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1.
In order to improve the oxidation resistance properties of 30 at.% Mo5Si3/MoSi2 composite at high temperature in air, a molybdenum disili-tide coating was prepared on its surface by a molten salt technology. XRD and SEM analysis showed that only tetragonal MoSi2 phase ex-isted in the coating after being siliconized for 5 h at 900℃. The oxidation film formed on the uncoated sample was not dense, so that oxygen diffused easily through it. The volatilization of MoO3 resulted in the oxidation film separating from the substrate. The MoSi2coating was proved to be an effective method to prevent 30 at.% MosSi3/MoSi2 composites from being oxidized at 1200℃. A dense glassy SiO2 film was formed on the MoSi2 coating surface, which acted as a barrier layer for the diffusion of oxygen atoms to the substrate. The 30at.% Mo5Si3/MoSi2 composites with a MoSi2 coating showed much better oxidation resistance at high temperature.  相似文献   

2.
A multilayered oxidation protection coating consisting of MoSi2 outer layer, Mo5Si3 internal layer, and Mo5SiB2/MoB inner layer was developed on the surface of Mo–12Si–8.5B 1.0 wt% ZrB2 alloy via Si pack cementation. The multilayered coating significantly enhanced the oxidation resistance of the alloy at 900°C, 1100°C, and 1300°C in the air by exhibiting negligible oxidation recession. MoSi2 outer layer provided admirable oxidation protection for the alloy at high temperatures by forming a thin and protective SiO2-rich glass scale on its surface. This was supplemented by the Mo5Si3 internal layer and Mo5SiB2/MoB inner layer that reduced the thermal expansion mismatch between the MoSi2 outer layer and substrate, and therefore no obvious cracks were found in the MoSi2 outer layer. More importantly, the Mo5SiB2/MoB layer as an in situ barriers of Si interdiffusion ensured the stable existence of MoSi2 and Mo5Si3 layers without obvious thickness change during oxidation at 900°C and 1100°C. Mechanical property test indicated that the formation of the coating layers could not affect the fracture toughness of the alloy.  相似文献   

3.
由于在细晶Mo-Si-B合金中制备双峰分布的α-Mo晶粒能够在不显著降低合金强度的前提下大幅提高其断裂韧性,为了加强双峰结构合金的表面防护,同时保持其优异的力学性能,通过包埋渗在合金表面上制备了一个具有多层结构(MoSi2,Mo5Si3和Mo5SiB2/MoB)的涂层。研究结果表明,相比在细晶结构基体上制备的涂层,双峰结构基体上的涂层表面较为粗糙,并且也表现出双峰分布的微观组织。此外,覆盖涂层后的双峰结构合金的断裂韧性依然良好,并且分布在涂层中的La2O3颗粒能够增韧涂层。具有涂层的双峰结构合金在1100~1300 ℃下展现出了卓越的抗氧化性,这是由于氧化过程中在涂层表面快速形成了一个薄且能自愈合的SiO2-B2O3膜。随着氧化温度升高,SiO2-B2O3膜的粘度降低,使得SiO2-B2O3膜的厚度和氧化产物Mo5Si3均增加。并且,升高温度促进了Si和B的互扩散,加速了Mo5Si3和Mo5SiB2/MoB层的增长。在1300 ℃下,由于单峰结构的MoSi2涂层拥有更多的晶界,使得含涂层的细晶合金相比含涂层的双峰结构合金表现出更多的氧化增重。  相似文献   

4.
Induction plasma-spray processing was used to produce free-standing parts of Mo5Si3-B composite and MoSi2 materials. The oxidation resistance, up to 1210 °C, of the Mo5Si3-B composite was compared with MoSi2, which is known to be resistant to high-temperature oxidation. The deposits were oxidized isothermally in air at atmospheric pressure. The structural performance of these materials under high-temperature oxidation conditions was found to depend on the boron content in the specimens. In particular, the composite containing 2 wt.% boron exhibited excellent resistance to oxidation, as indicated by the specimen mass change, which was found to be near zero after the 24 h oxidation test.  相似文献   

5.
利用连续沉积的包埋渗法,在钼表面制备了(Ti,Mo)Si2/MoSi2复合涂层。利用X射线衍射、扫描电子显微镜、能谱仪和热力学计算对涂层进行了表征与反应机理分析。结果表明,共沉积法无法实现Ti的有效沉积。先渗Ti、再渗Si的两步沉积工艺能有效制备Ti改性硅化物涂层。涂层分为3层,最外层为(Ti,Mo)Si2三元化合物层,次外层为MoSi2层,次外层与基体间为Mo5Si3过渡层。渗硅温度对涂层结构无明显影响。Ti改性硅化物涂层的生长速率略低于单一渗硅涂层的生长速率。(Ti,Mo)Si2/MoSi2复合涂层的形成由Ti、Si内扩散控制。Ti元素集中在涂层表层,Si元素通过(Ti,Mo)Si2化合物层与基体作用形成MoSi2层和Mo5Si3过渡层。渗Ti过程中,埋渗料间反应会引入游离态铝氟化物AlF3。在随后的渗硅过程中,游离态Al以Al3Mo的形式在(Ti,Mo)Si2层中靠近MoSi2层的上界面处析出。在1200 ℃周期性氧化过程中,(Ti,Mo)Si2/MoSi2复合涂层持续循环氧化180 h后未出现明显失重。(Ti,Mo)Si2层氧化形成的SiO2与TiO2致密复合氧化层能填充涂层表面裂纹,持续阻碍氧扩散,因此其在周期性氧化环境下的抗氧化性能显著优于单一渗硅涂层。  相似文献   

6.
The two-layer MoSi2/MoB composite coatings were developed using the halide activated pack cementation (HAPC) method on Mo substrate. Oxidation resistance property and microstructural evolution of the coatings at high temperatures were investigated. During oxidation exposure, the coatings exhibited a good oxidation resistance property. The mass gains of the coated specimens oxidized at 1200 °C for 100 h and at 1300 °C for 80 h were 0.270 and 0.499 mg/cm2, respectively. Compared with the monolithic MoSi2 coatings, the transformation of MoSi2 phase in the MoSi2/MoB composite coatings was more sluggish at elevated temperatures. The growth rate constant of the Mo5Si3 layer in the composite coatings was two orders of magnitude lower than that of the Mo5Si3 layer in the monolithic coatings at 1300 °C. The microstructural degradation of MoSi2 in the composite coatings at high temperatures was slowed by the introduced MoB layer. The MoB layer in the composite coatings is useful to prolong the service life of MoSi2 coatings at high temperatures.  相似文献   

7.
《Intermetallics》2005,13(1):93-100
To establish quantitative basis for oxidation-protective coating of Mo–Si–B ternary alloys by MoSi2, phase transformations in MoSi2 vs. Mo5SiB2 diffusion couples have been studied. Two layers are formed on reaction diffusion at temperatures between 1400 and 1600 °C: a single-phase layer of Mo5Si3 and a two-phase layer consisting of Mo5Si3 and MoB. The growth obeys the parabolic low for both the layers, and the rate constants of the two layers are found to be approximately equal. The interdiffusion coefficient in the T1 layer has also been evaluated. The microstructural evolution in the diffusion zone is modeled in terms of mass conservation, as well as that of a Mo–9Si–18B two-phase alloy coated with MoSi2 reported previously [Intermetallics 12 (2004) 407].  相似文献   

8.
In this study, molybdenum disilicide (MoSi2) coatings were fabricated by vacuum plasma spraying technology. Their morphology, composition, and microstructure characteristics were intensively investigated. The oxidation behavior of MoSi2 coatings was also explored. The results show that the MoSi2 coatings are compact with porosity less than 5%. Their microstructure exhibits typical lamellar character and is mainly composed of tetragonal and hexagonal MoSi2 phases. A small amount of tetragonal Mo5Si3 phase is randomly distributed in the MoSi2 matrix. A rapid weight gain is found between 300 and 800 °C. The MoSi2 coatings exhibit excellent oxidation-resistant properties at temperatures between 1300 and 1500 °C, which results from the continuous dense glassy SiO2 film formed on their surface. A thick layer composed of Mo5Si3 is found to be present under the SiO2 film for the MoSi2 coatings treated at 1700 °C, suggesting that the phenomenon of continuous oxidation took place.  相似文献   

9.
The rapid, destructive low-temperature oxidation (pesting) of MoSi2 is an important limitation to its practical use. The growth of molybdenum silicide diffusion coatings by a halide-activated pack cementation method results in an adherent superficial, salt by-product, whose composition depends on the halide activator used to grow the coating. As a consequence of the residual salt deposit, coatings grown by a NaF-activated pack did not pest after 2500 hours of isothermal oxidation or after cyclic oxidation for 600 1 hour cycles in air at 500°C. An additional minor improvement in the pesting resistance was observed for the germanium-doped MoSi2 Coatings. The growth kinetics for a three-layer Ge-doped Mo(Si, Ge)2/Mo5(Si, Ge)3/Mo3(Si, Ge) coating are compared with rates calculated for the diffusion-controlled growth of an undoped three-layer silicide and for three-layer germanide coatings. The activation energy for the solid-state diffusional growth of MoSi2 is the same as that for Mo(Si, Ge)2, but the growth rates for Mo(Si, Ge)2 are faster. The activation energies for the solid state diffusional growth of the inner Mo5(Si, Ge)3 and Mo3(Si, Ge) layers are similar to Mo5Ge3 and Mo3Ge, but the rates are slower. The chemical demixing of Mo(Si, Ge)2 under a chemical potential gradient creates a maximum in the Ge concentration at the Mo(Si, Ge)2/Mo5(Si, Ge)3 interface, which produces unusual growth kinetics for the Mo5(Si, Ge)3 and Mo3(Si, Ge) layers.  相似文献   

10.
The topic “Materials for temperatures above 1500°C in oxidizing atmospheres” is discussed in a 3 part publication. In the first part a literature survey had been performed leading to the conclusion that either particle or fiber reinforced MoSi2‐based materials or RSiC coated with a MoSi2‐based layer are suitable for applications at such high temperatures. In the present part such material systems are investigated experimentally at 1500 and 1600°C with respect to their oxidation resistance in air. Particular interest was given to the influence of the Mo5Si3 content in MoSi2 and the influence of second phase particles in MoSi2 consisting of ZrB2 and SiC. Furthermore, the oxidation resistance of several dip‐coatings on RSiC which were manufactured from a polysiloxane precursor by subsequent pyrolysis were also investigated. Part III which reports about “contact corrosion” between different materials at these temperatures will follow in the next issue.  相似文献   

11.
The growth kinetics and silicon diffusion coefficients of intermediate silicide phases in MoSi2-3.5 vol.% Si3N4-5.0 vol.% WSi2/Mo diffusion couple prepared by spark plasma sintering were investigated in temperatures ranging from 1200 to 1500 °C. The intermediate silicide phases were characterized by x-ray diffraction. The microstructures and components of the MoSi2-Si3N4-WSi2/Mo composites were investigated using scanning electron microscope with energy-dispersive spectroscopy. A special microstructure with MoSi2 core surrounded by a thin layer of (Mo,W)Si2 ring was found in the MoSi2-Si3N4-WSi2 composites. The intermediate layers of Mo5Si3 and (Mo,W)5Si3 in the MoSi2-Si3N4-WSi2/Mo diffusion couples were formed at different diffusion stages, which grew parabolically. Activation energy of the growth of intermediate layers in MoSi2-3.5 vol.% Si3N4-5.0 vol.% WSi2/Mo diffusion couple was calculated to be 316 ± 23 kJ/mol. Besides, the hindering effect of WSi2 addition on the growth of intermediate layers was illustrated by comparing the silicon diffusion coefficients in MoSi2-3.5 vol.% Si3N4-5.0 vol.% WSi2/Mo and MoSi2-3.5 vol.% Si3N4/Mo diffusion couples. MoSi2-3.5 vol.% Si3N4-5.0 vol.% WSi2 coating on Mo substrate exhibited a better high-temperature oxidation resistance in air than that of MoSi2-3.5 vol.% Si3N4 coating.  相似文献   

12.
Effects of ternary additions on the microstructure and thermal stability of directionally-solidified MoSi2/Mo5Si3 eutectic composites have been studied for twelve different elements (Ti, V, Cr, Fe, Co, Ni, Nb, Ta, W, Ir, B and C) paying special attention to the variation of lattice misfits and interface segregation behavior with ternary additions. Among six elements (type-1: Ti, V, Cr, Nb, Ta and W) with a relatively high solubility in MoSi2 and Mo5Si3, Ta and W are found to be beneficial to microstructure refinement. All other six ternary elements (type-2: Fe, Co, Ni, Ir, B and C) with a negligibly low solubility in MoSi2 and Mo5Si3 exhibit a strong tendency to segregate on MoSi2/Mo5Si3 interfaces, resulting in both microstructure refinement and the modification of the interface morphology.  相似文献   

13.
The microstructure of an in-situ Mosi2/β-SiC nanocomposite coating formed by the solid-state displacement reactions of Si deposited by chemical vapor deposition (CVD) with Mo-carbide layers at 1100°C, which had previously been formed on the surface of a Mo substrate by a CVD process, was investigated. The Mo-carbide layers formed by the simultaneous CVD of Mo and carbon at 900°C for 5 h using a gas mixture of C2H4−MoCl5−Ar consisted of two layers, an inner layer of Mo2C and an outer layer of MoC. While the monolithic MoSi2 coating showed a typical colummar microstructure perpendicular to the Mo substrate, the MoSi2/β-SiC nanocomposite coating formed by the solid-state displacement reactions between the Mo-carbide layers and Si was composed of equiaxed MoSi2 grains with an average size of 150–500 nm and β-SiC particles with an average size of 80–105 nm. The β-SiC particles exhibited an oblate-spheroidal shape and were located mostly at the grain boundaries of MoSi2. The volume percentage of β-SiC particles ranged from 18.5 to 29.2% with respect to the carbon concentration in Mo-carbide layers.  相似文献   

14.
以工业废弃硅化钼棒为原料,采用浆料涂刷法在钼表面制备MoSi2基抗氧化涂层.研究涂层的显微组织、相组成及在1500℃的高温氧化行为.结果表明,以废弃硅化钼棒和纯MoSi2粉末为原料制备的涂层和基体之间形成明显的连接层.纯MoSi2制备的涂层(PM)在烧结后出现少量裂纹,而以废弃硅钼棒为原料制备的涂层(SM)在烧结后没有...  相似文献   

15.
The MoSi2 coating on C 103 niobium based alloy was prepared by pack cementation method. The formative mechanism, morphology and structure of coating were investigated. The silicide coating was formed by reactive diffusion obeying parabolic rule during pack cementation process. It is found that the composite structural coating is composed of three inferior layers as follows. The main layer is composed of MoSi2, the two phases' transitional layer consists of NbSi2 and a few NbsSi3 and the diffuse layer is composed of NbsSi3. The dense amorphous glass layer formed on the surface at high temperature oxidation circumstance can effectively prevent the diffusion of oxygen into coating.  相似文献   

16.
Lee  D. B.  Kim  D J. 《Oxidation of Metals》2004,61(5-6):423-437
From the pre-ceramic polymer of polymethylsiloxane (PMS) and powders of MoSi2, SiC and Si, new ceramic composites that consisted primarily of an amorphous SiOC matrix containing dispersed particles of MoSi2 and SiC were synthesized. The composites displayed superior oxidation resistance at both high and low temperatures by forming SiO2 on the surface. The thin, amorphous SiO2 layer that formed initially gradually to crystallized during oxidation between 1000 and 1300°C. An outer highly porous and an inner superficial SiO2 layer that formed from the initial stage of oxidation between 400 and 500°C protected the composites from pesting.  相似文献   

17.
Plasma spraying combined with halide activated pack cementation (HAPC) was used to deposit silicide coating on Nb-based alloy. X-ray diffraction (XRD) and energy disperse spectrum (EDS) indicate the formation of the siliconized NbSi2 transition layer and the sprayed MoSi2 outer layer. NbSi2 layer prepared with HAPC exhibits relatively uneven surface which could promote the deposition of the sprayed MoSi2. The coating specimen with 5 h siliconizing presented the best oxidation resistance with only 0.18% mass gain after 25 h oxidation at 1200 °C in air. The synergistic protection effect, depending on the continuous silica layer formed on the coating surface and the dispersal silica within the coating and interface, is responsible for the excellent oxidation resistance of the coating.  相似文献   

18.
《Intermetallics》2000,8(9-11):1147-1158
A key materials issue associated with the future of high-temperature structural silicides is the resistance of these materials to oxidation at low temperatures. Oxidation tests were conducted on Mo-based silicides over a wide temperature range to evaluate the effects of alloy composition and temperature on the protective scaling characteristics and pesting regime for the materials. The study included Mo5Si3 alloys that contained several concentrations of B. In addition, oxidation characteristics of MoSi2–Si3N4 composites that contained 20–80 vol.% Si3N4 were evaluated at 500–1400°C.  相似文献   

19.
MoSi2 and Mo(Si, Al)2 coatings were prepared on Mo–0.5Ti–0.1Zr–0.02C alloy using pack cementation process. Oxidation studies revealed that Mo(Si, Al)2 coating had a much superior oxidation resistance in the temperature range from 400 to 900 °C, where pest disintegration of MoSi2 occurs due to internal oxidation. The growth kinetics of Al2O3 layer formed on Mo(Si, Al)2 coating was much slower than that of SiO2 layer formed on MoSi2 coatings during oxidation.  相似文献   

20.
To protect carbon/carbon (C/C) composites from oxidation, a dense coating has been produced by a two-step pack cementation technique. XRD and SEM analysis shows that the as-obtained coating was composed of MoSi2, SiC and Si with a thickness of 80-100 μm. The MoSi2-SiC-Si coating has excellent anti-oxidation property, which can protect C/C composites from oxidation at 1773 K in air for 200 h and the corresponding weight loss is only 1.04%. The weight loss of the coated C/C composites is primarily due to the reaction of C/C substrate and oxygen diffusing through the penetration cracks in the coating.  相似文献   

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