Microstructure, mechanical properties and oxidation resistance of SiCf/SiC composites incorporated with boron nitride nanotubes

Guangxiang Zhuabc, Shaoming Dong*ab, Dewei Niab, Chengying Xud and Dengke Wangab
aState Key Laboratory of High Performance Ceramics and Superfine Microstructure, Shanghai Institute of Ceramics, Chinese Academy of Sciences, Shanghai 200050, China. E-mail: composites@mail.sic.ac.cn; Tel: +86-21-52414324
bStructural Ceramics and Composites Engineering Research Center, Shanghai Institute of Ceramics, Chinese Academy of Sciences, Shanghai 200050, China
cUniversity of Chinese Academy of Sciences, Beijing 100049, China
dDepartment of Mechanical Engineering, Florida State University, Tallahassee, FL 32310, USA

Received 26th June 2016 , Accepted 27th August 2016

First published on 29th August 2016


Abstract

SiCf/BNNTs–SiC hierarchical composites were fabricated via firstly in situ growth of boron nitride nanotubes (BNNTs) on the surface of silicon carbide (SiC) fibers using boron powder as a raw material and subsequently matrix densification by chemical vapor infiltration (CVI) and polymer impregnation/pyrolysis (PIP) methods. With the incorporation of BNNTs, energy dissipation mechanisms at the nanoscale triggered by BNNTs such as pullout, debonding, crack deflection and crack bridging are observed. But the positive effect of BNNTs on mechanical properties have not been raised due to the offset from the negative effect of pores in composites. Additionally, the residual boron powder results in an improved oxidation resistance and parabolic oxidation kinetics of SiCf/SiC composites at 900 °C, thanks to the protective effect of the B2O3 glassy phase formed by the oxidation of boron. Consequently, a better strength retention after oxidation is obtained. Moreover, it is believed that the remaining strengthening and toughening mechanisms aroused by BNNTs surviving after oxidation probably also make a contribution to the better strength retention.


Introduction

Continuous silicon carbide (SiC) fiber reinforced SiC matrix (SiCf/SiC) composites have been universally used in aero-engine hot section components including exhaust cones, flame stabilizers, nozzle flaps etc. due to their excellent properties, such as outstanding high-temperature strength, high fracture toughness, good thermal stability and low density.1–3 By embedding continuous SiC fibers in the monolithic SiC ceramic matrix, energy dissipation mechanisms can be triggered including debonding at the fiber/matrix interface, crack deflection, fiber bridging, sliding and pullout and so on, which ensures that SiCf/SiC composites exhibit a non-catastrophic failure mode.3 Nonetheless, these energy dissipation mechanisms merely originate from micron scale fibers. The matrix at the micron scale among fibers cannot be strengthened and toughened by the above-mentioned mechanisms, thus still shows a brittle behavior. Such matrixes at the micron scale are weak points in SiCf/SiC composites, the mechanical properties of which remain to be further improved.

In recent years, the development of one dimensional (1D) nanoscale reinforcements with extraordinary mechanical properties such as carbon nanotubes (CNTs) offers an effective approach to solve the above-mentioned problem. 1D nanoscale reinforcements can be introduced into the matrix at micron scale among micron-diameter fibers.4 The existence of nanoscale reinforcements are expected to arouse additional energy dissipation mechanisms at nanoscale and improve the mechanical properties of matrix at micron scale. To avoid the agglomeration of nanostructures in matrix resulting from directly dispersion in the precursor,4,5 in situ growing nanostructures directly on the surface of conventional micro-scale fibers to build fiber/nanostructures hierarchical (or multi-scale or hybrid) structures is a favorable method to introduce nanoscale reinforcements into matrix of composites. And then, hierarchical composites are fabricated by depositing matrix into fiber/nanostructures hierarchical structures. To date, many researchers have reported fiber/CNTs hierarchical composites with remarkably improved mechanical properties by CNTs.5–9 However, CNTs exhibit relatively poor oxidation resistance and readily oxidize in air above 400 °C,10 thus leading to partial or total malfunction of strengthening and toughening mechanisms ascribed to CNTs and limiting their further applications at high temperatures.

As a new kind of advanced 1D nanomaterial, boron nitride nanotubes (BNNTs) have drawn tremendous attention from scientists recently by virtue of their remarkable properties.11 On account of structural similarity to CNTs, BNNTs also present excellent properties such as high elastic modulus, high tensile strength and high thermal conductivity,11–13 which endows BNNTs a potential application in composites as nanoscale reinforcements like CNTs. Moreover, BNNTs show much higher thermal and chemical stability than CNTs and possess good oxidation resistance up to 900 °C.10,14 This superiority, therefore, makes BNNTs more suitable than CNTs as nanoscale reinforcements in hierarchical composites for enduring service at high temperature in oxidizing environment. However, to the best of our knowledge, until now, almost no studies have been reported on the subject of fiber/BNNTs hierarchical composites.

In the present study, we report, for the first time, the fabrication of SiC fiber/BNNTs hierarchical reinforced SiC matrix composites (SiCf/BNNTs–SiC) by two steps: firstly in situ growth of BNNTs on the surface of SiC fibers to build fiber/BNNTs hierarchical structures, which has been reported in our previous work,15 and subsequently matrix densification of hierarchical structures via chemical vapor infiltration (CVI) and polymer impregnation/pyrolysis (PIP) methods. In this paper, boron powder was employed as boron source for the growth of BNNTs. Moreover, it is anticipated that the residual part of boron powder after the growth of BNNTs can also serve as boron-bearing species that self-healing composites usually contain. The boron-bearing species can easily oxidize to form glassy phase (B2O3) to seal the cracks or pores and hinder the in-depth diffusion of oxygen, thus giving rise to improved oxidation resistance at relatively low temperatures (500–1000 °C).2,16 To confirm the existence of BNNTs in SiCf/SiC composites, the morphology, microstructure and chemical composition of nanoscale reinforcements were studied and discussed in this paper. What's more, microstructure, mechanical properties and oxidation resistance of SiCf/BNNTs–SiC hierarchical composites were investigated systematically.

Experimental

Synthetic procedures

The fabrication of SiCf/BNNTs–SiC hierarchical composites was carried out by two steps: (1) at first, in order to build SiCf/BNNTs hierarchical structures, BNNTs were in situ grown on the surface of SiC fibers via a simplified ball milling, impregnation and annealing method using boron powder as raw material, as reported in our previous work.15 Herein, SiC fiber (with an impurity element of oxygen: about 2.5 wt%) cloths (0/90°) with a size of 7 cm × 7 cm were adopted for the synthesis of SiCf/BNNTs hierarchical structures. Additionally, previous to in situ growth of BNNTs, pyrolytic carbon/silicon carbide multilayered interphases (PyC/SiC)n (n = 3) were deposited on SiC fiber cloths. PyC interphase accounts for about 7 wt% of the fiber cloths. (2) Subsequently, CVI and PIP methods were employed to introduce the SiC matrix into the SiCf/BNNTs hierarchical structures. The fiber clothes with BNNTs in situ grown were stacked, and compressed together with a volume fraction of fibers of about 40%. Then those stacked fiber clothes were put into the CVI furnace and the SiC matrix was deposited into SiCf/BNNTs hierarchical structures at the temperature of 1000 °C using methyltrichlorosilane (MTS, CH3SiCl3) and hydrogen (H2) as the precursors with the molar ratio of H2 to MTS of 10. The CVI process was repeated for several cycles. Then some relatively large pores failing to be fully occupied with matrix during the CVI process were further densified via PIP method, in which polycarbosilane (PCS) was employed as the precursor of SiC matrix and pyrolyzed at 900 °C in argon (Ar) atmosphere. Finally, the relatively dense SiCf/BNNTs–SiC hierarchical composites were achieved. SiCf/SiC composites without BNNTs were fabricated via the same CVI and PIP process as described above for comparison.

Characterization

To investigate the oxidation resistance of composites, static oxidation test was carried out in a muffle furnace in static air at 900 °C for 40 h. The specimens were put into the furnace when the furnace was heated up to the desired temperature. Weight changes of the specimens were measured by an analytical balance with a sensitivity of ±0.01 mg. Bulk density and open porosity of the composites were measured by Archimedes method. Flexural strength of the composites before and after oxidation was evaluated by a three-point bending test with a span of 30 mm at a cross head speed of 0.5 mm min−1 on bar specimens with the dimension of 2.9 mm × 5.0 mm × 45 mm. The flexure strength value (σf) was determined by eqn (1):17
 
σf = 3FL/(2bd2) (1)
where F, L, b and d are the load at the fracture point, the span length, the sample width and the sample thickness, respectively. In addition, fracture toughness was measured using single edge notched beam (SENB) method with a span of 30 mm on bar specimens with the dimension of 2.9 mm × 5.0 mm × 45 mm (with a notch of 2.5 mm in depth). The fracture toughness value (KIC) was calculated by eqn (2):4
 
KIC = (3pl/(2bw3/2))[1.93 − 3.07(a/w) + 1.45(a/w)2 − 25.07(a/w)3 + 25.8(a/w)4] (2)
where p is the breaking load, l is the span length, b is the sample thickness, w is the sample width and a is the notch depth. The above mechanical properties measurements were carried out on an Instron-5566 universal testing machine. A small piece of the fiber cloth with BNNTs grown was used for the morphology characterization of BNNTs via a Hitachi SU8220 field-emission scanning electron microscopy (FESEM). To investigate the microstructure of the composites, the polished cross-sections and fracture surfaces of the composites were studied by FESEM. A JEM-2100F field emission transmission electron microscopy (FETEM) was used to characterize the microstructure of BNNTs. For microstructure analysis of BNNTs, a piece of the fiber cloth with BNNTs grown was ultrasonically vibrated in ethanol for 1–2 h to collect adequate quantity of BNNTs from fibers first. Then the dispersion solution was dripped onto copper grids with a holey carbon film for TEM investigations. An X-ray energy dispersive spectroscopy (EDS) attached to FETEM was employed to determine chemical composition of BNNTs. The distributions of different elements in the polished cross-sections of the composites after oxidation were investigated via an X-ray EDS attached to FESEM.

Results and discussion

A simplified ball milling, impregnation and annealing method was employed to in situ grow BNNTs on the surface of SiC fibers. The morphology, microstructure and chemical composition of as-grown BNNTs were exhibited in Fig. 1. It can be seen that the surface of fiber cloth is utterly encompassed by BNNTs, obscuring individual fiber within the cloth, as displayed in Fig. 1a–c. As-grown BNNTs have a length of around several tens of micrometers and entangle with each other, appearing to form a thick blanket besieging fibers. As estimated according to the weight change of fiber cloth before and after the growth of BNNTs, as-grown BNNTs account for about 2 wt% of the fiber cloth. The typical TEM images in Fig. 1d and e obviously reveal that BNNTs exhibit a multi-walled and bamboo-like structure with the average diameter of 30–160 nm. Additionally, almost all the BNNTs apparently possess the bubble-chain walls, as indicated in Fig. 1d and e. The formation mechanism of bamboo-like BNNTs with bubble-chain walls can be well explained with stress-induced sequential growth mode in vapor–liquid–solid (VLS) mechanism, as elaborately discussed in our previous work.15 From the inset in Fig. 1e, it can be illustrated that the nanotube has perfect crystalline structure with clear parallel fringes. The spacing between the parallel fringes is ∼0.335 nm, which is in line with d002 inter-planar distance of bulk h-BN. The EDS spectra of the nanotubes shown in Fig. 1f confirms that the nanotubes are BNNTs according to the strong B and N peaks. The Fe element is attributable to the steel particles which are introduced by ball-milling treatment with stainless steel balls and act as the catalysts for BNNTs growth. The Cu peak derives from the copper TEM grid and O element may be ascribed to the surrounding air absorbed on the surface of nanotubes.15 These nanoscale “filaments”, i.e. BNNTs, are incorporated with micro-scale SiC fibers to form hierarchical structures, which are used to fabricate SiCf/BNNTs–SiC hierarchical composites subsequently.
image file: c6ra16496j-f1.tif
Fig. 1 (a–c) Low-magnification SEM images of BNNTs in situ grown on fiber cloth. (d) and (e) TEM images of bamboo-like BNNTs. The inset shows the parallel fringes of nanotubes, between which the spacing is ∼0.335 nm, as labeled in the inset. (f) EDS spectra of BNNTs. The strong B and N peaks confirm that the nanotubes are BNNTs. The Fe element is attributable to the steel particles introduced by ball-milling treatment with stainless steel balls. The Cu peak derives from the Cu TEM grid and O element may be ascribed to the surrounding air absorbed on the surface of nanotubes.

After densification by CVI and PIP methods, SiCf/SiC composites and SiCf/BNNTs–SiC hierarchical composites with about 1 wt% BNNTs in situ grown were obtained. The density, open porosity, flexural strength and fracture toughness of these two kinds of composites were measured and given in Table 1. It can be seen that SiCf/BNNTs–SiC hierarchical composites have an average density of 2.58 ± 0.04 g cm−3 and an open porosity of 5.11 ± 1.30% while 2.69 ± 0.03 g cm−3 and 4.22 ± 1.12% for SiCf/SiC composites. This result implies that the incorporation of BNNTs into SiCf/SiC composites gives rise to a decline in average density of the composites and correspondingly an increase in open porosity. This phenomenon is also affirmed by the observation of the polished cross-sections of the composites, as exhibited in Fig. 2. In Fig. 2a, several relatively small intra-bundle pores are observed in the fiber bundle of SiCf/SiC composites resulting from the stop of matrix densification when the surface pores are closed, which is inevitable and an intrinsic flaw of CVI method.18 However, in this case, although intra-bundle pores exist, all the fibers are deposited with matrix with the thickness of at least about 3 μm, which can be seen in the inset in Fig. 2a. So the SiCf/SiC composites are relatively dense with a lower open porosity compared with the SiCf/BNNTs–SiC hierarchical composites. On the contrary, in the SiCf/BNNTs–SiC hierarchical composites, much more and larger intra-bundle pores are observed in the fiber bundle, as shown in Fig. 2b. What's worse, almost all the fibers in the center region of fiber bundle fail to be deposited with matrix and only the fibers close to the surface of fiber bundle are densified with matrix. This phenomenon results in a lower density of the SiCf/BNNTs–SiC hierarchical composites, which also bothers Manocha et al.19 in SiC/C composites incorporated with CNTs. Considering that the two kinds of composites are fabricated under the same condition with the same fiber fabric, the only possible reason for this different densification is the introduction of BNNTs in situ grown on the surface of fibers into SiCf/BNNTs–SiC hierarchical composites. The existence of BNNTs divides the micro-scale pores into nanoscale ones among fibers. During CVI process, the nanoscale pores diminish quickly and can be sealed easily, resulting in an earlier clogging of the pore channels in the surface region of fiber bundle and therefore leading to an improper infiltration of matrix in the center region.20 In other words, to some extent, BNNTs in situ grown in the surface region of fiber bundle exacerbate the intrinsic downside of CVI method as mentioned above. Such large intra-bundle pores unfilled with enough matrix as structural defects in SiCf/BNNTs–SiC hierarchical composites definitely will pose stress concentration in the matrix and undermine the effective load transfer from matrix to fibers. They also will impair the positive interfacial friction between matrix and fibers during the fiber pullout. So eventually these structural defects will give rise to the great decrease of mechanical properties including strength and toughness. It is in consistence with the reported results about declined strength of polymer, ceramic or carbon/carbon composites reinforced by BNNTs or CNTs,21–24 which is also ascribed to the lower density and higher porosity in the composites incorporated with nanotubes. Nevertheless, by comparing mechanical properties of two kinds of composites, as listed in Table 1, it can be noticed that SiCf/BNNTs–SiC hierarchical composites have an average flexural strength of 442.7 ± 24.8 MPa, which is only slightly lower than that of 482.9 ± 45.6 MPa for SiCf/SiC composites. What's more, the average fracture toughness of SiCf/BNNTs–SiC hierarchical composites is 15.3 ± 1.0 MPa m1/2, which is almost equivalent to that of 15.5 ± 2.8 MPa m1/2 for SiCf/SiC composites. This result as discussed above hints that the incorporation of BNNTs into SiCf/SiC composites indeed yields a positive effect on the mechanical properties of the composites.

Table 1 Properties of SiCf/SiC composites and SiCf/BNNTs–SiC hierarchical composites
Composites BNNTs content (wt%) Density (g cm−3) Open porosity (%) Flexural strength (MPa) Fracture toughness (MPa m1/2)
SiCf/SiC 0 2.69 ± 0.03 4.22 ± 1.12 482.9 ± 45.6 15.5 ± 2.8
SiCf/BNNTs–SiC 1.0 2.58 ± 0.04 5.11 ± 1.30 442.7 ± 24.8 15.3 ± 1.0



image file: c6ra16496j-f2.tif
Fig. 2 Low-magnification SEM images of the polished cross-sections of the fiber bundle in (a) SiCf/SiC composites and (b) SiCf/BNNTs–SiC hierarchical composites. Pores are observed in both two composites, as indicated by white arrows. The inset shows the enlarged image of the polished cross-section of the fiber bundle in SiCf/SiC composites.

To identify the evidence about positive effect of BNNTs on mechanical properties of the composites, morphologies of the polished cross-sections and fracture surfaces of SiCf/BNNTs–SiC hierarchical composites were investigated via FESEM, as displayed in Fig. 3 and 4. Fig. 3a and b show the low-magnification SEM images of the polished cross-sections of SiCf/BNNTs–SiC hierarchical composites. It can be found that space among horizontal and vertical fibers is not fully densified with matrix, which is in line with the low density of composites as discussed before. In these areas with an insufficiently deposited matrix, many apparent micro-scale rods can be readily observed. The high-magnification SEM image of micro-scale rods (Fig. 3c) reveals that such micro-scale rods twine with each other with the diameters of 0.8–1 μm. These micro-scale rods are believed to develop from the original nanotubes after the subsequent CVI matrix densification process. During the CVI process, matrix is deposited on the surface of nanotubes, but fails to be dense. It can be confirmed from a broken micro-scale rod as shown in Fig. 3d, which clearly displays that there is a BNNT inside the micro-scale rod. The above result also demonstrates that BNNTs were successfully introduced into the matrix among fibers. The morphology of the fracture surfaces of matrix among fibers in SiCf/BNNTs–SiC hierarchical composites was exhibited in Fig. 4. It can be clearly seen that BNNTs pull out from matrix, leading to some pores or slots left in the matrix, as shown in Fig. 4a and b. Fig. 4c apparently indicates that the interfacial debonding between BNNTs and matrix occurs in the fracture surface. In addition, it is believed that crack deflection definitely also happens during above mentioned pullout and debonding.25 Moreover, from Fig. 4d, it also can be observed that crack is bridged by a BNNT with its ends firmly embedded in matrix. It is universally acknowledged that pullout, debonding, crack deflection and crack bridging are the major strengthening and toughening mechanisms for micro-scale fibers reinforced composites. In our work, such strengthening and toughening mechanisms are observed as well in the matrix of SiCf/SiC composites incorporated with BNNTs, which are aroused by nanoscale reinforcements of BNNTs. When the propagating crack encounters BNNTs vertical to the propagation direction or with a certain angle (indicated in Fig. 4a by arrow 1 and 2, respectively), the crack is deflected and BNNTs are stretched across the crack, exhibiting the phenomenon of crack bridging as shown in Fig. 4d. BNNTs will break when reaching their critical strain or pull out when reaching the interfacial bonding strength. These processes will dissipate some fracture energy.22 In addition, BNNTs parallel to the propagation direction of crack also deflect the crack and are peeled away from the matrix after the interfacial debonding, as displayed in Fig. 4c, which also absorbs some energy.26 These above-discussed energy dissipation mechanisms at nanoscale triggered by BNNTs spotlights the evidence that the incorporation of BNNTs into SiCf/SiC composites is propitious for improving mechanical properties of the composites. Merely, the real contribution of BNNTs to mechanical properties of the composites may be partially offset by the negative effect of the low density and high porosity. It suggests that careful consideration is needed for the densification of hierarchical composites in our further study to avoid above flaw. There are two possible ways to reduce the porosity of the hierarchical composites. The first one is to slow down the deposition rate of SiC matrix during the CVI process by decreasing the deposition pressure (i.e. the concentration of precursors in the CVI furnace) or temperature so that the nanoscale pore channels in the surface region of fiber bundle will not be clogged too early. In this case, more time for the matrix deposition in the center region of fiber bundle is obtained. This method is a widely-used way to relieve the above-mentioned intrinsic flaw of CVI process. The other approach to increase the density and decrease the porosity of the hierarchical composites is using polymer impregnation/pyrolysis (PIP) method to introduce SiC matrix into the center region of fiber bundle. The PIP method used in this paper is only for the densification of some relatively large pores among fiber bundles, as mentioned in the Experimental section. When it is adopted for the densification of the center region of fiber bundle, the capillary force from the nanoscale pores channels will be beneficial for the polymer precursor infiltration into the fiber bundle, thus being good for reducing the porosity.


image file: c6ra16496j-f3.tif
Fig. 3 Low-magnification SEM images of the polished cross-sections of SiCf/BNNTs–SiC hierarchical composites: (a) horizontal and (b) vertical fibers. High-magnification SEM images of micro-scale rods in the areas with an insufficiently deposited matrix, showing (c) the overall morphology of micro-scale rods and (d) a broken micro-scale rod with a BNNT inside.

image file: c6ra16496j-f4.tif
Fig. 4 High-magnification SEM images of the fracture surfaces of matrix among fibers in SiCf/BNNTs–SiC hierarchical composites, showing typical morphology of (a) and (b) the pullouts of BNNTs, (c) debonding between BNNTs and matrix and (d) crack bridging by BNNTs.

On the other hand, as exhibited in Fig. 4b, the pullouts of BNNTs vertical to the fracture surface are very short, which may limit the toughening effect arising from the interfacial friction during the pullout. According to the results reported by Wang et al.26 and Tatarko et al.,27 a rather strong interface bonding, which originates from chemical reaction between matrix and the reinforcement phase, may be responsible for the short pullout length. However, given that BNNTs are chemically stable and the surfaces of BNNTs pulling out or debonding from matrix (as indicated in Fig. 4a and c, respectively) are very smooth without adhered matrix, this explanation can't hold water for our study. In fact, as discussed before about the microstructure of BNNTs, almost all the BNNTs have the bubble-chain walls with obvious periodical knots. These knots can act as structural anchors and cause mechanical interlocking between the matrix and BNNTs, thus resulting in strong interface bonding and short pullout length. It also has been found in ceramic or mental reinforced by bamboo-like CNTs or SiC nanowires with obvious knots.28,29 Additionally, unlike cylindrical nanotubes, bamboo-like BNNTs prefer to break at the inner joints due to the discontinuity of the lattice,27,30 as affirmed in Fig. 4b, which also brings about short pullout length.

To evaluate the oxidation resistance of SiCf/SiC composites and SiCf/BNNTs–SiC hierarchical composites, static oxidation test was conducted at 900 °C for 40 h. Fig. 5a and b show the overall morphologies of the polished cross-sections of the composites after oxidation. By comparison with that before oxidation as displayed in Fig. 2, it can be found that after oxidation fibers and intra-bundle matrix of SiCf/SiC composites seem to be fragmented. Clear comparisons about high-magnification SEM images of the fiber bundle in SiCf/SiC composites before and after static oxidation are exhibited in Fig. 5c–f. Before oxidation, the polished cross-section is smooth and multilayered interphases (PyC/SiC)n (n = 3) are intact, as shown in Fig. 5c and e. After oxidation, it can be seen from Fig. 5d that the polished cross-section is bumpy and a lot of annular slots appear circumferential to fibers in SiCf/SiC composites. Fig. 5f obviously reveals that these slots arise from the disappearance of oxidized PyC interphase. However, by contrast, no significant distinction about the overall morphology of the polished cross-sections of SiCf/BNNTs–SiC hierarchical composites before and after oxidation can be observed from Fig. 2b and 5b. Only PyC interphase close to the crack that is the diffusion channel of oxygen into fiber bundles is oxidized and multilayered interphases are partly broken, as indicated by white arrows in the inset in Fig. 5b. The above result infers that SiCf/BNNTs–SiC hierarchical composites have a better oxidation resistance than SiCf/SiC composites. To pin down the oxidation kinetics of the composites, the weight losses of composites as a function of oxidation time were recorded. From the experimental data (square dots) and corresponding fitting curves (red lines) of the weight losses of composites as depicted in Fig. 6, it can be seen that the weight loss of SiCf/SiC composites increases linearly with respect to the oxidation time while that of SiCf/BNNTs–SiC hierarchical composites exhibits a parabolic behavior. As discussed above, the disappearance of oxidized PyC interphase is responsible for the weight losses of composites. In this paper, it can be estimated that PyC interphase accounts for about 2.5 wt% of the composites. After oxidation at 900 °C for 40 h, the weight loss of SiCf/SiC composites reaches 0.47 wt% while that of SiCf/BNNTs–SiC hierarchical composites is only 0.37 wt%. The PyC interphase is oxidized above 400 °C, of which the key steps are given as follows: (1) diffusion of oxygen to PyC interphase. (2) Chemical reaction between oxygen and PyC interphase. (3) Diffusion of the products CO and/or CO2 away from PyC interphase.31 The oxidation behavior of PyC interphase in SiCf/SiC composites can be described by linear-parabolic kinetics:32

 
x2/kp + x/k1 = t (3)
where x is the recession distance, t is the oxidation time, kp is the parabolic rate constant and k1 is the linear rate constant. In eqn (3), the first part is related to the diffusion of oxygen and the second one is concerned with the carbon and oxygen reaction. When the diffusion of oxygen to PyC interphase is very easy through the cracks or pores, the interior has a high concentration of oxygen and the oxidation reaction is nearly uniform. Namely, in this case kp is higher than k1 and the first part can be ignored.32,33 The oxidation of PyC interphase is a reaction-controlled process and corresponds to linear kinetics, as shown in Fig. 6a. On the contrary, when the diffusion of oxygen is hindered, there is a starvation for oxygen in the interior and the oxidation reaction only occurs near the outside surface where oxygen is abundant. So kp is smaller than k1 and the oxidation of PyC interphase is a diffusion-controlled process, exhibiting a parabolic behavior, as affirmed in Fig. 6b. From above discussion, it can be demonstrated that the diffusion of oxygen in SiCf/BNNTs–SiC hierarchical composites is blocked to a great extent. Additionally, it needs to be especially clarified that the above explanation is based on the assumption that the oxidation of SiC at 900 °C can be neglected due to its low passive oxidation rate.32,34 However, in fact it can't be ignored especially when long oxidation time such as several tens of hours is concerned.35–37 The formation of silica from the passive oxidation of SiC can result in the weight gain of composites and narrow the cracks, thus giving rise to a decreasing weight loss and a tendency of transition of oxidation behavior from linear to parabolic kinetics. A slight sign of this phenomenon can be observed from experimental data in Fig. 6a. But the influence of this phenomenon is limited because the amount of silica is relatively small and the cracks are not completely but slightly narrowed.34,38,39 Hence, extremely clear parabolic oxidation kinetics of SiCf/BNNTs–SiC hierarchical composites should be attributed to some other mechanisms.


image file: c6ra16496j-f5.tif
Fig. 5 Low-magnification SEM images of the polished cross-sections of (a) SiCf/SiC composites and (b) SiCf/BNNTs–SiC hierarchical composites after static oxidation at 900 °C for 40 h. The enlarged view of fibers near the crack is inserted in the right image. High-magnification SEM images of the fiber bundle in SiCf/SiC composites: (c) and (e) before and (d) and (f) after oxidation.

image file: c6ra16496j-f6.tif
Fig. 6 Weight losses of (a) SiCf/SiC composites and (b) SiCf/BNNTs–SiC hierarchical composites as a function of time oxidized in static air at 900 °C for 40 h: experimental data (square dots) and fitting curves (red lines). The curve-fitting equations and corresponding coefficients of determination (R2) are given in the figures.

To develop a comprehensive understanding of the mechanism of oxidation resistance, the distributions of different elements in the fiber bundle after oxidation were investigated by EDS. Fig. 7 and 8 show the SEM images of the polished cross-sections of SiCf/BNNTs–SiC hierarchical composites and SiCf/SiC composites after oxidation, along with corresponding EDS elemental mapping images of O, B, Si and C. The Si and C elemental mapping images are in good agreement with the distributions of SiC matrix and fibers in both composites. Additionally, it can be seen from Fig. 7e that the concentration of C element circumferential to fibers in SiCf/BNNTs–SiC hierarchical composites is relatively high, which is hardly found in SiCf/SiC composites from Fig. 8d. Such relatively high concentration of C element is ascribed to the PyC interphase surviving after oxidation. Moreover, as shown in Fig. 7b and c, O element aggregation is observed near the outside surface of the fiber bundle, especially in the area where B element is located, inferring that the glassy phase (B2O3) is produced by the reaction of oxygen and boron powder in such area.2,16 This glassy phase has a low viscosity at 900 °C and can seal the diffusion channel of oxygen further into the fiber bundle in some degree.16 So the concentration of O element in the interior of the fiber bundle is relatively low. By contrast, in SiCf/SiC composites O element diffuses into the fiber bundle very easily, thus inducing the oxidation of the PyC interphase and even the fibers. Consequently, oxygen is mainly distributed in the fibers as exhibited in Fig. 8b. In fact, SiC fibers cannot be oxidized completely because of their low passive oxidation rate at 900 °C. So precisely speaking, O element diffusing from the exterior should be distributed in the silica layer at the edges of fibers. O element in the center of the fiber is regarded as an inevitable impurity element that as-received SiC fibers often contain. Further investigation on the distributions of different elements from the matrix to the fiber after oxidation were also conducted by EDS. Fig. 9 shows EDS elemental line scan profiles of the polished cross-sections of SiCf/BNNTs–SiC hierarchical composites and SiCf/SiC composites after oxidation. Apparently, it can be noticed from Fig. 9a and b that in SiCf/BNNTs–SiC hierarchical composites O element is mainly distributed outside the multilayered interphases (PyC/SiC)n (n = 3) where the residual boron powder is situated. It implies that oxygen is blocked outside the multilayered interphases and the fiber by the oxidation of the residual boron powder, from which the glassy phase (B2O3) with a low viscosity can seal the diffusion channel of oxygen. Hence, from the multilayered interphases to the fiber, almost no oxygen can be found. The PyC interphase succeeds to survive after oxidation for 40 h at 900 °C, as affirmed by the three peaks of C concentration curve in Fig. 9b corresponding to three layers of PyC interphases. On the contrary, O element is detected in the multilayered interphases and even the fiber in SiCf/SiC composites, as revealed in Fig. 9c and d. At the positions where three layers of PyC interphases are located, no peaks of C concentration curve can be observed. Moreover, the concentration of O element in the fiber is obviously higher than that in the matrix, which is not observed in SiCf/BNNTs–SiC hierarchical composites (Fig. 9b). It gives the evidence that because of no obstruction to the diffusion of oxygen towards the multilayered interphases, the PyC interphase is easily oxidized and even eventually O element also diffuses into the fiber. The above analysis of EDS results demonstrates that the anticipation that after the growth of BNNTs the residual boron powder besieging the multilayered interphases can hinder the in-depth diffusion of oxygen towards the PyC interphases by oxidizing to form glassy phase (B2O3) is realized, which is considered to be responsible for better oxidation resistance and parabolic oxidation kinetics of SiCf/BNNTs–SiC hierarchical composites at 900 °C for 40 h.


image file: c6ra16496j-f7.tif
Fig. 7 (a) SEM image of the polished cross-section of SiCf/BNNTs–SiC hierarchical composites after oxidation, along with corresponding (b–e) EDS elemental mapping images of O, B, Si and C. O element aggregation is observed in the area where B element is located.

image file: c6ra16496j-f8.tif
Fig. 8 (a) SEM image of the polished cross-section of SiCf/SiC composites after oxidation, along with corresponding (b–d) EDS elemental mapping images of O, Si and C. O element is mainly distributed in the fibers.

image file: c6ra16496j-f9.tif
Fig. 9 EDS elemental line scan profiles of the polished cross-sections of (a) and (b) SiCf/BNNTs–SiC hierarchical composites and (c) and (d) SiCf/SiC composites after oxidation. The positions of SiC matrix, multilayered interphases (PyC/SiC)n (n = 3), boron powder and SiC fiber before oxidation are depicted in the two images on the right.

The flexural strength and strength retention of SiCf/SiC composites and SiCf/BNNTs–SiC hierarchical composites after oxidation in static air at 900 °C for 40 h were also evaluated and summarized in Table 2. After oxidation, the flexural strength of SiCf/BNNTs–SiC hierarchical composites declines from 442.7 ± 24.8 MPa to 419.1 ± 34.0 MPa while from 482.9 ± 45.6 MPa to 424.4 ± 50.4 MPa for SiCf/SiC composites. By comparing the strength retentions of two composites, it can be found that after oxidation SiCf/BNNTs–SiC hierarchical composites can retain 94.7% of the initial flexural strength while only 87.8% for SiCf/SiC composites. No doubt that it is the direct reflection of improved oxidation resistance of SiCf/BNNTs–SiC hierarchical composites thanks to the residual boron powder that ensures that little PyC interphase is oxidized for 40 h at 900 °C. Fig. 10 shows the morphology of the fracture surface of matrix among fibers in SiCf/BNNTs–SiC hierarchical composites after oxidation. The pullouts of BNNTs clearly can be seen in the matrix, as indicated by white arrows in Fig. 10. It infers that BNNTs in composites succeed to survive after oxidation and still can play a role as nanoscale reinforcements to bring about strengthening and toughening mechanisms at nanoscale in SiCf/BNNTs–SiC hierarchical composites. So it is believed that the surviving BNNTs in composites probably also make a contribution to the better strength retention after oxidation.

Table 2 Flexural strength and strength retention of SiCf/SiC composites and SiCf/BNNTs–SiC hierarchical composites before and after oxidation in static air at 900 °C for 40 h
Composites BNNTs content (wt%) Flexural strength (MPa) Strength retention (%)
Before oxidation After oxidation
SiCf/SiC 0 482.9 ± 45.6 424.4 ± 50.4 87.8
SiCf/BNNTs–SiC 1.0 442.7 ± 24.8 419.1 ± 34.0 94.7



image file: c6ra16496j-f10.tif
Fig. 10 High-magnification SEM image of the fracture surface of matrix among fibers in SiCf/BNNTs–SiC hierarchical composites after oxidation, showing typical morphology of the pullouts of BNNTs.

Conclusions

SiCf/BNNTs–SiC hierarchical composites were fabricated via firstly in situ growth of BNNTs on the surface of SiC fibers and subsequently matrix densification via CVI and PIP methods. The as-grown BNNTs utterly encompass the fiber cloth and exhibit a multi-walled and bamboo-like structure with an average diameter of 30–160 nm and a length of several tens of micrometers. In addition, almost all the BNNTs apparently possess the bubble-chain walls. BNNTs in SiCf/SiC composites divide the micro-scale pores into nanoscale ones among fibers. Due to an earlier clogging of these nanoscale pore channels and thus an improper infiltration of matrix during CVI process, the incorporation of BNNTs into SiCf/SiC composites gives rise to a decline in density of composites and correspondingly an increase in open porosity. However, even with these insufficient filled pores as structural defects, flexural strength of the SiCf/BNNTs–SiC hierarchical composites is only slightly undermined while fracture toughness displays almost no decrease. Pullout, debonding, crack deflection and crack bridging attributed to BNNTs are observed, which are considered as energy dissipation mechanisms at nanoscale triggered by nanoscale reinforcements. It verifies the positive effect of BNNTs on the mechanical properties of the composites. Additionally, SiCf/BNNTs–SiC hierarchical composites achieve an improved oxidation resistance and parabolic oxidation kinetics at 900 °C for 40 h. It is attributable to the mechanism that after the growth of BNNTs the residual boron powder besieging the multilayered interphases can hinder the in-depth diffusion of oxygen towards the PyC interphases by oxidizing to form glassy phase (B2O3). Moreover, SiCf/BNNTs–SiC hierarchical composites possess a better strength retention after oxidation. This is believed to not only be the direct reflection of improved oxidation resistance thanks to the residual boron powder but also benefit from the remained strengthening and toughening mechanisms aroused by BNNTs surviving after oxidation.

Acknowledgements

This work is supported by the National Natural Science Foundation of China (Grant No. 51502323 and 51172256), Shanghai Key Project of Basic Research (Grant No. 14JC1406200) and Shanghai Scientific Research Project (Grant No. 13521101203).

Notes and references

  1. S. Schmidt, S. Beyer, H. Knabe, H. Immich, R. Meistring and A. Gessler, Acta Astronaut., 2004, 55, 409–420 CrossRef.
  2. R. Naslain, Compos. Sci. Technol., 2004, 64, 155–170 CrossRef CAS.
  3. W. Krenkel, Ceramic matrix composites: fiber reinforced ceramics and their applications, Wiley-VCH, Weinheim, 2008 Search PubMed.
  4. J. Hu, S. Dong, X. Zhang, H. Zhou, B. Wu and Z. Wang, et al., Composites, Part A, 2013, 48, 73–81 CrossRef CAS.
  5. H. Qian, E. S. Greenhalgh, M. S. Shaffer and A. Bismarck, J. Mater. Chem., 2010, 20, 4751–4762 RSC.
  6. A. Godara, L. Mezzo, F. Luizi, A. Warrier, S. V. Lomov and A. W. Van Vuure, et al., Carbon, 2009, 47, 2914–2923 CrossRef CAS.
  7. J. Hu, S. Dong, Q. Feng, M. Zhou, X. Wang and Y. Cheng, Carbon, 2014, 69, 621–625 CrossRef CAS.
  8. A. Y. Boroujeni, M. Tehrani, A. J. Nelson and M. Al-Haik, Composites, Part B, 2014, 66, 475–483 CrossRef CAS.
  9. E. Bekyarova, E. T. Thostenson, A. Yu, H. Kim, J. Gao and J. Tang, et al., Langmuir, 2007, 23, 3970–3974 CrossRef CAS PubMed.
  10. Y. Chen, J. Zou, S. J. Campbell and G. Le Caer, Appl. Phys. Lett., 2004, 84, 2430–2432 CrossRef CAS.
  11. C. Zhi, Y. Bando, C. Tang and D. Golberg, Mater. Sci. Eng., R, 2010, 70, 92–111 CrossRef.
  12. A. Pakdel, C. Zhi, Y. Bando and D. Golberg, Mater. Today, 2010, 15, 256–265 CrossRef.
  13. C. Y. Zhi, Y. Bando, C. C. Tang, Q. Huang and D. Golberg, J. Mater. Chem., 2008, 18, 3900–3908 RSC.
  14. M. Schulz, V. Shanov and Z. Yin, Nanotube Superfiber Materials: Changing Engineering Design, William Andrew, New York, 2013 Search PubMed.
  15. G. Zhu, S. Dong, J. Hu, Y. Kan, P. He and L. Gao, et al., RSC Adv., 2016, 6, 14112–14119 RSC.
  16. R. Naslain, A. Guette, F. Rebillat, R. Pailler, F. Langlais and X. Bourrat, J. Solid State Chem., 2004, 177, 449–456 CrossRef CAS.
  17. M. Du, J. Q. Bi, W. L. Wang, X. L. Sun and N. N. Long, Mater. Sci. Eng., A, 2012, 543, 271–276 CrossRef CAS.
  18. W. Feng, L. Zhang, Y. Liu, X. Li, L. Cheng and B. Chen, Mater. Sci. Eng., A, 2015, 626, 500–504 CrossRef CAS.
  19. L. M. Manocha and R. Pande, J. Nanosci. Nanotechnol., 2010, 10, 3822–3827 CrossRef CAS PubMed.
  20. W. J. Kim, S. M. Kang, J. Y. Park and W. S. Ryu, Fusion Eng. Des., 2006, 81, 931–936 CrossRef CAS.
  21. C. Y. Zhi, Y. Bando, W. L. Wang, C. C. Tang, H. Kuwahara and D. Golberg, J. Nanomater., 2008, 2008, 145–152 Search PubMed.
  22. Y. F. Chen, J. Q. Bi, W. L. Wang, Y. Zhao, G. L. You and C. L. Yin, et al., Mater. Sci. Eng., A, 2014, 590, 16–20 CrossRef CAS.
  23. A. Peigney, Nat. Mater., 2003, 2, 15–16 CrossRef CAS PubMed.
  24. H. Zhang, L. Guo, Q. Song, Q. Fu, H. Li and K. Li, Prog. Nat. Sci., 2013, 23, 157–163 CrossRef.
  25. H. H. Yu, S. R. Wang and L. Y. Yang, Appl. Compos. Mater., 2013, 20, 947–960 CrossRef CAS.
  26. W. L. Wang, J. Q. Bi, S. R. Wang, K. N. Sun, M. Du and N. N. Long, et al., J. Eur. Ceram. Soc., 2011, 31, 2277–2284 CrossRef CAS.
  27. P. Tatarko, S. Grasso, H. Porwal, Z. Chlup, R. Saggar and I. Dlouhý, et al., J. Eur. Ceram. Soc., 2014, 34, 3339–3349 CrossRef CAS.
  28. M. Olek, J. Ostrander, S. Jurga, H. Möhwald, N. Kotov and K. Kempa, et al., Nano Lett., 2004, 4, 1889–1895 CrossRef CAS.
  29. Y. Chu, H. Li, Y. Wang, L. Qi and Q. Fu, Surf. Coat. Technol., 2013, 235, 577–581 CrossRef CAS.
  30. D. M. Tang, C. L. Ren, X. Wei, M. S. Wang, C. Liu and Y. Bando, et al., ACS Nano, 2011, 5, 7362–7368 CrossRef CAS PubMed.
  31. N. Jacobson, D. Hull, J. Cawley and D. Curry, Kinetics and mechanism of oxidation of the reinforced carbon/carbon on the space shuttle orbiter, Proceedings of 34th international conference and exposition on advanced ceramics and composites, 2010, pp. 3–21 Search PubMed.
  32. A. J. Eckel, J. D. Cawley and T. A. Parthasarathy, J. Am. Ceram. Soc., 1995, 78, 972–980 CrossRef CAS.
  33. J. D. Cawley, E. Ave and W. Bld, Modeling the oxidation kinetics of continuous carbon fibers in a ceramic matrix, Proceedings of 23rd Annual Conference on Composites, Advanced Ceramics, Materials, and Structures-B: Ceramic Engineering and Science Proceedings, 1999, p. 87 Search PubMed.
  34. Y. Xu and W. Zhang, Numerical simulation of oxidation-assisted failure of CMC-SiC at intermediate temperature, Proceedings of 8th High Temperature Ceramic Matrix Composites Conference: Ceramic Transactions, 2013, pp. 65–76 Search PubMed.
  35. R. H. Jones, C. H. Henager, C. A. Lewinsohn and C. F. Windisch, J. Am. Ceram. Soc., 2000, 83, 1999–2005 CrossRef CAS.
  36. I. Sebire-lhermitte, M. Gomina and J. Vicens, J. Microsc., 1993, 169, 197–205 CrossRef CAS.
  37. Ö. Ünal, A. J. Eckel and F. C. Laabs, Mechanical properties and microstructure of oxidized SiC/SiC composites, Proceedings of 20th Annual Conference on Composites, Advanced Ceramics, Materials, and Structures-B: Ceramic Engineering and Science Proceedings, 1996, pp. 333–341 Search PubMed.
  38. C. E. Ramberg, G. Cruciani, K. E. Spear, R. E. Tressler and C. F. Ramberg, J. Am. Ceram. Soc., 1996, 79, 2897–2911 CrossRef.
  39. L. Filipuzzi and R. Naslain, J. Am. Ceram. Soc., 1994, 77, 467–480 CrossRef CAS.

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