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2018, HAL (Le Centre pour la Communication Scientifique Directe)
https://doi.org/10.1002/ADEM.201600372…
6 pages
1 file
In order to better understand the thermomechanical behaviors of Ti 3 SiC 2 and Ti 2 AlC ceramics, sintered by spark plasma sintering process (SPS), ultrasonic pulse echography in "long bar mode" (US) and acoustic emission (AE) techniques are applied. High-temperature investigations of the evolution of Young's modulus (E) and AE activity are carried out up to 1 473 and 1 623 K. Results show a decrease of E with increasing temperature which is more marked around maximal temperature of the thermal cycle for Ti 2 AlC material. Moreover, the increase of the maximal temperature of the thermal cycle influences the number of recorded cumulated hits. Both measurements (US þ AE) highlight the role of the plastic deformation mechanism (motion of dislocation) activated over the brittle-to-plastic transition temperature.
1990
Thermomechanical testing techniques recently developed for monolithic structural alloys were successfully extended to continuous fiber reinforced composite materials in plate form. The success of this adaptation was verified on a model metal matrix composite (MMC) material, namely SiC(SCS-6)/Ti-15V-3Cr-3Al-3Sn. Effects of heating system type and specimen preparation are also addressed. Cyclic lives determined under full thermo-mechanical conditions were shown to be significantly reduced from those obtained under comparable isothermal and in-phase bi-thermal conditions. Fractography and metallography from specimens subjected to isothermal, out-of-phase and in-phase conditions reveal distinct differences in damage-failure modes. Isothermal metallography revealed extensive matrix cracking associated with fiber damage throughout the entire cross-section of the specimen. Out-of-phase metallography revealed extensive matrix damage associated with minimal (if any) fiber cracking. However, ...
Processing and Application of Ceramics
SiC-TiC composites, with 0, 5, 10 and 20 vol.% of TiC, were sintered by the hot-pressing technique at temperature of 2000?C under argon atmosphere. SiC sintering process was activated by liquid phase created by the reaction between Al2O3 and Y2O3, in which it is possible to dissolve passivating oxide layers (SiO2 and TiO2) and partially SiC and TiC carbides. Microstructure observation and density measurements confirmed that the composites were dense with uniformly distributed components. Differences in thermal expansion coefficients between SiC and TiC led to complex stress state occurrence. These stresses combined with the liquid-derived separate phase between grains boundaries increased fracture toughness of the composites, which ranged from 5.8 to 6.3MPa?m0.5. Opposite to the bending strength, fracture toughness increased with the TiC volume fraction. By means of simulation of residual thermal stresses in the composites, it was found that with the increasing volume fraction of Ti...
Journal of the Ceramic Society of Japan, 1992
The characteristic low brittle-ductile transition tem perature of TiC was utilized to toughen SiC matrix composites at high temperatures. AlN, Ti and C pow ders were used as a dopant to alter the intrinsic proper ties of SiC matrix or dispersed TiC particles. The frac ture toughness of the SiC matrix was improved in the temperature from room temperature to 1600•Ž by the incorporation of dispersed TiC particles. At low tem peratures, the toughening mechanism in SiC/TiC com posites was crack deflection or crack bridging while above 1200•Ž, it was plastic deformation of TiC parti cles.
1999
Ceramic matrix composites exhibit significant nonlinear stress-strain behavior that makes them attractive as potential materials for many high temperature applications. The mechanisms for this nonlinear stress-strain behavior are all associated with various types of damage in the composites, e.g. transverse matrix cracks and individual fiber failures. Modal acoustic emission has been employed to aid in disceming the damage accumulation that occurs during elevated temperature tensile stress-rupture of woven Hi-Nicalon TM fiber, BN interphase, SiC matrix composites. It is shown that modal acoustic emission is an effective monitor of the relative damage accumulation in the composites and locator of the damage and failure events as a function of strain (stress), time at temperature, and temperature gradients along the length of the elevated temperature test specimen.
Proceedings of the 2015 Asia International Conference on Quantitative InfraRed Thermography, 2015
The aim of the study is to characterize the composite by visualizing the different stages of deformation on the tensile specimen of Al/SiC metal matrix composite using Infrared thermography technique. Infrared thermography is a Non-contact technique to record the surface temperature distribution. Infrared thermography is a powerful non-destructive evaluation tool for online monitoring the different stages of deformation and to predicting the exact region of fracture with respect to temperature variations. The Infrared images are acquired from the specimens for the material characterization. It is a high sensitive Nondestructive testing technique for detecting the active microscopic events the material. Al/SiC composites has high strength, high resistance to wear and low weight properties make them demand full in many industrials applications such as marine, electronic packages, cost-effective solutions for many thermal management problems, automotive and aerospace industries. In this present study, SiC (220 mesh) particulates reinforced in the AL6061-T6 alloy matrix and fabricated the composites by low cost stir casting technique with 10% of SiC and 90% of Aluminum alloy by weight. The tensile tests was conducted with displacement control and a constant crosshead speed of 2 mm/min. Studies were conducted to determine the tensile properties, modulus of elasticity, ultimate tensile strength, fracture load, yield point and variation of temperature of the specimens. Interpretation of heat emission signals acquired from the Al/SiC MMCs specimens during proof testing with the Infrared thermography images may give a better platform for the prior prediction of the ultimate strength of the specimens while tensile loading. The experimental result reveals that the ultimate temperature rise and the rate of temperature rise is having a good correlation with the deformation behavior of the Al/SiC materials during tensile loading. Also Success of this proposed research work would be a good feed for the composite industries at which the characterization is very much essential.
Ceramics International, 2020
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International Journal of Applied Ceramic Technology, 2019
The hot pressing process of monolithic Al 2 O 3 and Al 2 O 3-SiC composites with 0-25 wt.% of submicron silicon carbide was done in this paper. The presence of SiC particles prohibited the grain growth of the Al 2 O 3 matrix during the sintering at the temperatures of 1450 °C and 1550 °C for 1 h and under the pressure of 30 MPa in vacuum. The effect of SiC reinforcement on the mechanical properties of composite specimens like fracture toughness, flexural strength and hardness was discussed. The results showed that the maximum values of fracture toughness (5.9 ± 0.5 MPa.m 1/2) and hardness (20.8 ± 0.4 GPa) were obtained for the Al 2 O 3-5 wt.% SiC composite specimens. The significant improvement in fracture toughness of composite specimens in comparison with the monolithic alumina (3.1 ± 0.4 MPa.m 1/2) could be attributed to crack deflection as one of the toughening mechanisms regarding to the presence of SiC particles. In addition, the flexural strength was improved by increasing SiC value up to 25 wt.% and reached 395 ± 1.4 MPa. The SEM observations verified that the increasing of flexural strength was related to the fine-grained microstructure.
International Journal of Applied Ceramic Technology, 2019
The hot pressing process of monolithic Al2O3 and Al2O3‐SiC composites with 0‐25 wt% of submicrometer silicon carbide was done in this paper. The presence of SiC particles prohibited the grain growth of the Al2O3 matrix during sintering at the temperatures of 1450°C and 1550°C for 1 h and under the pressure of 30 MPa in vacuum. The effect of SiC reinforcement on the mechanical properties of composite specimens like fracture toughness, flexural strength, and hardness was discussed. The results showed that the maximum values of fracture toughness (5.9 ± 0.5 MPa.m1/2) and hardness (20.8 ± 0.4 GPa) were obtained for the Al2O3‐5 wt% SiC composite specimens. The significant improvement in fracture toughness of composite specimens in comparison with the monolithic alumina (3.1 ± 0.4 MPa.m1/2) could be attributed to crack deflection as one of the toughening mechanisms with regard to the presence of SiC particles. In addition, the flexural strength was improved by increasing SiC value up to 2...
Materials, 2019
Metal-ceramic composite (MCC) materials can be used for manufacturing high-responsibility structures such as jet engines or cutting tools. One example of these materials is a two-phase wolfram carbide (WC) and cobalt (Co) composite. This MCC is a combination of hard WC grains with a Co metallic ductile binder. The resulting microstructure is a combination of two phases with significantly different mechanical behaviors. In this study, we investigate impact conditions, starting with an illustrative example of the Taylor impact bar where—although the process is very rapid—the equivalent plastic strain and temperature are higher in the adiabatic solution than those in the coupled solution. On exposing the WC/Co composite with a metallic binder to impact loading, heat is generated by plastic deformation. If the process is fast enough, the problem can be treated as adiabatic. However, a more common situation is that the process is slower, and the heat is generated in the ductile metallic ...
Scripta Materialia, 1997
Many Mg-based metal matrix composites (MMCs) have been developed and manufactured during the last decade (1) as prospective light high-performance constructional materials. The microstructure and mechanical properties of MMCs are influenced significantly by the interfaces between the matrix and the reinforcement. When a MMC is submitted to temperature changes (cooling down from the temperature of fabrication, cyclic temperature changes during operation of structural parts) thermal stresses arise at the interfaces owing to a considerable mismatch of the thermal expansion coefficient of the matrix and that of the reinforcement. Even slight temperature changes may produce thermal stresses which exceed the matrix yield stress, consequently, generating new dislocations at the interfaces causing microstructural changes and plastic deformation of the matrix. Long-term exposure may also result in fatigue damage. It is noteworthy that the effect of temperature variations is similar to creep under non-stationary loading conditions. Hitherto, the microstructural response of MMC on changes in temperature has been investigated mainly indirectly (post mortem) (2-5). The generation of new dislocations has been demonstrated by etch pit technique (2), transmission electron microscopy (3,4) and internal friction (5). However, it is difficult to assess the evolution of the dynamic structure, i. e. to obtain a direct correlation of the structure to the temperature using these methods. In situ studies (by transmission electron microscopy -TEM) (6) can establish such a correlation but that is only of a local character and the stress state is most probably influenced by the relatively small thickness of TEM specimens.
Composites Science and Technology, 2006
The present work deals with the development of anisotropic damage in alumina/alumina continuous fiber ceramic composites (CFCCs). The composites were isothermally exposed to a corrosive/high temperature environment at 1100°C, which simulates the working conditions of a gas turbine. Stiffness matrix components and strength were experimentally defined as a function of exposure duration by means of ultrasonic stiffness measurements and quasi-static tensile tests.
Journal of Synchrotron Radiation, 2022
A high-temperature multi-axial test is carried out to characterize the thermo-mechanical behaviour of a 3D-woven SiC/SiC composite aeronautical part under loads representative of operating conditions. The sample is L-shaped and cut out from the part. It is subjected to severe thermal gradients and a superimposed mechanical load that progressively increases up to the first damage. The sample shape and its associated microstructure, the heterogeneity of the stress field and the limited accessibility to regions susceptible to damage require non-contact imaging modalities. An in situ experiment, conducted with a dedicated testing machine at the SOLEIL synchrotron facility, provides the sample microstructure from computed micro-tomographic imaging and thermal loads from infrared thermography. Experimental constraints lead to non-ideal acquisition conditions for both measurement modalities. This article details the procedure of correcting artefacts to use the volumes for quantitative expl...
Ceramics International, 2020
Titanium carbide (TiC) composites containing 10 vol% silicon carbide whisker (SiC w) were spark plasma sintered at different temperatures of 1800, 1900, and 2000°C under a pressure of 40 MPa and a holding time of 7 min. At the sintering temperature of 1900°C, the relative density, Vickers hardness, and flexural strength of the sintered samples hit their maximum values of 98.7%, 24.4 GPa, and 511 MPa, respectively. The microstructural characteristics of the sintered samples were assessed by optical and field emission scanning electron microscopy (FESEM) and XRD. The results revealed that at 1900°C, the dispersion of SiC w in the TiC matrix was homogenous, no chemical reaction took place between the reinforcement and the matrix, and produced a fine-grained microstructure. It was found that the thermal conductivity of SPSed samples did not have the same trend with relative density and mechanical properties. A maximum value of 32.3 W/mK was measured for the thermal conductivity of the composite sintered at 2000°C.
Materials Science and Engineering A-structural Materials Properties Microstructure and Processing, 2011
Dense SiC-TiB 2 composites with 24 vol% TiB 2 were fabricated by pressureless sintering at 1940 • C. Al 2 O 3 and Y 2 O 3 were used as sintering additives to create a liquid phase and promote densification. TiB 2 was formed by an in situ reaction between TiO 2 , B 4 C and C. The sintered samples were subsequently heattreated at temperatures ranging from 1850 • C to 2000 • C. The effect of temperature of post-sintering heat treatment on microstructure and mechanical properties of the SiC-TiB 2 composite was presented. Heat treatment at 1970 • C considerably improved the strength and the fracture toughness of sintered samples while maintaining high density. The elongation of ␣-SiC grains during the heat treatment was found to be responsible for an increase in fracture toughness. The presence of liquid phase assisted the elongation of grains which, in turn, activated crack bridging and crack deflection toughening mechanisms. Maximum strength of 540 MPa was found to be the result of improved fracture toughness. Heat treatment at temperatures above 1970 • C led to a deterioration of mechanical properties.
Open Chemistry
The scope of this study, that is, the effect of the elastic modulus obtained by ultrasonic method on the physical and mechanical properties of tungsten carbide (WC)-based ceramic–metal composites, which have Ni and Co metallic binder composition produced by powder metallurgy and represented by high strength and hardness criteria, was investigated. In order to obtain composite samples in the study, it was sintered in a microwave furnace at different temperatures to combine the powder particles prepared at the rate of 60% Ni, 20% Co, and 20% WC by weight. Then, the velocities and longitudinal attenuation values of longitudinal and shear ultrasonic waves along the composite sample were measured using the ultrasonic pulse-echo method. The elastic modulus of the composites was determined using ultrasonic velocities and sample density. Hardness testing, scanning electron microscopy (SEM), and X-ray diffraction (XRD) analyses were also performed. The results show that the elastic modulus i...
European Journal of Science and Technology
In this study, an experimental study was carried out to examine the variation of some ultrasonic parameters such as wave attenuation coefficients on metal matrix SiC doped composite samples. Ultrasonic longitudinal and shear attenuation values of produced coppersilicon carbide composite samples were measured at 4 MHz frequency by pulse-echo technique. Variations of longitudinal and shear attenuation values and hardness with % SiC volume percentages were determined. The experimental results obtained are discussed and analyzed to improve the ultrasonic nondestructive testing method for microstructure determination
Journal of Materials Science Letters, 1998
Ceramics International, 2018
SiC-TiC composite containing 5-30 vol% TiC particles was fabricated by conversion of TiO 2 to TiC during pressureless sintering. The presence of very fine and uniformly distributed, in-situ created TiC particles increased driving force for sintering allowing fabrication of high density SiC-TiC composite without the use of external pressure. The highest mechanical properties were measured in samples sintered at 1885 o C for 1 h. The highest values for hardness (~20 GPa) and fracture strength (~490 MPa) were measured in samples containing 5 vol% TiC, whereas the highest fracture toughness (~5.5 MPa•m 1/2) was measured in samples containing 10 vol% TiC. The presence of in-situ created, uniformly distributed TiC particles was beneficial for activation of not only the crack deflection mechanism but also mechanism called toughening by residual stress crated due to the difference of thermal expansion between SiC matrix and TiC particles. The 2 compressive stress field around TiC particles acts to close the propagating crack and thus to increase fracture toughness.
Composites Part A: Applied Science and Manufacturing, 2014
The acoustic emission (AE)-based technique is considered to be a promising way to real-time monitoring of microstructural changes and damage evolution in Ceramic Matrix Composites (CMCs). The present paper proposes a testing protocol that combines acousto-ultrasonics (AU) and acoustic emission (AE) monitoring, with a view to obtain both global and local definite characteristics on damage modes and kinetics. It is developed and assessed on SiC/SiC minicomposites, which are appropriate test specimens to establish sound relations between mechanical behavior and damage modes. AU wave velocity measurements provide a global measure of matrix cracking damage and the relations between crack growth and damage characteristics. AE monitoring allows accurate localization of AE sources taking into account wave velocity dependence to damage as well as differentiation of the damage modes, which control the mechanical behavior. Finally, multivariate analysis of AE data allowed classification of signals into clusters, which were successfully associated to the various damage modes.
Materials Science and Engineering: A, 2001
Microyield phenomena during thermocycling of Al 7075 alloy/15 vol.% SiC metal-matrix composite due to mismatch of the thermal expansion coefficients of the matrix and the SiC particles are studied over the temperature range from 50 to 300 K by means of internal friction techniques. The transient component of the internal friction is measured in the infrasonic frequency range, whereas the structural strain amplitude-independent and strain amplitude-dependent internal friction is investigated at ultrasonic frequencies. Combining the two techniques enables us to follow the variation of the defect structure during thermocycling as well as to evaluate basic contributions to the microyield phenomenon. The following conclusions are drawn: (1) thermal stresses are responsible for creation of fresh, i.e. mobile dislocations, whose density does not differ significantly, for the same temperature, during heating and cooling or in consecutive thermocycles; (2) yielding is much more pronounced during the first cooling from a stress-free state than in the consecutive thermocycles; this pronounced yielding is due to long-range motion of approximately the same amount of fresh dislocations as in consecutive thermocycles; and (3) during thermocycling, the matrix undergoes dynamic strain ageing; its intensity depends strongly on temperature and therefore varies continuously in a thermocycle.
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