Relevant bibliographies by topics / Titanium matrix composites (TMCs)

Contents

  1. Journal articles
  2. Dissertations / Theses
  3. Books
  4. Book chapters
  5. Conference papers
  6. Reports

Academic literature on the topic 'Titanium matrix composites (TMCs)'

Author: Grafiati
Published: 4 June 2021
Last updated: 17 February 2022

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Journal articles on the topic "Titanium matrix composites (TMCs)"

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Sung, Si Young, Bong Jae Choi, and Young Jig Kim. "Casting and Modeling of Titanium Matrix Composites." Key Engineering Materials 345-346 (August 2007): 1213–16. http://dx.doi.org/10.4028/www.scientific.net/kem.345-346.1213.

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The aim of this study is to establish the net-shape forming of titanium matrix composites (TMCs) shot sleeve for Al alloys die-casting using a casting route. In-situ synthesis and casting of TMCs were carried out in a vacuum induction melting furnace. The synthesized (TiC+TiB) TMCs were examined using an scanning electron microscopy and electron probe micro-analyzer. The thermo-physical variables estimated by casting process were applied to the modeling of TMCs shot-sleeve casting using the Magmasoft®. The results of the investment casting and modeling of TMCs confirm that the casting route can be an effective approach for the economic net-shape forming of TMCs shot sleeve.
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Sung, Si Young, Keun Chang Park, Myoung Gyun Kim, and Young Jig Kim. "Investment Casting of Titanium Matrix Composites." Materials Science Forum 475-479 (January 2005): 2551–54. http://dx.doi.org/10.4028/www.scientific.net/msf.475-479.2551.

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The aim of the present work is to investigate the possibility of in-situ synthesis and net-shape of the titanium matrix composites (TMCs) using a casting route. From the scanning electron microscopy (SEM), electron probe micro-analyzer (EPMA), X-ray diffraction (XRD) and thermodynamic calculations, the spherical TiC and needle like TiB reinforced hybrid TMCs could be obtained by the conventional casting route between titanium and B4C. No melts-mold reaction could be possible between (TiC+TiB) hybrid TMCs and the SKKU mold, since the mold is composed of interstitial and substitutional reaction products. Not only the sound in-situ synthesis but also the economic net-shape of TMCs could be possible by conventional casting route.
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Choi, Bong Jae, Si Young Sung, and Young Jig Kim. "Evaluation of Interfacial Reaction between Titanium Matrix Composites and Aluminium Alloy." Key Engineering Materials 334-335 (March 2007): 433–36. http://dx.doi.org/10.4028/www.scientific.net/kem.334-335.433.

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The main purpose of this study is to evaluate the interfacial reaction between titanium matrix composites (TMCs) and A380 alloy in aluminum die-casting. In-situ synthesized titanium matrix composites and H13 tool steel were immersed in molten A380 alloy in a mold at 993 K for times varying from 0 to 1200 s. In-situ synthesis TMCs and interfacial reaction between TMCs and A380 alloy were examined by X-ray diffraction, optical microscope, scanning electron microscope and electron probe micro-analyzer. The reaction behavior shows that TMCs can a substitution for H13 tool steel.
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Sung, Si Young, Bong Jae Choi, and Sang Hwa Lee. "Interfacial Reaction between Molten Al Alloys and Titanium Matrix Composites." Materials Science Forum 510-511 (March 2006): 310–13. http://dx.doi.org/10.4028/www.scientific.net/msf.510-511.310.

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The aim of this study is to investigate the applicability of titanium matrix composites (TMCs) sleeve to Al alloys die-casting. Ti and 1.88 mass% B4C were prepared for the synthesis of 10 vol% (TiC+TiB) hybrid TMCs. In-situ synthesis and net-shape forming of TMCs were carried out in a vacuum induction melting furnace. The synthesized (TiC+TiB) TMCs were examined using scanning electron microscopy, an electron probe micro-analyzer, X-ray diffraction and transmission electron microscopy. The resistance-ability of (TiC+TiB) TMCs to molten Al alloys attack was also examined. Their reactions were carried out in a furnace at 993 K for times varying from 0 to 1200 s. In the case of conventional sleeve material, H13 steel, there were severe interfacial reactions and erosion after 60 s. On the other hand, the resistance of (TiC+TiB) TMCs to interfacial reactions and erosion by molten A380 alloy was significantly increased.
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Yu, Qing Yu, Jing Wang, Yuan Chao Gan, Wei Dong Song, and Xiao Nan Mao. "Dynamic Constitutive Model for TiC-Particulate Reinforced Titanium Matrix Composites." Materials Science Forum 833 (November 2015): 141–44. http://dx.doi.org/10.4028/www.scientific.net/msf.833.141.

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A coupled model of damage and plasticity is presented to describe the dynamic behaviors of TiC-particulate reinforced titanium matrix composites (TiCp/TMCs) subjected to shock loadings. The TiCp/TMCs are assumed as homogeneous continuum with pre-existing micro-cracks and micro-voids. Damage to TiCp/TMCs is caused due to micro-crack nucleation, growth and coalescence, and defined as the probability of fracture at a given crack density. In terms of crack growth model, micro-cracks are activated, and begin to propagate gradually. When crack density reaches a critical value, the smashing destroy takes place. The model parameters for TiCp/TMCs are determined using plate impact experiments. Comparison with the test results shows that the proposed model can give consistent predictions of the dynamic behaviors of TiCp/TMCs subjected to impact loadings.
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Sung, Si Young, Bong Jae Choi, and Young Jig Kim. "Synthesis and Forming of Titanium Matrix Composites by Casting Route." Key Engineering Materials 334-335 (March 2007): 297–300. http://dx.doi.org/10.4028/www.scientific.net/kem.334-335.297.

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The aim of this study is to evaluated the possibility of the in-situ synthesized (TiC+TiB) reinforced titanium matrix composites (TMCs) for the application of structural materials. In-situ synthesis and casting of TMCs were carried out in a vacuum induction melting furnace with Ti and B4C. The synthesized TMCs were characterized using scanning electron microscopy, an electron probe micro-analyzer and transmission electron microscopy, and evaluated through thermodynamic calculations. The spherical TiC plus needle-like and large, many-angled facet TiB reinforced TMCs can be synthesized with Ti and B4C by a melting route.
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Huan, Hai Xiang, Jiu Hua Xu, Hong Hua Su, Yu Can Fu, and Ying Fei Ge. "Experimental Study on Milling of Titanium Matrix Composites." Key Engineering Materials 589-590 (October 2013): 281–86. http://dx.doi.org/10.4028/www.scientific.net/kem.589-590.281.

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Titanium matrix composites (TMCs) possess many outstanding properties and have increasing and potential application in aerospace, automobile and other industries. However, TMCs are typical difficult-to-machining material due to the rapid tool wear rate and excessive machining induced defects. In this paper, tool wear, cutting forces, cutting temperature and surface roughness were investigated when milling TMCs with Polycrystalline Diamond (PCD) and carbide tools. The results showed that the values of surface roughness obtained by carbide tools were higher than that of PCD tools under the same cutting conditions. The value of cutting temperature for PCD tool was about 75% of the carbide tools, and the main cutting force value of PCD tool was about 85% of the carbide tool. Abrasive and adhesive wear were the main wear mechanisms of PCD and carbide tools. In all, PCD tools had a better cutting performance than carbide tools during finishing milling titanium matrix composites.
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Choi, Bong Jae, Kyung Eui Hong, Jeong Il Youn, and Young Jig Kim. "In Situ Synthesis and Wear Resistance of Titanium Matrix Composites." Advanced Materials Research 89-91 (January 2010): 107–11. http://dx.doi.org/10.4028/www.scientific.net/amr.89-91.107.

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The main purpose of this research is to evaluate the wear resistance of titanium matrix composites (TMCs). Reinforcements, TiB and TiC, were formed by in-situ reaction between boron carbide and commercial pure titanium. The confirmation of the sound synthesis of TMCs was done by phase identification. And then, sliding wear test were carried out to verify the wear resistance of TMCs by means of the coefficient of friction, wear loss and morphology wear track. The results of wear test indicate that TMCs have superior resistance than AISI H13 tool steel at the condition of severe loads.
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Choi, Bong Jae, Si Young Sung, and Young Jig Kim. "(TiB+TiC) Hybrid Titanium Matrix Composites Shot Sleeve for Aluminum Alloys Diecasting." Advanced Materials Research 15-17 (February 2006): 231–35. http://dx.doi.org/10.4028/www.scientific.net/amr.15-17.231.

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The aim of this study is to fabricate an α-case free (TiB+TiC) hybrid titanium matrix composites (TMCs) shot sleeve for aluminum alloy diecasting by in-situ synthesis and investment casting. Granular 1.88 wt% B4C was added to a titanium matrix in a vacuum induction melting furnace. The synthesized (TiB+TiC) TMCs were examined using electron probe micro-analysis and transmission electron microscopy. The results of the in-situ synthesis and investment casting of the TMCs show that our casting route constitutes an effective approach to the economic net-shape forming of TMC sleeves.
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Du, Lihua, Zhusheng Shi, Yuanfei Han, Jie Shao, Kailun Zheng, Yong Li, and Weijie Lu. "Development of constitutive equations for hot working of titanium matrix composites." MATEC Web of Conferences 321 (2020): 03033. http://dx.doi.org/10.1051/matecconf/202032103033.

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This research is devoted to modelling the viscoplastic deformation behaviour and microstructure evolution of particle reinforced titanium matrix composites (TMCs) at hot working conditions. A series of Gleeble hot compression tests were conducted to obtain the stress-strain curves. According to the dominant mechanisms of TMCs during deformation, a set of mechanism-based constitutive equations was developed and fitted based on the experiment data. Lamellar alpha globularisation, dynamic recrystallization and damage were considered and incorporated into the constitutive equations to describe the viscoplastic flow behaviour.
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Dissertations / Theses on the topic "Titanium matrix composites (TMCs)"

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Yuan, Fei (Fred) Materials Science &amp Engineering Faculty of Science UNSW. "Properties of titanium matrix composites reinforced with titanium boride powders." Awarded by:University of New South Wales. Materials Science & Engineering, 2007. http://handle.unsw.edu.au/1959.4/40750.

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Metal matrix composites can produce mechanical and physical properties better than those of the monolithic metal. Titanium alloys are widely used matrix materials as they can offer outstanding specific strength, corrosion resistance and other advantages over its competitors, such as aluminium, magnesium and stainless steel. In past decades, titanium matrix composites served in broad areas, including aerospace, military, automobile and biomedical industries. In this project, a revised powder metallurgy method, which contains cold isostatic pressing and hot isostatic pressing, was adopted to refine the microstructure of monolithic titanium. It was also used to manufacture titanium matrix composites. TiH2 powder was selected as the starting material to form Ti matrix and the reinforcements were sub-micron and nano-metric TiB particles. Mechanical properties and microstructure of commercial titanium composites exhaust valves from Toyota Motor Corporation have been studied as the reference of properties of titanium composites manufactured in this project. It has been shown that tensile strength and hardness of exhaust valves increase about 30% than those of similar matrix titanium alloys. Examination on powder starting materials of this project was also carried out, especially the dehydrogenation process shown in the DSC result. Mechanical properties and microstructures of titanium matrix composites samples in this project, as related to the process parameter, have also been investigated. The density of these samples reached 96% of theoretical one but cracks were found through out the samples after sintering. Fast heating rates during the processing was suspected to have caused the crack formation, since the hydrogen release was too fast during dehydrogenation. Hardness testing of sintered samples was carried out and the value was comparable and even better than that of commercial exhaust valves and titanium composites in literature. Microstructure study shows that the size of reinforcements increased and the size of grains decreased as the increasing amount of TiB reinforcements. And this condition also resulted in the increasing amount of the acicular alpha structure.
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Tesha, Joseph Valerian. "Processing of SiC/titanium metal matrix composites." Thesis, Cranfield University, 1993. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.358232.

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Pollard, Sarah Louise. "Processing and properties of titanium metal matrix composites." Thesis, University of Birmingham, 2011. http://etheses.bham.ac.uk//id/eprint/7605/.

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This thesis addresses aspects of the development of both processing methods and the assessment of the mechanical properties of titanium metal matrix composites in order for the material to be introduced with confidence into aero-engine applications. Assessment of the SM1140+ fibre has been carried out and compared with the SCS-6 and Trimarc fibres in order to gain an appreciation of the performance of these fibres in relation to each other to aid fibre selection and to aid further development of composite components. The SM1140+ fibre is found to fail almost always from the core and is consistent with a statistical distribution that can be modelled by a unimodal Weibull approach. The development of the SM2156 fibre was made in an effort to produce both a UK source and a lower cost source of fibre. Mechanical testing of fibre in both as-received and composite form revealed a decrease in strength when compared with results for the virgin, uncoated fibre and by deduction from SCS-6 composite mechanical behaviour. The deterioration of fibre properties appears to be caused by the rough surface of the SiC fibre causing a ‘keying’ effect that inhibits interfacial sliding. The high rate sputtering deposition process has been developed in order to obtain an alternative, lower cost method of producing matrix coated fibre. Testing of the MCF showed a mild deterioration of fibre strength during processing (due to fibre spooling), but still demonstrated the composite shows potential for production given further development.
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Jong, Edwin Nyon Tchan. "Particulate-reinforced metal matrix composites based on titanium alloys." Thesis, Imperial College London, 1992. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.261498.

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Dear, Matthew Nicholas. "Fatigue in SiC fibre reinforced titanium metal matrix composites." Thesis, University of Birmingham, 2016. http://etheses.bham.ac.uk//id/eprint/6603/.

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The fatigue and interfacial characteristics of a unidirectional, SiC (SCS 6), fibre reinforced Ti 6Al 4V metal matrix composite have been investigated using a series of fatigue crack propagation, total life, and interfacial characterisation techniques. A room temperature crack arrest to catastrophic failure (CA/CF) transition was quantified using the initial stress intensity factor range ΔKapp. This transition occurred between 21 and 18 MPa√m in the three point bend geometry, and was found to be dependent on volume fraction of intact fibres bridging the crack. Increasing the test temperature to 300˚C had different effects on the resistance to fatigue crack growth depending on crack opening displacements and test piece stiffness. Total life fatigue tests revealed that the dominant failure mechanism was matrix fatigue cracking and fibre bridging. The extent of fatigue crack growth and fibre bridging was dependant on the applied stress and test temperature. The introduction of a dwell period at maximum load resulted in a small reduction in the total fatigue life. Post fatigue fibre push out tests identified that fatigue caused a reduction of interfacial properties below the as received levels. This reduction of interfacial properties was dependent on fatigue test temperature and initial loading conditions.
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Hunt, Michael Patrick. "Pressureless Densification of Alumina - Titanium Diboride Ceramic Matrix Composites." Thesis, Virginia Tech, 2009. http://hdl.handle.net/10919/31326.

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The research focus was to determine diffusion mechanisms responsible for densification behavior of SHS produced Al2O3/TiB2 Ceramic Matrix Composites (CMCs). Previous research has shown SHS produced Al2O3/TiB2 composites exhibited unique microstructural properties that contributed to high strength, fracture toughness, and hardness properties. Pressureless densification of SHS produced Al2O3/TiB2 composites would provide a cost savings because the equipment for pressureless densification is less expensive and less complicated than equipment required for densification with pressure. Models for sintering of CMCs and calculation of Sintering Time Constants (STC) were used to predict the densification behavior of the SHS produced Al2O3/TiB2 composite. The Levin, Dirnfeld, Shwam equation was used to determine the Rate Controlling Diffusion Mechanism (RCDM) and activation energy for sintering. X-Ray Diffraction (XRD) analysis of the as-milled reaction product powder revealed the presence of an aluminum borate (Al18B4O33) as a third phase, as well as, in pressureless heat treated samples. Based on experimental results and analysis, it seemed possible the Al18B4O33 compound may have formed by reaction of Al2O3 with TiB2 along their interfaces. Aluminum borates have been observed to form Al18B4O33 (s) + B2O3 (l) at temperatures above 1000°C. The RCDM for densification of SHS produced Al2O3/TiB2 was found to be liquid phase diffusion with volume diffusion also likely being active during densification. In addition, Al18B4O33 seemed to be the preferred compound formed during oxidation. Further research should be performed to control formation of Al18B4O33; as well as, on the oxidation behavior of the SHS produced Al2O3/TiB2.
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Marte, Judson Sloane. "High temperature flow behavior of titanium aluminide intermetallic matrix composites /." This resource online, 1996. http://scholar.lib.vt.edu/theses/available/etd-11012008-063708/.

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Patil, Amit k. "ADVANCED PROCESSING OF NICKEL-TITANIUM-GRAPHITE BASED METAL MATRIX COMPOSITES." Cleveland State University / OhioLINK, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=csu1560298763233401.

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Marte, Judson Sloan. "High temperature flow behavior of titanium aluminide intermetallic matrix composites." Thesis, Virginia Tech, 1996. http://hdl.handle.net/10919/45422.

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Al₃Ti, Al₅CuTi₂, and Al₆₆Mn₁₁Ti₂₃, intermetallic matrices reinforced with 30, 40, and 50 volume % TiB, have been produced by XD™ processing and densified into bulk form by powder metallurgy techniques. The compressive flow behavior of the Al₃Ti and Al₅CuTi₂, composites have been evaluated at temperatures ranging from 1000°C to 1200°C and strain rates of 0.0001 and 0.001 sec⁻¹. The results have been analyzed by a correlation to the resulting microstructure, especially with regards to the intermetallic matrix composition, TiB₂ size, and interparticle spacing. The results of these analyses are applied to a constitutive equation based upon the flow stress equation. It has been shown that at in this temperature regime, all deformation occurs within the intermetallic matrix. This is substantiated by the lack of TiB₂-dependent behavior with variations in volume percentage of reinforcement. In all cases, the composites are readily deformed at relatively low loads. The average strain-rate sensitivity values were 0.349 for the Al₃Ti-based composites, and 0.247 for the Al₅CuTi₂, variants. The average activation energies were calculated to be 485 kJ/mol and 920 kJ/mol for the Al₃Ti-and Al₅CuTi₂-matrices, respectively. The structure constant was calculated based upon these values. The Zener-Hollomon parameter was used to plot the flow stress along lines of constant temperature and strain rate, and serves as one type of constitutive equation. In addition, the flow stress was evaluated as a function of the strain rate and temperature. These models were found to provide adequate correlation to the measured flow behavior.
Master of Science
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Baker, Adam M. "Interfacial and processing studies in Ti/SiC metal matrix composites." Thesis, University of Oxford, 1998. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.301852.

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Books on the topic "Titanium matrix composites (TMCs)"

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Huang, Lujun, and Lin Geng. Discontinuously Reinforced Titanium Matrix Composites. Singapore: Springer Singapore, 2017. http://dx.doi.org/10.1007/978-981-10-4449-6.

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North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Characterisation of fibre reinforced titanium matrix composites. Neuilly sur Seine, France: AGRD, 1994.

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North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Characterisation of fibre reinforced titanium matrix composites. Neuilly sur Seine, France: AGARD, 1994.

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Johnson, S., J. Larsen, and B. Cox, eds. Life Prediction Methodology for Titanium Matrix Composites. 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959: ASTM International, 1996. http://dx.doi.org/10.1520/stp1253-eb.

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Johnson, W. S. Fatigue damage growth mechanisms in continuous fiber reinforced titanium matrix composites. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.

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Johnson, W. S. Fatigue damage growth mechanisms in continuous fiber reinforced titanium matrix composites. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.

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Johnson, W. S. Damage development in titanium metal matrix composites subjected to cyclic loading. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1992.

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Ding, Wei. Modelling and experimental studies of damage in titanium metal matrix composites. Birmingham: University of Birmingham, 1997.

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Ibbotson, Andrew Robert. Fatigue crack growth in continuous fibre reinforced titanium alloy matrix composites. Birmingham: University of Birmingham, 1994.

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Castelli, Michael G. Thermomechanical and isothermal fatigue behavior of a (90) titanium matrix composite. Cleveland, Ohio: Lewis Research Center, National Aeronautics and Space Administration, 1993.

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Book chapters on the topic "Titanium matrix composites (TMCs)"

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Lütjering, Gerd, and James C. Williams. "Titanium Matrix Composites." In Titanium, 313–28. Berlin, Heidelberg: Springer Berlin Heidelberg, 2003. http://dx.doi.org/10.1007/978-3-540-71398-2_9.

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Gieskes, Sebastiaan A., and Marten Terpstra. "Reinforced Composites Based on Titanium." In Metal Matrix Composites, 80–93. Dordrecht: Springer Netherlands, 1991. http://dx.doi.org/10.1007/978-94-011-3666-2_2.

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Leyens, C., J. Hausmann, and J. Kumpfert. "Continuous Fiber Reinforced Titanium Matrix Composites: Fabrication, Properties and Applications." In Titanium and Titanium Alloys, 305–31. Weinheim, FRG: Wiley-VCH Verlag GmbH & Co. KGaA, 2005. http://dx.doi.org/10.1002/3527602119.ch12.

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Huang, Lujun, and Lin Geng. "Introduction." In Discontinuously Reinforced Titanium Matrix Composites, 1–15. Singapore: Springer Singapore, 2017. http://dx.doi.org/10.1007/978-981-10-4449-6_1.

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Huang, Lujun, and Lin Geng. "Design and Fabrication of Network-Structured Pure Ti Matrix Composites." In Discontinuously Reinforced Titanium Matrix Composites, 17–38. Singapore: Springer Singapore, 2017. http://dx.doi.org/10.1007/978-981-10-4449-6_2.

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Huang, Lujun, and Lin Geng. "Microstructure Characteristics of Ti6Al4V Matrix Composites with Network Microstructure." In Discontinuously Reinforced Titanium Matrix Composites, 39–55. Singapore: Springer Singapore, 2017. http://dx.doi.org/10.1007/978-981-10-4449-6_3.

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Huang, Lujun, and Lin Geng. "Mechanical Behaviors of Network-Structured TiBw/Ti64 Composites." In Discontinuously Reinforced Titanium Matrix Composites, 57–74. Singapore: Springer Singapore, 2017. http://dx.doi.org/10.1007/978-981-10-4449-6_4.

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Huang, Lujun, and Lin Geng. "Hot Deformation Behaviors of TiBw/Ti6Al4V Composites with Network Microstructure." In Discontinuously Reinforced Titanium Matrix Composites, 75–107. Singapore: Springer Singapore, 2017. http://dx.doi.org/10.1007/978-981-10-4449-6_5.

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Huang, Lujun, and Lin Geng. "Effects of Heat Treatment on Microstructure and Properties of TiBw/Ti6Al4V Composites." In Discontinuously Reinforced Titanium Matrix Composites, 109–22. Singapore: Springer Singapore, 2017. http://dx.doi.org/10.1007/978-981-10-4449-6_6.

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Huang, Lujun, and Lin Geng. "TiCp/Ti6Al4V and (TiCp+TiBw)/Ti6Al4V Composites with Network Architecture." In Discontinuously Reinforced Titanium Matrix Composites, 123–45. Singapore: Springer Singapore, 2017. http://dx.doi.org/10.1007/978-981-10-4449-6_7.

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Conference papers on the topic "Titanium matrix composites (TMCs)"

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Li, Yunze, Dongzhe Zhang, and Weilong Cong. "Ultrasonic Vibration-Assisted Laser Directed Energy Deposition of B4C-Ti Composite: Effect of Laser Power and Ultrasonic Vibration." In ASME 2021 16th International Manufacturing Science and Engineering Conference. American Society of Mechanical Engineers, 2021. http://dx.doi.org/10.1115/msec2021-60388.

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Abstract Compared with pure titanium, ceramic reinforced titanium matrix composites (TMCs) have the advantages of higher microhardness, higher wear resistance, and better load endurance properties, which enable their further applications under severe friction and cyclic loading conditions. B4C-Ti composite, as a kind of TMCs, has been fabricated by laser directed energy deposition (DED) technology. However, there are still some problems needed to be solved. First, the B4C particles are not fully melted. It suppresses the reactions between B4C and titanium and reduced the generation of TiB and TiC during the fabrication, which deteriorates the hardness of the B4C-Ti composite. Second, the reinforcement materials are not evenly distributed in the titanium matrix, which damages the performance of the B4C-Ti composite. In this study, B4C-Ti composite parts are fabricated by the ultrasonic vibration-assisted laser DED process. The effects of laser power and ultrasonic vibration on the phase compositions, microstructure, and hardness are investigated.
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Baik, K. H., and P. S. Grant. "Optimisation of Concurrent Fibre Winding and Low Pressure Plasma Spraying for the Manufacture of Titanium Matrix Composite Rings." In ITSC 1998, edited by Christian Coddet. ASM International, 1998. http://dx.doi.org/10.31399/asm.cp.itsc1998p1193.

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Abstract A concurrent fibre winding and low pressure plasma spraying (LPPS) process has been developed to manufacture multiple fibre reinforced titanium matrix composite (TMC) rings in a single spraying operation. Optimisation of the LPPS parameters has been successively performed for two different sizes of Ti-6Al-4V powders by experimental design and statistical analysis, which provided minimum porosity and surface roughness for both powders. The most important LPPS parameters affecting porosity and surface roughness of deposits were Ar gas flow rate and chamber pressure. During TMC manufacture, the coarse Ti-6Al-4V powder spraying provided enhanced infiltration between fibres but caused degradation of fibre tensile strength, as well as a rough ring surface. The fine Ti-6Al-4V powder gave no significant degradation of fibre strength and a relatively smooth ring surface. Four-ply SiC fibre reinforced TMCs manufactured by the spray-wind process have also been evaluated in terms of porosity, fibre distribution and fibre damage.
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Rohan, Pavel, Marie Kolaříková, Stanislav Krum, Zdeněk Hazdra, Josef Šepitka, and Jiří Kuchař. "Pulsed-PTA Preparation of B4C-Based Titanium Matrix Cermet." In ITSC2021, edited by F. Azarmi, X. Chen, J. Cizek, C. Cojocaru, B. Jodoin, H. Koivuluoto, Y. C. Lau, et al. ASM International, 2021. http://dx.doi.org/10.31399/asm.cp.itsc2021p0298.

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Abstract Pulsed plasma transferred arc surfacing is presently used in many industrial applications to make protective layers against corrosion, temperature exposition, and excessive wear. Increasing wear resistance is especially important in areas of industry where titanium alloys are used, such as aviation and cosmonautics, because the wear resistance of titanium alloys is often weak. One way to increase the wear resistance is to deposit or form a cermet with a titanium matrix (TMC) on the surface of the part. The present study deals with the fabrication and characterization of TMC based on B4C. TMC with B4C was formed by cofeeding Ti6Al4V and B4C powder into a melting pool. It has been found that the deposited, relatively thick layers have homogeneously dispersed B4C grains in the matrix. The deposits are metallurgically connected to the substrate - Ti6Al4V. The TMCs were investigated in terms of microstructure and chemical composition. Wear resistance was determined using the linear pin test.
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Singerman, S. A., and J. J. Jackson. "Titanium Metal Matrix Composites for Aerospace Applications." In Superalloys. TMS, 1996. http://dx.doi.org/10.7449/1996/superalloys_1996_579_586.

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Castelli, Michael G., and John Gayda. "An Overview of Elevated Temperature Damage Mechanisms and Fatigue Behavior of a Unidirectional SCS-6/Ti-15-3 Composite." In ASME 1993 Design Technical Conferences. American Society of Mechanical Engineers, 1993. http://dx.doi.org/10.1115/detc1993-0075.

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Abstract The fatigue behavior of a unidireclionally reinforced titanium matrix composite (TMC), SiC/Ti-15-3, was thoroughly characterized to support life prediction modeling of advanced TMC disks designed for gas turbine engine rotor applications. The results of this coupon-level experimental investigation are reviewed in this paper. On a stress basis, the isothermal fatigue behavior of the [0°] TMC revealed significant improvements over the unreinforced matrix. In contrast, the [90°] TMC exhibited degraded properties and lives for similar comparisons. This was attributed to the weak fiber/matrix interfacial bond. Encasing the [0°] TMC with a Ti-15-3 case did not affect isothermal fatigue lives at higher strain levels. However, at lower strain levels, relatively rapid initiation and propagation of large fatigue cracks in the case degraded the fatigue lives. Thermomechanical fatigue (TMF) lives were significantly reduced for the [0°] TMC when compared to isothermal lives. At high strains, in-phase TMF produced extremely short lives. This degradation was attributed to fiber overload failures bought about by stress relaxation in the matrix. At low strains, out-of-phase TMF conditions became life-limiting. Environment-assisted surface cracking was found to accelerate fatigue failure. This produced extensive matrix damage with minimal fiber damage. For the [90°] TMC, TMF conditions did not promote an additional degradation in cyclic life beyond that observed under isothermal conditions.
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Baldini, S. Eric, David J. Tubbs, and William A. Stange. "Embedding fiber optic sensors in titanium matrix composites." In San Jose - DL tentative, edited by Richard O. Claus and Eric Udd. SPIE, 1990. http://dx.doi.org/10.1117/12.24856.

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BALDINI, S., and WILLIAM STANGE. "Development of fiber optic sensors for titanium matrix composites." In 2nd International Aerospace Planes Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1990. http://dx.doi.org/10.2514/6.1990-5237.

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Smith, Robert A. "High Frequency Ultrasonic NDE of Titanium Metal Matrix Composites." In QUANTITATIVE NONDESTRUCTIVE EVALUATION. AIP, 2006. http://dx.doi.org/10.1063/1.2184639.

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Pouzet, S., P. Peyre, C. Gorny, O. Castelnau, T. Baudin, F. Brisset, C. Colin, and P. Gadaud. "Direct metal deposition of titanium matrix composites using B4C powder." In ICALEO® 2015: 34th International Congress on Laser Materials Processing, Laser Microprocessing and Nanomanufacturing. Laser Institute of America, 2015. http://dx.doi.org/10.2351/1.5063239.

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Elumalai, N., M. K. Karthik, V. Giridharan, and C. Suresh Kumar. "Mechanical properties of titanium carbide reinforced aluminum metal matrix composites." In INTERNATIONAL CONFERENCE ON MECHANICAL, ELECTRONICS AND COMPUTER ENGINEERING: ICMECE 2020. AIP Publishing, 2020. http://dx.doi.org/10.1063/5.0024764.

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Reports on the topic "Titanium matrix composites (TMCs)"

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Wiezorek, Joerg M., and Michael J. Mills. Microstructural Characterization of Interfaces in SiC-Reinforced Titanium Alloy-Matrix Composites. Fort Belvoir, VA: Defense Technical Information Center, July 1998. http://dx.doi.org/10.21236/ada351754.

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Ghonem, H., and D. Osborne. High-Temperature Interphase Properties of SiC Fiber Reinforced Titanium Metal Matrix Composites. Fort Belvoir, VA: Defense Technical Information Center, October 1996. http://dx.doi.org/10.21236/ada326145.

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Ghonem, Hamouda. Durability and Damage Tolerance of High Temperature Advanced Titanium Metal Matrix Composites. Fort Belvoir, VA: Defense Technical Information Center, August 2000. http://dx.doi.org/10.21236/ada382904.

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Rangaswamy, P., M. A. M. Bourke, R. Von Dreele, K. Bennett, J. A. Roberts, M. Daymond, and N. Jayaraman. Texture and residual strain in SiC/Ti-6-2-4-2 titanium matrix composites. Office of Scientific and Technical Information (OSTI), December 1998. http://dx.doi.org/10.2172/350859.

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Osborne, D., and H. Ghonem. Experimental and Computational Study of Interphase Properties and Mechanics in Titanium Metal Matrix Composites at Elevated Temperatures. Fort Belvoir, VA: Defense Technical Information Center, March 2005. http://dx.doi.org/10.21236/ada438848.

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