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Original article
08 2023
:16;
104901
doi:
10.1016/j.arabjc.2023.104901

Microwave curing carbon fiber composites automobile rearview mirror

Faculty of Metallurgical and Energy Engineering. Kunming University of Science and Technology, Kunming 650093, China
State Key Laboratory of Complex Nonferrous Metal Resources Clean Utilization, Kunming University of Science and Technology, Kunming 650093, China

⁎Corresponding authors. 20040051@kust.edu.cn (Shenghui Guo), houmingkmust@163.com (Ming Hou)

Disclaimer:
This article was originally published by Elsevier and was migrated to Scientific Scholar after the change of Publisher.

Peer review under responsibility of King Saud University.

Abstract

Microwave curing technology was used to fabricate the automobile rear-view mirror, which is a specially shaped component of carbon fiber/epoxy resin composite. Through dynamic thermo-mechanical analysis, differential scanning calorimetry, scanning electron microscope, and infrared spectroscopic analysis, the curing degree and structure of microwave-cured and conventionally cured samples were compared and analyzed. The results showed that the curing mechanism of microwave curing is different from that of thermal curing. Microwave curing improves the curing reaction rate and shortens the curing period. It was found that the curing degree of microwave-cured samples was significantly higher than that of conventionally cured samples.

Keywords

Carbon fiber prepreg
Microwave curing
Dynamic thermo-mechanical
1

1 Introduction

Carbon fiber is a high-strength and high-modulus fiber with a carbon content above 90%, and its resistance to high temperatures ranks first among all chemical fibers. It is also an excellent material for manufacturing high-tech equipment for industries such as aerospace (He, 2004). Carbon fiber-reinforced composites are a type of material that is made up of carbon fiber or carbon fiber fabric as the reinforcement and a matrix, like resin or ceramics. Carbon fiber-reinforced composites have low density, good strength at high temperatures, high stiffness, higher fracture toughness, fatigue resistance, and creep resistance. It also has a small thermal expansion coefficient, a high specific heat capacity, low thermal conductivity, and excellent thermal shock and friction resistance, making it an important part of modern aerospace and aviation, automobiles, and the energy industry (Robertson et al., 2018).

Compared to metal materials, cryogenic propellant tanks, made of composites like carbon fiber, can lose 20–40% of their weight to accomplish the goals of reducing aircraft cost and increasing aircraft capacity (Zhang and Zhang, 2014). Moreover, carbon fiber composites are also widely used in advanced large civil aircraft, making up over 20% of overall structural weight (Du, 2007). Comparing the properties of materials used in automobiles at present, it can be found that carbon fiber composites have great advantages in terms of lightweight, safety, comfort, reliability, and improving the development level of car bodies (Zhang Ailing Zhang Youheng, 2017). When used as an automobile part material, it can reduce the dead weight by 1/3 and make the automobile lightweight, which not only saves fuel and protects the environment but also moves down the center of gravity of the whole automobile, improves the handling stability of the automobile, and makes the operation of the automobile safer and more stable (Ma Xiaokun et al., 2020). For instance, the renowned Mercedes-Benz manufacturer will produce automobiles composed entirely of carbon fiber-reinforced resin matrix composites. The maximum speed of the car can reach 350 km/h, and it can attain an acceleration from 0 to 100 kmph in only 1.8 s (Song Yanli Yang Long Guo Wei Hua Lin, 2017). Thus, it can be seen that the applications of carbon fiber-reinforced composites in auto parts have brought about new revolutions and breakthroughs in the automobile industry.

Generally, curing is an essential step in manufacturing components of carbon fiber composites, which refers to the process of curing sticky resin matrix into the solid phase at certain temperatures via a chemical reaction or physical melting. However, because of the high cost of carbon fiber composites and the lack of high-speed preparation techniques, carbon fiber composites cannot be widely used in the automobile industry. It is estimated that the global requirement for carbon fiber composites will increase to 150,000 tons by the year 2023 (Lin, 2022).

In the modern curing process of carbon fiber composites, the autoclave process is widely used and also the most common molding method. It compacts materials in the confined tank and heats them through air circulation (Zhang Linglin et al., 2018). It has a wide application range and a stable and reliable molding process. However, this method has low production efficiency, poor temperature control, a long curing time, a high cost, and high energy consumption (Xie et al., 2013; Fernández et al., 2003). It may also cause environmental pollution, particularly with the current advocacy for energy conservation and environmental protection (Zhou Wenying et al., 2005). Therefore, searching for a new, high-efficiency, energy-saving curing method is imperative.

Besides the current pressing need for a viable composite molding technology and to solve the problems of the long production cycle and high manufacturing cost of the traditional composite molding process, the researchers put forward a process of curing carbon fiber-reinforced resin matrix composite components by microwave heating. It is found that microwave curing is a method of integral heating of composite materials, which can greatly shorten the process cycle and enhance the molding rate of components (Galos, 2020). It is a selective heating, energy-saving, and efficient process. It allows fast, real-time control of the process, and the equipment cost of this method is also low (microwave curing furnace). For the same process conditions, microwave curing of polymer matrix composites is superior to (traditional) thermal curing (Ogonna et al., 2020).

Aniruddh Vahisth and coworkers put a microwave curing process into the carbon fiber composite curing field and found that the curing process can be completed in a short time in the presence of microwaves. They demonstrated a consecutive prepreg manufacturing method and got the required temperature by controlling translational velocity via a RF application (Aniruddh Vashisth et al., 2020). Wang Chunwen (Wang Chunwen et al., 2021) cured carbon fiber composites by combining microwave heating with the curing process. The results showed that the tensile strength and modulus of the microwave-cured test-piece were both higher than those of the traditional thermal curing test-piece, which showed that microwave curing not only significantly reduced curing residual stress inside the material but further improved its tensile property. S. K. Dasari and M. Rangapuram (Dasari et al., 2021) compared the difference between microwave curing and traditional curing. The research showed that the short beam strength and flexural strength of the microwave-cured plane plate were the same as those of the control test-piece, with the flexural modulus, peak impact force, and spring back energy increasing by 12%, 6%, and 18%, respectively. Through previous studies, it is found that the carbon fiber composites prepared with microwave curing had better combination properties than those prepared with the traditional heating process. Therefore, microwave curing is regarded as a promising method of processing composites. Unfortunately, researchers are mainly committed to the study of carbon fiber composite plates, and there are few special-shaped materials. At present, the microwave curing process rarely involves the three-dimensional (3D) movement of heated materials in a microwave cavity.

In this work, 3D special-shaped components of carbon fiber/epoxy resin composites were prepared and studied by the microwave curing process. In the current microwave curing technology, the biggest problem is uneven curing, which, through research, can be found in the laminate. Microwave curing will have uneven curing due to the existence of temperature differences in different locations. The shape of the car mirror shell is more complex, so it would be more difficult to control the uniformity of microwave curing. Through a large number of experiments, the location of a more uniform microwave field was found inside the device, and the uniformity of the entire rearview mirror housing was controlled through a complementary method of cold and hot spots. The microstructure information and relevant properties of samples produced with different methods were analyzed and compared. The fabrication of 3D special-shaped carbon fiber-reinforced composite components and the use of novel microwave curing will boost the development of carbon fiber-reinforced composites.

2

2 Experimental section

2.1

2.1 Experimental equipment

The microwave curing is done using the self-made equipment of Kunming University of Science and Technology. As shown in Fig. 1(a), the curing equipment has a large cylindrical resonant cavity. The material and the microwave field can move relatively. There is an electric motor in the cavity that enables the material to simultaneously carry out reciprocating linear and rotation motion inside the cavity, which pushes the laminate to move in multiple dimensions inside the cavity. The electromagnetic field distribution inside the laminated plate is constantly changing to ensure uniform heating. The microwave curing equipment has six microwave inputs, which are controlled by six magnetrons (Fig. 1(b)). The power of each magnetron ranges from 100 W to 3000 W, and the furnace contains support that can reciprocate. The cylindrical cavity design and large cavity size adopted are shown in Fig. 1(b). The six magnetrons serve as microwave sources, of which three magnetrons are mounted on each side. The electromagnetic field distribution shown in Fig. 2 is obtained by software simulation. It can be seen that the magnetic field distribution inside the cavity is relatively uniform, and only the area near the circular end face has the phenomenon of field intensity concentration.

(a) Microwave curing equipment; (b) Equipment cavity and magnetron distribution.
Fig. 1
(a) Microwave curing equipment; (b) Equipment cavity and magnetron distribution.
Simulation of the magnetic field in the furnace.
Fig. 2
Simulation of the magnetic field in the furnace.

2.2

2.2 Experimental materials

The layer used in this experiment is T300 carbon fiber unidirectional prepreg, model USN10000, with a resin content of about 30%. The resin system of this prepreg is epoxy resin, and the type of curing agent is bisphenol A. The prepreg can be stored at room temperature for one month, at 0 °C for six months, and at −18 °C for one year. Other supporting auxiliary materials, such as demoulding cloth, isolation film, breathable felt, and vacuum bags, were provided by Tianjin Ertek, and the experimental mold was provided by Shenzhen Hengxinda Plastic Hardware Products Co., Ltd. The mold material is polytetrafluoroethylene. Because polytetrafluoroethylene has a low complex dielectric constant and is also a wave-transparent material, it does not cause any change in the effect of microwaves on carbon fiber prepreg in the experiment.

2.3

2.3 Sample preparation

Samples were prepared as follows: First of all, the mold release agent was coated on the mold, and then the carbon fiber prepreg was laid on the mold in three layers. Then we apply aluminum foil tape to cover the edges of the carbon fibers to prevent the generation of electrostatic charges at the ends of the fiber film. Then the mold release cloth, isolation film, and breathable felt were laid out in turn, and the mold was packaged in a vacuum bag. After packaging, it was vacuumed until its vacuum degree reached 150 mbar.

The laying of carbon fiber prepreg on the mold is shown in Fig. 3. The laying in such a manner will result in carbon fiber prepreg with different thicknesses due to the curvature. Therefore, the carbon fiber prepreg is cut into small squares at the thin laying to supplement the uniform thickness of the laying of carbon fiber prepreg on the mold.

Carbon fiber prepreg lay-up.
Fig. 3
Carbon fiber prepreg lay-up.

2.4

2.4 Experimental process

2.4.1

2.4.1 Conventional oven curing

The sample was put into the oven and heated from room temperature (25 °C) to 120 °C at a rate of 3 °C/min and kept for 2 h to obtain the sample. At the end of the holding time, the instrument was turned off and the sample was allowed to cool down naturally to room temperature within the furnace.

2.4.2

2.4.2 Curing by microwave heating

The prepared sample and mold were placed inside the microwave equipment, the optical fiber was affixed at the position shown outside the vacuum bag to observe the temperature change, and thermal insulation cotton was laid on. The following Fig. 4 shows the position of the optical fiber. All six magnetrons were then turned on simultaneously, and the output power of each magnetron was set to 100 W. The reciprocating linear movement of the mold started after the microwave output was turned on for 2 s, the mold displaced at a rate of 0.01 m/s for 200 mm. After 23 min of microwave irradiation, the output power of six magnetrons was increased to 150 W and the samples were irradiated for another 19 min. The samples were then kept warm for 2 h without microwave irradiation. The heating process is shown in Fig. 5. At the end of the holding time, the instrument was turned off and the sample cooled down to room temperature naturally. In the heating process, as shown in the Fig. 5, the temperature will not exceed 120 °C because when the temperature inside the microwave instrument reaches the specified limit, the magnetron will stop radiating, and without a heat source, the temperature will not continue to rise.

The arrangement of the optical fiber temperature measuring probe when the rearview mirror of the car is cured.
Fig. 4
The arrangement of the optical fiber temperature measuring probe when the rearview mirror of the car is cured.
Temperature time power curve.
Fig. 5
Temperature time power curve.

2.4.3

2.4.3 Microwave heating process

The same sample was used to repeat the above-mentioned heating process without holding for 2 h to obtain incompletely cured samples. At the end of the heating process, the magnetron was turned off and the sample naturally cooled down to room temperature within the microwave oven.

2.5

2.5 Characterization of experimental results

In this experiment, four methods were used to characterize raw materials and finished products. Also, the curing processes of both microwave curing and conventional curing were compared and calculated. The curing degree of samples and prepared products were analyzed by a Netzsch DSC 200 F3 differential scanning calorimeter (DSC) made in Germany. The glass transition temperature of the finished product was analyzed by the TA DMA850 Dynamic Thermomechanical Analyzer (DMA). The functional groups of raw materials and finished products were analyzed by Bruker Tensor 27 Fourier Transform Infrared Spectroscopy (FTIR). The cross sections of raw materials and prepared products were analyzed by TESCAN MIRA LMS scanning electron microscope (SEM).

3

3 Results and discussion

3.1

3.1 Conventional and microwave-cured samples

Fig. 6 is a conventionally cured sample, some umbilications can be observed on the side. Fig. 7(a) is a microwave-cured sample with multiple repetitions of the microwave optimum process, and Fig. 7(b) is an enlarged view of one of the individual samples, which can be observed to be smooth and flat with a stable shape, although a small amount of vacuum glue has adhered to the sample.

Conventionally cured samples.
Fig. 6
Conventionally cured samples.
(a) Enlarged view of a single sample at the microwave optimal curing process; (b) Multiple samples under multiple iterations of the microwave optimal curing process.
Fig. 7
(a) Enlarged view of a single sample at the microwave optimal curing process; (b) Multiple samples under multiple iterations of the microwave optimal curing process.

3.2

3.2 Curing result characterization

3.2.1

3.2.1 Differential scanning calorimeter analysis

Differential scanning calorimetry (DSC) is used to monitor the thermal behavior of the sample cured through different methods during the heating process, and the heat flow result is shown in Fig. 8. The step-like curve at a temperature above 100 °C implies the occurrence of the glass transition. The obtained glass transition temperature ( T g ) and specific heat change after glass transition are listed in Table 1.

Heat flow curves for samples after different curing processes.
Fig. 8
Heat flow curves for samples after different curing processes.
Table 1 T g and specific heat change for the different curing processes.
Curing types T g from DSC(°C) Specific heat change
Incomplete curing 108.64 0.081
Microwave curing 113.87 0.116
Conventional curing 105.74 0.099

T g of the sample through microwave curing is about 8 °C higher than that of conventional curing, and T g for an incompletely cured sample through microwave curing is moderate. The gradual enhancement of the T g indicates an increase in the curing degree (Zhou et al., 2019). Besides, the specific heat change of the sample after microwave curing is 17.2% greater than that of conventional curing. The larger specific heat change reflects an enlargement of absorbed thermal energy for a specific mass of the sample to rise one degree in temperature (Baghad and El Mabrouk, 2022). Since the resin releases heat during the curing process, the more complete the curing, the more heat is released. Consequently, in the reverse process for glass transition of the sample with a higher curing degree, the freezing polymer chains at a glassy state need to absorb more heat to overcome the higher energy barrier after curing and become movable (Strobl, 2007). Therefore, it absorbs much more heat. At the same time, we found that the glass transition process for the sample under incomplete curing is not as obvious as it is for the other two samples in the heat flow curve. This could be explained by the inhomogeneous internal structure of the material; only part of the chemical structure formed cross-links during curing, while others remained uncured. Therefore, the flow curve reflects both the cured and uncured transition processes of the whole material, and the distinguishable step-like heat flow curve implies a homogeneous structure of samples through completed curing. It is worth noting that a lot of experiments have been done with the microwave curing method mentioned in this paper and that several DSC tests have been conducted. The test results in this section are typical.

3.2.2

3.2.2 Dynamic mechanical analysis

Dynamic mechanical analysis (DMA) can measure the relationship between the mechanical properties of viscoelastic materials and time, temperature, or frequency. It is widely used in the study of the viscoelastic properties of material and can obtain the dynamic storage modulus, loss modulus, and loss tangent of materials. The energy storage modulus (E') reflects the elastic characteristics of the sample, the degree to which the sample can recover from deformation, and the capacity of the sample to store energy under the influence of stress. The loss modulus (E“) reflects the viscous characteristics of the sample, the degree of heat consumption (loss) of the sample during the deformation process, and the energy dissipation capacity of the material. The loss angle ( tan δ ) is the ratio of the loss modulus to the energy storage modulus, DMA results of three samples treated with incomplete curing, microwave curing, and conventional curing are shown in Fig. 9. The glass transition temperature in DMA is determined by the position of tan δ maximum, and the occurrence of glass transition leads to a one-magnitude drop in the storage modulus (E'). For the incompletely cured sample and conventionally cured sample, the peak of maximum loss appears at about 132.8 °C, while in the microwave-cured sample, a sub-peak appears at 155 °C after the main peak at 127.25 °C, as Fig. 9(b) shows. We deduce that the main peak derives from the transition process, which is the same as the glass transition occurring in the other two samples, while the sub-peak indicates that microwave curing forms a small range of stacked chains. With microwave curing, the flexibility of a part of the molecules becomes worse, and a higher temperature is needed to overcome the energy barrier, leading to a sub-peak occurrence. It can be seen from the data that the glass transition temperature from the conventional curing method is almost the same as that of incomplete curing, and microwave curing reduces the temperature of the main transition process while causing a sub-transition temperature, and the loss tangent of the sub-transition is lower than that of the main transition. The combination of two transition peaks implies that the overall transition process is not completed until the temperature reaches 155 ℃. It can be concluded that microwave curing results in a higher curing degree.

Dynamic thermal mechanical analyzing results of the sample under (a) incomplete curing, (b) microwave curing, and (c) conventional curing. (d) Comparison of T g and storage modulus at glassy state after different curing methods.
Fig. 9
Dynamic thermal mechanical analyzing results of the sample under (a) incomplete curing, (b) microwave curing, and (c) conventional curing. (d) Comparison of T g and storage modulus at glassy state after different curing methods.

A comparison of T g from both the DSC and DMA tests as well as the storage modulus at glassy state for three samples is shown in Fig. 9(d). Here we found that the storage modulus of the sample with conventional curing is much lower than that of microwave curing, by about one-magnitude. The storage modulus of the completed microwave-cured sample and the incomplete microwave-cured sample are at the same degree. This modulus difference indicates the material cured through microwaves has better mechanical strength, which is very important for application (Li et al., 2017). The T g obtained from the DSC and DMA tests demonstrates a similar result: that the sample completely cured by microwave has the highest glass transition temperature and indicates the highest degree of curing. To note, the difference in T g obtained through DSC and DMA is due to the different measuring mechanisms. The T g determined from DSC is a result of thermal behavior change during the transition, while the T g determined from DMA is a direct result of the modulus change when the polymer chain is movable.

3.2.3

3.2.3 FTIR analysis

To understand the influence of different curing methods on chemical reactions, the Fourier transform infrared spectrum (FTIR) is used, and the results of the uncured, incompletely cured, microwave-cured, and conventionally cured specimens are shown in Fig. 10.

FITR spectrum for samples with (a) no curing, (b) incomplete curing, (c) microwave curing, and (d) conventional curing.
Fig. 10
FITR spectrum for samples with (a) no curing, (b) incomplete curing, (c) microwave curing, and (d) conventional curing.

The vibration of epoxy ring molecules causes a peak at a wavenumber of 908 cm−1, and the intensity becomes weaker along the curing process, which implies the original chemical bonds in the epoxy ring are broken and new cross-links are formed in molecules; this is also the nature of curing (Xu et al., 2016). This chemical reaction also leads to the reduction of peak intensity at 1630 cm−1, which presents the N–H in-plane bending vibration. The chemical group vibrations shown in the FTIR spectrum are listed in Table 2.

Table 2 Chemical groups exhibited in the FTIR spectrum.
Wavenumber/cm−1 Chemical group
831 C–H out-of-plane deformation on para-substituted benzene ring
908 Epoxy ring vibration
1036 C–H in-plane deformation on para-substituted benzene ring
1245 C-O-C antisymmetric stretching
1365 Bis-methyl symmetric deformation vibration of bisphenol-A
1510 Para-substituted benzene ring -C = C- bending vibration
1607 Benzene ring -C = C- bending vibration
1630 N–H in-plane bending vibration

The same positions of peak appearance under microwave curing and conventional curing indicate the same products after the chemical reaction; therefore, the formed cross-link networks are also the same. However, the peak intensity shows a small difference and means a divergence in the curing degree. The relative curing ratio between the two curing methods is therefore calculated through the relative peak height between epoxy ring vibration and C–H vibration on the benzene ring, following the equation. Relativecuringratio = O - A microwave O - A conventional

Where O, Amicrowave and Aconventional are the relative peak heights for uncured material, microwave-cured material, and conventionally cured material, respectively. According to the relative peak height, the curing degree of the microwave-cured sample is 1.918 times that of the conventionally cured sample. Notably, due to the superposition of neighboring peaks, the approximate result calculated from peak height might deviate from the real ratio.

3.2.4

3.2.4 SEM analysis

According to the DMA analysis, the microwave-cured composite showed a higher storage modulus than the conventionally cured specimens, which is mainly influenced by the reinforced resin matrix. SEM micrographs of the composite composed of the resin matrix and local fiber, as displayed in Fig. 11, show the direct influence of different curing methods on materials.

SEM micrographs of samples experiencing incomplete curing, microwave curing, and conventional curing from left to right. (a)-(c) composites; (c)-(d) local carbon fiber.
Fig. 11
SEM micrographs of samples experiencing incomplete curing, microwave curing, and conventional curing from left to right. (a)-(c) composites; (c)-(d) local carbon fiber.

Compared to incomplete curing and conventional curing, it is obvious that the specimen under microwave curing shows a homogenous matrix that is uniform and compact, as Fig. 11(b) exhibits, while the resin matrix in Fig. 11(c), under conventional curing, is inhomogeneous. The matrix at the bottom of Fig. 11(c) is well-cured, while the matrix in other areas shows a loose state. The incomplete curing matrix in Fig. 11(a) is uniform, but to a lower degree than in Fig. 11(b). The different homogeneity of the results is due to the different heating mechanisms. Microwave curing generates heat through dielectric loss throughout the material (Mgbemena, et al., 2018). When an alternating electromagnetic field is applied, all dipoles tend to align along the direction of the electromagnetic field the violent movement and collision of molecules would generate heat; therefore, the total material can be cured uniformly (Chen, 2018). However, the conventional method conducts heat from an external source to the inside through radiation, leading to a large temperature gradient inside the material, resulting in uneven curing of resin along the thickness direction, and making it easy to produce large internal stresses (Mgbemena, et al., 2018). The unevenly cured resin consequently can not support the whole structure and results in a lower modulus. Furthermore, the loose structure of the conventionally cured samples contains more voids than the compact sample, which would lead to a reduction in the mechanical properties of composites, especially the shear stress and compressive modulus (Baghad et al., 2021). As for the carbon fiber, the local morphology can be observed in Fig. 11(c-d d-f). There is no distinguishable difference in the morphology from different curing processes, and the high curing degree of microwave curing does not lead to defects in the carbon fiber composites. At the same time, the process of microwave curing involves heating the resin in the carbon fiber prepreg to produce a crosslinking reaction. The reaction does not affect the carbon fiber in the prepreg because the carbon fiber does not participate in the reaction; hence, the scanning electron microscope reveals no change in the carbon fiber.

3.3

3.3 Comparison of microwave and conventional curing processes

According to the above analysis, it can be stated that microwave curing is a novel and effective method to prepare carbon fiber composite mirror housing for automobiles. To further study the energy efficiency of microwave curing, the energy consumption was calculated. The used apparatus and related energy consumption parameters are listed in Table 3. The total energy consumption from microwave curing is 3.422 kWh, 34% lower than that of conventional curing (5.2 kWh), which proves microwave curing is an efficient and energy-saving method for preparing carbon fiber composite automobile mirror housing. The difference in energy consumption is related to the heating mechanisms of conventional heating and microwave heating. The energy consumption of conventional curing is mainly from a hot blast stove, which involves the transfer of energy or heat inside the material and results in huge energy dissipation during the process. While for microwave heating, the microwave has a very strong penetration ability and can be straight when used on a material. The energy is dissipated inside the material due to the conversion of electromagnetic energy to internal energy. Different from the traditional heating mode, microwave heating does not require a high-temperature medium, and most of the microwave energy is absorbed by the medium and converted into the heat required for heating. Therefore, the heat transfer process is avoided.

Table 3 Apparatus and related energy consumption parameters.
Equipment Power/W Working hours/min Energy consumption/KW·h Total energy consumption/KW·h
Conventional curing Hot blast stove 2050 140 4.78 5.2
Vacuum pump 180 140 0.42
Microwave curing Magnetron 600 23 1.34 3.422
900 74
Control system 200 142 0.473
Cooling system 300 142 0.71
Vacuum pump 180 142 0.426
Linear motor 200 142 0.473

4

4 Conclusion and future prospects

The effects of microwave curing and conventional curing methods on T300 carbon fiber unidirectional prepreg were studied. The thermal behavior, modulus, products of curing, as well as the microscale morphology of samples experiencing different curing methods were studied using DSC, DMA, FTIR, and SEM. The glass transition temperature of samples cured by microwave is 8 °C higher than conventional curing, and the specific heat change is also 17.2% greater. T g obtained by DMA gives a similar result. At the same time, the result indicates a local chain stack was formed. The storage modulus of the conventionally cured sample is one order of magnitude lower than that of the microwave-cured sample. Although the cured products are the same for both methods, the calculated result based on the FTIR peak height indicates the degree of curing through microwave is 1.918 times that of the conventional curing. SEM micrographs demonstrate a more homogeneous matrix for microwave curing. It could be concluded that the application of microwave curing led to a higher curing degree, a higher storage modulus, and a more uniform resin matrix. These results can give some basic references for the practical application of the microwave curing method.

It is hoped that this paper will provide more insight on the application of microwaves to three-dimensional components and that, in future, there will be more opportunities to conduct more relevant experiments and produce more diverse three-dimensional components to verify the advantages of microwave curing. Also, other applications of microwave curing can be explored, such as bonded repair of carbon fiber composites on three-dimensional shaped components.

Acknowledgement

This work was supported by the China Petrochemical Corporation (Sinopec Group) (grant numbers: GFS21-L3-009, and 219025-2).

Declaration of Competing Interest

The authors declare that they have no known competing financial interests or personal relationships that could have appeared to influence the work reported in this paper.

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