Science and Technology of Nuclear Installations

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Safety Features of High Temperature Gas Cooled Reactor

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Volume 2017 |Article ID 2126876 |

Xiaotong Chen, Zhenming Lu, Hongsheng Zhao, Bing Liu, Junguo Zhu, Chunhe Tang, "The Electric Current Effect on Electrochemical Deconsolidation of Spherical Fuel Elements", Science and Technology of Nuclear Installations, vol. 2017, Article ID 2126876, 6 pages, 2017.

The Electric Current Effect on Electrochemical Deconsolidation of Spherical Fuel Elements

Academic Editor: Robert Morris
Received30 Dec 2016
Revised31 Mar 2017
Accepted19 Apr 2017
Published18 May 2017


For High-Temperature Gas-Cooled Reactor in China, fuel particles are bonded into spherical fuel elements by a carbonaceous matrix. For the study of fuel failure mechanism from individual fuel particles, an electrochemical deconsolidation apparatus was developed in this study to separate the particles from the carbonaceous matrix by disintegrating the matrix into fine graphite powder. The deconsolidated graphite powder and free particles were characterized by elemental analysis, X-ray photoelectron spectroscopy (XPS), X-ray diffraction (XRD), scanning electron microscopy (SEM), energy dispersive spectrometer (EDS), and ceramography. The results showed that the morphology, size distribution, and element content of deconsolidated graphite matrix and free particles were notably affected by electric current intensity. The electrochemical deconsolidation mechanism of spherical fuel element was also discussed.

1. Introduction

The fuel elements of High-Temperature Gas-Cooled Reactor (HTR) are spherical and have an overall diameter of 60 mm. A 5 mm thick unfueled matrix graphite shell comprises the outer portion of the sphere. The central, fueled region of the fuel element is 50 mm in diameter and is composed of 0.92 mm diameter tristructural isotropic- (TRISO-) coated fuel particles that are overcoated and pressed into a 50 mm diameter sphere [1]. The graphite matrix covered more than 95% weight of the fuel element. To study the irradiation behaviors of the spent fuel element, coated particles need to be separated and sampled from the matrix graphite from the inside out for further inspections of fission products distribution [2]. Therefore, the structural integrity of coated particles and the complete separation of coated particles from matrix graphite are two key issues for exact measurements. Intact coated particles consisting of silicon carbide (SiC) and outer/inner pyrolytic carbon (PyC) layers should be maintained, with graphite matrix and overcoating layers removed [3, 4]. Most practical methods of disintegration of HTR fuel elements studied in the past made use of the fact that graphite forms so-called intercalation compounds with certain elements, accompanied by enlargement of the C-spacing of graphite lattice [57]. In this process graphite matrix is loosened to such an extent that it disintegrates into fine graphite powder to liberate the coated particles.

Electrochemical deconsolidation method is based on anodic oxidation of graphite in electrolytes including strong acids [810] and salt solution [11, 12]. Under the concentration gradient and electrostatic potential gradient, anions would transport towards anodic graphite matrix, with insertion into the graphite layer to form the well-known graphite intercalation compounds. Since the compounds are not stable, they could decompose naturally in the presence of water, resulting in the destruction of the graphite matrix [13, 14]. If the deconsolidation is conducted in strong acid, carbon oxidization caused by dissociated acid cations would also lead to the destruction of the graphite matrix. During the deconsolidation, the electric current is considered as one of main factors that affect the deconsolidation procedure. In this study, the electric current effect on the electrochemical deconsolidation of spherical fuel elements was investigated in HNO3 electrolyte. Unirradiated spherical graphite balls with ZrO2 kernels produced by the similar processing of UO2 fuel elements were used as the test samples in this work.

2. Experimental

The apparatus in this work contains electrolyzing cell, rotator (1), anode (2), Pt cathode (3), HNO3 electrolyte (4), and DC electrolytic power supply and control system (Figure 1). The sample sphere is connected to a direct current source as well as a gear motor using a motor rod linker. The motor rod linker is only inserted about 4 mm into the unfueled portion of the sphere to avoid particle damage as a result of the deconsolidation process. The deconsolidation process involves two steps. In the first part of the deconsolidation process, the sample sphere rotates (1 rpm) with the outer circumference submerged in electrolyte solution, leaving a 2 cm-cylinder in diameter at the end. In the second part of the process, the remaining cylinder is rotated by 90° and lowered into the electrolyte in discrete steps. The tested electric currents in this work are 2 A (2.4 V), 7 A (6.4 V), 10 A (8.5 V), and 13 A (10.7 V). Each step yields a sample of electrolyte solution, graphite matrix, and associated coated particles after a series of separation methods. Then unbonded particles are collected and packaged separately, providing a profile of fuel from the edge to the center of the sphere.

The deconsolidated powders were washed by SB-50 sonicator (Xinzhi, China) and dried by DHG-9030A (Yiheng, China). The samples were weighed by QUINTIX124-1CN (Sartorius, German). The X-ray diffraction (XRD) spectra of samples before and after deconsolidation were characterized by D8 X-ray diffractometer (Bruker, German); the X-ray photoelectron spectrometry (XPS) properties of samples were characterized by 250XI XPS instrument (Thermo, USA); the element contents of the samples were measured by Various ELIII element analysis instrument (Elementar, German); the scanning electron microscope (SEM) images were measured by S-3000N (Hitachi, Japan) equipped with energy dispersive spectrometer (EDS). The particle size was measured by Mastersizer 2000 laser particle size analyzer (Malvin, UK).

For elemental analysis, the deconsolidated samples were firstly sonicated by high purified water to remove HNO3 and filtrated by vacuum for times until the filter liquor pH reached above 6.0. Afterwards, the samples were dried at 120°C in a vacuum drying oven for 6 h to remove H2O with the weights measured. Then the samples were dried at 120°C for another 0.5 h and weighed. Once the weights differences before and after drying were smaller than 0.2 mg, H2O was thought to be completely removed and the samples were sent for elemental analysis.

3. Results and Discussion

3.1. The Electric Current Effect on Deconsolidation Rate

The electric current effect on deconsolidation rate is shown in Figure 2. The deconsolidation rate is defined as the mass of disintegrated graphite fragments per hour. According to the results, a positive influence of current on the disintegration rate can be observed. It seems that a larger current leads to a faster disintegration rate. However, if the current is further increased to 20 A, the disintegration rate will deviate from the linear relationship (not shown in the figure), which might be caused by competitive H2O electrolyzation.

3.2. The Components of Graphite Matrix before and after Deconsolidation
3.2.1. Elemental Analysis

If collected after deconsolidation, the graphite fragments gain an obvious weight of around 7–15% compared to those before deconsolidation. To examine the component of samples, elemental analysis was carried out for C, H, N, and O contents (Table 1). Based on the mass balance, the difference between the overall mass and those of C, H, and N can be ascribed to the mass of O. According to the elemental analysis results, C is still the main component of the fragments. The slight change of N content indicates the formation of graphite-nitrate compounds, which are probably intercalation compounds. The O increasing from graphite matrix to deconsolidated samples indicates that graphite matrix might be oxidized to some degree during the chemical deconsolidation, which results in the weight gain.

SampleN% (mea.)C% (mea.)H% (mea.)O% (calc.)O/C

Graphite matrix0.0698.800.220.910.009
Deconsolidated by 2 A (2.4 V)0.9880.60.6017.800.22
Deconsolidated by 7 A (6.2 V)1.1478.680.8819.310.25
Deconsolidated by 10 A (8.5 V)0.6281.480.8117.090.21
Deconsolidated by 13 A (10.7 V)0.7580.910.7917.550.22

3.2.2. XPS Results

Since elemental analysis result is a mean value of the bulk of the sample, we further used XPS to characterize the sample surface with extensive functionalization. XPS spectra for graphite before and after deconsolidation by different electric currents are shown in Figure 3. By means of deconvolution, one spectrum can be fit to three peaks at 284.6, 286.8, and 289.0 eV, separately [15], which can be assigned to C-C(H), C-O, and O-C=O peaks (Table 2). According to XPS results, the graphite crystal accounted for more than 99.8% before electrochemical treatment, which decreased from 65.3% to 45.6% if the current intensity increased from 2 A to 10 A. It is noted that the graphite proportion increased to 60.9% when the electric current further increased to 13 A, which is probably due to the discounted oxidation effect with decreasing O/C ratio at too rapid electrochemical rate (Table 2). Larger O/C calculated from XPS results compared to those from elemental analysis results implies that more abundant graphite oxide was formed on the surface of graphite debris after deconsolidation.

Sample284.6 eV286.8 eV289.0 eVO/C

Graphite matrix>99.8%<0.1%<0.1%0.04
Deconsolidated by 2 A (2.4 V)65.3%29.8%4.8%0.39
Deconsolidated by 7 A (6.2 V)73.2%16.2%10.5%0.24
Deconsolidated by 10 A (8.5 V)45.6%37.5%16.9%0.59
Deconsolidated by 13 A (10.7 V)60.9%33.8%5.2%0.56

3.2.3. XRD Results

The XRD results (Figure 4) also provide evidences about the formation of graphite oxide. The strong single peak at 26.5° can be attributed to 002 diffraction peak of graphite crystal [16], indicating a high graphitization degree and an ordered arrangement of micrographite crystal layers. During the deconsolidation, the formation of covalent bond between oxygen and carbon atoms enhances the spacing in graphite crystal along -axial, and the peak at around 12° corresponds to the reflection of graphite oxides [17]. If we calculate the graphitization, value, according to (1), a declined graphitization can be observed for deconsolidated samples compared to the matrix (Table 3). Since the deconsolidated samples are inhomogeneous mixture of various carbon species, the graphitization is not dependent on current but lies in the range of 0.80–0.89. [18], where is wavelength of the X-rays, is distance between 002 planes, and is the angle of incidence of the X-ray beam.


Graphite matrix26.540.95
Deconsolidated by 2 A (2.4 V)26.460.83
Deconsolidated by 7 A (6.2 V)26.480.86
Deconsolidated by 10 A (8.5 V)26.500.89
Deconsolidated by 13 A (10.7 V)26.440.80

3.3. The Current Intensity Effect on Particle Size of Graphite Matrix after Deconsolidation

If we look further into the current intensity effect on the particle size of graphite matrix after deconsolidation (Figure 5), the following can be found: as the current increased from 2 A to 10 A, the particle size decreased from 365 nm to 148 nm, which was correspondent to the previous study [7, 19]; as the current further increased to 13 A, the particle size slightly increased to 240 nm. These results indicate that when the electric current is relatively small, larger deconsolidated particles are more likely to be formed caused by more graphite oxidization inside the bulk. In this case, the permeation rate of H2O is faster than electrolysis rate, and the latter is a rate-control step. Inversely, when the electric current becomes large enough, fine particles are more likely to be formed caused by more graphite oxidation on the interface. On one hand, both electrolysis rates of graphite matrix and H2O become larger as current increases; on the other hand, the permeation rate of H2O into graphite matrix would become smaller with increasing H2O electrolysis rate. In this case, the permeation rate of H2O is slower than electrolysis rate of graphite matrix, and the former becomes the control step. Therefore, 10 A is a turning point where the rate-control step changes from electrolysis rate-control to permeation rate-control. According to these results, the electric current range from 7 A to 13 A would be recommended, because the large difference in particle sizes between graphite fragments and TRISO-particles benefits better separation of deconsolidated graphite powders and TRISO-particles. However, the OPyC layer may be degraded or broken at higher currents, which will be discussed in additional analysis in Section 3.4.

The raw graphite matrix powder is composed of natural graphite, synthetic graphite, and resin binder in a certain proportion, which experience a series of high-temperature treatment to form graphite matrix [20]. The binder phenol resin is used to provide adhesion to mixture and helps to adhere the graphite matrix powder to TRISO-coated fuel particles during the overcoating process and will harden into a carbonaceous carbon during the subsequent carbonization process [21]. Compared to natural and synthetic graphite, the structure of carbonaceous graphite is not so ordered, so it is probably easier to be electrochemically oxidized. Also, micropore structure will be formed on the surface or in the bulk after manufacture processing due to powder compression and volatilization of light components in binder. According to SEM of the deconsolidated graphite sample (Figure 6), the graphite matrix surface is relatively smooth despite the porous structure, whereas the surface after deconsolidation becomes rough, displaying the shape of graphite raw materials. The electric current exerted little effect on the microstructure of the graphite. Since graphite microcrystalline is more ordered with higher reaction activation energy, it is reasonable to deduce that the carbonaceous carbon with turbostratic structure is easier to be broken in electrochemical process. During the electrolysis, the nitric acid electrolyte gradually infiltrated into the micropores of graphite matrix, and the electrochemical reaction would take place around micropore structure as well as on matrix surface. With much higher surface reaction capability due to large specific area of micropore structure, the expansion stress originated from inner surface of micropores widened the c-spacing of the layer lattice of carbonaceous carbon, which was thought to be one of the main driving forces of deconsolidation.

3.4. The Characterization of TRISO-Particles after Deconsolidation

During the deconsolidation, it is critical to maintain intact structure of obtained TRISO-particles for further analysis. According to ceramography (Figure 7) and EDS characterization of TRISO-particle surface after deconsolidation (Figure S1, Supplementary Material available online at, Si (1.740 eV) was detected besides C (0.277 eV) and O (0.523 eV) if the samples are treated by large electric current like 10 A and 13 A, indicating that the outer PyC layer was broken and SiC layer was exposed. Moreover, the detected Si peak at 13 A is stronger than that at 10 A. Therefore, larger electric current might increase the breakage risk of PyC layer. Combining the above results for graphite fragments and TRISO-particles, the current of 7 A (6.2 V) is preferred in this study.

4. Conclusions

In this work, the effect of different electric current intensities on deconsolidation of spherical fuel element was studied. It is shown that increased electric current improved deconsolidation rate. Particle size and components of deconsolidated graphite fragments were also related to the current intensity. According to the structure and surface analysis results, graphite oxide was produced after the deconsolidation, the content of which was also related to current intensities. The expansion stress originated from inner surface of micropores of carbonaceous carbon was thought to be one of the main driving forces of deconsolidation. Considering that larger electric current than 10 A would cause the breakage of OPyC layer and the exposure of SiC layer, the electric current of 7 A is preferred in this study.


Part of this work has been presented on a paper in Embedded Topical 2016 ANS Winter Meeting.

Conflicts of Interest

The authors declare that they have no conflicts of interest.


This work is supported by National Natural Science Foundation of China 21405092, the National S&T Major Project (Grant no. ZX06901), Tsinghua University Initiative Scientific Research Program 2014z21025, and Nuclear Energy Development Project.

Supplementary Materials

Supplementary materials provided EDS characterizations of triso-particle surface after deconsolidation by 2 A, 7 A, 10 A and 13 A.

  1. Supplementary Material


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