Co-reporter:Quansheng Ma, Yizhuo Gu, Min Li, Shaokai Wang, Zuoguang Zhang
Applied Surface Science 2016 Volume 379() pp:199-205
Publication Date(Web):30 August 2016
DOI:10.1016/j.apsusc.2016.04.075
Highlights
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Effects of surface treating on T700 grade high strength carbon fiber were discussed.
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The fiber surface roughness, surface energy and chemical properties are analyzed.
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The surface treating significantly affect the properties of carbon fiber.
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The composite with electrolysis and sizing-fiber has the highest mechanical properties.
Co-reporter:Zhenchong Zhang, Yizhuo Gu, Jiayu Bi, Shaokai Wang, Min Li, Zuoguang Zhang
Composites Part A: Applied Science and Manufacturing 2016 Volume 85() pp:172-180
Publication Date(Web):June 2016
DOI:10.1016/j.compositesa.2016.03.025
Barium titanate@silicon dioxide (BT@SiO2) core@shell fillers with an average diameter of 100 nm were prepared by a facile sol–gel synthesis. The thickness of SiO2 shell can be easily tuned by varying different mass ratio of BT to tetraethyl orthosilicate (TEOS). Polyvinylidene fluoride (PVDF) based composite films reinforced by BT and BT@SiO2 were fabricated via a solution casting method. The effects of SiO2 shell on morphology structure, wettability, interfacial adhesion, dielectric, electrical and energy performances of composites were investigated. Compared with BT/PVDF, BT@SiO2/PVDF composites show significantly increased breakdown strength due to enhanced interfacial adhesion and suppressed charge carrier conduction. Benefiting from enhanced breakdown strength and reduced remnant polarization induced by SiO2 shell, BT@SiO2/PVDF shows increased release energy density (energy density which can be fully discharged and applicable). Especially, BT@SiO2/PVDF with SiO2 thickness of 4 nm exhibits the highest release energy density of 1.08 J/cm3 under applied electric field of 145 kV/mm.
Co-reporter:Zhenchong Zhang, Yizhuo Gu, Shaokai Wang, Qingwen Li, Min Li, Zuoguang Zhang
Carbon 2016 107() pp: 405-414
Publication Date(Web):1 October 2016
DOI:10.1016/j.carbon.2016.05.068
The fabrication and performance of a novel continuous carbon nanotube (CNT) sheet reinforced polyvinylidene fluoride (PVDF) film with sandwich structure are firstly reported. Continuous CNT sheet fabricated by means of floating catalyst chemical vapor deposition was used. A dispersion-free technique for the sandwich composite film was adopted. For the prepared film with sandwich structure, CNT sheet/PVDF acts as a highly conductive layer to raise dielectric permittivity, while two PVDF films at top and bottom of composite are used as insulating layers to suppress dielectric loss. Thionyl chloride doping treatment was done for CNT sheet and the effects of dopant on chemical composition, structure and properties of CNT sheet and composite film were investigated. Resulted from unique performances of the modified CNT sheet and strong interfacial polarization process, the sandwich composite film possesses excellent dielectric and mechanical properties, where dielectric permittivity of 32, dielectric loss of 0.08, tensile strength of 90 MPa and modulus of 3 GPa are shown for optimized chlorine-doping duration time and composite composition. Such composite material and structure have potential applications in hybrid capacitors due to high permittivity, low dielectric loss, good flexibility and ease of processability.
Co-reporter:Ran Li, Yizhuo Gu, Zhongjia Yang, Min Li, Shaokai Wang, Zuoguang Zhang
Journal of Nuclear Materials 2015 Volume 466() pp:100-107
Publication Date(Web):November 2015
DOI:10.1016/j.jnucmat.2015.07.037
•The properties of basalt fiber reinforced epoxy resin matrix composite under 60Co γ irradiation up to 2.0 MGy were studied.•Basalt fiber can weaken the aging effects of γ irradiation on the resin matrix.•Tensile property of basalt fiber composite remains stable and flexural property has a low degree of attenuation.•Basalt fiber composite is an ideal candidate of structural material for nuclear industry.Gamma-ray (γ-ray) irradiation is a crucial reason for the aging in materials used for nuclear industry. Due to high specific strength and stiffness, light weight and good corrosion resistance, fiber reinforced composites are regarded as an alternative of traditional materials used on nuclear facilities. In this study, basalt fiber (BF)/AG80 epoxy composite laminates were fabricated by autoclave process and treated with 60Co gamma irradiation dose up to 2.0 MGy. Irradiation induced polymer chain scission and oxidation of AG80 resin were detected from physical and chemical analysis. The experimental results show that the tensile and flexural performances of irradiated BF/AG80 composite maintain stable and have a low amplitude attenuation respectively, and the interlaminar shear strength has increased from irradiation dose of 0–1.5 MGy. Furthermore, the comparison between the studied BF composite and reported polymer and composite materials was done for evaluating the γ resistance property of BF composite.
Co-reporter:Libing Jiao, Yizhuo Gu, Shaokai Wang, Zhongjia Yang, Han Wang, Qingwen Li, Min li, Zuoguang Zhang
Composites Part A: Applied Science and Manufacturing 2015 Volume 71() pp:116-125
Publication Date(Web):April 2015
DOI:10.1016/j.compositesa.2015.01.008
Materials used in low earth orbit are exposed to damaging atomic oxygen (AO). AO exposure behaviors of carbon nanotube (CNT) film and CNT/epoxy composite film were evaluated when exposed to a nominal AO fluence of about 3.0 × 1020 atoms/cm2. Properties of the films before and after AO exposure were evaluated by mass loss, Raman spectroscopy, X-ray photoelectron spectroscopy, tensile and electrical conductivity tests. Results show similar mass loss and different surface erosion for two kinds of films. CNT bundles collapse with the emergence of a tight arrangement of particles, and porous CNT film has more serious interior CNT erosion than dense CNT/epoxy composite film. Decreases of tensile strength and electrical conductivities are seen.
Co-reporter:Min Li, Hongxin Liu, Yizhuo Gu, Yanxia Li, Zuoguang Zhang
Applied Surface Science 2014 Volume 288() pp:666-672
Publication Date(Web):1 January 2014
DOI:10.1016/j.apsusc.2013.10.093
Highlights
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We study the changes of interfacial fracture energy before and after water aging.
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We discuss the surface characteristics effect on interfacial hygrothermal resistance.
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The impact of activated carbon atom on interfacial hygrothermal resistance is little.
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The silicon element results in the irreversible variations of interfacial bonding.
Co-reporter:Z.J. Zhou;M. Li;Y.Z. Gu;X.Q. Ma;Y.X. Li;L.J. Jia;Z.G. Zhang
Polymer Composites 2014 Volume 35( Issue 4) pp:681-690
Publication Date(Web):
DOI:10.1002/pc.22711
In this article, a novel method of measuring resin flow front under vacuum condition is presented. The in situ monitoring system with metal hollow probe based on gas flow balance can be used in resin film infusion (RFI) process, where resin film is used and transverse flow is dominated along thickness direction of fiber preform. The diameter of the probe was chosen to increase the measuring accuracy, and the reliability of the method was evaluated by comparison of visualization experiment. Experimental results demonstrate that the method is suitable for monitoring resin flow in RFI process with and without autoclave, and can obtain the information about resin filling time, nonuniform flow front, and the permeability of fiber preform. Furthermore, by means of the established monitoring system, the influences of pressure and lay-up sequence of carbon fiber fabric on epoxy resin flow during RFI process were investigated. In addition, resin flow pattern with changing viscosity of epoxy resin was studied. POLYM. COMPOS., 35:681–690, 2014. © 2013 Society of Plastics Engineers
Co-reporter:Kaomin Zhang, Yizhuo Gu, Min li, Zuoguang Zhang
Materials & Design 2014 54() pp: 624-631
Publication Date(Web):February 2014
DOI:10.1016/j.matdes.2013.08.065
•Properties of rapid curing composite were investigated.•Process time of composite fabricated by VARIM was controlled within 16 min.•The highest flexural strength is obtained from the preheating process.•Slightly non-uniformity of properties exists along resin flow direction.•Preheating of fiber is believed to be suitable for rapid VARIM process.Long processing cycle makes vacuum assisted resin infusion molding (VARIM) only suitable for low and medium volumes of production, and shortening of curing time is critical to improving the processing efficiency of automotive composite parts. In this paper, unidirectional carbon fiber reinforced composite laminates were fabricated by VARIM. Three different processes (namely quick, quick-post and preheating) were employed, in which a kind of rapid curing epoxy resin is used. The preheating of mold and fiber was conducted to shorten the filling time compared with that of quick process. Quick-post process with a post cure stage was investigated to verify the composite properties fabricated by quick process. The cycle time was 16 min for preheating process, about 30% shorter than that of quick process, simultaneously, flexural strength and interlaminar shear strength (ILSS) were respectively improved by 29% and 7% compared with those of quick process. The non-uniformity of mechanical properties at different positions along resin flow direction under preheating process was found, but the processing quality of composite was good. The preheating process is confirmed to be suitable for the improvement of processing efficiency of VARIM with good mechanical properties. In addition, the composite fabricated by quick-post process has better mechanical properties, which is attributed to the alleviation of residual stress during post curing process.
Co-reporter:Min Li, Yizhuo Gu, Yanan Liu, Yanxia Li, Zuoguang Zhang
Carbon 2013 Volume 52() pp:109-121
Publication Date(Web):February 2013
DOI:10.1016/j.carbon.2012.09.011
An aqueous suspension deposition method was used to coat the sized carbon fibers T700SC and T300B with commercially carboxylic acid-functionalized and hydroxyl-functionalized carbon nanotubes (CNTs). The CNTs on the fiber surfaces were expected to improve the interfacial strength between the fibers and the epoxy. The factors affecting the deposition, especially the fiber sizing, were studied. According to single fiber-composite fragmentation tests, the deposition process results in improved fiber/matrix interfacial adhesion. Using carboxylic acid-functionalized CNTs, the interfacial shear strength was increased 43% for the T700SC composite and 12% for the T300B composite. The relationship between surface functional groups of the CNTs and the interfacial improvement was discussed. The interfacial reinforcing mechanism was explored by analyzing the surface morphology of the carbon fibers, the wettability between the carbon fibers and the epoxy resin, the chemical bonding between the fiber sizing and the CNTs, and fractographic observation of cross-sections of the composites. Results indicate that interfacial friction, chemical bonding and resin toughening are responsible for the interfacial improvement of nanostructured carbon fiber/epoxy composites. The mechanical properties of the CNT-deposited composite laminate were further measured to confirm the effectiveness of this strategy.
Co-reporter:Zhongjia Yang;Lili Yuan;Min Li;Zhijie Sun ;Zuoguang Zhang
Journal of Applied Polymer Science 2013 Volume 130( Issue 3) pp:1479-1488
Publication Date(Web):
DOI:10.1002/app.39326
ABSTRACT
Phenolic foams reinforced with pristine and functionalized multiwalled carbon nanotubes (MWCNTs) were fabricated to develop fire-resistant materials with improved mechanical properties. The influences of the contents of carboxyl multi-walled carbon nanotubes (MWCNTs-COOH) and of MWCNTs types on the compressive properties of the composite foams were investigated. The microstructure and detailed failure behavior of MWCNTs/phenolic composite foams were studied using scanning electron microscopy (SEM) and in situ quasistatic compression inside SEM, respectively. In addition, thermal performances were evaluated by thermogravimetric analysis (TGA) and vertical burning method. It is found that as heterogeneous nucleation agents, MWCNTs increase cell density and decrease cell size of the produced foams, and that as reinforcements located in cell walls, MWCNTs impart high strength and stiffness to brittle foams. Moreover, MWCNTs reinforced foams have higher thermal stability than raw foams and exhibit similar excellent resistance to flame, confirming the effectiveness of MWCNTs as stabilizers. © 2013 Wiley Periodicals, Inc. J. Appl. Polym. Sci. 130: 1479–1488, 2013
Co-reporter:F.L. Shan;Y.Z. Gu;M. Li;Y.N. Liu ;Z.G. Zhang
Polymer Composites 2013 Volume 34( Issue 1) pp:41-50
Publication Date(Web):
DOI:10.1002/pc.22375
Abstract
Carbon fiber-reinforced epoxy composites, with incorporated carboxylic multiwall carbon nanotubes (CNTs), were prepared using vacuum-assisted resin infusion (VARI) molding, and the in-plane and out-of-plane properties, including mode-I (GIc) and mode-II (GIIc) interlaminar fracture toughness, interlaminar shear strength (ILSS), tensile, and flexural properties were measured. A novel spraying technique, which sprays a kind of epoxy resin E20 with high viscosity after spraying the CNTs, was adopted to deposit the CNTs on the surface of carbon fiber fabric. The E20 was used to anchor CNTs on the fabric surface, avoiding that the deposited CNTs were removed by the infusing resin during VARI process. The spraying processing, including spraying amount and spraying sequence, was optimized based on the distribution of CNTs on the fibers. After that, three composite specimen groups were fabricated using different carbon fiber fabrics, including as-received, CNT-deposited with E20, and CNT-deposited without E20. The effects of CNTs on the processing quality and mechanical properties of carbon fiber-reinforced polymer composites were studied. The experimental results show that all studied laminates have uniform thickness with designed values and no obvious defects form inside the laminates. Compared with the composite without CNTs, depositing CNTs with E20 increases by 24% in the average propagation GIc, by 11% in the propagation GIIc and by 12% in the ILSS, while it preserves the in-plane mechanical properties, However, depositing CNTs without E20 reduces interlaminar fracture toughness. These phenomena are attributed to the differences in the distribution of CNTs and the fiber/matrix interfacial bonding for different spraying processing. POLYM. COMPOS., 2013. © 2012 Society of Plastics Engineers
Co-reporter:X.Q. Ma;Y.Z. Gu;M. Li;Y.X. Li;D.M. Zhang;L.J. Jia;Z.G. Zhang
Polymer Composites 2013 Volume 34( Issue 12) pp:2008-2018
Publication Date(Web):
DOI:10.1002/pc.22608
A new cocured process called coresin film infusion (co-RFI) process, which combines RFI process and prepreg/autoclave process, was introduced and four kinds of commercial carbon fiber prepreg material systems and a kind of resin film were applied to fabricate co-RFI laminates. The compatibility between the resin film and the prepreg matrix and the application of co-RFI process were investigated based on the resin flowability, glass transition temperature of cured resin, processing quality of laminate, and variation in resin modulus on cocured interphase region measured by nanoindentation. Furthermore, mode I (GIC), mode II (GIIC) delamination fracture toughness, and flexural strength and modulus were measured to evaluate the mechanical properties of cocured laminates with different prepreg materials. The experimental results show that thickness and fiber volume fraction of co-RFI laminates with the four kinds of prepreg materials are similar to those of prepreg laminates and RFI laminate with acceptable differences. In addition, there are no obvious defects in co-RFI laminates. Moreover, the reduced modulus of resin at cocured interface and glass transition temperature values of the mixed resin reflect good compatibility between prepreg matrix resin and RFI resin. The GIC, GIIC values, and flexural performances of cocured laminates lie between and even exceed those of prepreg laminates and RFI laminates, indicating no weakening effect in the cocured interface. Therefore, the co-RFI process is believed to effectively fabricate composite with low cost and it can be applied using various prepreg systems. POLYM. COMPOS., 34:2008–2018, 2013. © 2013 Society of Plastics Engineers
Co-reporter:X. X. Bian;Y. Z. Gu;J. Sun;M. Li;W. P. Liu;Z. G. Zhang
Applied Composite Materials 2013 Volume 20( Issue 5) pp:927-945
Publication Date(Web):2013 October
DOI:10.1007/s10443-012-9310-7
In this study, the effects of processing temperature and vacuum applying rate on the forming quality of C-shaped carbon fiber reinforced epoxy resin matrix composite laminates during hot diaphragm forming process were investigated. C-shaped prepreg preforms were produced using a home-made hot diaphragm forming equipment. The thickness variations of the preforms and the manufacturing defects after diaphragm forming process, including fiber wrinkling and voids, were evaluated to understand the forming mechanism. Furthermore, both interlaminar slipping friction and compaction behavior of the prepreg stacks were experimentally analyzed for showing the importance of the processing parameters. In addition, autoclave processing was used to cure the C-shaped preforms to investigate the changes of the defects before and after cure process. The results show that the C-shaped prepreg preforms with good forming quality can be achieved through increasing processing temperature and reducing vacuum applying rate, which obviously promote prepreg interlaminar slipping process. The process temperature and forming rate in hot diaphragm forming process strongly influence prepreg interply frictional force, and the maximum interlaminar frictional force can be taken as a key parameter for processing parameter optimization. Autoclave process is effective in eliminating voids in the preforms and can alleviate fiber wrinkles to a certain extent.
Co-reporter:H. X. Liu;Y. Z. Gu;M. Li;D. M. Zhang;Y. X. Li;Z. G. Zhang
Polymer Composites 2012 Volume 33( Issue 8) pp:1368-1375
Publication Date(Web):
DOI:10.1002/pc.22273
Abstract
The changes in interfacial fracture energy of three kinds of commercially sized carbon fiber (CF)/epoxy resin composites in the range from ambient temperature to 130°C were investigated using the single-fiber fragmentation test to evaluate the heat resistance of the interphase. The effects of CF sizing on the interfacial bonding property were studied using desized CF/epoxy resin composites. Thermogravimetric analysis and differential scanning calorimetry of the combination of sizing and matrix were employed to investigate the role of sizing on the variations in the fiber/matrix interfacial property under elevated temperature. The interfacial fracture energy values of all the studied CF composites were found to decrease quickly during the initial stage of temperature rise and drop gradually at higher temperature. At elevated temperature, the desized CF composites had higher heat resistance than the corresponding sized fiber composites. The differences in the interfacial heat resistance among the three kinds of CF composites and the difference in the interfacial thermal stability between the sized and the desized fiber composites were related to different glass transition temperatures of the interphases. The interaction between sizing and the matrix and the chain motion of the crosslink structure of the interphase has been suggested to determine the interfacial heat resistance. POLYM. COMPOS., 2012. © 2012 Society of Plastics Engineers
Co-reporter:Hongxin Liu;Min Li ;Zuoguang Zhang
Polymer Composites 2012 Volume 33( Issue 5) pp:716-722
Publication Date(Web):
DOI:10.1002/pc.22196
Abstract
The toughness of the interphase between carbon fibers and epoxy resin was characterized by the interfacial fracture energy, which was derived from the modified Wagner-Nairn-Detassis (WND) model, considering the moisture swelling stress. The characterization was used to evaluate the changes of interphase bonding before and after water aging, including boiling water and 70°C water immersion. The effects of the water aging on the parameters in WND model were analyzed. The mechanism of interphase degradation under water aging was interpreted considering the change of interphase thickness, which was measured using the dynamic nanomechanical mapping method. It is shown that the single-fiber fragmentation test with the proposed energy-based model can quantify the degradation of interphase toughness after water aging. For the studied system, the interphase thickness has a close relationship with the interfacial fracture energy, indicating that the swelling of the resin matrix and interphase results in an increase in interphase thickness and a decrease in interphase bonding property. POLYM. COMPOS., 2012. © 2012 Society of Plastics Engineers
Co-reporter:Chaobo Xin;Min Li;Yanxia Li ;Zuoguang Zhang
Polymer Composites 2011 Volume 32( Issue 2) pp:314-323
Publication Date(Web):
DOI:10.1002/pc.21048
Abstract
Resin pressure is one of the most important parameters in manufacturing composites during autoclave process. It not only greatly influences resin flow behavior, but also has effects on void formation and elimination. Online monitoring resin pressure can provide an important guidance for the optimization of the processing parameters and the control of the quality of composites. In this study, a resin pressure online measuring system for autoclave process was established based on the principle of pressure transfer in liquid, and the size of the measuring probe of the system was optimized to increase the accuracy of measured resin pressure. The results indicate that the accuracy and the dynamic response of the system can meet the requirements of resin pressure measurement during autoclave process. Furthermore, by means of this proposed resin pressure measuring system and the measurements of compaction properties of the fabric stacks, the resin pressures inside carbon fiber fabric/epoxy resin and glass fiber fabric/epoxy resin prepreg stacks during autoclave process were investigated, especially for the zero-bleeding process which is prevailing for aircraft composite structures. It is demonstrated that during zero-bleeding process, the resin pressures, which conform to the spring and piston model, uniformly distribute along through-thickness and in-plane directions. In addition, the resin pressure profile is significantly influenced by the fiber volume fraction of the prepregs, indicating that fiber content of prepreg should be optimized for achieving free defects and uniform fiber distribution. POLYM. COMPOS., 2011. © 2010 Society of Plastics Engineers
Co-reporter:C.B. Xin, Y.Z. Gu, M. Li, J. Luo, Y.X. Li, Z.G. Zhang
Composites Part A: Applied Science and Manufacturing 2011 Volume 42(Issue 10) pp:1353-1360
Publication Date(Web):October 2011
DOI:10.1016/j.compositesa.2011.05.018
Rubber molds are used to intensify and uniformly redistribute the pressure on the angle-bended composite laminates during autoclave processing. However, the optimization of flexible tool is difficult and time-consuming. In this paper, experiments were performed to study the effect of different configurations of male rubber mold on the thickness distribution of L-shaped laminates processed on metal female tool in autoclave processing. Based on numerical analysis, we compared the compaction forces transferred on the prepreg stacks with different male rubber molds. Furthermore, a flexible mold was modified based on the simulated data. The results indicate that the stiffness of male tool significantly influences the degree of corner thickening and pressure distribution on the laminates. Moreover, the corner and flat regions require different stiffness of the corresponding regions of male tool to ensure uniform compaction, and the laminates with uniform thickness were obtained using the modified flexible molds.
Co-reporter:Yizhuo Gu, Min Li, Ji Wang, Zuoguang Zhang
Carbon 2010 Volume 48(Issue 11) pp:3229-3235
Publication Date(Web):September 2010
DOI:10.1016/j.carbon.2010.05.008
The interphase of fiber reinforced polymer composites is a narrow region around the fiber, and the mechanical performance of a composite strongly depends on the properties of the interphase. The interphase of carbon fiber reinforced polymer composites (CFRPs) is difficult to quantitatively characterize because of its nanometer dimension. To solve this problem, we present a nanomechanical imaging technique for mapping the dynamic mechanical property around the interphase region in CFRPs, and for providing nanoscale information of the interfacial dimension. The experimental results show that this method can determine the width and topography of the interphase with nanoscale lateral resolution, based on the storage modulus profile on the cross section of the composite. The average interphase thicknesses of a T300 carbon fiber/epoxy resin composite and a T700 carbon fiber/bismaleimide resin composite are 118 nm and 163 nm, respectively, and the size of interphase is uneven in width and “river-like”, which is consistent with the surface topography of the carbon fibers. Furthermore, the effect of water-aging on the interphase of the T300/epoxy composite was analyzed using the in situ imaging technique. An increase in the interphase width and interface debonding were revealed, implying a degradation in the interphase region.
Co-reporter:Yizhuo Gu;Min Li;Zuoguang Zhang ;Zhijie Sun
Polymer Composites 2010 Volume 31( Issue 9) pp:1562-1571
Publication Date(Web):
DOI:10.1002/pc.20944
Abstract
For resin matrix composites, voids are common defects that can seriously deteriorate the properties of the composite parts. Thus, the elimination of voids is a crucial element in controlling the manufacturing process of composite parts. This article focuses on void formation originating from hygroscopic water for resin matrix composite laminates prepared with hot pressing process. The Kardos void formation model was developed to analyze the critical resin pressure for the initiation of voids, and the influencing factors were investigated experimentally to validate the modified model. It is found that resin pressure and gel temperature are the two key parameters to control void defects and that entrapped air in prepreg stacks must be considered in the void formation model. Furthermore, a simple method was established to measure the relationship between porosity and the processing parameters, and the void formation conditions of the resin and the prepreg stack were also studied. The theoretically predicted void formation conditions and the experimental results were compatible for the studied cases. These results are valuable for eliminating void defects, optimizing processing parameters, and enhancing the performance of composite parts. POLYM. COMPOS., 31:1562–1571, 2010. © 2009 Society of Plastics Engineers
Co-reporter:Yizhuo Gu;Min Li;Zuoguang Zhang ;Yanxia Li
Polymer Composites 2009 Volume 30( Issue 8) pp:1081-1090
Publication Date(Web):
DOI:10.1002/pc.20659
Abstract
The ability to predict the viscosity of thermoset resin is important to understand the manufacturing process of composites and optimize the processing parameters. During resin or prepreg storage course, the cure reaction may happen and the degree of cure increases gradually. The storage aging effect reduces the fluidity of resin, and hence alters the processability of resin. In this article, the rheological properties of an epoxy resin and a bismaleimide resin used in composite autoclave process were measured and a viscosity model was established, which can predict the viscosity progression during cure for different aging degree of resin. Moreover, a computer simulation method was used to study the effects of aging degree on the composite consolidation and the processing operations. It is found that the viscosity model of aged resin can be obtained by modified dual Arrhenius model of fresh resin with the dynamic rheological measurement. The resin aging strongly alters the flowability, so influences composite consolidation. According to the simulated results, the processing parameters need to be adjusted to achieve cured composites with appropriate fiber content. POLYM. COMPOS., 2009. © 2008 Society of Plastics Engineers
Co-reporter:Min Xie, Zuoguang Zhang, Yizhuo Gu, Min Li, Yuqin Su
Thermochimica Acta 2009 Volume 487(1–2) pp:8-17
Publication Date(Web):10 April 2009
DOI:10.1016/j.tca.2009.01.001
Dynamic mechanical analysis (DMA) is an alternative method to chemical techniques in investigating cure processes. However, methods to evaluate mechanical cure state and kinetic analysis for incomplete isothermal curing have not been properly developed. The objective is to find a suitable method to characterize cure state of epoxy prepreg by DMA, and to better understand mechanical incomplete cure processes. Single cantilever mode was applied to the prepreg. A new method was proposed using the dynamic storage modulus data to estimate the cure state, and to calculate ultimate mechanical conversions. Based on this method, the incomplete cure phenomenon was investigated. A linear relationship of the ultimate mechanical conversions with isothermal temperatures was observed. Two types of conversion curves were seen at high and low temperatures respectively. The Kamal model with the diffusion effect was fitted to the incomplete isothermal mechanical conversion curves, and can well predict the mechanical conversions at high temperatures.
Co-reporter:Ran Li, Yizhuo Gu, Gaolong Zhang, Zhongjia Yang, Min Li, Zuoguang Zhang
Composites Science and Technology (3 May 2017) Volume 143() pp:
Publication Date(Web):3 May 2017
DOI:10.1016/j.compscitech.2017.03.002
For protecting human body and equipment against radiation in nuclear power industry, radiation medicine and aerospace exploration, advanced materials possessing good shielding capability, low density and high mechanical strength and modulus are in urgent demand. In this study, radiation protective basalt fiber (BF) reinforced epoxy matrix composite containing erbium oxide (Er2O3) particles was fabricated by prepreg-autoclave process, in order to make a novel mechanical/radiation shielding composite. For prepared unidirectional and quasi-isotropic BF/Er2O3 composite laminates, basalt fibers and Er2O3 particles distributed uniformly, and no obvious agglomeration of particles and defects were found. NaI(Tl) detector was used to test mass attenuation coefficient for evaluating X and gamma rays shielding performance at different photon energies ranging from 31 keV to 662 keV. The experimental results indicate that BF/Er2O3 composite shows good X and gamma rays shielding performance, and mass attenuation coefficient of BF/Er2O3 composite is much larger than that of aluminum in relatively low energy from 31 keV to 80 keV. The effect of prepreg stacking consequence on shielding performance was also discussed. In addition, to verify the applicability of classic “mixture role” on mass attenuation coefficient of anisotropic composites, theoretical mass attenuation coefficient at different photon energies was calculated using XCOM software based on the weight fraction and mass attenuation coefficient of each constituent element among BF/Er2O3 composite. It is found that there is maximum deviation of 10.3% between experimental and theoretical results. Thus, it is believed that the method is suitable for predicting shielding performance of continuous fiber reinforced composite materials. Considering the advantages in light weight and high mechanical property, the studied three-phase composite is promising for using in radiation shielding structure application.
Co-reporter:Ran Li, Yizhuo Gu, Zhongjia Yang, Min Li, Yingwei Hou, Zuoguang Zhang
Materials & Design (15 June 2017) Volume 124() pp:121-130
Publication Date(Web):15 June 2017
DOI:10.1016/j.matdes.2017.03.045
•Adding W and Er2O3 can significantly improve γ ray shielding ability of basalt fiber reinforced composite.•Measured and calculated attenuation coefficients are given, and their discrepancy is clarified based on photon interaction.•An empirical model is established to accurately predict mass attenuation coefficient of the studied composite.•Functional fillers modified basalt fiber composites are believed to be lightweight structural/radiation shielding materials.Functional shielding filler modified fiber reinforced polymer matrix composites are novel structural/radiation shielding materials with great potentials in applications such as nuclear industry and radioactive therapy. In this study, unidirectional basalt fiber reinforced epoxy resin matrix composite laminates containing different contents of tungsten (W) and erbium oxide (Er2O3) fillers were fabricated. Experimental measurement and theoretical calculation of mass attenuation coefficients of γ ray were carried out and analyzed based on photon shielding mechanism. The effects of filler content and photon energy of γ ray on shielding property of composite were studied. It is found that adding W and Er2O3 fillers significantly increases mass attenuation coefficient of basalt fiber composite, especially for low photon energy. The discrepancy between measured and calculated results is obvious at low filler content, and is believed to come from different considerations on penetrating photons, which have undergone slight Compton scattering. The corresponding mechanism was discussed. An empirical model based on photoelectric absorption effect, Compton scattering effect and effective atomic number is established to modify calculated mass attenuation coefficient. A good accuracy was validated, so the model can be used to design this kind of composite for better shielding ability.Download high-res image (304KB)Download full-size image