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Communication

The ZrO2 Formation in ZrB2/SiC Composite Irradiated by Laser

1
School of Materials Science and Engineering, Beijing Institute of Technology, Beijing 100081, China
2
National Key Laboratory of Science and Technology on Materials under Shock and Impact, Beijing 100081, China
*
Author to whom correspondence should be addressed.
Materials 2015, 8(12), 8745-8750; https://doi.org/10.3390/ma8125475
Submission received: 3 November 2015 / Revised: 30 November 2015 / Accepted: 3 December 2015 / Published: 14 December 2015
(This article belongs to the Section Advanced Composites)

Abstract

:
In order to clearly understand the details of ZrO2 formation during ablation, high intensity continuous laser was chosen to irradiate ZrB2/SiC. The results reveal that there are two different modes of ZrO2 formation depending on whether liquid SiO2 is present. When liquid SiO2 is present, ZrO2 generated by the oxidation of ZrB2 is firstly dissolved into SiO2. Then, ZrO2 will precipitate again, the temperature will decrease and the SiO2 will evaporate. Otherwise, the ZrB2 will be oxidized to ZrO2 directly.

1. Introduction

Ultra high temperature ceramics (UHTCs) refer to a class of refractory materials with melting temperatures in excess of 3000 °C, such as diborides and carbides of transition metals [1,2]. As a member of UHTCs, zirconium diboride (ZrB2) has been widely attractive for decades. Because of its excellent properties, such as high melting temperature, high thermal conduction, excellent mechanical properties, etc., ZrB2 can be operated as leading edges in hypersonic vehicles.
According to previous research, ZrB2/SiC exhibited excellent ablation resistance against oxyacetylene torch, arc jet or plasma arc [3,4,5]. No obvious mass loss or macroscopic damage appears. Some products, like SiO2 and ZrO2, can be detected ona microscopic scale, and have been proved to be helpful to improve ZrB2/SiC’s ablation resistance [6,7]. However, the upper surface of the sample is wholly heated by the above ablation method, and we could only obtain the information of phase and microstructure until the ablated sample cools completely. Longer cooling time contributes to ablation transformation. So some important characterized information has been concealed or disappeared during the cooling process. Researchers only observed that the ablated layer of ZrB2/SiC was composed by ZrO2 skeleton and liquid SiO2 [8,9]. The real process and details of the formation of oxidation product, especially ZrO2, are still unknown.
If the information of phase and microstructure under high temperature can be preserved by fast cooling, the real transformation will be easily observed at room temperature. Because of thistheory, the high intensity laser ablation method with rapid heating rate was utilized. The local temperature of ZrB2/SiC at the spot center can reach thousands of degrees instantaneously at the beginning of laser irradiating. When laser loading stops, the sample can cool down rapidly to room temperature (which is similar to quenching), since the heating area is very small and the emissivity and conductivity of ZrB2/SiC are very high [10,11].
In this paper, ZrB2/20 vol % SiC composite (donated as ZS hereafter) was prepared and irradiated by high intensity continuous laser. The phase and microstructure evolution of ZrB2/SiC was investigated.

2. Results and Discussion

Figure 1 shows the polished surface microstructure of the as-sintered material. ZrB2 with grain size of about 5 μm is present as a grey matrix, while the dark SiC homogeneously distributes in the matrix.
Figure 1. The microstructure of as-sintered ZrB2/SiC composite.
Figure 1. The microstructure of as-sintered ZrB2/SiC composite.
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The X-ray diffraction (XRD) result of the ZrB2/SiC surface after laser ablation for 20 s is shown in Figure 2. According to the XRD, m-ZrO2 and ZrB2 are the major phases on the surface. It reveals that some ZrB2 are oxidized into ZrO2 while parts of ZrB2 are not oxidized at all. No peaks of SiO2 can be observed on the spectrum, because SiO2 is amorphous on the surface. However, small amounts of ZrSiO4 aredetected, as shown in the spectrum. This proves that SiO2 forms, and that parts of ZrO2 dissolve into SiO2 to form ZrSiO4.
Figure 2. X-ray diffraction (XRD) of the sample surface afterablation for 20 s.
Figure 2. X-ray diffraction (XRD) of the sample surface afterablation for 20 s.
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The surface macrostructure of ZrB2/SiC after laser ablation for 20 s is shown in Figure 3. Since the local heating of the laser induces extremely high temperature at the spot center, a great temperature gradient is generated along the radial direction, shown bythe arrow in Figure 3. Significant differences in ablation behavior between area 1 and area 2 were detected.
Figure 3. The surface macrostructure of the sample after ablation for 20 s.
Figure 3. The surface macrostructure of the sample after ablation for 20 s.
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The surface morphology of area 1 after laser ablation is shown in Figure 4. From Figure 4a, the surface performs a porous structure. The energy dispersive spectroscopy (EDS) result reveals that only ZrO2 exists on the surface; neither ZrB2 nor SiC can be detected. A typical flushing morphology is clearly shown as Figure 4b. It should be attributed to the liquid splashing and the following rapid solidification. This means that the oxidized ZrO2 in this region has been totally melted during laser ablation. Meanwhile, SiC is totally decomposed because the temperature here is higher than its decomposition point of 2300 °C.
Figure 4. The microscopic morphology of area 1 (a) with a typical flushing morphology (b).
Figure 4. The microscopic morphology of area 1 (a) with a typical flushing morphology (b).
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The different microstructure in area 2 is shown in Figure 5. According to Figure 5a, lots of white or dark grey particles implant in amorphous substance. Based on the EDS result as shown in Table 1, the particles are ZrO2 while the amorphous substance is SiO2. This also can be confirmed by the XRD result shown in Figure 2. The region shown in Figure 5b is farther fromthe spot center than the region shown in Figure 5c. As can be seen in Figure 5b, very fine sub-micron ZrO2 distributes evenly in amorphous SiO2. With the temperature increases from left to right in Figure 5b, amorphous SiO2 reduces gradually, while the quantity and size of ZrO2 particles increase gradually. In Figure 5c, amorphous SiO2 is much lower, even almost disappearing at the right side, which results from the evaporation of SiO2. Moreover, ZrO2 grains close to the spot center grow gradually, and can even be seen to sinter obviously.
Table 1. The energy dispersive spectroscopy (EDS) results of area B and C in Figure 2.
Table 1. The energy dispersive spectroscopy (EDS) results of area B and C in Figure 2.
ElementsArea BArea C
Weight Ratio %Atomic Ratio %Weight Ratio %Atomic Ratio %
O K36.3267.8526.5266.30
Si K15.3216.311.512.15
Zr L48.3615.8571.9731.55
Figure 5. The microscopic morphology of area 2 (a) and the further amplified morphology of region B (b) and C (c).
Figure 5. The microscopic morphology of area 2 (a) and the further amplified morphology of region B (b) and C (c).
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According to the equilibrium phase diagram of ZrO2-SiO2 shown as Figure 6 [12], the melting temperature (2700 °C) of ZrO2 can be decreased by liquid SiO2, while ZrO2 has high solubility, about 43.3% in SiO2 at 2235 °C. With increasing temperature, the solubility of ZrO2 will increase gradually. When laser begins to irradiate on the material, the surface temperature soars up rapidly. A large number of ZrB2 are oxidized into ZrO2 between 600–700 °C. Meanwhile, SiC transforms into SiO2 at 1200 °C, and SiO2 exhibits as a liquid above 1400 °C. When the temperature approaches 1687 °C, the oxidized ZrO2 begins to dissolve into SiO2. SiO2 is unstable when the temperature is higher than 1800 °C [13]. The evaporation of SiO2 at high temperature makes the ZrO2 solubility decrease, so the extremely fine ZrO2 grains precipitate. With the evaporation proceeding, the solubility of ZrO2 dissolved into SiO2 significantly decreases. A lot of ZrO2 will precipitate from liquid SiO2 to form the morphology shown in Figure 5b. As precipitated ZrO2 is still subject to intense high temperature, fine ZrO2 grains with strong activity gradually grow up and sinter together for a short time to form the morphology as shown in Figure 5c. Therefore, the processing of ZrO2 dissolution and precipitation is the main transformation mechanism during ablation when liquid SiO2 is present.
Figure 6. Thermal equilibrium phase diagram of SiO2-ZrO2.
Figure 6. Thermal equilibrium phase diagram of SiO2-ZrO2.
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The surface microstructure of ZrB2/SiC at the edge is shown in Figure 7. The temperature is lower than 1200 °C in this region away from the spot center. SiC oxidation and liquid SiO2 are not observed on the surface. The morphology of ZrB2 has changed because of oxidation. A lot of nano-crystals closely pack on the surface. This is proved to be ZrO2 according to the EDS result. This indicates that ZrB2 is directly oxidized into nano-ZrO2. The results reveal that there is another formation mechanism of ZrO2 during ablation when liquid SiO2 is absent.
Figure 7. The morphology of ZrB2/SiC at the edge after ablation (a) with nano ZrO2 crystals packing on the surface (b).
Figure 7. The morphology of ZrB2/SiC at the edge after ablation (a) with nano ZrO2 crystals packing on the surface (b).
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3. Experimental Section

The ZS composite was prepared using commercial powders listed as follows: ZrB2 (Alfa Aesar Ward Hill, MA, USA, 99.0%, particlesize ~50 μm); SiC (Alfa Aesar, 99.5%, particlesize 1–2 μm). The raw powders were accurately weighted by volume ratioof 4:1 and milled for 6 h in ethanol using zirconia milling media. The mixture powders were sintered by spark plasma sintering technology (SPS, DR. SINTER type 3.20, Fuji Electronic Industrial Co. Ltd., Kanagawa, Japan) at 1750 °C for 5 min with a rate of 200 °C/min. An axial pressure of 50 MPa was applied during the whole process.
The laser irradiation experiment in this paper was carried out by using ytterbium laser system (YLS-2000) (IPG Photonics Co. Ltd., Pittsfiels, MA, USA), with 1070 nm wave-length in atmospheric environment. The spot size of the Gaussianlaser was set as about 10 mm. The power density at the spot center reached 20 MW/m2 in Gaussian laser, and the duration time was 20 s. The dimensions of the ablation specimen were Φ25 mm × 3 mm.
The phase of the sample surface after ablation was detected by X-ray diffraction (XRD, X’pert PRO MPD, PANalytical B.V. Co. Ltd., Amsterdam, The Netherlands, Cu Kα). The surface microstructures of the sample before and afterablation were examined by scanning electron microscope (SEM, Philips S-4800, Hitachi Ltd., Yokohama, Japan). The composition of the sample was identified by energy dispersive spectroscopy (EDS, Oxford Instruments Co. Ltd., Oxfordshire, UK).

4. Conclusions

The ZrO2 formation in ZrB2/SiC composite during ablation was investigated in this paper. A characterized phenomenon at elevated temperature is preserved by using high intensity continuous laser with the rapid heating rate to irradiate. Two mechanisms of the ZrO2 formation are directly obtained, depending on whether liquid SiO2 is present. When liquid SiO2 is present, oxidized ZrO2 firstly dissolves into SiO2. Fine ZrO2 grains precipitate with the evaporation of liquid SiO2, and then grow, and even sinter together. Otherwise, the ZrB2 will be oxidized into ZrO2 directly.

Acknowledgments

This work was financially supported by the National Natural Science Foundation of China (No. 51102016) and Program for New Century Excellent Talents in University (NCET-11-0788).

Author Contributions

Ling Liu discussed the experiment and wrote the manuscript. Zhuang Ma and Shizhen Zhu conceived and designed the experiments. Zhenyu Yan and Lihong Gao performed the experiments and analyzed the data.

Conflicts of Interest

The authors declare no conflict of interest.

References

  1. Savino, R.; Fumo, M.D.; Paterna, D. Aerothermodynamic study of UHTC-based thermal protection systems. Aerosp. Sci. Technol. 2005, 9, 151–160. [Google Scholar] [CrossRef]
  2. Squire, T.H.; Marschall, J. Material property requirements for analysis and design of UHTC components in hypersonic applications. J. Eur. Ceram. Soc. 2010, 30, 2239–2251. [Google Scholar] [CrossRef]
  3. Jin, X.X.; He, R.J.; Zhang, X.H.; Hu, P. Ablation behavior of ZrB2-SiC sharp leading edges. J. Alloy. Compd. 2013, 566, 125–130. [Google Scholar] [CrossRef]
  4. Wang, X.G.; Liu, J.; Peng, L.M. ZrB2-SiC composite parts in oxyacetylenic torch tests: Experimental and computational assessment of chemical, thermal and mechanical behavior. Mater. Sci. Eng. A 2011, 528, 6896–6906. [Google Scholar] [CrossRef]
  5. Frederic, M.; Raffaele, S.; Stefano, F.M.; Andrea, M. Plasma wind tunnel testing of ultra high temperature ZrB2-SiC composites under hypersonic re-entry conditions. J. Eur. Ceram. Soc. 2009, 30, 2313–2321. [Google Scholar]
  6. Fahrenholtz, W.G.; Hilmas, G.E.; Chamberlain, A.L.; Zimmermann, J.W. Processing and characterization of ZrB2-based ultra-high temperature monolithic and fibrous monolithic ceramics. J. Mater. Sci. 2004, 39, 5951–5957. [Google Scholar] [CrossRef]
  7. Zhang, X.H.; Hu, P.; Han, J.C. Structure evolution of ZrB2-SiC during the oxidation in air. J. Mater. Res. 2008, 23, 1961–1972. [Google Scholar] [CrossRef]
  8. Rezaie, A.; Fahrenholtz, W.G.; Hilmas, G.E. Evolution of structure during the oxidation of zirconium diboride-silicon darbide in air up to 1500 °C. J. Eur. Ceram. Soc. 2007, 27, 2495–2501. [Google Scholar] [CrossRef]
  9. Carney, C.M. Oxidation resistance of hafnium diboride-silicon carbide from 1400 to 2000 °C. J. Mater. Sci. 2009, 44, 5673–5681. [Google Scholar] [CrossRef]
  10. Meng, S.H.; Chen, H.B.; Hu, J.H.; Wang, Z.W. Radiative properties characterization of ZrB2-SiC-based ultrahigh temperature ceramic at high temperature. Mater. Design. 2011, 32, 377–381. [Google Scholar] [CrossRef]
  11. Fahrenholtz, W.G.; Hilmas, G.E. Refractory diborides of zirconium and hafnium. J. Am. Ceram. Soc. 2007, 90, 1347–1364. [Google Scholar] [CrossRef]
  12. Butterman, W.C.; Foster, W.R. Zircon stability and the ZrO2-SiO2phase diagram. Am. Mineral. 1967, 52, 880–885. [Google Scholar]
  13. Eakins, E.; Jayaseelan, D.D.; Lee, W.E. Toward oxidation resistant ZrB2-SiC ultra high temperature ceramics. Metall. Mater. Trans. A 2011, 42, 878–887. [Google Scholar] [CrossRef]

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MDPI and ACS Style

Liu, L.; Ma, Z.; Yan, Z.; Zhu, S.; Gao, L. The ZrO2 Formation in ZrB2/SiC Composite Irradiated by Laser. Materials 2015, 8, 8745-8750. https://doi.org/10.3390/ma8125475

AMA Style

Liu L, Ma Z, Yan Z, Zhu S, Gao L. The ZrO2 Formation in ZrB2/SiC Composite Irradiated by Laser. Materials. 2015; 8(12):8745-8750. https://doi.org/10.3390/ma8125475

Chicago/Turabian Style

Liu, Ling, Zhuang Ma, Zhenyu Yan, Shizhen Zhu, and Lihong Gao. 2015. "The ZrO2 Formation in ZrB2/SiC Composite Irradiated by Laser" Materials 8, no. 12: 8745-8750. https://doi.org/10.3390/ma8125475

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