1. Introduction
Ceramic materials classified as ultra-high-temperature ceramics (UHTC) are characterised by high melting point, good mechanical properties also at high temperature and high oxidation resistance. As they are increasingly used, more demands are placed on them [
1,
2]. The group of materials classified as UHTC includes metal borides of the 4
th group of the periodic table of chemical elements, i.e. TiB
2, ZrB
2 and HfB
2. These borides have very high melting points (approx. 3000°C), good thermal and electrical conductivity, high hardness, good mechanical properties and oxidation resistance. These valuable properties of AlB
2 – type borides are result of dominant covalent bonds present in their structure, which on the other hand has a negative effect on sinterability of boride ceramics [
1,
2,
3,
4].
Improved sinterability of boride ceramics is achieved by using sintering additives (sintering activators) such as; nitrides: TiN, AlN, Si
3N
4 or HfN [
2,
5,
6,
7,
8,
9], carbides: TaC, SiC, B
4C, TaC [
2,
10,
11,
12,
13,
14,
15], silicides: MoSi
2, TiSi
2, TaSi
2 [
4,
16,
17,
18,
19,
20,
21,
22,
23] or oxides: ZrO
2 [
24,
25,
26,
27,
28]. The most commonly used sintering activators for boride ceramics including TiB
2 are MoSi
2 and SiC [
2,
4,
13,
15,
16,
17,
21]. The effect of silicide additives on the sinterability and properties of TiB
2 was, among others, studied by Raju, Murthy et al [
17,
20]. With introduction of 2.5% MoSi
2 additive and the use of hot pressing technique the authors of the discussed papers obtained dense composites at 1700°C. According to the authors, MoSi
2 removes oxide impurities and then deforms plastically due to high temperature, filling spaces between TiB
2 grains. In another paper, Murthy et al [
4] investigated materials sintered by hot pressing with 0 to 25% MoSi
2 addition leading do samples with density close to 98%, grain size of 2-5 μm, high hardness of 25 – 27 GPa and fracture toughness of 5.1 MPa·m
0.5. The optimum amount of MoSi
2 was 10% which resulted in fine-grained microstructure of the sinters and hardness of 27 GPa.
The paper presents results of studies on effect of carbon and MoSi2 additives and effect of combined carbon and MoSi2 additives on sinterability and mechanical properties of titanium diboride.
2. Materials and experimental procedure
The samples were prepared from the commercial powders: TiB2, ABCR Company (GRADE F, cat.no. AB 134577), MoSi2, Morton Thiokol (99%, cat.no. 48108). As a carbon precursor, phenol-formaldehyde resin of the NOVOLAK type (Organika Sarzyna, Poland) was used. During sintering it undergoes pyrolysis leaving 50 wt.% of amorphous carbon.
A reference sample of pure TiB
2 and three series of samples with various additives additions were made. The first series with addition of: 1%, 2%, 3% and 4% wt. carbon; the second with addition of: 2.5% , 5% and 10% wt. MoSi
2, and the third containing constant amount of 2% wt. of carbon and 2.5% , 5% or 10% wt. of MoSi
2. The sample denominations used in the work are summarised in
Table 1.
The powder mixture components were weighted and then homogenised in ethanol in a ball mill for 12 h using SiC spherical grinding media. Then the alcohol was evaporated and the powders mixtures were granulated by passing through a nylon 6 sieve. Cylindrical samples with diameter 12 mm and height 3 – 4 mm were formed by an uniaxial double-ended pressing and then subjected to dilatometric analysis.
Dilatometric sintering analysis was performed in a high-temperature graphite dilatometer of the own construction. Sintering in the dilatometer was carried out in an argon flow with a heating rate 10°C/min. The end of sintering was an appearance of a characteristic plateau on a of linear dimensions change as a function of temperature. The dilatometric analysis made possible determination of the final temperature of the hot – pressing.
The granulated powders were hot–pressed in graphite dies in argon flow using Thermal Technology Inc. press.
The reference sample and the samples with carbon addition were sintered at 25 MPa at 2100°C, and the samples with MoSi2 and MoSi2 and carbon addition were sintered at 25 MPa at 1800°C. All samples were kept at the final temperature for one hour. The heating rate in each case was 10°C/min.
Apparent density of the sintered samples was measured using the Archimedes method. The relative density was calculated using 4.52 g/cm3 as the theoretical density of TiB2. Surface of the samples was ground and polished using LaboPol (Struers) polishing machine. Their microstructure was analysed using Scios2 DualBeam (ThermoFisher) SEM microscope along with the EDS chemical analysis. In order to determine phase composition, XRD analysis was performed with the X'Pert Pro apparatus (PANanlitycal). The quantitative phase composition of the sinters was determined using the Rietveld method. Hardness measurements were carried out by the Vickers method using a FV-810 (Future-Tech) hardness tester. A standard load of 1 kg and an indenter pressing time of 10 seconds were used. The fracture toughness (KIc) was determined using the indentation method at 3 kg load of. The Niihara formula was used to calculate the critical stress intensity factor (KIc). Young's modulus measurements were carried out using the ultrasonic method by measuring velocity of transverse and longitudinal waves passing through the specimen using EPOCH 3 (Panametrics) ultrasonic defectoscope.
4. Results discussion
On the basis of results of the investigations, a favourable effect of all used additives, i.e. carbon, MoSi2 and MoSi2+C, on sinterability of TiB2 titanium diboride was found. Firstly, a dilatometric sintering analysis was carried out, which showed the validity of the mentioned above sintering activators (Fig. 1 and Fig. 2). Furthermore, it is clear from the dilatometric measurements that the use of 10% MoSi2 addition and the combination of both additives significantly reduces the sintering temperature of TiB2 (Fig. 2). The sintering temperature of polycrystals with carbon and MoSi2 additives does not exceed 1800°C. For polycrystals with MoSi2, only a 10% addition of molybdenum disilicide reduces the sintering temperature to 1900°C (Fig. 2).
Based on dilatometric sintering analysis, the hot pressing temperatures of all composites were determined. Composites with carbon as well as the reference sample were hot-pressed at 2100°C, while composites with MoSi2 and composites with carbon and MoSi2 were hot-pressed at 1800°C. In many cases, polycrystals with a relative density of 100% were obtained. In the case of carbon addition, the highest densities were obtained when the carbon addition was between 2 and 4 wt.%. Dense polycrystals were produced by adding 5 or 10 wt.% MoSi2 as well as 2 wt.% carbon together with 5 or 10 wt. % MoSi2 (Figs. 3, 7 and 10).
The addition of carbon makes possible to obtain single-phase polycrystals, as evidenced by the phase composition analysis, according to which only TiB
2 is present in such sinters. Also, the microstructures shown in Fig. 5 are characteristic of single-phase and dense sinters when carbon addition is in the range of 2 to 4 wt.%. Phase composition analyses demonstrate the effectiveness of using carbon as an oxide impurity reducer. According to the literature [
33], carbon can react both with B
2O
3 and SiO
2 at temperatures close to 1000°C in low vacuum (20 Pa). The local EDS analysis of the chemical composition carried out during SEM observations showed the trace presence of fine particles, whose chemical composition suggests that they may be particles of carbon or boron and titanium carbides (Fig. 6).
The phase composition of the polycrystals sintered with MoSi
2 (
Table 2) and with carbon and MoSi
2 additives shows that composites (
Table 4) were obtained in which dominated two TiB
2 phases with different lattice parameters (
Table 3 and
Table 5). In addition, molybdenum carbide was identified in all composites sintered with MoSi
2 only, and only the sample with the highest MoSi
2 addition showed the presence of this additive. In contrast, for composites with both additives, the dominant are two titanium boride phases with different lattice parameters (
Table 5). Silicon and titanium carbides were also identified in these composites, and a complex carbide with the formula (Mo,Ti)C
2 was found in samples with 5 and 10 % wt MoSi
2 additions. Substitutions of titanium (a
r=140 pm) by Mo (a
r=145 pm), Si (a
r=145 pm) cations as well as boron (a
r=75 pm) by carbon (a
r=70 pm) can led to the presence of hexagonal titanium boride phases with different lattice parameters or in other words to the presence of solid solutions [
34]. The presence of (Mo,Ti,Si)B
2 solid solutions can be evidenced by a microstructure similar to the one of core-shell cermets. This type of microstructure is often found in composites based on metal borides of the 4
th group of the periodic table of chemical elements [
21,
23,
35,
36,
37]. SEM micrographs of the TiB2_10.0 composite (
Figure 13) show TiB
2 cores and solid-solution shells typical of cermets.
The EDS chemical element distribution maps made during the SEM observations further showed that in both groups of composites with MoSi
2 additive, there are areas enriched in oxygen and silicon (Fig. 9 and Fig. 12). During sintering, a variety of reactions can occur in all composites, including cabothermal reduction of oxides passivating boride particles (Eq.1-2) and reactions between MoSi
2 and oxide impurities (Eq.3-5) [
4,
16,
35,
38,
39], leading to the formation of silica, monoborides and carbides, among others.
As it is shown by the composites microstructures in Fig. 8 and Fig. 11, solid solutions can be formed at grain boundaries or, more commonly, at the surface of the boride grains. The literature reports that the formation of the solid solutions in question can be related to the presence of liquid phases with compositions resulting from the initial chemical composition of the composites [
4,
17,
21,
36,
38,
40,
41,
42]. The most likely formation of liquid phases is from the Si – B – O system, in which the elements forming the components of the composite can dissolve. It should be added, that in the case of the MoSi
2 additive alone, the passivating oxides do not reduce as readily as under the influence of carbon. During cooling, epitaxial precipitation from the liquid phase and the formation of solid solutions can occur [
4,
17,
21,
36,
42]. The occurrence of the solid solutions discussed, as well as silicide, carbide and SiO
2 phases, may be an indirect evidence of the presence of liquid phases during the sintering of composites with MoSi
2 addition. Furthermore, oxygen-rich and silicon-rich particles are identified during the chemical composition analysis, even when MoSi
2 and carbon were used as additives (Fig. 12).
According to the literature [
30,
31,
32], the occurrence of liquid phases from the Si – B – O system is mainly possible in boride composites with silicide additives. These phases can effectively support sintering under pressure by facilitating, among other things, the movement of grains relative to each other [
43]. In this case, if the oxides are not fully reduced, even when a small addition of carbon is introduced, it is possible for a reaction between SiO
2 and B
2O
3 to take place resulting in the formation of a liquid phase from the Si – B – O system, in which elements present in the initial compounds forming the composites can dissolve.
Furthermore, the sintering temperature of composites with MoSi
2 is 1800°C and does not exceed the melting point of the silicide (T
m=2050°C) [
41,
44] but, as reported in the literature [
43,
44,
45,
46], at temperature higher than 800°C silicides, including molybdenum silicide deform plastically and can fill pores during sintering.
The relationship between density of the composites and the values of the tested mechanical properties is observed. The composites with the highest density, regardless of the additive used, show a high Vickers hardness of 23 to 26 GPa. Also in terms of fracture toughness, all the composites tested show a high value of the critical stress intensity factor K
Ic (
Table 6). The lowest values of K
Ic from 4.18 to 4.79 MPa·m
0.5 are exhibited by composites with two additives, the fracture toughness of composites with 2 to 4 wt.% carbon addition oscillates around 5 MPa·m
0.5, while in composites with MoSi
2 it ranges from 6.25 to 4.86 MPa·m
0.5 for 5 wt.% MoSi
2 and 10 wt.% MoSi
2 addition, respectively. The typical phenomena leading to increase in effective fracture energy are observed in the composites such as intergranular cracking (
Figure 14a and
Figure 14c), crack deflection as well as crack defragmentation (Fig. 14e and Fig. 14f). It is noteworthy, that the grain boundaries (bonding phase) in composites with 5 wt.% MoSi
2 addition are weaker than those in composites with 10 wt.% MoSi
2 addition (compare Fig. 14a with Fig. 14b, and Fig. 14c with Fig. 14d). This results in a lower value of the critical stress intensity factor in composites with 10 wt.% MoSi
2 addition (
Table 6). The fracture then runs predominantly in through the grains as well as along the TiB
2 grain boundaries (Fig. 14b and Fig. 14d).
All high-density composites can be classified as low deformability materials, as evidenced by high values oh their Young's modulus (
Table 6).
The values of hardness, fracture toughness and Young's modulus showed by the investigated composites are similar to and often better than those reported in the literature [
4,
16,
38,
47].
Figure 1.
Dilatrometric sintering curves of the reference sample and samples with carbon addition.
Figure 1.
Dilatrometric sintering curves of the reference sample and samples with carbon addition.
Figure 2.
Dilatometric sintering curves of samples with: a) MoSi2 , b) carbon and MoSi2 addition.
Figure 2.
Dilatometric sintering curves of samples with: a) MoSi2 , b) carbon and MoSi2 addition.
Figure 3.
Relative density of the sintered samples containing various amounts of carbon .
Figure 3.
Relative density of the sintered samples containing various amounts of carbon .
Figure 4.
SEM images of the reference TiB2 sample (TiB2_0).
Figure 4.
SEM images of the reference TiB2 sample (TiB2_0).
Figure 5.
SEM images of TiB2 samples with carbon addition: a,b ) 1 %C; c,d ) 2 %C ; e,f ) 3 %C ; g,h ) 4% C.
Figure 5.
SEM images of TiB2 samples with carbon addition: a,b ) 1 %C; c,d ) 2 %C ; e,f ) 3 %C ; g,h ) 4% C.
Figure 6.
Local chemical composition analysis of the black areas in the TiB2 sample with 4 wt.% carbon addition .
Figure 6.
Local chemical composition analysis of the black areas in the TiB2 sample with 4 wt.% carbon addition .
Figure 7.
Relative density of the sintered samples containing various amounts of MoSi2.
Figure 7.
Relative density of the sintered samples containing various amounts of MoSi2.
Figure 8.
SEM microphotographs of TiB2 samples sintered with various amounts of MoSi2 addition: 2.5 wt.%. (a, b); 5.0 wt.%. (c, d) and 10 wt.%. (e, f).
Figure 8.
SEM microphotographs of TiB2 samples sintered with various amounts of MoSi2 addition: 2.5 wt.%. (a, b); 5.0 wt.%. (c, d) and 10 wt.%. (e, f).
Figure 9.
Results of the local chemical composition analysis of TiB2 with 10 wt.% MoSi2 addition.
Figure 9.
Results of the local chemical composition analysis of TiB2 with 10 wt.% MoSi2 addition.
Figure 10.
Relative density of sintered samples with 2 wt.% carbon and various amounts of MoSi2.
Figure 10.
Relative density of sintered samples with 2 wt.% carbon and various amounts of MoSi2.
Figure 11.
SEM images of TiB2 samples with 2% carbon and different amounts of MoSi2 addition: 2.5% (a, b), 5.0% (c, d) and 10% (e, f).
Figure 11.
SEM images of TiB2 samples with 2% carbon and different amounts of MoSi2 addition: 2.5% (a, b), 5.0% (c, d) and 10% (e, f).
Figure 12.
EDS element distribution maps of the TiB2+2% C+10% MoSi2 composite.
Figure 12.
EDS element distribution maps of the TiB2+2% C+10% MoSi2 composite.
Figure 13.
SEM microstructure of the composite with 10 wt.% MoSi2 addition characteristic of cermets.
Figure 13.
SEM microstructure of the composite with 10 wt.% MoSi2 addition characteristic of cermets.
Figure 14.
Course of cracks in composites: a) TiB2_5.0; b) TiB2_10.0; c) TiB2_2C_5.0; d) TiB2_2C_10.0; e) TiB2_3C and f) TiB2_4C.
Figure 14.
Course of cracks in composites: a) TiB2_5.0; b) TiB2_10.0; c) TiB2_2C_5.0; d) TiB2_2C_10.0; e) TiB2_3C and f) TiB2_4C.
Table 1.
Denomiantion of the samples.
Table 1.
Denomiantion of the samples.
The initial composition |
Name |
TiB2
|
TiB2_0 |
TiB2+1%C |
TiB2_1C |
TiB2+2%C |
TiB2_2C |
TiB2+3%C |
TiB2_3C |
TiB2+4%C |
TiB2_4C |
TiB2+2.5%MoSi2
|
TiB2_2.5MS |
TiB2+5%MoSi2
|
TiB2_5.0MS |
TiB2+10%MoSi2
|
TiB2_10MS |
TiB2+2%C+2.5%MoSi2
|
TiB2_2C_2.5MS |
TiB2+2%C+5%MoSi2
|
TiB2_2C_5.0MS |
TiB2+2%C+10%MoSi2
|
TiB2_2C_10MS |
Table 2.
Quantitative phase composition of TiB2+ MoSi2 composites.
Table 2.
Quantitative phase composition of TiB2+ MoSi2 composites.
Initial phase composition, wt.% |
Phase composition of the HP sinters, wt. % |
97.5% TiB2, 2.5% MoSi2
|
68.8% TiB2 1, 29.7% TiB2 2, 1.5% MoC |
95% TiB2, 5.0% MoSi2
|
69.8% TiB2 1, 28.7% TiB2 2, 1.5% MoC |
90% TiB2, 10% MoSi2
|
83.0% TiB2 1, 9.4% TiB2 2, 1.0% MoC, 6.6% MoSi2
|
Table 3.
Lattice parameters of titanium boride phases identified in TiB2+MoSi2 composites.
Table 3.
Lattice parameters of titanium boride phases identified in TiB2+MoSi2 composites.
Lattice parameter, Å
|
Theoretical unit cell parameters of TiB2, [29] |
TiB2+2.5% MoSi2 |
TiB2+5.0% MoSi2 |
TiB2+10% MoSi2 |
TiB2 1 |
TiB2 2 |
TiB2 1 |
TiB2 2 |
TiB2 1 |
TiB2 2 |
a |
3.028 |
3.030 |
3.028 |
3.030 |
3.030 |
3.029 |
3.029 |
b |
3.028 |
3.030 |
3.028 |
3.030 |
3.030 |
3.029 |
3.029 |
c |
3.228 |
3.230 |
3.230 |
3.230 |
3.231 |
3.231 |
3.230 |
Table 4.
Quantitative phase composition of TiB2+2%C+x%MoSi2 composites.
Table 4.
Quantitative phase composition of TiB2+2%C+x%MoSi2 composites.
Initial phase composition, wt.% |
Phase composition of the HP sinters, wt.% |
95.5% TiB2, 2.0% C, 2.5% MoSi2
|
96.8% TiB2 1, 0.1% TiB2 2, 1.7% TiC, 1.4% SiC |
95% TiB2, 2.0% C, 5.0% MoSi2
|
66.3% TiB2 1, 28.9% TiB2 2, 1.8% SiC, 3.0% (Ti,Mo)C2
|
90% TiB2, 2.0% C, 10% MoSi2
|
76.1% TiB2 1, 18.6% TiB2 2, 3.1% SiC, 2.2% (Ti,Mo)C2
|
Table 5.
Lattice parameters of titanium boride phases identified in TiB2+2%C+x%MoSi2 composites.
Table 5.
Lattice parameters of titanium boride phases identified in TiB2+2%C+x%MoSi2 composites.
Lattice parameter, Å
|
Theoretical unit cell parameters of TiB2, [29] |
TiB2+2%C +2.5% MoSi2
|
TiB2+2%C +5.0% MoSi2
|
TiB2+2%C +10% MoSi2
|
TiB2 1 |
TiB2 2 |
TiB2 1 |
TiB2 2 |
TiB2 1 |
TiB2 2 |
a |
3.028 |
3.027 |
3.034 |
3.029 |
3.027 |
3.029 |
3.027 |
b |
3.028 |
3.027 |
3.034 |
3.029 |
3.027 |
3.029 |
3.027 |
c |
3.228 |
3.233 |
3.220 |
3.230 |
3.231 |
3.230 |
3.232 |
Table 6.
Relative density and selected mechanical properties of the composites.
Table 6.
Relative density and selected mechanical properties of the composites.
Sample |
Sintering temperaturę (HP), °C
|
Relative density, % *)
|
Vickers hardness, GPa
|
KIC, MPa·m0.5
|
Young's modulus, GPa |
TiB2_0 |
2150 |
88.2±0.3 |
19.09±6.30 |
- |
- |
TiB2_1C |
2150 |
94.3±0.1 |
26.31±5.86 |
- |
526±12 |
TiB2_2C |
2150 |
97.8±0.1 |
25.31±0.77 |
5.16±0.28 |
536±9 |
TiB2_3C |
2150 |
96.9±0.4 |
23.34±2.17 |
5.26±0.47 |
496±16 |
TiB2_4C |
2150 |
95.9±0.3 |
25.68±5.29 |
5.52±0.20 |
542±10 |
TiB2_2.5MS |
1800 |
84.3±0.6 |
16.97±2.86 |
- |
- |
TiB2_5.0MS |
1800 |
98.5±0.2 |
26.21±2.25 |
6.25±0.51 |
536±11 |
TiB2_10MS |
1800 |
100.0±0.4 |
26.78±3.37 |
4.86±0.19 |
504±24 |
TiB2_2C_2.5MS |
1800 |
89.1±0.8 |
17.19±1.87 |
- |
440±14 |
TiB2_2C_5.0MS |
1800 |
98.8±0.4 |
24.88±2.03 |
4.79±0.52 |
543±6 |
TiB2_2C_10MS |
1800 |
100.0±0.2 |
24.41±1.90 |
4.17±0.31 |
533±12 |
*) the theoretical density of TiB2 was 4.52 g/cm3, |