Relevant bibliographies by topics / Metal Matrix Composite (MMC)

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

Academic literature on the topic 'Metal Matrix Composite (MMC)'

Author: Grafiati
Published: 4 June 2021
Last updated: 16 June 2025

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Journal articles on the topic "Metal Matrix Composite (MMC)"

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Dilip Raja, N., R. Velu, S. T. Selvamani, and K. Palani Kumar. "The Comparative Analysis of Mechanical Properties on MMC (AA6061 + SiCp 10% wt) before and after Age Hardening." Applied Mechanics and Materials 766-767 (June 2015): 276–80. http://dx.doi.org/10.4028/www.scientific.net/amm.766-767.276.

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Discontinuously reinforced SiCp/Al composites were extensively used in space applications including joints and attachment fittings for truss structures, electronic packages, thermal planes, mechanism housing and bushing. In this research work, the metal matrix composite of AA6061+ SiCp10% were produced by stir casting method with an aim to predict the mechanical properties of a Metal Matrix Composite (MMC) subjected to age hardening. The Ultimate tensile test and Vickers hardness test was carried on the both condition of produced MMC and Age hardened (HMMC). A comparative study of the mechanical properties of the MMC before and after age hardening has been reported.
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Ghias, A. Siddique Ahmed, and B. Vijaya Ramnath. "Investigation of Tensile Property of Aluminium SiC Metal Matrix Composite." Applied Mechanics and Materials 766-767 (June 2015): 252–56. http://dx.doi.org/10.4028/www.scientific.net/amm.766-767.252.

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The composite material is a combination of two or more materials with different physical and chemical properties. The composite has superior characteristics than those individual components. A hybrid composite is the one which contains at least three materials. When the matrix material is a metal, the composite is termed as metal matrix composites (MMC). The MMC is a composite material with two constituent parts, one being a metal. The other material may be another metal, ceramic or fiber. Among all the MMC’s, Aluminium is the most widely used matrix material due to its light weight, high strength and hardness. This paper deals with the fabrication and mechanical investigation of hybrid metal matrix composite Al - SiC. The fabrication is done by stir casting by adding the required quantities of additives into the stirred molten Aluminium. The results show significant effect of mechanical properties such as tensile strength, yield stress and flexural strength. The internal structure of the composite is observed using Scanning electron microscope (SEM) and found that are formation of pores in them.
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Bedolla-Becerril, Egberto, Josefina Garcia-Guerra, Víctor H. Lopez-Morelos, et al. "Tribological Behaviour of Al-2024/TiC Metal Matrix Composites." Coatings 13, no. 1 (2022): 77. http://dx.doi.org/10.3390/coatings13010077.

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Pin-on-disk tests were performed to evaluate the wear behaviour of a 2024 aluminium alloy metal matrix composite (MMC) reinforced with 52 vol.% of TiC particles (Al-2024/TiC) in a fabricated and thermal-treated (T6) condition. The MMC was produced via pressureless infiltration of partially sintered TiC preforms with an average particle size of 1.1 μm at 1200 °C for 2 h under flowing argon. Microstructural and mechanical characterisation were carried out on both the monolithic alloy (MM) and the MMC with and without heat treatment. The effect of T6 heat treatment on the tribological behaviour of MMC has been investigated under dry sliding wear conditions under normal loads of 2, 5 and 10 N against ceramic α-Al2O3 and SAE 52100 steel spherical counterparts. Results indicate a substantial improvement in the microhardness (289–343 HV), hardness (25–34 HRC), and wear resistance of the MMC after T6 heat treatment (1 × 10−3 to 5 × 10−5 mm3/Nm). For a better understanding of the wear mechanisms, surfaces of the worn tracks were studied. Oxidation and abrasion were found as the dominant wear mechanisms in both MM and MMC samples. Even though MM exhibited a lower coefficient of friction (COF) (0.50–0.80), composites showed superior wear resistance by 5-fold higher than the base alloy.
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Martides, Erie, Candra Dewi Romadhona, Djoko Hadi Prajitno, and Budi Prawara. "Pengaruh Proses Oksidasi Lapisan Metal Matrix Composite pada Substrat SS316." JTERA (Jurnal Teknologi Rekayasa) 4, no. 2 (2019): 277. http://dx.doi.org/10.31544/jtera.v4.i2.2019.277-282.

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Material SS316 seringkali digunakan untuk komponen yang bekerja pada temperatur tinggi dengan resiko mengalami oksidasi yang menyebabkan penurunan sifat material dan umur pakai dari komponen. Deposisi Metal Matrix Composite (MMC) NiCr+Cr3C2+Al2O3 dan NiCr+WC12Co+Al2O3 menggunakan metode High Velocity Oxygen Fuel (HVOF) thermal spray coating dengan parameter konstan dilakukan sebagai proses perlakuan pada permukaan SS316 untuk meningkatkan nilai kekerasan dan ketahanan terhadap oksidasi. Tujuan penelitian ini adalah untuk mengetahui pengaruh proses oksidasi lapisan MMC pada material substrat SS316. Proses oksidasi dilakukan dengan variasi temperatur 500° dan 600°C, penahanan temperatur selama 6 jam, kemudian diteruskan dengan karakterisasi serta perhitungan laju oksidasi. Hasil penelitian menunjukkan spesimen MMC NiCr+Cr3C2+Al2O3 yang dilakukan proses oksidasi pada suhu 500°C memiliki laju oksidasi terendah yaitu 6,67 x 10-7 gram/mm2 jam.
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Nandakumar, A., and D. Dinakaran. "Effect of Nanoparticles in Reinforced Metal Matrix Composite on the Machinability Characteristics - A Review." Applied Mechanics and Materials 813-814 (November 2015): 625–28. http://dx.doi.org/10.4028/www.scientific.net/amm.813-814.625.

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Metal Matrix nanoComposites (MMNC) refer to materials consisting of a ductile metal or alloy matrix in which some nanosized reinforcement materials is implanted. These materials combine metal and ceramic features, i.e., ductility and toughness with high strength. Thus, metal matrix nanocomposites are suitable for production of materials with high strength in shear/compression processes and high service temperature capabilities. Both Metal Matrix Composite (MMC) and Ceramic Matrix Composites (CMC) with Carbon nanoTubes (CNT) nanocomposites hold promise, but also pose challenges for real success. In the present paper deals an inclusive review of literature in effect of nanoparticles in reinforced metal matrix composites on the machinability characteristics of the composite materials.
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FUKUMOTO, I., S. MEKARU, S. SHIBATA, and K. NAKAYAMA. "MMC-08: Fabrication of Composite Material Using Alumina Agglomerated Sludge and Aluminum Powder by Spark Plasma Sintering(MMC-II: METALS AND METAL MATRIX COMPOSITES)." Proceedings of the JSME Materials and Processing Conference (M&P) 2005 (2005): 9. http://dx.doi.org/10.1299/jsmeintmp.2005.9_3.

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Aminnudin, Aminnudin, and Moch Agus Choiron. "Heat treatment effect on metal matrix composite with brass matrix and fly ash." MATEC Web of Conferences 204 (2018): 05020. http://dx.doi.org/10.1051/matecconf/201820405020.

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Metal matrix composite (MMC) is a combination of two or more materials using metal as a matrix. In this paper we used brass as the matrix and fly ash as for the particle. The fly ash used is fly ash which is produced from coal combustion in the Paiton power plant. Fly ash composition in the MMC are 5% and 10%. The MMC was produced with gas furnace. Heat tratment to MMC was done at 350 and 400 °C.Hard testing process, tensile test and impack test are carried out at MMC before heat treatment and after heat treatment. From the test results showed an increase in hardness, tensile strength and impact test showed the heat treatment process at a temperature of 350 °C. Heat treatment at a temperature of 400 °C does not improve the mechanical properties of MMC
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Manikandan., K., K. Karthikraja., A. Murali., V. Prithiviraj., and S. Saravanan. "Experimental and Investigation of Wheel Hub by using Aluminium and Magnesium Composite Material and Evaluate the Mechanical Properties." International Journal of Multidisciplinary Research Transactions 5, no. 5 (2023): 44–55. https://doi.org/10.5281/zenodo.7882947.

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Metal Matrix Composites (MMC’s) have been developed to meet the demand for lighter materials with high specific strength, and wear resistance. Among Metal matrix composites particulate reinforced aluminium and magnesium composites are attractive due to significant improvements in mechanical and physical properties. In this work, an effort has been designed to raise the reliability of using Al-Mg composites with other alternatively materials for wheel hub. This paper analysis the wheel hub material on mechanical properties of the Al-Mg composite material by using composite model plate evaluate the mechanical properties.
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Dybowski, B., T. Rzychoń, B. Chmiela, and A. Gryc. "The Microstructure of WE43 MMC Reinforced with SiC Particles." Archives of Metallurgy and Materials 61, no. 1 (2016): 393–98. http://dx.doi.org/10.1515/amm-2016-0072.

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It is well known that the properties of a metal matrix composites depend upon the properties of the reinforcement phase, of the matrix and of the interface. A strong interface bonding without any degradation of the reinforcing phase is one of the prime objectives in the development of the metal matrix composites. Therefore, the objective of this work is to characterize the interface structure of WE43/SiC particles composite. Magnesium alloys containing yttrium and neodymium are known to have high specific strength, good creep and corrosion resistance up to 250°C. The addition of SiC ceramic particles strengthens the metal matrix composite resulting in better wear and creep resistance while maintaining good machinability. In the present study, WE43 magnesium matrix composite reinforced with SiC particulates was fabricated by stir casting. The SiC particles with 15 μm, 45 μm and 250 μm diameter were added to the WE43 alloy. The microstructure of the composite was investigated by optical microscopy, scanning electron microscopy, scanning transmission electron microscopy and XRD analysis. YSi and Y2Si reaction products are observed at the interfaces between SiC particles and WE43 matrix in the composite stirred at 780°C. Microstructure characterization of WE43 MMC with the 45 μm, stirred at 720°C showed relative uniform reinforcement distribution. Moreover, the Zr-rich particles at particle/matrix interface were visible instead of Y-Si phases. In the case of composite with 15 μm particles the numerous agglomerates and reaction products between SiC particles and alloying elements were observed. The presence of SiC particles assisted in improving hardness and decreasing the tensile strength and plastic properties.
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HASAN, R., I. JAUHARI, H. OGIYAMA, S. M. YUNUS, R. D. RAMDAN, and N. R. N. MASDEK. "MMC-02: Kinetic Study on Boronized Duplex Stainless Steel(MMC-I: METALS AND METAL MATRIX COMPOSITES)." Proceedings of the JSME Materials and Processing Conference (M&P) 2005 (2005): 4. http://dx.doi.org/10.1299/jsmeintmp.2005.4_4.

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Dissertations / Theses on the topic "Metal Matrix Composite (MMC)"

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Abdullah, Abu. "Machining of aluminium based Metal Matrix Composite (MMC)." Thesis, University of Warwick, 1996. http://wrap.warwick.ac.uk/34661/.

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The machining of aluminium 2618 particulate reinforced Metal Matrix Composite (MMC) with 18 vol. % silicon carbide (SiC) using cemented carbide cutting tools has been undertaken. Two grades of cemented carbide inserts, uncoated K68 grade and coated KC910 grade (coated with TiC and A1203) having negative and positive rake angles (with and without chip breaker) have been used to machine this material in order to understand the machining process, tool failure modes and wear mechanisms. Turning tests in the speed range 15 - 10 m/min have been carried out at 0.2,0.4 and 0.6 mm/rev feed rates and 2 mm and 4 mm depths of cut. Both cemented carbide tools have been shown to be capable of machining the MMC and give reasonable tool lives. Low speed and high feed rate are found to be a good combination in order to machine this material effectively. Coated KC910 grade inserts with negative rake angle gave the best performance. The use of a chip breaker has no significant effect on the machining process of the NMC because the material is one which inherently short chips due to ductility limitations caused by the particles. Tool failure mode studies showed that the tools failed by flank wear. Tool wear mechanism analysis indicated that abrasion wear was the tool life controlling factor under all cutting conditions. The tool wear is related to the direct contact between the abrasive hard SiC particles and the cutting edge and their relative motion to the rake and clearance face. Hence, the hardness of the SiC particles is a dominant factor for the tool wear. Two separatem odels of abrasio. n haye.b een suggested.B uilt-up edge (BUE) which has a distinct shape was more pro i1ounced at lower cutting speeds, high feed rates and greater depth of cut. The presence of BUE has been found to increase tool life and reduce tool wear but at the expense of surface finish. The increase in tool life or reduction in tool wear is likely due to the protective layer that the BUE formed on the tool surface preventing a direct contact between the tool and chip. Linear regression analysis showed that the value of Taylor exponent n is high (0.8-1.0) compared to the values of n (0.2-0.3) obtained when machining steel. This indicates that the tool life is less sensitive to cutting speed for MMC than it is for steel.
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Daymond, Mark Richard. "Evolution of internal stresses in a whisker reinforced MMC undergoing thermal cycling." Thesis, University of Cambridge, 1996. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.266242.

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Coelho, Reginaldo Teixeira. "The machinability of aluminium-based SiC reinforced metal matrix composite (MMC) alloy with emphasis on hole production." Thesis, University of Birmingham, 1995. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.340966.

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Li, Maojun. "Drilling of carbon fibre reinforced plastic (CFRP) and metal matrix composites (MMC)." Thesis, University of Birmingham, 2015. http://etheses.bham.ac.uk//id/eprint/5953/.

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The use of carbon fibre reinforced plastic (CFRP) and metal matrix composites (MMC) is steadily increasing as an alternative to traditional metallic materials in various industrial sectors. The overall aim of the project is to assess the machinability when drilling epoxy based CFRP and Al/SiCp MMC composites and understand its effects on feature quality and workpiece integrity. Specific objectives of the project relate to establishing preferred/optimum operating parameters (cutting speed, feed rate and drill strategies) and investigating the influence of cutting environment (dry, chilled air, high pressure internal/external supplied coolant and low pressure flood) for drilling specific composite material systems. Key response measures include tool wear/life, thrust force/torque, hole size and geometrical accuracy, hole edge quality (delamination, uncut fibres and burrs) as well as workpiece surface integrity (surface roughness, microhardness, fibre/particle pullout, subsurface damage, etc.). The latest cutting tool materials and advanced diamond coatings, drill geometry and design format (e.g. domed PCD) were assessed in an attempt to improve productivity levels, tool life and hole quality. Tool wear mechanisms and its effect on hole surface quality were also investigated.
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Kenningley, Scott David Peter. "High temperature thermal and mechanical load characterisation of a steel fibre reinforced aluminium metal matrix composite (AlMMC) for automotive diesel pistons." Thesis, University of Manchester, 2014. https://www.research.manchester.ac.uk/portal/en/theses/high-temperature-thermal-and-mechanical-load-characterisation-of-a-steel-fibre-reinforced-aluminium-metal-matrix-composite-almmc-for-automotive-diesel-pistons(5cc789fc-d64e-4905-bc1c-beb0e3b9c0df).html.

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In modern automotive engines, the vast majority of light vehicle diesel (LVD) pistons are made from gravity die cast monolithic AlSi based alloy systems. Presently, the market drivers for reduced emissions, more efficient fuel consumption and increased specific power output are providing cyclic thermal and mechanical fatigue loading above the safe life durability threshold for the current AlSi based alloy systems. Peak temperatures in the diesel piston’s fatigue critical combustion bowl region are presently 420 °C for the AlSi based alloys, which represents a homologous TH value in excess of 0.8. In combination with peak temperatures of 420 C, the pistons are subject to cylinder pressures up to 220 bar, inducing mechanical stress amplitudes 15-20% greater than the allowable component fatigue strength for 1x108 cycles, in some applications. This durability deficit naturally leads to a requirement for new material and process solutions aimed at improving thermal and mechanical fatigue resistance at temperatures in excess of 420 C.One solution to this problem is to locally reinforce the pistons combustion bowl edge with a metal matrix composite (MMC) system. In this study, an aluminium based metal matrix composite (AlMMC) has been investigated and has shown some promise with increases in iso-thermal high cycle (1x 107) fatigue strength of 50 % compared to standard monolithic piston alloys. The AlMMC consists of a premium AlSi based LVD piston alloy matrix reinforced with 0.15 Vf of an interconnected network of 2-4 mm long Fe based fibres. The AlMMC is manufactured by pressure assisted infiltration of a sintered metallic fibre preform with as cast materials having a pore density of 0.2 %. In contrast to the use of ceramic fibre reinforcement systems generally requiring high pressure infiltration techniques, preform infiltration is considered possible with a comparably inexpensive manufacturing route. The Fe based fibre preforms can be infiltrated at lower pressure due to the reactivity between the Fe based fibres and the AlSi based matrix alloy. Unfortunately, this increased reactivity, although an advantage for preform infiltration, can result in (FeAlXX)Si(+X) interfacial reaction products forming between the fibre and matrix at operating temperatures of greater than 440 °C. These interfacial reactions result in a 15-20 m interfacial intermetallic layer after prolonged periods of exposure (>500 hrs), resulting in depleted fibre Vf and void formations on the matrix side of the interface.
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Xia, Ji. "TENSION AND FATIGUE BEHAVIOR OF AL-2124/SIC-PARTICULATE METAL-MATRIX COMPOSITES." Case Western Reserve University School of Graduate Studies / OhioLINK, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=case1548169132710822.

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Pallikonda, Mahesh Kumar Pallikonda. "FORMING A METAL MATRIX NANOCOMPOSITE (MMNC) WITH FULLY DISPERSED AND DEAGGLOMERATED MULTIWALLED CARBON NANOTUBES (MWCNTs)." Cleveland State University / OhioLINK, 2017. http://rave.ohiolink.edu/etdc/view?acc_num=csu1503937490966191.

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Tu, Zhiqiang. "Fabrication and Mechanical Properties of Carbon Fiber Reinforced Aluminum Matrix Composites by Squeeze Casting." Thesis, Université d'Ottawa / University of Ottawa, 2020. http://hdl.handle.net/10393/40523.

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Rapid modern technological changes and improvements bring great motivations in advanced material designs and fabrications. In this context, metal matrix composites, as an emerging material category, have undergone great developments over the past 50 years. Their primary applications, such as automotive, aerospace and military industries, require materials with increasingly strict specifications, especially high stiffness, lightweight and superior strength. For these advanced applications, carbon fiber reinforced aluminum matrix composites have proven their enormous potential where outstanding machinability, engineering reliability and economy efficiency are vital priorities. To contribute in the understanding and development of carbon fiber reinforced aluminum matrix composites, this study focuses on composite fabrication, mechanical testing and physical property modelling. The composites are fabricated by squeeze casting. Plain weave carbon fiber (AS4 Hexcel) is used as reinforcement, while aluminum alloy 6061 is used as matrix. The improvement of the squeeze casting fabrication process is focused on reducing leakage while combining thermal expansion pressure with post-processing pressing. Three different fiber volume fractions are investigated to achieve optimum mechanical properties. Piston-on-ring (POR) bend tests are used to measure the biaxial flexural stiffness and fracture strength on disc samples. The stress-strain curves and fracture surfaces reveal the effect of fiber-matrix interface bonding on composite bend behaviour. The composites achieved up to 11.6%, 248.3% and 90.1% increase in flexural modulus, strain hardening modulus and yield strength as compared with the unreinforced aluminum alloy control group, respectively. Analytical modelling and finite element modelling are used to comparatively characterise and verify the composite effective flexural modulus and strength. Specifically, they allowed iii evaluating how far the experimental results deviate from idealized assumptions of the models, which provides an insight into the composite sample quality, particularly at fiber-matrix interfaces. Overall, the models agree well with experimental results in identifying an improvement in flexural modulus up to a carbon fiber volume fraction of 4.81vol%. However, beyond a fiber content of 3.74vol%, there is risk of deterioration of mechanical properties, particularly the strength. This is because higher carbon fiber volume fractions restrict the infiltration and wetting of carbon fibre by the liquid, potentially leading to poor fiber-matrix interface bonding. It is shown that higher thermal expansion pressures and subsequent post-processing pressing can overcome this challenge at higher carbon fiber volume contents by reducing fiber-aluminum contact angle, improving infiltration, reducing defects such as porosity, and overall improving fiber-matrix bonding.
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Vargas, Alexandro. "Machinability Study on Silicon Carbide Particle-Reinforced Aluminum Alloy Composite with CVD Diamond Coated Tools." Scholarly Commons, 2017. https://scholarlycommons.pacific.edu/uop_etds/215.

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Particle-reinforced MMCs (pMMC) such as aluminum alloys reinforced with ceramic silicon carbide particles (AlSiC) require special cutting tools due to the high hardness and abrasive properties of the ceramic particles. Diamond coated cutting tools are ideal for machining this type of pMMC. Previous research studies focus on the machinability of pMMCs with low ceramic content. The aim of this research is to determine the optimal cutting parameters for machining AlSiC material containing high silicon carbide particle reinforcement (>25%). The optimal cutting parameters are determined by investigating the relationship between cutting forces, tool wear, burr formation, surface roughness, and material removal rate (MRR). Experimental milling tests are conducted using CVD diamond coated end mills and non-diamond tungsten carbide end mills. It was found that low tool rotation speeds, feed rates and depths of cut are necessary to achieve smoother surface finishes of R a < 1 μm. A high MRR to low tool wear and surface roughness ratio was obtainable at a tool rotation speed of 6500 r/min, feed rate of 762 mm/min and depth of cut of 3 mm. Results showed that a smooth surface roughness of the workpiece material was achieved with non-diamond tungsten carbide end mills, however, this was at the expense of extreme tool wear and high burr formation. The use of coolant caused a 50% increase in tool wear compared to the dry-cutting experiments which had lower cutting tool forces.
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Stjernstoft, Tero. "Machining of Some Difficult-to-Cut Materials with Rotary Cutting Tools." Doctoral thesis, KTH, Production Engineering, 2004. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-3693.

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<p>Automobile and aero industries have an increasing interestin materials with improved mechanical properties. However, manyof these new materials are classified as difficult-to-cut withconventional tools. It is obvious that tools, cutting processesand cutting models has to be devel-oped parallel to materialsscience. In this thesis rotary cutting tools are tested as analternative toexpensive diamond or cubic bore nitridetools.</p><p>Metal matrix composites mostly consist of a light metalalloy (such as aluminium or titanium) reinforced with hard andabrasive ceramic parti-cles or fibres. On machining, thereinforcement results in a high rate of tool wear. This is themain problem for the machining of MMCs. Many factors affect thelife length of a tool, i.e. matrix alloy, type, size andfraction of the reinforcement, heat treatment, cuttingconditions and tool properties.</p><p>In tests, the Al-SiC MMC formed a deformation layer duringmilling, probably affected by lack of cooling. The dominatingfactor for tool life was the cutting speed. Water jet or CO2cooling of turning did not provide dramatic increase in toollife. With PCD, cutting speeds up to 2000 m/min were usedwithout machining problems and BUE formation. Tool flank wearwas abrasive and crater wear created an "orange-peel type" wearsurface. PCD inserts did not show the typical increase in flankwear rate at the end of its lifetime.</p><p>The use of self-propelled rotary tools seems to be apromising way to increase tool life. No BUE was formed on therotary tool at high cutting data. The measurements indicatethat the rotary tool creates twice as good surface as PCDtools. The longest tool life was gained with an inclinationangle of 10 degrees. Tool costs per component will beapproximately the same, but rotary cutting tool allows higherfeeds and therefore a higher production rate and thus a lowerproduction cost.</p><p>The rotary cutting operation might have a potential toincrease productiv-ity in bar peeling. The lack of BUE withrotary cutting gives hope on higher tool life. The test resultsshow that tool wear was 27% lower with rotary cutting tools.Increase of cutting speed from 22 to 44 m/min did not affectcutting forces. This indicates that the cutting speed canincrease without significant change in tool wear rate.</p><p>Issues related to rotary cutting like cutting models,cutting processes, standards, tools and models have beendiscussed. A tool wear model with kinetic energy has beendiscussed.</p><p><b>KEYWORDS:</b>Difficult-to-Cut material, Metal MatrixComposite (MMC), Machining, Machinability, Rotary Cutting Tool,Acoustic Emission</p>
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Books on the topic "Metal Matrix Composite (MMC)"

1

Abdullah, Abu. Machining of aluminium based Metal Matrix Composite (MMC). typescript, 1996.

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G, Wadley H. N., and Lewis Research Center, eds. Cost models for MMC manufacturing processes: Tog. National Aeronautics and Space Administration, [Lewis Research Center, 1996.

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United States. National Aeronautics and Space Administration., ed. Computer simulation of time-dependent effects for metal matrix composites (MMC) using METCAN. National Aeronautics and Space Administration, 1996.

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Coelho, Reginaldo Teixeira. The machinability of aluminium-based SiC reinforced metal matrix composite (MMC) alloy with emphasis on hole production. University of Birmingham, 1995.

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S, Majumdar Bhaskar, and United States. National Aeronautics and Space Administration., eds. In-phase thermomechanical fatigue mechanisms in an unidirectional SCS-6/Ti 15-3 MMC. National Aeronautics and Space Administration, 1995.

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S, Majumdar Bhaskar, and United States. National Aeronautics and Space Administration., eds. In-phase thermomechanical fatigue mechanisms in an unidirectional SCS-6/Ti 15-3 MMC. National Aeronautics and Space Administration, 1995.

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S, Majumdar Bhaskar, and United States. National Aeronautics and Space Administration., eds. In-phase thermomechanical fatigue mechanisms in an unidirectional SCS-6/Ti 15-3 MMC. National Aeronautics and Space Administration, 1995.

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B, Gurganus T., Walker J. A. 1939-, and Langley Research Center, eds. Development and characterization of powder metallurgy (PM) 2XXX series Al alloy products and metal matrix composite (MMC 2XXX Al/SiC materials for high temperature aircraft structural applications. National Aeronautics and Space Administration, Langley Research Center, 1992.

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Engineers, Society of Automotive, and International Congress and Exposition (1994 : Detroit, Mich.), eds. Metal matrix composites. Society of Automobile Engineers, 1994.

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(Firm), Knovel, ed. Composite materials handbook: Metal matrix composites. U.S. Department of Defense, 2002.

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Book chapters on the topic "Metal Matrix Composite (MMC)"

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Weinert, K., M. Buschka, and M. Lange. "Machining Technology Aspects of Al-MMC." In Metal Matrix Composites. Wiley-VCH Verlag GmbH & Co. KGaA, 2006. http://dx.doi.org/10.1002/3527608117.ch6.

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Krug, P., and G. Sinha. "Spray Forming - An Alternative Manufacturing Technique for MMC Aluminum Alloys." In Metal Matrix Composites. Wiley-VCH Verlag GmbH & Co. KGaA, 2006. http://dx.doi.org/10.1002/3527608117.ch11.

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Vignesh, M., G. Ranjith Kumar, M. Sathishkumar, G. Rajyalakshmi, and R. Ramanujam. "Study of Machinability, Mechanical, and Tribological Properties of Hybrid Al-MMC." In Metal Matrix Composites. CRC Press, 2023. http://dx.doi.org/10.1201/9781003345466-6.

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Evans, Alexander, Christopher San Marchi, and Andreas Mortensen. "MMC Companies in Alphabetical Order." In Metal Matrix Composites in Industry. Springer US, 2003. http://dx.doi.org/10.1007/978-1-4615-0405-4_5.

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Kishawy, H. A., S. Kannan, and G. Parker. "Traditional Machining Processes of MMC." In Machining of Metal Matrix Composites. Springer London, 2011. http://dx.doi.org/10.1007/978-0-85729-938-3_4.

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Nieto, Andy, Arvind Agarwal, Debrupa Lahiri, Ankita Bisht, and Srinivasa Rao Bakshi. "Carbon Nanotube Reinforced Metal Matrix Composite (CNT-MMC) Systems." In Carbon Nanotubes. CRC Press, 2021. http://dx.doi.org/10.1201/9780429299582-5.

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Shin, Yung C., and Chinmaya Dandekar. "Mechanics and Modeling of Chip Formation in Machining of MMC." In Machining of Metal Matrix Composites. Springer London, 2011. http://dx.doi.org/10.1007/978-0-85729-938-3_1.

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Farahmand, Bahram. "Metal Matrix Composites (MMCs) (Methods of Manufacturing MMC Parts)." In Fundamentals of Composites and Their Methods of Fabrications. Springer Nature Switzerland, 2025. https://doi.org/10.1007/978-3-031-80201-0_5.

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Silber, M., M. Wenzelburger, and R. Gadow. "Advanced Manufacturing for Fiber Reinforced Metal Matrix Composites (MMC)." In Sustainable Automotive Technologies 2010. Springer Berlin Heidelberg, 2010. http://dx.doi.org/10.1007/978-3-642-10798-6_25.

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Borsellino, C., S. Casto, E. Valvo, and V. F. Ruisi. "Metal Matrix Composites - Mmc - Turning: Comparison of Tool Materials." In AMST’02 Advanced Manufacturing Systems and Technology. Springer Vienna, 2002. http://dx.doi.org/10.1007/978-3-7091-2555-7_14.

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Conference papers on the topic "Metal Matrix Composite (MMC)"

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Hansen, Bruce, Jason Fetty, Timothy Demers, and Treven Baker. "Aluminum Metal Matrix Composite Liner Testing." In Vertical Flight Society 71st Annual Forum & Technology Display. The Vertical Flight Society, 2015. http://dx.doi.org/10.4050/f-0071-2015-10248.

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Bearing liners are used in rotorcraft gearboxes to reduce wear between the bearing race and housing during aircraft operations. Bearing liners are typically made of steel, but a new aluminum Metal Matrix Composite (MMC) bearing liner material is currently being developed under the Future Advanced Rotorcraft Drive System (FARDS) program. These new bearing liners have the benefit of reduced weight compared to existing steel liners. Seeded fault testing was performed which demonstrated the liners ability to withstand the loads generated due to failing bearings and still left the housing assembly in serviceable condition after removal. The test was in support of a viability study evaluating use of aluminum MMC liners for weight savings.
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Monteiro, Othon R., Radhika Suresh, Sankaran Murugesan, and Valery Khabashesku. "Corrosion Resistance of Ni-Metal Matrix Composite Coatings: Effect of Microstructure." In CORROSION 2017. NACE International, 2017. https://doi.org/10.5006/c2017-09806.

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Abstract Metal matrix composite (MMC) and nanocomposite coatings are being proposed as alternatives to their monolithic counterparts to improve protection against wear in chemically-aggressive environments. Corrosion resistance of MMC coatings is strongly dependent on the coating microstructure, which is affected by the physical and chemical nature of the dispersed particles, as well as the particle concentration. In this paper, we present the results of our tests on the corrosion response of Ni-P MMC coatings with micro-crystalline and nano-crystalline diamond as the dispersed phase. Potentiodynamic and electrochemical impedance spectroscopy tests were performed to compare the corrosion of Ni-P composites and nanocomposites, and the results are analyzed in terms of their microstructures. The corrosion potential is primarily determined by the P content and the heat treatment carried out after deposition, and is weakly dependent on the particle content. In low-P coatings, the presence of micrometer-size particles has no significant impact on Ecorr and Icorr. Heat treatment increases Ecorr and decreases Icorr. Similar trends are observed in the high-P coatings. EIS results suggest self-healing behavior with some microstructures.
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Aylor, Denise M., and Patrick J. Moran. "An Investigation of Corrosion Properties and Protection for Graphite/Aluminum, and Silicon Carbide/Aluminum Metal Matrix Composites." In CORROSION 1986. NACE International, 1986. https://doi.org/10.5006/c1986-86202.

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Abstract The corrosion resistance of graphite/aluminum (Gr/Al) and silicon carbide/aluminum (SiC/Al) metal matrix composites (MMCs) and various composite corrosion protection methods was evaluated in marine environmental exposures of 1 to 42 months. Continuous Gr/Al and SiC/Al exhibited accelerated corrosion when both the Gr or SiC reinforcement and the Al were exposed to the environment; discontinuous SiC/Al MMC exhibited localized and less severe corrosion. Aluminum thermal spraying was found to be a successful corrosion protection method for discontinuous SiC/Al composites. Thermal spraying was not recommended for continuous Gr/Al and SiC/Al due to the thin Al surface foils in these composites, which suffer severe warpage during surface preparation for spraying. Sulfuric acid anodizing provided good corrosion protection to the continuous fiber- reinforced MMCs and ion vapor deposited aluminum and organic coatings were identified as other potentially suitable coatings.
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Flores, Juan F., A. Neville, N. Kapur, and A. Gnanavelu. "Electrochemical and Microstructural Response of Metal Matrix Composites at Different Erosion-corrosion Conditions." In CORROSION 2011. NACE International, 2011. https://doi.org/10.5006/c2011-11249.

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Abstract The electrochemical and microstructural response of metal matrix composites (MMCs) under different erosion-corrosion conditions is assessed in this paper. The MMCs are plasma transferred arc (PTA) overlays, produced by reinforcing two iron base and two nickel base hardfacing matrices with tungsten carbide (WC) particles. The microstructures are examined using scanning electron microscopy (SEM) and stereology techniques. The electrochemical response under erosion-corrosion conditions, assessed by in-situ potentiodynamic techniques, is analyzed as a function of sand content (10 and 50 g/l) and slurry temperature (20 and 65°C). The degradation mechanisms of the MMCs microstructural components are analyzed by SEM. The microstructural analysis showed that WC grains were partially dissolved in the molten matrix, promoting the formation of secondary phases in the matrix phase. The in-situ electrochemical results show that there is a correlation between the MMCs microstructural characteristics and their electrochemical response and that the nickel base MMC, shows significantly lower current density values at all sand content. On the other hand, the iron base MMC showed a fully active behavior at all erosion-corrosion conditions. Finally the erosion-corrosion tests in conjunction with post-test surface analysis demonstrates that as the sand content and temperature increases under erosion-corrosion conditions, every microstructural component is significantly affected and the corrosion of the matrix undermined the WC grains and the integrity of the secondary phases.
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Neville, A., F. Reza, S. Chiovelli, and T. Revega. "Assessing MMCs for Corrosion and Erosion-Corrosion Applications in the Oil Sands Industry." In CORROSION 2004. NACE International, 2004. https://doi.org/10.5006/c2004-04125.

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Abstract Erosion-corrosion arising from aqueous slurry environments can be a significant problem in the oil sands industry. Interactions between erosion and corrosion are complex and as such it is difficult to determine the rate of material loss with sufficient accuracy for reliable prediction of equipment lifetime. One material which has been successfully used on production critical equipment is tungsten carbide (WC) metal matrix composite (MMC) weld overlays. Four WC-based hardfacings with different particle size distributions were investigated. These overlays were comprised of 65 wt % WC hard phase with a metal matrix binder consisting of mainly Ni, Cr, Si, B and Fe. The Metal Matrix Composites (MMCs) overlays were applied using the plasma transferred arc (PTA) welding process Electrochemical corrosion tests in a simulated recycle cooling water environment were conducted to investigate the corrosion behaviour of the MMCs. In static corrosion tests, little change in the corrosion rate with different WC grain sizes was observed. The smallest WC grain size distribution did show a slight decrease in corrosion resistance. Similarly, little difference in erosion-corrosion was recorded for the different WC grain size fractions tested with larger grain sizes showing a slight reduction in erosion-corrosion resistance. The interactions between erosion and corrosion can be identified and are important in the MMC degradation. The corrosion mechanisms in static condition and the erosion-corrosion mechanisms can be directly linked to the complex microstructure of the MMCs.
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Bavarian, Behzad B., S. Metha, C. Davison, B. Aguilar, and Mehrooz Zamanzadeh. "Evaluation of the Environmentally Assisted Cracking of Aluminum-Metal Matrix Composites in Marine Enviroment." In CORROSION 1993. NACE International, 1993. https://doi.org/10.5006/c1993-93285.

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Abstract A series of mechanical and electrochemical experiments were performed on samples of 6091 + 25% SiCp and 6092 + 25% SiCp in oder to investigate potential applications for these promisyng materials in the high speed aircrafts such as Hogh Speed Civil Transport(HSCT). The objective of these experiments was to evaluate the susceptibility of these materials to environment induced cracking in marine environment. Variables examined include pH, applied potential, and concentration of cholride ions. Results of these investigation showed these materials to be susceptible to stress corrosion cracking only under specific electrochemical condition. Corrosion of Al-MMC +25% SiCp was observed only when the breakdown of passive film occured, which exposed active aluminum and noble SiC particles to the corrosive environment and initaite a galvanic corrosion. Satisfactory corrosion performance was observed whenever a stable passive film was present on the composite surface andbreakdown of the passive film was retarded.
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Thomas, Joshua D., and Danijela Milosevic-Popovich. "Cobalt/Chromium Carbide Composite Coatings Applied by Brush Plating for Use as an Alternative to Hard Chrome." In CONFERENCE 2022. AMPP, 2022. https://doi.org/10.5006/c2022-18228.

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Abstract Due to increased concern for both environmental and worker safety from governments around the world, many significant industrial chemicals are being phased out of production processes. One example is the use of hexavalent chromium compounds for the electrodeposition of hard chrome. Electrodeposited chrome is typically used for improved hardness, lubricity, wear resistance, and corrosion resistance. This work will support the use of a metal matrix composite composed of cobalt and chromium carbide particles as an alternative for chrome coatings deposited from hexavalent chromium compounds. Metal matrix composite (MMC) coatings consist of two phases co-deposited during plating: a continuous metal phase such as cobalt and small (&amp;lt;100 μm) particles of another chemical species distributed throughout. The physical qualities of the composite (such as hardness) are strongly dependent on the ratio and distribution of the two constituent phases. The composition of the plating solution and the parameters used during plating both play important roles in the composition and quality of the final deposit. While most research has focused on applying metal matrix composites by tank electroplating methods, this presentation will focus on applying the coating via brush plating. Brush plating is a portable electrodeposition technique where solution is applied to the part by a plating solution saturated sleeve on the anode when contact is made to a localized area. Brush plating operations typically use less masking when plating small areas of a larger part. Less solution is needed because the part does not need to be immersed. And the brushing action allows for faster solution replenishment at the electrode surface. This paper will show examples of a matrix material of cobalt co-deposited with either 1 μm or 6 μm chromium carbide particles. It will be described how the concentration of the particles in solution determines the range of particle incorporation; as well as develop an understanding of how tailoring the plating parameters to the system of particle and matrix is vital to creating a deposit for specific deposit characteristics.
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Chan, W. M., F. T. Cheng, L. K. Leung, R. J. Horylev, and T. M. Yue. "Corrosion Behavior of Magnesium Alloy AZ91 and Its MMC in NACl Solution." In CORROSION 1997. NACE International, 1997. https://doi.org/10.5006/c1997-97441.

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Abstract The corrosion behaviors of magnesium alloy AZ91C and its Al2O3(short fibre)-reinforced metal matrix composite (MMC) in alkaline solutions (pH 10.5) containing chloride were compared using potentiodynamic polarization measurements, electrochemical impedance spectroscopy (EIS) and immersion tests. Dependence of polarization characteristics (corrosion potential and corrosion current density) on chloride concentration was similar for both materials. The corrosion potential Ecorr decreased linearly with the logarithm of chloride concentration, while the corrosion current density icorr increased rapidly at chloride concentrations larger than 0.1%, with the icorr for the MMC consistently higher than that for AZ91C, reaching a factor of about 3 in 3.5% sodium chloride solution. EIS data indicated that the protective film on the MMC was inferior to that on the matrix alloy. With stirring and at frequencies higher than 5 Hz, the electrode/electrolyte interface might be described by the simplified Randles model for both materials. Immersion tests showed that the corrosion rate of the MMC, in terms of weight loss, was about 7 times that of the matrix alloy. Thus the present investigation indicated that in alkaline solutions containing chloride ions, the presence of Al2O3 short fibres in the alloy did not drastically alter the corrosion behavior, but significantly reduced its corrosion resistance.
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Flores, J. F., A. Neville, N. Kapur, and A. Gnanavelu. "Erosion-Corrosion Performance of Plasma Transferred Arc Overlays in Slurry Conditions." In CORROSION 2009. NACE International, 2009. https://doi.org/10.5006/c2009-09482.

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Abstract This paper reports interactions between corrosion and solid particles erosion in slurry conditions. The materials tested in this investigation are intended to be used as hardfacing protective overlays in critical areas of the hydrotransport process in the oilsands industry, where erosion-corrosion can dramatically reduce the pumping and piping equipment lifetime. The materials under investigation were: two Ni-based and one Fe-based metal matrix composites (MMCs) with tungsten carbide (WC) as the reinforcing phase. The microstructure of the overlays was analyzed and mainly comprised a matrix phase with the presence of embedded intermetallics and the WC reinforcing phase grains. The corrosion behavior is assessed as a function of temperature, the Ni-based MMCs showed a pseudo-passive behavior at low temperature; however at high temperature their corrosion resistance was dramatically reduced. In contrast, the Fe-based MMC showed active corrosion behavior. The erosion- corrosion degradation mechanisms were assessed as a function of sand loading and aqueous environment. It was found that the presence of intermetallics in the matrix phase and around the WC grains played an important role in the erosion-corrosion performance of the MMCs overlays. At low sand loading and high temperature, the corrosion behavior of the MMCs dramatically affected their erosion-corrosion performance, whereas at high solid loading and low solution corrosivity, the microstructural features and matrix microhardness of the overlays determined their erosion-corrosion performance.
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Songmene, V., T. F. Stephenson, and A. E. M. Warner. "Machinability of Graphitic Silicon Carbide Aluminum Metal Matrix Composite GrA-Ni™." In ASME 1997 International Mechanical Engineering Congress and Exposition. American Society of Mechanical Engineers, 1997. http://dx.doi.org/10.1115/imece1997-1152.

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Abstract Metal-Matrix Composites (MMC) are being developed for high wear resistance applications. A new MMC, a graphitic aluminum metal matrix composite consisting of an aluminum matrix reinforced with SiC particles and nickel-coated graphite particles, GrA-Ni™, has been developed by INCO Limited. The addition of nickel-coated graphite to SiC particulate reinforced aluminum plays a similar role to flake graphite in grey cast iron. However, like other MMCs, this composite is demanding in terms of requirements for cutting conditions and cutting tool materials. This paper assesses the machining data for this new composite, in regards to tool life, surface finish and cutting forces. The tests included milling, turning, and drilling conducted with carbide and diamond tools. The test results showed that GrA-Ni™ with 10 vol% SiC – 5 vol% Gr, is easier to machine than existing aluminum composites reinforced with SiC particles, such as 20 vol% SiC reinforced aluminum composite.
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Reports on the topic "Metal Matrix Composite (MMC)"

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Weiss, David C., and Gerald A. Gegal. Energy-Saving Melting and Revert Reduction Technology (E-SMARRT): Development of Elevated Temperature Aluminum Metal Matrix Composite (MMC) Alloy and Its Processing Technology. Office of Scientific and Technical Information (OSTI), 2014. http://dx.doi.org/10.2172/1131418.

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Rigdon, Michael A., and Donald Groves. Summary of the DoD Metal Matrix Composites (MMC) Steering Committee Meeting. Hosted by the Institute for Defense Analyses, Alexandria, VA, 5-6 October 1989. Defense Technical Information Center, 1989. http://dx.doi.org/10.21236/ada217611.

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Smith, Don D. Steel-SiC Metal Matrix Composite Development. Office of Scientific and Technical Information (OSTI), 2005. http://dx.doi.org/10.2172/967387.

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De Rosset, William S. Nondestructive Evaluation of a Metal Matrix Composite. Defense Technical Information Center, 2003. http://dx.doi.org/10.21236/ada419365.

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Lavender, C. A., and M. T. Smith. Evaluation of waterjet-machined metal matrix composite tensile specimens. Office of Scientific and Technical Information (OSTI), 1986. http://dx.doi.org/10.2172/5754921.

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Wu, Yufeng. Fabrication of metal matrix composite by semi-solid powder processing. Office of Scientific and Technical Information (OSTI), 2011. http://dx.doi.org/10.2172/1082974.

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Levoy, Nancy F. Ductile - Ductile Beryllium Aluminum Metal Matrix Composite Manufactured by Extrusion1. Defense Technical Information Center, 1995. http://dx.doi.org/10.21236/ada289519.

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Raja, Krishnan, and Ravi subramanian. COLD SPRAY COATED METAL MATRIX NANO-COMPOSITE SURFACE LAYERS ON INCONEL 617. Office of Scientific and Technical Information (OSTI), 2022. http://dx.doi.org/10.2172/1868153.

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Lee, H. R., W. Yun, Z. Cai, W. Rodrigues, and D. S. Kupperman. X-ray microdiffraction studies to measure strain fields in a metal matrix composite. Office of Scientific and Technical Information (OSTI), 1997. http://dx.doi.org/10.2172/555507.

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Howell, Paul R. Microstructural Development in a Spray Formed Aluminum-Silicon Carbide Based Metal Matrix Composite. Defense Technical Information Center, 1992. http://dx.doi.org/10.21236/ada251425.

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