Eric W. Neumana and Greg E. Hilmas
Materials Science and Engineering Department, Missouri University of Science and Technology, Rolla, MO, USA
This chapter focuses on the mechanical properties of zirconium diboride (ZrB2)-based ultra-high temperature ceramics (UHTCs), including elastic modulus, strength, and fracture toughness at ambient and elevated temperatures. The materials covered include ZrB2 ceramics with additions of various sintering aids, silicon carbide, and transition metal silicides. Reporting of carbide, nitride, and oxide additions is limited to instances where materials were added in small quantities or as sintering aids.
To produce structures using UHTCs, designers need to have a robust set of mechanical property data detailing their elastic properties, fracture toughness, and strength. These data will need to include microstructural relations, as well as specimen processing and testing procedures. Currently, much of the published mechanical property data are not accompanied by microstructural analysis. Further, a wide variety of testing methods are utilized for measuring the mechanical properties. Lack of microstructural characterization confounds the analysis, which is directly related to the microstructural features. Further, the use of various testing standards and specimen preparation methods make comparisons between studies difficult. Microstructural information is included in the proceeding discussion, when provided. Differences in testing methods will be noted, but only minimally discussed.
The chapter also discusses improvements in mechanical properties that have been obtained using modern powders and processing techniques compared to historic studies from the 1960s and 1970s. The main contributions to the improvement in properties of the modern materials are the use of powder with higher purity and finer particle sizes, along with the use of sintering aids and isothermal reaction holds to remove impurities, such as surface oxides, from the starting powders.
Zirconium diboride (ZrB2), a transition metal boride compound, is part of a class of materials known as UHTCs. This family of compounds is characterized by melting points in excess of 3000°C [1]. These ceramics are candidates for applications including molten metal crucibles [2, 3], furnace electrodes, cutting tools [4, 5], control rods for fission reactors, and wing leading edges on future hypersonic aerospace vehicles. Additionally, particulate-reinforced ZrB2 matrix composites, especially those with silicon carbide (SiC) additives, have displayed enhanced properties. ZrB2–SiC composites exhibit room temperature strengths in excess of 1000 MPa [6–8], fracture toughness values as high as 5.5 MPa · m½ [6, 7, 9], and hardness values exceeding 22 GPa [6, 8, 10]. These properties are comparable to other commonly used structural ceramics (Al2O3, ZrO2, Si3N4, etc.). In addition, ZrB2 offers chemical stability and increased refractoriness. The following discussion highlights the room temperature elastic modulus, strength, and fracture toughness of ZrB2-based UHTCs.
Elastic modulus values reported for selected ZrB2 ceramics with and without sintering additives are summarized in Table 8.1. Elastic modulus ranges from approximately 350 to approximately 530 GPa depending on porosity and additives (Fig. 8.1). Fitting the data to the Einstein (linear) [42], Spriggs [43], and Nielson [40, 41] models (Table 8.2) gives a value for fully dense ZrB2 of 511 GPa compared to measured values of 490–500 GPa in previous studies [38, 44]. However, the materials in the historic studies were not fully dense, and fitting the historic data to similar models predicts an elastic modulus of 519 GPa for dense ZrB2. Zhang et al. [45] calculated the elastic modulus of ZrB2 from first principles to be 520 GPa, in good agreement with the fitted data. Recent work by Okamoto et al. calculated the polycrystalline elastic modulus of ZrB2 from single crystal measurements to be 525 GPa [46]. The modulus of 99.8%-dense ZrB2 was measured to be 489 GPa [26]. However, additions of AlN, Si3N4, B4C, and C, as well as impurities picked up during powder milling (i.e., WC, ZrO2), affect the elastic modulus of ZrB2 ceramics. Small additions of B4C and/or C increase the elastic modulus of ZrB2 [20, 22, 29]. Additions of AlN and Si3N4 lower the elastic modulus [11, 32]. Additions affect the elastic modulus primarily through interactions with impurities on the surface of the starting powders. Additives such as C and B4C remove low modulus surface oxides, which increases modulus, whereas additives such as AlN (308 GPa) [47] and Si3N4 (310 GPa) promote formation of low modulus grain boundary phases, which reduces modulus [44]. The elastic modulus of 99.4% dense ZrB2 with 0.5 wt% C added as a sintering aid was 524 GPa [29]. This material was nearly phase pure (residual C not observed) and the modulus matched Okamoto's predicted polycrystalline value of 525 GPa. The reported modulus values for ZrB2 are typically impacted porosity and/or impurities, but the intrinsic elastic modulus seems to be approximately 525 GPa.
Table 8.1. Elastic modulus, Vickers hardness, fracture toughness by direct crack method, and four-point flexure strength of ZrB2 ceramics with and without sintering additives
Composition | Relative density | Grain size | Elastic modulus | Hardness | Fracture toughness | Flexure strength | References |
(vol%) | (%) | (µm) | (GPa) | (GPa) | (MPa · m½) | (MPa) | |
ZrB2 | 87 | 10 | 346 ± 4 | 8.7 ± 0.4 | 2.4 ± 0.2a | 351 ± 31 | [11–14] |
ZrB2 | 90 | — | — | 16.1 ± 1.1 | 1.9 ± 0.4 | 325 ± 35b | [15] |
ZrB2 | 90.4 | 6.1 | 417 | — | 4.8 ± 0.4 | 457 ± 58 | [16–18] |
ZrB2 | 95.8 | 10 | — | 16.5 ± 0.9 | 3.6 ± 0.3 | 450 ± 40b | [19] |
ZrB2 | 97 | 8.1 | 479 ± 8 | 16.7 ± 0.6 | 2.8 ± 0.1 | 452 ± 27 | [20] |
ZrB2 | 97.2 | 5.4 ± 2.8 | 498 | — | — | 491 ± 22 | [21] |
ZrB2 | 98 | 9.1 | 454 | 14.5 ± 2.6 | — | 444 ± 30 | [22, 23] |
ZrB2 | >98 | — | — | 14.7 ± 0.8 | — | 300 ± 40 | [24] |
ZrB2 | ~99 | 20 | 491 ± 34 | — | — | 326 ± 46 | [25] |
ZrB2 | 99.8 | ~6 | 489 | 23 ± 0.9 | 3.5 ± 0.3c | 565 ± 53 | [26–28] |
ZrB2 + 0.5 wt% C | 99.4 | 19 ± 13 | 524 ± 17 | 14.3 ± 0.7 | 2.9 ± 0.2a | 381 ± 41 | [29, 30] |
ZrB2 + 4 wt% B4C | 100 | 8 | 530 | 18 | 3.1 | 473 | [22] |
ZrB2 + 4 wt% Ni | 98 | 5–15 | 496 | 14.4 ± 0.8 | 3.4 ± 0.4a | 371 ± 24 | [12, 31] |
ZrB2 + 4.6 AlN | ~92 | — | 407 ± 5 | 9.4 ± 0.5 | 3.1 ± 0.1a | 580 ± 80 | [32] |
ZrB2 + 5 Si3N4 | 98 | 3 | 419 ± 5 | 13.4 ± 0.6 | 3.7 ± 0.1a | 600 ± 90 | [11, 33–35] |
ZrB2 + 3 YAG | 95 | 7.5 | — | — | 5.4 ± 0.2d | 629 ± 31b | [36] |
ZrB2 + 2 wt% B4C + 1 wt% C | 100 | 4.1 | 507 | 19.6 ± 0.4 | 3.5 | 575 ± 29 | [22, 37] |
ZrB2 + 2 wt% B4C + 1 wt% C | 100 | 2.5 | 509 ± 11 | 19.7 ± 0.6 | 3.0 ± 0.1 | 547 ± 35 | [20] |
aChevron notched beam.
bThree-point flexure.
cIndentation strength in bending.
dSingle-edge notched beam.
Figure 8.1. Room-temperature elastic modulus as a function of porosity for ZrB2 (left) with and without sintering aids [11–14, 16, 17, 20–23, 25–29, 31–35, 37–39]. Line represents fitted relationship of elastic modulus to porosity according to Nielsen's relationship [40, 41].
Table 8.2. Summary of various fitted models of elastic modulus as a function of porosity for ZrB2
Equation | E0 | b | R2 |
E = E0(1 − bP) | 511 ± 10 | 2.0 ± 0.3 | 0.6416 |
E = E0e− bP | 512 ± 11 | 2.4 ± 0.4 | 0.6614 |
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511 ± 11 | 0.8 ± 0.2 | 0.6665 |
Room temperature flexure strengths for ZrB2 ceramics with and without sintering aids are also given in Table 8.1. The strength ranges from 250 to 630 MPa depending on grain size and additives (Fig. 8.2). In general, the strength of ZrB2 follows an inverse square root relation with grain size (GS−½), as expected for ceramics free of other larger flaws. The line in Figure 8.2 highlights the GS−½ relationship, but is not intended as a fit of the data. This relation indicates that flaw-free ZrB2 with a fine grain size has improved strengths.
Figure 8.2. Room-temperature flexure strength as a function of grain size for ZrB2 (left) with and without sintering additives [11–14, 16–29, 31, 33, 34, 36, 37, 48]. Line is not fitted to data, and is meant to guide the eye.
The fracture toughness of ZrB2 is generally in the range of 3.0–4.5 MPa · m½, with most values being reported near approximately 3.5 MPa · m½. Unfortunately, the effects of porosity or grain size on fracture toughness have not been investigated. Also, the possibility of R-curve behavior has not been investigated, even though the CTE mismatch between the a-axis (6.9 × 10−6 K−1) and c-axis (6.7 × 10−6 K−1) [49] of the hexagonal unit cell leads to residual stresses that could induce R-curve behavior.
The four-point flexure strength of ZrB2–SiC ceramics without additives is shown in Table 8.3. Although ZrB2 grain size is a factor, the room temperature strength of ZrB2–SiC is controlled by the size of the dispersed SiC particles or clusters [7–9]. Rezaie et al. [7] and Watts et al. [8] used linear elastic fracture mechanics to show that critical flaw sizes correlated to the SiC cluster size in ZrB2–30 vol% SiC ceramics. This conclusion is consistent with the CTE mismatch between ZrB2 and SiC (for α-SiC: αa-axis = 4.3 × 10−6 K−1, αc-axis = 4.7 × 10−6 K−1) [55]. Watts et al. [56] used neutron diffraction to measure the thermal residual stresses present in ZrB2–30 vol% SiC. They found that the thermal residual stresses begin to accumulate at approximately 1400°C, resulting in residual tensile stresses in the ZrB2 and compressive stresses in the SiC at room temperature. Assuming constant strain across the interface between SiC and ZrB2, the maximum tensile stress in the ZrB2 was determined to be approximately 1000 MPa [8]. Watts predicted a critical grain size range for microcracking between 6.5 and 13.8 μm. This matches well with the critical SiC particle size of approximately 11.5 μm observed by Watts experimentally (estimated by fitting the major axis of the clusters to ellipses, as discussed later).
Table 8.3. Elastic modulus, Vickers hardness, fracture toughness by direct crack method, and four-point flexure strength of ZrB2–SiC ceramics
Composition | Relative density | ZrB2 Grain size | SiC Grain size | Elastic modulus | Hardness | Fracture toughness | Flexure strength | References |
(vol%) | (%) | (µm) | (µm) | (GPa) | (GPa) | (MPa · m½) | (MPa) | |
ZrB2 + 10SiC | — | 3 | — | 507 ± 4 | — | 4.8 ± 0.3a | 835 ± 35 | [13] |
ZrB2 + 10SiC | 93.2 | ~3 | — | 450 | 24 ± 0.9 | 4.1 ± 0.3b | 713 ± 48 | [26, 28] |
ZrB2 + 10SiC | 97.1 | 2.2 | ~0.2 | — | — | 5.7 ± 0.2c | 720 ± 55d | [50] |
ZrB2 + 10SiC | 97.4 | 4.5 ± 1.6 | 0.8 ± 0.4 | — | — | — | 524 ± 63 | [16, 18] |
ZrB2 + 10SiC | 99.8 | 4.3 ± 1.4 | — | 500 ± 16 | 18 ± 0.9 | 3.8 ± 0.3 | 393 ± 114d | [51] |
ZrB2 + 15SiC | 96.5 | 4.4 ± 1.7 | 0.9 ± 0.5 | — | — | — | 714 ± 59 | [16, 18] |
ZrB2 + 15SiC | 99 | 2 | — | 480 ± 4 | 17.7 ± 0.4 | 4.1 ± 0.1a | 795 ± 105 | [52] |
ZrB2 + 20SiC | — | 1.8 | ~0.2 | — | — | 6.8 ± 0.1c | 1009 ± 43d | [50] |
ZrB2 + 20SiC | 97.3 | 4.2 ± 1.9 | 0.9 ± 0.5 | — | — | — | 608 ± 93 | [16, 18] |
ZrB2 + 20SiC | 99.7 | ~3 | — | 466 | 24 ± 2.8 | 4.4 ± 0.2b | 1003 ± 94d | [26, 28] |
ZrB2 + 20SiC | 99.7 | 4.0 ± 1.1 | — | 506 | 22.1 ± 0.1 | 4.2 ± 0.8 | 487 ± 68d | [51] |
ZrB2 + 20SiC | 5.62 g/cm3 | 4.1 ± 0.9 | — | 505 ± 3 | 21.3 ± 0.7 | 3.9 ± 0.3 | 937 ± 84d | [53] |
ZrB2 + 30SiC | — | 3 | ~0.2 | — | — | 5.9 ± 0.2c | 860 ± 70d | [50] |
ZrB2 + 30SiC | 97.2 | 2.2 ± 1.2 | 1.2 ± 0.6 | 516 ± 3 | 20 ± 2.0 | 5.5 ± 0.3b | 1063 ± 91 | [7] |
ZrB2 + 30SiC | 97.5 | 3.9 ± 0.9 | — | 487 ± 12 | 24.4 ± 0.6 | 4.4 ± 0.5 | 425 ± 35d | [51] |
ZrB2 + 30SiC | 99.8 | 1.5 ± 1.2 | — | 510 | 27.0 ± 2.2 | 2.1 ± 0.1 | 800 ± 115 | [54] |
ZrB2 + 30SiC | 99.4 | ~3 | — | — | 24.0 ± 0.7 | 5.3 ± 0.5b | 1089 ± 152 | [26, 28] |
ZrB2 + 30SiC | 99.8 | 1.2 ± 0.4 | 1.0 ± 0.4 | 520 ± 7 | 20.7 ± 1.0 | 4.6 ± 0.1b | 909 ± 136 | [9] |
ZrB2 + 30SiC | >99 | 10.6 | 1.6 | 541 ± 22 | 21.4 ± 0.6 | — | 1150 ± 115 | [8] |
aChevron notched beam.
bIndentation strength in bending.
cSingle-edge notched beam.
dThree-point flexure.
Microstructure–mechanical property relationships for ZrB2-based ceramics are complex. Because the size of the particulate-reinforcing phase controls the strength, a uniform dispersion of SiC is required to maximize strength, even for compositions and starting particle sizes that should be below the percolation threshold for the system. The method of estimating grain size from image analysis data also affects the interpretation of microstructure–property relations. Figure 8.3 shows the flexure strength of ZrB2–30 vol% SiC as a function of cluster size estimated using equivalent area diameter, one of the most used methods for reporting grain size. This method assumes a spherical particle, and underestimates the critical grain size for microcracking as approximately 3 μm (Fig. 8.3). Figure 8.3 also shows flexure strength as a function of the maximum measured equivalent area diameter (EADmax). Since failure occurs at the largest flaw, a measurement that reports the largest flaw size is more useful, but still may not accurately describe the behavior of the material. From Figure 8.3, below the critical grain size determined by EADmax, the strength shows a linear trend with grain size, instead of the inverse square root relationship predicted by Griffith analysis.
Figure 8.3. Room-temperature flexure strength as a function of SiC cluster size (equivalent area diameter) for ZrB2–30 vol% SiC ceramics produced by hot pressing [7–9].
Figure 8.4 shows flexure strength, elastic modulus, and hardness as a function of the SiC cluster size that was estimated using the maximum measured major axis from ellipses (MEmax) fitted to the SiC clusters. All three properties experience a sudden, discontinuous decrease at approximately 11.5 μm. Below the critical grain size, the strength follows an inverse square root relation with cluster size. Fitting ellipses to the clusters is preferred because it more closely resembles the morphology of the clusters. Taking this analysis even further, measuring the maximum Feret's diameter of the cluster, should more accurately correlate to the flaw size by freeing the analysis from assumptions of circularity.
Figure 8.4. Room-temperature flexure strength, elastic modulus, and Vickers hardness as a function of maximum SiC cluster size (major axis of ellipse) for ZrB2–30 vol% SiC ceramics prepared by hot pressing. The dashed line indicates the microcracking threshold that occurs at an SiC cluster size of approximately 11.5 μm [8].
The effect of SiC concentration on the strength of ZrB2–SiC ceramics is shown in Figure 8.5. In general, the strength (Table 8.3) increases with SiC content. From Chamberlain et al., the strength of ZrB2 increases from 560 to 1090 MPa with addition of up to 30 vol% SiC [26]. However, the strength is still controlled by the size of the SiC inclusions as discussed previously. Chamberlain was able to achieve high strengths through dispersion of the SiC particulate during processing. When percolation clusters begin to form, or the size of the SiC particles is large, strengths will decrease. Liu et al. produced ZrB2–SiC ceramics using nanometer-sized SiC powder [50]. They produced strengths comparable to Chamberlain, except at the level of 30 vol% additions, where SiC began to form large percolation clusters, resulting in a material with lower strength than expected based solely on the submicron SiC particle size. Zhang et al. produced pressurelessly sintered ZrB2–SiC that resulted in large asymmetric SiC grains from the long isothermal holding times (3 h) required for densification [57]. Even though Zhang achieved good dispersion of the SiC particles, the resulting SiC grain size (up to 13 μm long) was larger than the critical grain size for microcracking of approximately 11.5 μm, thus resulting in reduced strengths (490 MPa).
Figure 8.5. Room-temperature flexure strength [16, 22, 26, 37, 50, 57] and fracture toughness [16, 22, 26, 37, 50, 57] as a function of SiC concentration for ZrB2–SiC ceramics produced by hot pressing and pressureless sintering.
The fracture toughness of ZrB2–SiC ceramics as a function of SiC additions is also shown in Figure 8.5. In general, fracture toughness (Table 8.3) increases with increasing SiC additions. Chamberlain reported a fracture toughness of 3.5 MPa · m½ for pure ZrB2, increasing to 5.3 MPa · m½ for ZrB2–30 vol% SiC. Liu's work [50] showed that toughness followed a similar trend to strength for nanosized SiC, increasing from 3.1 MPa · m½ for ZrB2 to 6.8 MPa · m½ for 20 vol% SiC then decreasing to 5.9 MPa · m½ for 30 vol% SiC (along with observed formation of percolation clusters). SiC additions increase the fracture toughness of ZrB2 by increasing the tortuosity of the crack path. Figure 8.6 shows a polished and etched specimen of ZrB2–SiC exhibiting crack bridging and crack deflection. The ZrB2 grains typically fail by transgranular fracture, while cracks deflect at or near ZrB2–SiC interfaces. This behavior is consistent with residual stresses resulting from CTE mismatch between SiC and ZrB2. Further, R-curve behavior has been observed in ZrB2–SiC, as expected based on the CTE mismatch between the phases. Kurihara et al. [59] reported falling R-curve behavior for ZrB2–10 vol% SiC and Bird et al. [60] reported rising R-curve behavior for ZrB2–20 vol% SiC. Further increases in fracture toughness will likely require second-phase additions with higher aspect ratios, such as whiskers, rods, or platelets (discussed later), or the fabrication of laminate-type architectures [61].
Figure 8.6. Thermally etched cross section of ZrB2–30 vol% SiC. The image shows the crack path from a Vickers indent with arrows indicating predominantly transgranular fracture for the ZrB2 grains and crack deflection near the ZrB2–SiC interfaces.
Reproduced from [58].
The elastic modulus of ZrB2 with SiC (475 GPa) [62] additions follows a simple linear volumetric rule of mixtures trend (Fig. 8.7). Small variations in elastic modulus from the expected values may be attributed to the impact of processing impurities on ZrB2–SiC, such as WC from milling media or the effect of thermal residual stresses.
Figure 8.7. Elastic modulus as a function of additive content for selected hot-pressed ZrB2-based composites with SiC [16, 18, 26, 28, 52, 54, 63] , MoSi2 [14, 64–67] , and ZrSi2 [17] additives. Values have been corrected for porosity using a linear relationship and b = 2.0.
The effect of various additions to ZrB2–SiC is summarized in Table 8.4. Additions are typically introduced as sintering aids that may be designed to remove surface oxide impurities, as in the case of C and B4C, or interacting with surface oxides to form softer grain boundary phases, as in the case of Si3N4. ZrB2–SiC with other additions has similar room temperature mechanical properties to ZrB2–SiC without additions. Nitride additions typically increase toughness by formation of a weaker grain boundary phase that increases crack bridging and deflection. Han [70] and Wang [71] observed an increased toughness for ZrB2–20 vol% SiC (from ~4.2 to ~5.5 MPa · m½) with 5–10 vol% additions of aluminum nitride, while retaining a room temperature flexure strength of 830 MPa. This increase was likely due to improved densification, which resulted in a finer grain size, and the presence of weaker grain boundary phases (BN and Al2O3) that enhanced crack deflection. Small additions of oxides (such as YAG [11] and La2O3 [19]) follow a similar trend to the nitride additions with minimal improvements in toughness. This shows that small additions of nitrides and oxides can be added to ZrB2–SiC to provide additional means of controlling densification and microstructure without adversely affecting room temperature mechanical properties.
Table 8.4. Elastic modulus, Vickers hardness, fracture toughness by direct crack method, and four-point flexure strength of ZrB2–SiC ceramics with various additives
Composition | Relative density | ZrB2 Grain size | SiC Grain size | Elastic modulus | Hardness | Fracture toughness | Flexure strength | References |
(vol%) | (%) | (µm) | (µm) | (GPa) | (GPa) | (MPa · m½) | (MPa) | |
ZrB2 + 20SiC + 1 wt% B | >99.0 | 7.3 ± 0.8 | 3.3 ± 0.5 | — | 16.0 ± 0.4 | — | 519 ± 31a | [68] |
ZrB2 + 27SiC + 1B4C | 100 | 2 | 1 | 508 ± 6 | 22.6 ± 0.9 | 3.5 | 720 ± 140 | [63] |
ZrB2 + 30SiC + 2 wt% B4Cb | 100 | 1.9 ± 0.9 | 1.2 ± 0.5 | 513 ± 24 | 20.2 ± 0.5 | 4.9 ± 0.4c | 682 ± 98 | [69] |
ZrB2 + 20SiC + 3wt%C + 0.5wt%B4C | 99 | ~10 | ~8 | 374 ± 25 | 14.7 ± 0.2 | 5.5 ± 0.5d | 361 ± 44a | [39] |
ZrB2 + 30SiC + 4 wt% B4Cb + 5 wt% Ce | 99 | 2.8 ± 0.2 | 2 ± 0.8 | 511 ± 7 | — | 3.8 ± 0.2f | 604 ± 69 | [57] |
ZrB2 + 20SiC + 2 wt% La2O3 | 99.6 | 3.5 ± 0.4 | — | — | 19.3 ± 0.6 | 5.2 ± 0.5 | 600 ± 70a | [19] |
ZrB2 + 20SiC + 4Si3N4 | 98 | 2.4 ± 0.1 | — | — | 14.6 ± 0.3 | — | 730 ± 100a | [11] |
ZrB2 + 20SiC + 5AlN | 100 | 3 | — | — | 19.4 ± 0.6 | 5.4 ± 0.3d | 835 ± 26a | [70] |
ZrB2 + 20SiC + 10AlN | 100 | 2.5 | — | — | — | 5.6 ± 0.5d | 831 ± 12a | [71] |
ZrB2 + 15SiC + 4.5ZrN | 99 | — | — | 467 ± 4 | 15.6 ± 0.3 | 5.0 ± 0.1c | 635 ± 60 | [72] |
ZrB2 + 20SiC + 6ZrC | 99.1 | ~4 | — | — | 19.0 ± 0.5 | 6.5 ± 0.4d | 622 ± 64a | [73] |
ZrB2 + 21SiC + 5ZrC | 97.3 | <2 | — | — | 17.2 ± 0.8 | 5.2 ± 0.4 | 747 ± 101 | [74] |
ZrB2 + 13SiC + 15ZrC | >99 | — | — | — | 18.2 | 4.3 | 512 ± 50a | [75] |
ZrB2 + 20SiC + 10ZrC | 99.8 | 2.7 ± 0.5 | 1.6 ± 0.2 | — | 18.1 ± 0.6 | 5.3 | 662 ± 64a | [76] |
ZrB2 + 10SiC + 30ZrC | 99 | 2 | — | 474 | 18.8 ± 0.5 | 3.5 ± 0.2 | 723 ± 136 | [67] |
ZrB2 + 20SiC + 5VC | >99 | 1.9 ± 0.3 | 1.4 ± 0.3 | — | 15.8 ± 0.3 | 5.5 ± 0.5 | 804 ± 90a | [77] |
ZrB2 + 10HfB2 + 15SiC | 98.2 | 3 | — | 508 ± 4 | 18.2 ± 0.5 | 4.1 ± 0.8 | 765 ± 75 | [52] |
ZrB2 + 35HfB2 + 15SiC + 4.5ZrN | 99.5 | — | — | 494 ± 4 | 16.7 ± 0.7 | 4.8 ± 0.2c | 590 ± 25 | [72] |
ZrB2 + 9.6SiC + 28.9ZrC + 3.7Si3N4 | 99.5 | 2 | — | 450 | 21.1 ± 0.8 | 3.8 ± 0.1 | 510 ± 160 | [67] |
ZrB2 + 18.5SiC + 3.7Si3N4 + 1Al2O3+ 0.5Y2O3 | 98 | 2.5 ± 0.1 | — | 421 ± 5 | 14.2 ± 0.6 | 4.6 ± 0.1 | 710 ± 110 | [11] |
aThree-point flexure.
bZrB2 basis.
cChevron notched beam.
dSingle-edge notched beam.
eSiC basis.
fIndentation strength in bending.
In contrast to oxide and nitride additions, the mechanical properties of ZrB2–SiC ceramics with ZrC (Table 8.4) typically result in mechanical properties similar to ZrB2–SiC without ZrC additions (Table 8.3). This is most likely the result of closer CTE match between ZrC (7.6 × 10−6 K−1) [78] and ZrB2 compared to SiC and ZrB2, resulting in the SiC phase still dominating the mechanical behavior. With ZrC additions from 5 to 30 vol%, the flexure strengths (~500–750 MPa), fracture toughnesses (3.5–6.5 MPa · m½) are nominally the same as ZrB2–SiC. Similarly, it is reasonable to assume that the same microstructural controls used in ZrB2–SiC to improve mechanical properties can be employed in the ZrB2–SiC–ZrC system. Small additions of other carbides (C, B4C, VC, and WC) have little effect on the mechanical properties of ZrB2–SiC. However, these additions improve densification of ZrB2–SiC in the same manner as when added to ZrB2, through removal of surface oxides on the starting powders. Thus, small additions of carbides can also be used to improve the room temperature mechanical properties by allowing greater control of microstructure during sintering.
The flexure strength of ZrB2 with additions of ZrSi2, MoSi2, or TaSi2 is summarized in Table 8.5. Figure 8.8 shows the effect of MoSi2 and ZrSi2 additives on the strength of ZrB2. Guo [17] reported strengths for ZrB2–ZrSi2 in the range of 380 to 555 MPa depending on ZrSi2 content. Chamberlain [27] reported the effect of MoSi2 on strength of ZrB2, increasing from 565 MPa for ZrB2 to 1150 MPa for 10 vol% MoSi2, decreasing to approximately 1020 MPa for 20 and 30 vol% additions of MoSi2. Similarly, Guo [64] also reported the strength of ZrB2 to increase from 460 MPa for ZrB2 [17] to between 750 and 800 MPa for 10–40 vol% MoSi2 additions.
Table 8.5. Elastic modulus, Vickers hardness, fracture toughness by direct crack method, and four-point flexure strength of ZrB2–(Zr, Mo, Ta)Si2 ceramics
Composition | Relative density | ZrB2 Grain size | MeSi2 Grain size | Elastic modulus | Hardness | Fracture toughness | Flexure strength | References |
(vol%) | (%) | (µm) | (µm) | (GPa) | (GPa) | (MPa · m½) | (MPa) | |
ZrB2 + 10ZrSi2 | 96.6 | 2.3 ± 0.9 | 0.6 ± 0.4 | 432 | — | 3.8 ± 0.3 | 483 ± 22 | [17] |
ZrB2 + 20ZrSi2 | 99.1 | 2.5 ± 0.8 | 0.7 ± 0.6 | 445 | — | 4.4 ± 0.5 | 556 ± 54 | [17] |
ZrB2 + 30ZrSi2 | 99.8 | 2.6 ± 1.1 | 0.7 ± 0.6 | 427 | — | 4.4 ± 0.2 | 555 ± 42 | [17] |
ZrB2 + 40ZrSi2 | 99.2 | 2.7 ± 1.0 | 0.9 ± 0.7 | 397 | — | 3.9 ± 0.4 | 382 ± 78 | [17] |
ZrB2 + 2.3MoSi2 | 6.04 g/cm3 | 5 | — | 500 ± 2 | 18.1 ± 0.4 | 3.4 ± 0.3a | 750 ± 160 | [14] |
ZrB2 + 5MoSi2 | 96 | 2.6 | — | 516 ± 4 | 15.2 ± 1.0 | 2.9 ± 0.1a | 569 ± 54 | [79] |
ZrB2 + 10MoSi2 | 99.7 | 1.9 ± 0.6 | 1.8 ± 0.5 | 490 ± 7 | 15.8 ± 0.7 | 3.7 ± 0.3 | 800 ± 108 | [64] |
ZrB2 + 10MoSi2 | 6.19 g/cm3 | ~3 | — | 516 | 20.4 ± 2.2 | 4.1 ± 0.4b | 1151 ± 52 | [27, 28] |
ZrB2 + 10MoSi2 | 99.9 | — | — | — | 17.5 ± 0.4 | 3.8 ± 0.4 | 560 ± 115c | [80] |
ZrB2 + 15MoSi2 | 5.99 g/cm3 | 1.9 ± 0.6 | — | 452 ± 4 | 14.7 ± 0.6 | 3.5 ± 0.6a | 780 ± 87 | [66] |
ZrB2 + 15MoSi2 | 98.1 | 1.4 | — | 479 ± 4 | 16.2 ± 0.5 | 2.6 ± 0.3 | 643 ± 97 | [65–67] |
ZrB2 + 20MoSi2 | 99.9 | — | — | — | 14.9 ± 0.1 | 3.2 ± 0.2 | 680 ± 40c | [80] |
ZrB2 + 20MoSi2 | 6.17 g/cm3 | ~3 | — | 523 | 18.5 ± 2.7 | 3.0 ± 0.2b | 1008 ± 137 | [27, 28] |
ZrB2 + 20MoSi2 | 99.8 | 1.6 ± 0.6 | 2.7 ± 0.9 | 472 ± 6 | 16.3 ± 0.9 | 2.8 ± 0.2 | 750 ± 128 | [64] |
ZrB2 + 20MoSi2 | 99.1 | ~2.5 | — | 489 ± 4 | 16.0 ± 0.4 | 2.3 ± 0.2 | 531 ± 46 | [65, 79, 81, 82] |
ZrB2 + 30MoSi2 | 99.7 | — | — | — | 14.3 ± 0.2 | 3.2 ± 0.3 | 550 ± 65c | [80] |
ZrB2 + 30MoSi2 | 99.8 | 2.1 ± 0.7 | 2.4 ± 0.6 | 473 ± 3 | 15.4 ± 0.7 | 2.6 ± 0.2 | 757 ± 76 | [64] |
ZrB2 + 30MoSi2 | 6.29 g/cm3 | ~3 | — | 494 | 17.7 ± 1.6 | 4.0 ± 0.4b | 1031 ± 150 | [27, 28] |
ZrB2 + 40MoSi2 | 99.7 | 1.9 ± 0.7 | 2.6 ± 0.8 | 448 ± 4 | 13.2 ± 0.7 | 3.1 ± 0.3 | 790 ± 57 | [64] |
ZrB2 + 15TaSi2 | 99 | 2 | — | 444 ± 24 | 17.8 ± 0.5 | 3.8 ± 0.1a | 840 ± 33 | [83] |
aChevron notched beam.
bIndentation strength in bending.
cThree-point flexure.
Figure 8.8. Room-temperature flexure strength and fracture toughness as a function of disilicide concentration for ZrB2–MeSi2 ceramics produced by hot pressing [17, 27, 64].
The strength of ZrB2 with MoSi2 additions has been reported by numerous researchers. This has resulted in a wide range of reported strengths: ZrB2–10 vol% MoSi2, 560–1150 MPa; ZrB2–20 vol% MoSi2, 460–1010 MPa; ZrB2–30 vol% MoSi2, 550–1030 MPa. These values highlight the importance of microstructure and processing control similar to the ZrB2–SiC system. Unfortunately, microstructural effects of disilicide additions on the strength of ZrB2 have not been thoroughly investigated. This is further complicated by the tendency of the ZrB2–disilicide systems to form complex grain boundary phases and solid solution phases with the ZrB2. Silvestroni et al. [84] reported the formation of a ZrB2 core–(Zr,Mo)B2 rim structures during sintering. In addition, ZrC, ZrO2, MoB, and SiO2 were detected in the final microstructures. Further, they observed various Mo–Zr–B–Si phases that may have also contained C and O, as well as the core–rim structures. These complex chemistries and architectures make analysis of microstructure–mechanical properties' effects difficult. Though detailed microstructural analysis has not been performed on the other transition metal disilicide systems, similar processes presumably occur in these systems as well.
Table 8.5 shows the fracture toughness of ZrB2 with the addition of ZrSi2, MoSi2, or TaSi2. The effect of ZrSi2 and MoSi2 additions on the fracture toughness of ZrB2 is also shown in Figure 8.8. In general, MoSi2 additions result in fracture toughness values in the range of 3.2–4.0 MPa · m½. Chamberlain [27] reported indentation strength in bending (ISB) fracture toughness values of 3–4 MPa · m½ for ZrB2–MoSi2, but without a trend with MoSi2 content. Guo [64] measured fracture toughness of ZrB2–MoSi2 using the direct crack method (DCM) and reported values that decreased from 4.8 MPa · m½ for ZrB2 [17] to approximately 2.8 MPa · m½ for additions of 20–40 vol% MoSi2. Guo [17] also reported DCM toughness for ZrB2–ZrSi2 as 3.8 MPa · m½ for 10 vol% additions, increasing to 4.4 MPa · m½ for 20 and 30 vol% additions, and then decreasing to 3.9 MPa · m½ for 40 vol% ZrSi2 additions. Unlike SiC additions to ZrB2, no trend was observed for fracture toughness with disilicide additions.
Using the Griffith criteria and a Y-parameter of 1.99 (long, semi-elliptical surface flaw), the ZrB2–MoSi2 composites produced by Chamberlain and Guo both exhibit critical flaw sizes that correlated to the observed grain sizes. For example, Chamberlain's ZrB2–10 vol% MoSi2 has a calculated flaw size of 3.2 μm and a reported grain size of approximately 3 μm. However, Guo observed that the calculated critical flaw size was much larger than the observed grain size, suggesting that something other than grain size was controlling the strength of the ZrB2–ZrSi2 composites. From the microstructural analysis of polished cross sections and fracture surfaces, Guo observed that the ZrSi2 segregated to the grain boundaries during sintering, exhibiting a “string of pearls” type morphology and clustering of ZrSi2 grains. Further, small amounts of porosity were observed in the ZrSi2 clusters between the grains. For ZrB2–ZrSi2, the size and morphology of the ZrSi2 phase controls the failure behavior of the composite.
Table 8.5 also summarizes the hardness and elastic modulus of ZrB2 with the addition of ZrSi2, MoSi2, or TaSi2. The effect of additive concentration on the elastic modulus of ZrB2–MoSi2 and ZrB2–ZrSi2 is shown in Figure 8.7. The dashed lines represent the expected modulus based on linear volumetric rule of mixtures calculations assuming moduli of 510 GPa for ZrB2, 440 GPa for MoSi2 [85], and 235 GPa for ZrSi2 [86]. From Figure 8.7, it can be seen that the ZrB2–MoSi2 composites follow the rule of mixtures trend, but the values are consistently 10–20 GPa lower than expected. This is likely due to the formation of complex phases and solid solutions during densification ZrB2–MoSi2 composites. Thermal residual stresses resulting from the CTE mismatch between ZrB2 (αa-axis = 6.9 × 10−6 K−1, αc-axis = 6.7 × 10−6 K−1) [49] and MoSi2 (αa-axis = 8.2 × 10−6 K−1, αc-axis = 9.4 × 10−6 K−1) [87] may also play a role in the observed difference between the predicted and observed modulus. In the case of ZrB2–ZrSi2, the observed modulus is in good agreement with the predicted modulus. Since a tendency to form complex phases has not been observed in the ZrB2–ZrSi2 system, this likely explains why the elastic modulus of ZrB2–ZrSi2 follows predictions while ZrB2–MoSi2 has a more complex behavior.
The flexure strength and fracture toughness of several ZrB2–disilicide ceramics with SiC additions is shown in Figure 8.9. Guo [64] investigated the effect of SiC additions to ZrB2–20 vol% MoSi2 and ZrB2–40 vol% MoSi2 ceramics. The strength of both ZrB2–20 vol% MoSi2 and ZrB2–40 vol% MoSi2 increased with the addition of 5 vol% SiC, but decreased with SiC contents of more than 5 vol%. Further, toughness increased with the addition of SiC, but was relatively insensitive to the amount. The improvement in properties was the result of a finer grain size for the ZrB2 and MoSi2, with the addition of 5 vol% SiC. Further additions of SiC increased the observed average and maximum grain sizes for ZrB2, MoSi2, and SiC. A Griffith-type failure analysis revealed that the critical flaw size increased with the SiC content, and is consistent with the maximum observed MoSi2 grain size. Elastic modulus increased with a 5 vol% SiC addition, then decreased with further additions. Additions of SiC to ZrB2–TaSi2 [88, 89] resulted in similar trends in mechanical properties as additions to ZrB2–MoSi2. Additions of SiC to ZrB2–5 vol% TaSi2 and ZrB2–10 vol% TaSi2 increased the toughness. In general, additions of SiC to ZrB2 with disilicides results in improved toughness.
Figure 8.9. Room-temperature flexure strength and fracture toughness as a function of SiC content for ZrB2–MoSi2–SiC and ZrB2–TaSi2–SiC ceramics [64, 88, 89].
While several studies have reported elevated-temperature mechanical properties of ZrB2 ceramics, most have only reported a single property (i.e., strength) for a limited number of temperatures and have not provided a systematic evaluation of the effects of temperature on mechanical behavior. The following discussion highlights studies of the elevated-temperature elastic modulus, strength, and fracture toughness of various ZrB2-based UHTCs.
The elevated-temperature elastic modulus of hot-pressed ZrB2 with and without additives is shown in Figure 8.10. Only limited data on elastic behavior of ZrB2 have been published for elevated temperatures. Okamoto et al. [49] reported elastic modulus from single crystal values as being 525 GPa at room temperature, decreasing linearly to 490 GPa at 1100°C. Experimental results of bulk ZrB2 have resulted in lower values of elastic modulus than those reported by Okamoto. The historical work of Rhodes et al. [25] provided the only reported values for the elastic modulus of bulk ZrB2 tested in inert atmosphere. The modern studies by Zhu [20] and Neuman et al. [29] were conducted in air, and thus are affected by the formation of an oxide scale on the test articles. Unfortunately, the effect of the oxide scale on the measured elastic modulus was not investigated. Regardless, the elastic modulus of bulk ZrB2 decreased more rapidly than expected based on single crystal measurements presumably due to a grain boundary effect. The modulus decreased linearly from room temperature to approximately 1200°C (450 GPa). Above this temperature, the elastic modulus decreased more rapidly with temperature. The change in slope was thought to be a result of softening of grain boundary phases combined with the activation of grain boundary sliding and diffusional creep mechanisms [20, 25, 29, 69, 90]. Reported modulus values were similar up to 1600°C (250 MPa), despite the differences in testing methods. To date, Rhodes [25] is the only study to report the modulus above 1600°C, where it decreases to 100 GPa at 2000°C.
Figure 8.10. Elevated-temperature elastic modulus of hot-pressed ZrB2 with and without additives [20, 25,29].
The elevated-temperature elastic modulus of ZrB2–SiC ceramics is shown in Figure 8.11. Rhodes et al. [25] observed a steady decrease in modulus from 530 GPa at room temperature to 420 GPa at 1400°C. Above 1400°C, the modulus decreased dramatically to approximately 100 GPa at 1600°C. Neuman et al. [69] observed a steady decrease from 510 GPa at room temperature to 410 GPa at 1000°C. The slope of the modulus then changed, decreasing to 210 GPa at 1500°C, and then more rapidly to 110 GPa at 1600°C. As with ZrB2, the changes in slope of the elastic modulus are likely the result of softening of grain boundary phases, and grain boundary sliding and diffusional creep. In ZrB2–SiC, the softening was expected to occur at a lower temperatures to the presence of SiO2 (surface oxide impurity from SiC) and its interaction with the B2O3 and ZrO2 present from the ZrB2. Zou et al. [90] measured the internal damping in ZrB2–SiC prepared by milling with Si3N4 balls, and found that the damping peaks just above 800°C and again around 1400°C. The reduction in modulus with temperature for ZrB2–SiC ceramics is enhanced by the presence of oxides at the grain boundaries and triple junctions as well as the polycrystalline nature of the material.
Figure 8.11. Elevated-temperature elastic modulus of hot- pressed ZrB2–SiC with and without additives [25, 69].
The elevated-temperature four-point flexure strength of ZrB2 with and without additives is shown in Figure 8.12. In the historical study of Rhodes [25], a room-temperature strength of 325 MPa was measured for fully dense ZrB2 with an approximately 20 μm grain size. Strength increased between room temperature and 800°C (420 MPa), as a result of relief of thermal residual stresses. Strength decreased to 145 MPa at 1400°C, increased to 200 MPa at 1900°C, and then decreased to 50 MPa at 2200°C. The observed increase in strength from 1400 to 1900°C was thought to be caused by stress relief during testing through plastic flow, arising from diffusional creep. A general trend was observed that finer grain size, and lower porosity resulted in improved elevated-temperature strength, which was offset by enhanced creep in the finer-grained material. Similar results have been observed in other structural ceramic systems such as SiC, ZrO2, Al2O3, and Si3N4.
Figure 8.12. Elevated-temperature flexure strength of selected hot-pressed ZrB2 ceramics with and without additives in air and argon [11–13, 20, 25, 29, 30].
Since the historical work of Rhodes [25], several modern studies have investigated the strength of ZrB2 at elevated temperatures. Melendez-Martinez et al. [12] measured the flexure strength of an 87%-dense ZrB2 (350 MPa at room temperature) up to 1400°C in air (220 MPa). Zhu [20] produced dense ZrB2 and ZrB2–2 wt% B4C–1 wt% C with grain sizes of 8.1 and 2.5 μm, respectively. At room temperature, the ZrB2 had a strength of 450 MPa compared to 575 MPa for ZrB2–B4C–SiC. The ZrB2 strength increased up to 1200°C (500 MPa) before decreasing to 360 MPa at 1500°C. The strength of ZrB2–B4C–C increased to 630 MPa at 800°C, then steadily decreased to 370 MPa at 1500°C. Zhu performed his testing in air, and even though he used a protective SiO2 coating, the strength above 1200°C was likely controlled by flaws induced by oxidation damage (discussed in more detail later). For dense ZrB2 ceramic with 0.5 wt% carbon added as sintering aid and a grain size of approximately 19 μm [29] the room temperature strength of the modern ZrB2 was 380 MPa, compared to 325 MPa for the Rhodes material. The strength was maintained up to 1200°C before decreasing to a minimum of 170 MPa at 1500°C. Above 1600°C, the strength was approximately 220 MPa up to 2300°C. Chemical compatibility between ZrB2 and the graphite test fixture (Te = 2390°C) prevented testing at higher temperatures. The improvement in strength, especially above 2000°C, was most likely due to improved purity of modern ZrB2 powders (the ZrB2 used by Rhodes contained several percent ZrC and ZrO2). Additionally, the carbon sintering aid helped remove the surface oxides present on the ZrB2 starting powders [22], presumably leaving less oxide phase at the grain boundaries, which would improve high-temperature strength and stiffness.
The elevated-temperature flexure strength of several hot-pressed ZrB2–SiC ceramics with and without additives is shown in Figure 8.13. The ZrB2–20 vol% SiC studied by Rhodes [25] exhibited an increase in strength from 390 MPa at room temperature to 420 MPa at 800°C. The strength steadily decreased to 245 MPa at 1800°C and decreased more rapidly to 115 MPa at 2000°C. Modern ZrB2–SiC exhibited higher strengths at room and elevated temperature compared to Rhodes' material and similarly for all temperatures measured thus far. Zou et al. [90, 91] have reported the three-point bend strengths at elevated temperature for several compositions up to 1600°C in argon. Zou reported a strength of 550 MPa for ZrB2–20 vol% SiC at room temperature, increasing to 680 MPa at 1000°C, then steadily decreasing to 460 MPa at 1600°C. Zou added 5 vol% WC, which resulted in a room-temperature strength of 605 MPa that steadily increased to 675 MPa at 1600°C. Interestingly, the composition ZrB2–20SiC–5ZrC (not shown) exhibited a room-temperature strength of 1100 MPa, only slightly decreasing to 1020 MPa at 1000°C. Increasing temperatures resulted in a steep decrease in strength to 320 MPa at 1600°C. Grigoriev [15] measured the strength of a ZrB2–19 vol% SiC composite in air (not shown), reporting a room-temperature strength of 500 MPa that was maintained up to 1200°C, decreasing to 430 MPa at 1400°C. Not only do the room-temperature strengths vary widely for ZrB2–SiC, but the change in strength with temperature also varies.
Figure 8.13. Elevated-temperature flexure strength of selected hot-pressed ZrB2–SiC ceramics with and without additives in argon [25, 69, 90, 91].
Zou showed that the addition of WC to ZrB2–20SiC resulted in finer ZrB2 and SiC grain sizes plus enhanced removal of surface oxides from the starting powders. Reducing the amount of low-melting-point oxides present at the grain boundaries should result in a higher stiffness at elevated temperatures, thus also improving strength and resistance to creep. Similarly, the increase in strength for ZrB2–20SiC–5ZrC at room temperature was attributed to grain refinement. The steep drop in strength at elevated temperatures was attributed to the softening of residual oxides present at grain boundaries, since no favorable reactions with the surface oxides or ZrC were identified up to the sintering temperature. Further, creep was observed in the material during testing at 1600°C. Hence, the presence of oxide impurities reduces strength and increases creep at elevated temperatures.
Neuman et al. reported the elevated-temperature four-point flexure strengths of ZrB2–30SiC with 2 wt% B4C in both an inert argon atmosphere and air (not shown) [30, 69]. The strength of ZrB2–30SiC–2B4C in argon was 680 MPa at room temperature, steadily decreased to 540 MPa at 1800°C, then more rapidly decreased to 450 MPa at 2000°C, and finally reached 275 MPa at 2200°C. In air, the strength increased from 680 MPa at room temperature to approximately 740 MPa at 800 and 1000°C and decreased to approximately 370 MPa at 1500 and 1600°C. The increase in strength between room temperature and 1000°C was attributed to the healing of surface flaws from the formation of the ZrO2–B2O3 oxide scale. The size of the SiC clusters controlled the strength up to 1800°C in the inert atmosphere. In air, the size of the SiC clusters controlled strength up to 1000°C, while oxidation damage controlled strength above 1200°C, as discussed in the following. The elevated temperature testing performed by Neuman was different than other studies in that increasing testing rates were used at increasing temperatures to stay in the fast fracture regime and avoid creep effects, which is consistent with the methods described in ASTM C1211. The increased testing rate typically results in higher measured strengths compared to tests using a slower rate where nonlinear-elastic behavior is observed.
Figure 8.14 also shows the elevated-temperature flexure strengths of some ZrB2–SiC ceramics with various additives. Rhodes added graphitic carbon to ZrB2–SiC to improve the thermal shock resistance. The strength increased from 520 MPa at room temperature to 640 MPa at 600°C in argon and then steadily decreased to 260 MPa at 1800°C. Monteverde [11] added 4 vol% Si3N4 as a sintering aid to ZrB2–20 vol% SiC. The strength decreased from 730 MPa at room temperature to 250 MPa at 1200°C due to formation of various phases containing Zr, Si, and/or B with O and/or N at the grain boundaries and triple junctions. These phases begin to soften at temperatures as low as 800°C, leading to strength degradation with increasing temperatures. Bellosi [67] measured the strength of a ZrB2–10SiC–30ZrC composite in argon, showing a room-temperature strength of 720 MPa, which steadily decreased to 420 MPa at 1500°C. The decline in strength between 1200 and 1500°C was similar to the decline observed by Zou over a similar temperature range. Grigoriev made additions of 4 and 7 vol% ZrSi2 to ZrB2–18SiC and ZrB2–17SiC. In the case of the 4% addition, a strength of approximately 480 MPa was maintained up to 1200°C, before decreasing to 230 MPa. Adding 7 vol% ZrSi2 resulted in a decrease in strength from 400 MPa at room temperature to approximately 230 MPa at 1200 and 1400°C. Grigoriev did not speculate as to the effect of ZrSi2 on the response of strength at elevated temperatures, but it is likely due to the relatively low melting point of ZrSi2 of 1620°C and the formation of complex phases at the grain boundaries and triple junctions as seen with in ZrB2–MoSi2 as discussed in the following.
Figure 8.14. Elevated-temperature flexure strength of selected hot-pressed ZrB2–SiC ceramics with various additives in argon [11, 15, 25, 67].
Figure 8.15 shows the four-point flexure strengths at elevated temperatures in air for several ZrB2 ceramics containing MoSi2 or TaSi2. ZrB2–20 vol% SiC prepared by Rhodes is included as a comparison. Silvestroni [79] measured the strength of a pressurelessly sintered ZrB2–5 vol% MoSi2 ceramics, finding that the strength decreased only slightly from 570 MPa at room temperature to 490 MPa at 1500°C. Bellosi et al. [67] reported properties for a spark-plasma-sintered ZrB2–15MoSi2 ceramic, finding that the strength remained approximately 635 MPa from room temperature up to 1200°C, before decreasing to 360 MPa at 1600°C. In a follow-up study, Balbo and Sciti [66] reported similar results for a hot-pressed material of the same composition, speculating that the decrease in strength at 1500°C was the result of softening of silicate phases present in the material. Sciti et al. [81] also measured the strength of pressurelessly sintered ZrB2–20MoSi2 ceramics, in this case observing an increase in strength from 530 MPa at room temperature to 655 MPa at 1200°C, declining to 500 MPa at 1500°C. They attributed the increase in strength at 1200°C to healing of surface flaws due to formation of an oxide scale. Sciti et al. [83] also investigated the properties of hot-pressed ZrB2–TaSi2, reporting a strength of 840 MPa at room temperature that decreased to 375 MPa at 1500°C. This strength was slightly higher than they observed for a comparably processed ZrB2–15MoSi2 (705 MPa at room temperature, 335 MPa at 1500°C), but the strength followed a similar trend. The increased strength of ZrB2–TaSi2 was likely a result of the observed increase in fracture toughness between the MoSi2- and TaSi2-containing composites, but no further speculation was offered by the authors.
Figure 8.15. Elevated-temperature four-point flexure strength of selected ZrB2–MeSi2 ceramics in air [25, 65–67, 79, 82, 83].
The ZrB2–transition metal disilicide systems show promise for their retention of strength at elevated temperatures. Unfortunately, few data are available for these systems above 1500°C. In addition, no elastic properties or fracture toughness behavior have been reported at elevated temperatures. Chemical stability issues may also restrict the use of these composites in the ultra-high temperature regimes. These are discussed in more detail later, but should not be meant to diminish the promising properties these materials have demonstrated thus far.
Measuring the fracture toughness allows for the critical flaw size for failure to be calculated using the measured strength. Figure 8.16 shows the fracture toughness of ZrB2 [30] and ZrB2–30 vol% SiC [69] determined by chevron notched beam in flexure at elevated temperatures. The fracture toughness of ZrB2 with 0.5 wt% C increased from 2.9 MPa · m½ at room temperature to 5.2 MPa · m½ at 1200°C, above which toughness steadily decreased to 3.7 MPa · m½ at 2300°C. Using the Griffith criterion and a Y-parameter of 1.29 (semicircular surface crack), the critical flaw size was similar to the maximum grain size for nearly all temperatures. The critical flaw size calculated for the material at 1400°C was slightly higher than any features observed in the microstructure. The cause of this discrepancy is currently unknown, but could be due to a change in the stress state, since Watts [56] found that stresses begin to accumulate in ZrB2 below 1400°C and Rhodes [25] observed plasticity at 1400°C and higher.
Figure 8.16. Elevated-temperature fracture toughness (CNB) of hot-pressed ZrB2 and ZrB2–SiC ceramics [30, 69].
The fracture toughness of ZrB2–30SiC with 2 wt% B4C, was measured up to 1600°C in air [69]. The fracture toughness was approximately 4.8 MPa · m½ from room temperature to 800°C, steadily decreasing to 3.3 MPa · m½ at 1600°C. Failure analysis revealed that SiC clusters acted as critical flaws below 1000°C, while oxidation damage was the critical flaw above 1200°C. While the oxide scale is a logical choice for failure origin in these materials, the study by Neuman showed that regions of enhanced ingress of oxide scale were the critical flaws. Thus, control of the microstructure is only part of the solution to improving the performance of these ceramics at elevated temperatures in oxidizing atmospheres. Control of the oxidation behavior and the morphology of the oxide scale are also critical for improving their performance in structural applications in extreme environments.
Kalish et al. [92] reported an increase in the amount of transgranular fracture in ZrB2 from approximately 20% at room temperature up to approximately 60% at 1000°C. The amount of transgranular fracture then decreased to approximately 10% at 1200 and 1400°C. Similarly, Bird et al. [60] observed an increase in the amount of intergranular fracture in ZrB2–20 vol% SiC from approximately 5% at room temperature to approximately 95% at 1400°C. The amount of intergranular fracture increased between 800 and 1000°C. The increase in the amount of intergranular fracture with temperature corresponded to an increase in the observed plateau in toughness, which increased from approximately 2.8 MPa · m½ at room temperature to approximately 5.8 MPa · m½ at 1400°C.
This chapter presented a review of the current state-of-the-art of the mechanical properties of zirconium diboride-based ceramics. These ceramics offer a combination of properties that include high refractoriness, modulus, hardness, strength, and moderate fracture toughness. Their mechanical properties are controlled by their microstructures. The control of grain size, the dispersion and cluster size of second phases, and impurity phases are critical for the production of materials for use in extreme environment applications. Lack of sufficient control over the microstructure and impurities reduces the properties of these materials—for example, exceeding the microcracking threshold. The mechanical properties of these materials at elevated temperatures were also reviewed. To date, there has been a lack of fundamental research studies of the mechanical properties of these materials at elevated temperatures. Since the main driver for research into the ZrB2 system is for use in ultra-high temperature (>2000°C) applications, further effort is needed to evaluate the mechanical properties of these materials in relevant environments. It was shown that there is currently a lack of robust microstructure—property relations for the ZrB2-based systems. Microstructure and impurity characterization needs to be performed, and controlled, in future studies.
This chapter has shown that ceramics based on ZrB2 offer promise for use as structural materials in extreme environments. It was shown that ZrB2 ceramics offer mechanical properties at ultra-high temperatures that should allow designers to incorporate these materials for use in future applications for hypersonic vehicles and in other industrial applications where ceramics that can maintain strength (hundreds of MPa) at temperatures exceeding 1500°C are needed.