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AbstractAbstract
[en] The structure and properties of metallic composite materials and composite materials with metallic matrix are considered. In agreement with the morphology of constituent phases the following types of composite materials are described: dispersion-strengthened composite materials; particle-reinforced composite materials; fibrous composite materials; laminar composite materials. Data on strength and electric properties of the above-mentioned materials, as well as effect of the amount, location and geometric shape of the second phase on them, are presented
Original Title
Metallicheskie kompozitnye materialy
Primary Subject
Source
Cahn, R.W.; Haasen, P. (eds.); p. 550-574; 1987; p. 550-574; Metallurgiya; Moscow (USSR); 42 refs.; 23 figs.; 2 tabs.; translated from English.
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Book
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Frommeyer, G.; Rablbauer, R.
Max-Planck-Institut fuer Eisenforschung GmbH, Duesseldorf (Germany). Funding organisation: Bundesministerium fuer Bildung und Forschung, Berlin (Germany)2002
Max-Planck-Institut fuer Eisenforschung GmbH, Duesseldorf (Germany). Funding organisation: Bundesministerium fuer Bildung und Forschung, Berlin (Germany)2002
AbstractAbstract
[en] The microstructures as well as the mechanical and thermo-physical properties of the hypoeutectic NiAlCr27 alloys were characterised with regard to their applications for structural components like heat tiles and static blades in stationary gas turbines at maximum application temperatures of 1200 C. The alloy was cast at different cooling rates and processed by powder metallurgical (PM) technique. Further samples of PM and as-cast ingots were consolidated by hot extrusion. The mechanical properties like strength, plasticity and creep behaviour were determined in the initial state and after heat treatment. The NiAlCr27 alloys, solidified at low cooling rates, exhibit a high-temperature strength of 80 MPa at 1200 C and high thermal stability of the microstructure up to 1300 C. Macro alloying of the NiAlCr27 base alloy with Mo or Re contents up to 2 at% has only a little influence on plasticity and flow stress at room temperature and on the high temperature strength, as well. The oxidation resistance of NiAlCr27 and its modifications containing 0.1 and 0.4 mass% Hf or Y was characterized in the temperature range from 1000 C to 1200 C performing oxidation tests at constant temperatures and under thermal cyclic conditions. Micro alloying with 0.4 mass% Hf results in a strong adhesion of the oxide layer and reveals an improved oxidation resistance. High superplastic elongations were achieved on hot extruded PM NiAlCr27 specimen at 1150 C. The maximum superplastic elongation of 420% was determined at a strain rate of 8.10-4s-1. (orig.)
[de]
Die Mikrostrukturen sowie die mechanischen und thermophysikalischen Eigenschaften hypoeutektischer NiAlCr27-Legierungen wurden charakterisiert im Hinblick auf die Anwendung als Strukturkomponenten wie Hitzekacheln und Leitschaufeln in stationaeren Gasturbinen fuer die maximale Einsatztemperatur von 1200 C. Die Legierung wurde mit unterschiedlichen Abkuehlraten vergossen und pulvermetallurgisch (PM) prozessiert. Weitere PM- und Gussproben wurden durch Heissstrangpressen konsolidiert. Die mechanischen Eigenschaften wie Festigkeit, Plastizitaet und Kriechverhalten wurden im Ausgangszustand und nach Gluehbehandlungen bestimmt. Die mit niedrigen Abkuehlraten erstarrten NiAlCr27-Legierungsproben zeichnen sich durch eine Warmfestigkeit von 80 MPa bei 1200 C und eine hohe thermische Stabilitaet der Mikrostruktur bis 1300 C aus. Makrolegieren der NiAlCr27-Basislegierung mit Mo- bzw. Re-Gehalten bis zu 2 At.% zeigte einen geringen Einfluss auf die Plastizitaet und Fliessspannung bei Raumtemperatur sowie die Warmfestigkeiten. Die Oxidationsbestaendigkeit der NiAlCr27-Basislegierung und deren Modifikationen mit Hf- bzw. Y-Zusaetzen von jeweils 0,1 und 0,4 Masse% wurde im Temperaturbereich von 1000 C bis 1200 C bei konstanter Temperatur und in zyklischen Versuchen bestimmt. Das Mikrolegieren mit 0,4 Gew.% Hf fuehrte zu einer erhoehten Haftung der Oxidschicht und dadurch zu einer verbesserten Oxidationsbestaendigkeit. Hohe superplastische Dehnungen wurden an mittels Heissstrangpressens konsolidiertem PM NiAlCr27 bei 1150 C erzielt. Bei der Dehnrate von 8.10-4s-1 wurde die maximale superplastische Dehnung von 420% bestimmt. (orig.)Original Title
Intermetallische NiAl-Komponenten fuer Systeme zur umweltfreundlichen Energieumwandlung. Teilprojekt: Werkstoffcharakterisierung und -optimierung. Arbeitspaket A2: NiAl-Cr-Legierungen. Abschlussbericht
Primary Subject
Source
2002; 90 p; FOERDERKENNZEICHEN BMBF 09N2009E
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Miscellaneous
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AbstractAbstract
[en] The effect of the ternary element chromium in B2 ordered NiAl based alloys was studied by atom probe field ion microscopy. Samples of the compositions Ni50Al48Cr2, Ni49Al49Cr2, and Ni48Al50Cr2 were investigated after different heat treatments. The chromium concentrations of the NiAl matrix, measured by atom probe, increased with increasing Ni/Al ratio and heat treatment temperature. The site preference of solute Cr atoms for the Al sublattice was determined by layer resolved measurements. An antiphase boundary observed in Ni50Al48Cr2 showed a high local Cr concentration with Cr atoms substituting for Al atoms. Superdislocations in the quasi-stoichiometric Ni49Al49Cr2 were not dissociated into partial dislocations and showed no Cr segregation. These results are discussed in view of activation of a<1 1 1> slip systems
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Source
S092150930200672X; Copyright (c) 2002 Elsevier Science B.V., Amsterdam, The Netherlands, All rights reserved.; Country of input: International Atomic Energy Agency (IAEA)
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Journal Article
Journal
Materials Science and Engineering. A, Structural Materials: Properties, Microstructure and Processing; ISSN 0921-5093; ; CODEN MSAPE3; v. 353(1-2); p. 87-91
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AbstractAbstract
[en] The micro- and nano-structure of a NiAl-Re alloy with 1 at.% Re has been investigated by means of atom probe field ion microscopy (APFIM) and by scanning electron microscopy. The effect of heat treatments on this alloy were studied for annealing temperatures at 1000 deg. C in a time interval of 10-1000 h, and at 1300 deg. C for 1000 h. The results were compared with those from the as-cast samples. Rhenium contents of the NiAl matrix were determined by APFIM. It was found that the Re concentration in the primary NiAl crystals decreases with increasing annealing time. Layer-resolved atom probe measurements were performed in order to determine the site occupancy of Re atoms in the NiAl superlattice. The results clearly showed a site preference for the Ni sublattice
Primary Subject
Source
S0921509302006718; Copyright (c) 2002 Elsevier Science B.V., Amsterdam, The Netherlands, All rights reserved.; Country of input: International Atomic Energy Agency (IAEA)
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Journal Article
Journal
Materials Science and Engineering. A, Structural Materials: Properties, Microstructure and Processing; ISSN 0921-5093; ; CODEN MSAPE3; v. 353(1-2); p. 80-86
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AbstractAbstract
[en] The constitution of the quasi-binary eutectic NiAl-Re section of the ternary Al-Ni-Re phase diagram was reinvestigated by using differential thermal analysis, metallography and scanning electron microscopy. The alloys studied were stoichiometric NiAl and various NiAl-Rex (0.75< x<2.5 at.%) alloys. The microstructure of the as-cast NiAl-Re eutectic is of irregular fibrous morphology. Ingots with Re concentrations ≥1.25 at.% reveal non-equilibrium microstructures which consist of primary Re crystals, NiAl crystals, and eutectic. An ideal eutectic microstructure was achieved by unidirectional solidification of a NiAl-Re1.25 alloy using Bridgman technique at a low growth velocity of 30 mm h-1. The melting temperature of the stoichiometric NiAl compound is 1674 deg. C. The eutectic point of the quasi-binary section of the NiAl-Re system is determined to be at 1.25 at.% Re and a temperature of 1668 deg. C. The solidus temperatures of the NiAl-Re ingots exhibit a slight dependence on the Re concentration. The solid solubility of Re in NiAl is 0.6 at.% at the eutectic temperature and 0.2 at.% at 1300 deg. C
Primary Subject
Source
S092150930200388X; Copyright (c) 2002 Elsevier Science B.V., Amsterdam, The Netherlands, All rights reserved.; Country of input: International Atomic Energy Agency (IAEA)
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Journal Article
Journal
Materials Science and Engineering. A, Structural Materials: Properties, Microstructure and Processing; ISSN 0921-5093; ; CODEN MSAPE3; v. 343(1-2); p. 301-307
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AbstractAbstract
[en] The site occupancies of the transition metals Cr, Fe, and Re dissolved in NiAl of stoichiometric composition have been determined by atomic layer resolved atom probe field-ion microscopy (APFIM). The investigations were supported by X-ray diffraction studies to evaluate the lattice parameters. These are influenced by atomic size effects and constitutional lattice defects like Ni antistructure atoms in the Al sublattice and vacancies in the Ni sublattice. The APFIM results were compared with ALCHEMI data and calculated site preference energies published in the literature. Chromium additions to stoichiometric NiAl with 0.8 at% in solid solution exhibit a strong preference for Al sites. The lattice parameter of NiAl(Cr) solid solution is decreased. Iron atoms dissolved in higher concentrations of 5 at % in NiAl are almost equally distributed within both sublattices. They are possessing a weak preference for Al sites, which causes a lattice expansion of NiAl(Fe) solid solution. ALCHEMI results and site preference energy data show a strong site preference of Cr atoms for the Al sublattice. In contrast, iron atoms exhibit a weak site preference for Ni sites depending upon the stoichiometry of the NiAl host lattice. Re solutes in low concentrations of about 0.2 at % in NiAl possess a strong site preference for the Ni sublattice. The increase of the lattice parameter of NiAl(Re) is due to the pronounced size effect of Re atoms. For these species no ALCHEMI and site preference energy data are available in the literature
Primary Subject
Source
S0304399104000944; Copyright (c) 2004 Elsevier Science B.V., Amsterdam, The Netherlands, All rights reserved.; Country of input: International Atomic Energy Agency (IAEA)
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Journal Article
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AbstractAbstract
[en] Microcrystalline ultrahigh carbon steels, alloyed with up to 20 wt% vanadium and chromium, have been prepared by melt atomization and powder metallurgical techniques. The resulting microstructure contains a large volume fraction of carbides and a grain size of less than 1 micron. At room temperature, these microcrystalline steels exhibit a high yield stress while maintaining adequate toughness for practical applications. Exposure to higher temperatures softens the material considerably and it becomes superductile. The large elongation to failure and the high value of the strain rate sensitivity, m = 0.5, indicate superior superplastic properties of these extremely fine grained materials
Primary Subject
Secondary Subject
Source
Mc Queen, H.J.; Bailon, J.P.; Dickson, J.I.; Jonas, J.J.; Akben, M.G; p. 877-886; 1985; p. 877-886; Pergamon Books Inc; Elmsford, NY (USA); 7. international conference on the strength of metals and alloys; Montreal (Canada); 12-16 Aug 1985
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Book
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Conference
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ATOMIZATION, CARBIDES, CARBON STEELS, CHEMICAL PREPARATION, CHROMIUM ALLOYS, DUCTILITY, FRACTURE PROPERTIES, GRAIN SIZE, HARDENING, HIGH TEMPERATURE, MELTING, METALLURGY, MICROSTRUCTURE, PLASTICITY, POWDER METALLURGY, SENSITIVITY, STRAIN RATE, STRESS ANALYSIS, STRUCTURAL CHEMICAL ANALYSIS, TEMPERATURE DEPENDENCE, THERMODYNAMIC PROPERTIES, VANADIUM ALLOYS, YIELD STRENGTH
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AbstractAbstract
[en] Texture measurements were carried out on a Fe-26Al-5Cr alloy that was deformed by warm rolling at temperatures above and below the stress anomaly temperature in order to obtain information about a possible change of slip systems around that temperature. Special attention was paid to the initial microstructure, temperature during rolling and recrystallisation problems. Textures were determined by automatic crystal orientation mapping (ACOM) using electron backscatter diffraction (EBSD), which allows separation of measurement data from recrystallised and unrecrystallised fractions in the microstructure. A clear difference in texture evolution appears above and below the stress anomaly temperature; the most preferred orientations after rolling at 600 and 400 deg. C are ∼{5 5 7}<1 1 0> and ∼{1 1 1}<2 1 1>, respectively. This result suggests that the shear fraction of the active {1 1 2}1 1 1> slip systems increases with respect to that of the {1 1 0}<1 1 1> slip systems with increasing temperature around the stress anomaly temperature
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Source
13. international conference on the strength of materials; Budapest (Hungary); 25-30 Aug 2003; S0921509304006227; Copyright (c) 2004 Elsevier Science B.V., Amsterdam, The Netherlands, All rights reserved.; Country of input: International Atomic Energy Agency (IAEA)
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Journal Article
Literature Type
Conference
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Materials Science and Engineering. A, Structural Materials: Properties, Microstructure and Processing; ISSN 0921-5093; ; CODEN MSAPE3; v. 387-389(2-3); p. 950-954
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ALLOYS, ALUMINIUM ISOTOPES, BETA DECAY RADIOISOTOPES, BETA-PLUS DECAY RADIOISOTOPES, COHERENT SCATTERING, DIFFRACTION, FABRICATION, ISOTOPES, LIGHT NUCLEI, MATERIALS WORKING, MICROSTRUCTURE, NUCLEI, ODD-ODD NUCLEI, ORIENTATION, RADIOISOTOPES, SCATTERING, SECONDS LIVING RADIOISOTOPES, YEARS LIVING RADIOISOTOPES
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AbstractAbstract
[en] Schematical properties of refractory transition metals of the 5th and 6th periods of the periodic table are discussed in view of the atomic and structural parameters. The melting and boiling temperatures, the elastic moduli, the lattice stability and the conduction properties are of electronic nature. With increasing filling of the d-orbital intensive changes of the physical properties will be observed. The mechanical properties result from the strong elastic moduli, the lattice defect density and their thermal activation. The plastic deformability is caused by the described parameters including the lattice geometry and the microstructure. (orig.)
[de]
Systematische Eigenschaften hochschmelzender Uebergangsmetalle der 5. und 6. Perioden des Periodensystems werden anhand atomistischer und struktureller Parameter diskutiert. Die Schmelz- bzw. Siedetemperaturen, die Gitterstabilitaet, die elastischen Moduln sowie die Leitungseigenschaften sind elektronischer Natur und weisen mit zunehmender Auffuellung der d-Orbitale starke Aenderungen auf. Die Festigkeitseigenschaften resultieren aus den grossen elastischen Moduln, der Defektdichte und ihrer thermischen Aktivierbarkeit. Die plastische Verformbarkeit wird durch die vorstehend genannten Groessen einschliesslich der Kristallgittergeometrie und das Gefuege bestimmt. (orig.)Original Title
Metallkunde hochschmelzender Metalle und Legierungen
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Journal Article
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Metall; v. 32(7); p. 673-676
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AbstractAbstract
[en] Deformation twinning, martensitic phase transformation and mechanical properties of austenitic Fe-(15-30)wt%Mn alloys with additions of aluminium and silicon have been investigated. Tensile tests were carried out at different strain rates and temperatures. The formation of twins, α''- and ε-martensite during plastic deformation was analysed by optical microscopy, X-ray diffraction, scanning electron microscopy (SEM) and transmission electron microscopy (TEM). The stacking fault energy γfcc and the free energy ΔGγ→ε for the γ→ε phase transformation were calculated using the regular solution model. It is known that additions of aluminium increase γfcc and therefore strongly suppress the γ→ε transformation while silicon decrease γfcc and sustains the γ-ε transformation. The γ→ε phase transformation takes place in alloys with γfcc ≤ 20 mJ/m2. The stacking fault energy of the Fe-25Mn-3Si-3Al alloy was calculated as a function of temperature and related with microstructural changes of the strained sample at different temperatures. These steels with reduced density of about 7,3 g/cm-3 combine high tensile ductility up to 80% at high strain rates with true tensile strength of about 1000 MPa. The excellent plasticity induced by twinning and additional phase transformation up to extremely high strain rates of about ε = 103 s-1 results in an extraordinary shock resistance and enables deep drawing and backward extrusion operations of parts with complex shapes and high production rates. (orig.)
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Source
4. European symposium on martensitic transformations (ESOMAT-4); Enschede (Netherlands); 1-5 Jul 1997; 25 refs.
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