPLs, as indicated by the average m/z value. The spinning parameters of the MCPLs are summarized in Table 1. The parameters of a MCPL were determined by trial and error to produce the smallest fresh CFs while maintaining continuous winding. Among the three MCPLs, MCPL2 resulted in the smallest fresh CF at an extrusion pressure of 118 kPa and a collector speed of 267 m min−1. MCPL3 required 601 kPa and a 0.3 mm orifice, indicating a higher viscosity. MCPL1 was spun only at low drum velocity (134 m min−1) to avoid winding discontinuity. Other characterizations of MCPLs can be found in the Supplementary information. The elemental analysis is summarized in Table S3. The XRD pattern and Raman spectra are shown in S1; the extracted crystalline data are presented in Table S4. The polarized light micrographs are shown in S2. The XRD pattern and Raman spectra assist in elucidating the mechanism of heat treatment in section 2.4.
FTIR spectra were acquired to identify changes in functional groups during heat treatment. This information helps reveal the mechanism of heat treatment in section 2.4. The FTIR spectra of MCPLs, fresh CFs stabilized at SPs, and CFs are shown in Fig. 4. MCPLs showed multiple functional groups. The peak at 3040 cm−1 is due to C–H stretching vibration on the aromatic rings.58,59 No peaks were observed at 2955 cm−1; this wavenumber is assigned to stretching and in-plane bending of methyl groups (–CH3).60 A weak peak at 2922 cm−1 corresponded to the asymmetric C–H stretching of methylene groups on the naphthenic ring61 and the peak at 1440 cm−1 was assigned to methylene scissoring bending.61–63 The 900 and 670 cm−1 peaks are assigned to C–H out-of-plane bending of aromatic compounds.64 The peak at approximately 1587 cm−1 was due to the aromatic C
C bond.58,64 Aromatic and methylene groups were identified, but no methyl groups were found. This result indicates that the methylene groups of fresh CFs belonged to naphthenic rings or bridges between two aromatic rings. After the stabilization of fresh CFs, oxygen-containing functional groups appeared. A plateau between 1436 and 1152 resulted from multiple peaks. The peak at 1253 cm−1 was assigned to aryl ethers.62,65 After stabilization, the peaks centered at 3040, 1439, and between 900 and 700 cm−1 exhibit attenuated intensity. Due to the consumption of H,66–68 the vibration of C–H bonds diminished. The peaks between 1840 and 1650 cm−1 were due to the stretching vibration of carbonyl bonds from different functional groups. The tiny peak at 1840 cm−1 and the shoulder at 1771 cm−1 were assigned to the carboxylic anhydride; the vibrations of the carbonyl bond were attributed to asymmetric and symmetric stretching, respectively.69 The peak at 1734 cm−1 was assigned to a carbonyl bond of an ester.66 The peaks between 1717 and 1690 cm−1 belonged to C
O of aldehyde, carboxyl, and ketone groups.63 A tiny peak at 1655 cm−1, was due to stretching of quinone C
O.70 The band at 1300–1000 cm−1 was ascribed to the asymmetric stretching vibration of ether and hydroxyl (phenol and alcohol).67,68 After carbonization, all the above peaks disappeared because the carbonization process eliminated all the functional groups; the up-ramp of the spectrum was due to CFs having higher absorbance at lower wavenumbers.71
SEM images of CFs are shown in Fig. 5. Side views show linear streaks parallel to the fiber axis, cross-section views show different arrangements of streaks, CF2-289-1500 had a radial layout, and CF3-302-1500 and CF1-238-1500 had a random layout. These linear structures were edges of carbon sheets, typical of mesophase precursor-based CFs. Due to shear stress,10,57,72,73 melt-spinning process aligned mesophase molecules parallel to the fiber axis. These molecules became graphitic sheets after heat treatment.
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| Fig. 5 SEM images of CFs. Column 1: side view, column 2: cross-section view. (a) and (b): CF1-238-1500; (c) and (d): CF2-289-1500; (e) and (f): CF3-302-1500. | ||
The crystalline data of CFs are shown in Fig. 6a and b. They were determined from the XRD pattern and Raman spectra shown in Fig. S3a and b, and the complete data can be found in Table S5. In the Raman spectrum, theoretical graphite would exhibit a peak at approximately 1586 cm−1, known as the G band, resulting from the E2g vibration mode.74,75 Therefore, the peaks at 1586 cm−1 in the Raman spectra shown in Fig. S3b suggest a graphitic structure. An additional peak is visible at 1344 cm−1 in Fig. S3b, referred to as the D band. It has an A1g vibration mode for small crystallites or boundaries of larger crystallites.74,76 This peak confirms distorted or defective carbon. The presence of G and D bands suggests that the carbon sheets shown in the SEM images (Fig. 5) were graphitic sheets (defective graphene sheets). CF2-289-1500 had the lowest quantity of stacked layers and in-plane crystalline size (12.93 and 5.68 nm), and CF1-238-1500 had the highest (14.81 and 6.64 nm). The diameters and mechanical test results of CFs are shown in Fig. 6c and d, respectively; the detailed data are presented in Table S6. In the following discussion, diameter, Young's modulus, and tensile strength refer to their average values unless specified otherwise. The ranking of diameter is CF2-289-1500 < CF3-302-1500 < CF1-238-1500. Their Young's modulus and tensile strength followed the opposite trend: CF2-289-1500 > CF3-302-1500 > CF1-238-1500. CF2-289-1500 had the smallest diameter, and the highest Young's modulus and tensile strength: 10.8 μm, 194, and 0.85 GPa. However, CF2-289-1500 also had the lowest quantity of stacked layers and in-plane crystalline size, as discussed above. This is because crystalline data does not always align with mechanical properties, as shown in previous works.20,26,27,77 Section 2.3 will demonstrate that CFs fabricated from the same fresh CFs but with different heat treatments exhibit the same mechanical properties and crystalline data. Crystalline data help reveal the heat treatment mechanism, as discussed in section 2.4. CF2-289-1500 had the smallest diameter and highest stabilization temperature, allowing air to diffuse to the center and a thorough stabilization. CF1-238-1500 had the largest and the lowest stabilization temperature, resulting in insufficient cross-linking. During carbonization, some MCPL molecules slightly migrated or failed to polymerize with surrounding molecules. This undermined the mechanical properties. The spinning parameters and softening points of the MCPLs (Table 1) determined the diameters and stabilization temperatures, respectively, which influenced the mechanical properties. It was MCPLs that determined the mechanical performances of the CFs.
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| Fig. 7 SEM images of CFs. Column 1: side view, column 2: cross-section view. (a) and (b): CF2-266-1500; (c) and (d): CF2-312-1500; (e) and (f): CF2-335-1500. CF2-289-1500 is shown in Fig. 5c and d. | ||
Next, the soaking time of carbonization was extended from 10 min to 2 h, a “2 h” was added at the end of the label. Finally, graphitization was performed by heating fresh CF to 1500 °C at a rate of 10 °C min−1, soaking for 120 min, and then ramping to 2800 °C at a rate of 5 °C min−1, with a soaking time of 2 h. The resulting product was designated as CF2-312-2800-2h. The SEM images are shown in Fig. 8, although they bear a semblance to the CFs previously shown, crystalline data and mechanical tests indicate that they are different.
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| Fig. 8 SEM images of CFs. Column 1: side view, column 2: cross-section view. (a) and (b): CF2-312-1500-2h; (c) and (d): CF2-312-2800-2h. | ||
The crystalline data of CFs were summarized in Fig. 9a and b. They were obtained from XRD patterns and Raman spectra, as shown in Figs. S3c and d; complete data can be found in Table S5. The quantity of stacked layers and the in-plane crystalline size of CF2-289-1500 was 12.93 and 5.68 nm, slightly lower than CF2-312-1500 (12.97 and 5.75 nm). The quantity of stacked layers and in-plane crystalline size of CF2-312-1500-2h were 20.04 and 6.31 nm, respectively, higher than those of CF2-312-1500. The 2 h carbonization time enabled stacking in the Lc direction and expansion in the La direction. The crystalline structure of CF2-313-2800-2h was the closest to graphite. While other CFs' d002 and ID/IG were above 0.3383 nm and 0.70, CF2-313-2800-2h's dropped to 0.3356 nm and 0.05. Its quantity of stacked layers and in-plane crystalline size were 101.60 and 83.44, which are tremendously higher than those of CF2-312-1500-2h. Graphitic sheets were stacked in an orderly fashion and expanded with minimal interruption. The diameter, Young's modulus and tensile strength are shown in Fig. 9c and d. In the series of CF2-289-1500, CF2-312-1500, CF2-312-1500-2h, and CF2-312-2800-2h, crystalline data have the same trend with mechanical properties, i.e., the higher the quantity of stacked layers and in-plane crystalline size, the higher the Young's modulus and tensile strength. This suggests that if CFs are fabricated from the same fresh CFs but different heat treatment conditions, the mechanical performance and crystalline data will align. Young's modulus and tensile strength of CF2-312-1500-2h was 238 and 1.15 GPa. Although its tensile strength was almost equal to CF2-312-1500 (1.11 GPa), its Young's modulus was 18.4% higher (201 vs. 238 GPa). The Young's modulus and tensile strength of CF2-312-2800-2h reached 759 and 4.03 GPa.
Here, CFs fabricated in this work are classified based on their mechanical performances. In chapter 4 of “New Carbons”,13 Fig. 4-2 shows CFs with Young's modulus of 50–100 GPa, tensile strength of 0.5 to 1.1 GPa are general-purpose CFs. It also states “Carbon fibers with higher strength and modulus than GP-grade (general purpose-grade) are called high-performance grade (HP-grade)”. According to Chapter 11 of “Lignin in Polymer Composites”,14 “CFs with high tensile strength (>1.4 GPa) are called ‘high-performance carbon fibers’. Relatively low tensile strength CFs are called ‘general purpose carbon fibers’.”. Therefore, CF2-312-2800-2h is a high-performance CF, and the rest are general-purpose CFs. CF2-312-1500-2h and CF2-312-2800-2h were compared with CFs from other publications and commercial CFs, as shown in Table 2. Compared to other literature, CF2-312-2800-2h had high Young's modulus and tensile strength, and its performance was also comparable to commercial K1392U, K13916, YS-80A, XN-80-60S, and M60J.
| Ref. | CF | Precursor | Solvent | ST (°C) | C/G (°C) | d (um) | YM (GPa) | TS (GPa) | ε (%) |
|---|---|---|---|---|---|---|---|---|---|
| ST: stabilization temperature; C/G: carbonization/graphitization temperature; d: diameter; YM: Young's modulus; TS: tensile strength; ε: strain-to-failure. CTP: coal tar pitch; PP: petroleum pitch; THN: tetralin; 4HNP: tetrahydronaphthalene; MeNP: methylnaphthalene; FCC: fluid catalytic cracking, no solvents were used. ETHO: ethylene tar hydrodeconstructed oil. K1392U, K13916, and K13D2U: https://mccfc.com/pitch-fiber/, and ε was cited from https://www.hajime.com.tw/Upload/product_201805210812374.pdf. YS-80A: https://www.ngfworld.com/dcms_media/other/skill_catalog06-1.pdf. XN-80-60S: https://www.ngfworld.com/dcms_media/other/skill_catalog05.pdf. M60J: https://www.toraycma.com/products/carbon-fiber/. | |||||||||
| This work | CF2-312-1500-2h | Sufco coal | PDL | 313 | 1500 | 11.7 | 238 | 1.15 | 0.52 |
| This work | CF2-312-2800-2h | Sufco coal | PDL | 313 | 2800 | 8.2 | 759 | 4.03 | 0.59 |
| 25 | MHCTP-420-7 | Coal | 4H-NP | 280 | 2800 | 12.0 | 689 | 3.09 | — |
| 26 | CTP-20-GFs-1 | Coal | THN | 280 | 2850 | 10.5 | 656 | 3.72 | — |
| CTP-20-GFs-3 | Coal | THN | 280 | 2850 | 9.6 | 676 | 3.49 | — | |
| 27 | C-MP-CFs | Coal | FCC | 280 | 3000 | 10.3 | 620 | 3.86 | 0.62 |
| P-MP-CFs | Petroleum | FCC | 280 | 3000 | 10.0 | 725 | 2.89 | 0.41 | |
| C/P-MP-CFs | CTP : PP = 1 : 1 (mass) |
— | 280 | 3000 | 9.8 | 773 | 3.65 | 0.49 | |
| 28 | H3N3-TLE | GR bitumen coal | MeNP and THN | 270 | 1000 | 10.2 | 140 | 1.80 | 1.40 |
| H3N3.5-TLE | GR bitumen coal | MeNP and THN | 270 | 1000 | 10.5 | 130 | 1.80 | 1.40 | |
| H3N3-TLE | GR bitumen coal | MeNP and THN | 270 | 2800 | 9.3 | 450 | 3.00 | 0.70 | |
| H3N3.5-TLE | GR bitumen coal | MeNP and THN | 270 | 2800 | 9.8 | 370 | 2.40 | 0.70 | |
| 20 | DO*-CF | Decant oil | — | 300 | 2000 | 22.7 | 795 | 0.96 | 0.12 |
| SFDO-TS | Springfield coal | Decant oil | 300 | 2000 | 19 | 479 | 0.90 | 0.19 | |
| SFDO-THFS | Springfield coal | Decant oil | 300 | 2000 | 23.2 | 475 | 0.94 | 0.20 | |
| 77 | CMP-25-GFs | CTP | ETHO | 280 | 3000 | 12.8 | 658 | 3.56 | 0.54 |
| 78 | AR50, winding speed 800 RPM | Naphthalene pitch | THF | 270 | 2400 | 8.0 | 618 | 4.00 | 0.60 |
| 79 | MPGF-A | Petroleum pitch | — | 290 | 3000 | 16.9 | 855 | 3.09 | — |
| Mitsubishi | K1392U | CTP | — | — | — | — | 760 | 3.70 | 0.50 |
| Mitsubishi | K13916 | CTP | — | — | — | — | 760 | 3.20 | 0.40 |
| Mitsubishi | K13D2U | CTP | — | — | — | 10.0 | 935 | 3.70 | 0.40 |
| Nippon | YS-80A | Pitch | — | — | — | 7.0 | 785 | 3.63 | 0.50 |
| Nippon | XN-80-60S | Pitch | — | — | — | 10.0 | 780 | 3.43 | 0.50 |
| Toray | M60J | PAN | — | — | — | 5.0 | 588 | 3.82 | 0.70 |
Heat treatment includes multiple steps of stabilization and carbonization, and optional graphitization. Without stabilization, fresh CFs fuse during carbonization. Stabilization chemically crosslinks the fresh CFs, making them infusible. As shown in Fig. 4, after stabilization, the peaks of aromatic C–H and methylene groups shrink and disappear, and oxygen-containing groups appear. The mechanism of stabilization is illustrated in Fig. 11. When the temperature is below 250 °C, methylene groups are oxidized into ketone groups, and some studies have also found that aromatic C–H groups are converted into quinone groups.70 Crosslinking occurred at higher temperatures between 250 and 400 °C. The C–C bond on the naphthenic rings ruptured, and aldehyde, carboxyl, anhydride group, and intramolecular peroxide were formed subsequently.63 These functional groups on neighboring molecules are crosslinked by losing CO, CO2, or H2O, or simply radical recombination. The aromatic rings' surface was oxidized to phenol at this temperature interval.90 Temperatures above 400 °C produce excessive phenols and rupture aromatic rings by opening C–C bonds, leading to the formation of carboxylic acid.90 The defects of polyaromatic structures reduce mechanical properties.
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| Fig. 11 Proposed mechanism of stabilization when temperature is lower than 250 °C, and between 250 and 400 °C. | ||
Carbonization can be divided into several phases. Drbohlav et al.61 discussed the chemical reactions from a functional group perspective, and Oberlin89 summarized the mechanisms based on crystalline structures. The FTIR spectra in Fig. 4 show that all the functional groups disappeared after carbonization. As shown in Fig. 12, the crosslinks vaporize as CO, CO2, and H2O at between 400 and 600 °C,61 and C–C bond replaces the crosslinks. At a maximum temperature of 800 °C, all heteroatoms are eliminated.89 In MCPL, molecules are sheet-like aromatics, and multiple such aromatics are piled up in parallel, forming basic structural units.89 Melt-spinning loosely aligned these basic structural units parallel to the axis of fresh CFs. The effect of carbonization at 1500 °C is revealed by comparing crystalline data of MCPLs (Table S4) and corresponding CFs (Table S5, or Fig. 6a and b). When MCPL1, MCPL2, and MCPL3 were fabricated into CF1-238-1500, CF2-289-1500, and CF3-302-1500, respectively, the quantity of stacked layers increased by 48.55%, 17.33% and 38.10%, and the in-plane crystalline size increased by 27.45%, 10.29% and 0.71%. The increased percentage of stacked layers was larger than the in-plane crystalline size, suggesting that carbonization facilitated stacking rather than in-plane expansion of graphitic sheets.
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| Fig. 12 Proposed mechanisms of carbonization and graphitization. Upper: change of functional groups; lower: change of crystalline structure. | ||
Crystalline data also revealed that a longer soaking time benefited stacking and in-plane expansion. In Fig. 9a and b (from Table S5), the quantity of stacked layers and in-plane crystalline size of P4-313-1500-2h are 55.83% and 9.74% higher than P4-313-1500. The limited increase in the amount of stacked layers and in-plane crystalline size led to the development of general-purpose CFs. To produce high-performance CFs, graphitization is necessary at above 1500–2000 °C. The effect of graphitization can also be revealed in Fig. 9a and b (from Table S5). When graphitized at 2800 °C, the quantity of stacked layers and in-plane crystalline size of P4-313-2800-2h reached 101.60 and 83.44 nm, they are 5.07 and 13.22 times of P4-313-1500-2h, respectively. In contrast to carbonization, graphitization has a more pronounced effect on in-plane expansion. At temperatures above 1500 °C, the basic structural units disappeared,89 graphitic sheets merged into a stack of wrinkled, large ones at approximately 1700 °C. Wrinkles are eliminated between 1900 to 2100 °C, and above 2100 °C, the in-plane defects diminish. The schematic of organized graphitic sheets can be seen in Fig. 12.
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1. The mixture was heated under an initial H2 pressure of 6 Mpa at 450 °C for 60 min. After mild solvolysis liquefaction, the product, insoluble in hexane but soluble in THF is defined as coal–plastic liquid. To increase the mesophase content, coal–plastic liquid was thermally upgraded under N2 flow at various temperatures and durations, and the reactor's residual material is referred to as mesophase coal–plastic liquid (MCPL). HDPE hydrogeniolysis, mild-solvolysis liquefaction, and thermal upgrading were repeated three times to make sure repeatability. The characterization data (e.g. yield) were averaged.
The subsequent heat treatment procedure included stabilization and carbonization to produce general-purpose CF, and an extra graphitization was applied to produce high-performance CF. Stabilization was performed using a Thermo Scientific Lindberg Blue M tube furnace. Under air or oxygen, the temperature ramped at 0.5 °C min−1 to a set point (stabilization temperature) and maintained isothermally for 1 h. Carbonization was performed by heating at 10 °C min−1 to the final carbonization temperature and soaking. If graphitization was needed, the same carbonization protocol was followed, and after soaking, the furnace ramped at 5 °C min−1 to 2800 °C before another soaking. Details on soaking durations are provided in section 2.2 and 2.3. If only carbonization were performed and the soaking time were 10 minutes, a Carbolite HTRH 18/40/500 tube furnace would be used. Otherwise, for longer soaking times or graphitization, an MRF T-4X8-G-G-3000-VM-G high-temperature furnace was utilized. The heat-treated fibers were called carbon fibers (CFs). In this work, a category of CF was denoted as “CF2-289-1500”, meaning this CF was produced by spinning MCPL no. 2, stabilized at 290 °C for 1 h, and carbonized at 1500 °C for 10 min. If the CF was graphitized, only the graphitization temperature was shown, if soaking time was not 10 min, the actual time was given in the label. For example, “CF2-312-2800-2h” denoted this CF was graphitized at 2800 °C for 2 h.
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To observe the morphology and measure the diameters of CFs, a Quanta 450 FEG scanning electron microscope (SEM), a Thermo Scientific Helios 5 UX Focus Ion Beam/Scanning Electron Microscope (FIB-SEM), and a Leica Microsystems DM2900P microscope were used, depending on availability, to visualize CFs. The mechanical properties of CFs were measured on a HY005E single fiber strength tester. In this work, one fiber from a category of CFs is called a filament. The method was based on the ASTM C1557 standard. The sample mount was prepared by piercing A4 paper with a three-hole punch. A filament was glued by Gorilla super glue and JB Epoxy adhesive across the hole and dried for 24 h. During the mechanical test, the pull speed was 2 mm min−1, at least ten filaments were tested for each category of CFs, and the gauge length of the specimen was 7.5–30 mm. Young's modulus and tensile strength were determined by the stress–strain (σ–ε) curves.
The data that support the findings of this study are available from the corresponding author upon reasonable request.
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