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Refractory metals

From Wikipedia, the free encyclopedia
Heat- and wear-resistant metals

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  Refractory metals
  Wider definition of refractory metals[1]

Refractory metals are a class ofmetals that are extraordinarily resistant toheat andwear. The expression is mostly used in the context ofmaterials science,metallurgy andengineering. The definitions of which elements belong to this group differ. The most common definition includes five elements: two of thefifth period (niobium andmolybdenum) and three of thesixth period (tantalum,tungsten, andrhenium). They all share some properties, including a melting point above 2000 °C and highhardness at room temperature. They are chemically inert and have a relatively high density. Their high melting points makepowder metallurgy the method of choice forfabricating components from these metals. Some of their applications include tools to work metals at high temperatures, wire filaments, casting molds, and chemical reaction vessels in corrosive environments. Partly due to their high melting points, refractory metals are stable againstcreep deformation to very high temperatures.

Definition

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Most definitions of the term "refractory metals" list an extraordinarily high melting point as a key requirement for inclusion. By one definition, a melting point above 4,000 °F (2,200 °C) is necessary to qualify, which includesiridium,osmium,niobium,molybdenum,tantalum,tungsten,rhenium,rhodium,ruthenium andhafnium.[2] The five elementsniobium,molybdenum,tantalum,tungsten andrhenium are included in all definitions,[3] while the widest definition includes all elements with a melting point above 2,123 K (1,850 °C), such astitanium,vanadium,zirconium, andchromium.[4]Technetium is not included because of its radioactivity, though it would otherwise have qualified under the widest definition.[5]

Properties

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Physical

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Properties of the refractory metals
NameNiobiumMolybdenumTantalumTungstenRhenium
Period55666
Group56567
Melting point K[prop 1]27502896329036953459
Boiling point K[prop 2]50174912573162035869
Melting point °C[prop 1]24772623301734223186
Boiling point °C[prop 2]47444639545859305596
Density g·cm−3[prop 3]8.5710.2816.6919.2521.02
Young's modulus GPa105329186411463
Vickers hardness MPa1320153087334302450
  1. ^abConsensus values taken frommelting points of the elements with multiple references there.
  2. ^abConsensus values taken fromboiling points of the elements with multiple references there. Tungsten has a particularly wide band of discrepancy, with two primary sources reporting 5555 °C.
  3. ^Consensus values taken fromdensities of the elements with multiple references there.

Refractory metals have high melting points, with tungsten and rhenium the highest of all elements, and the others' melting points exceeded only byosmium andiridium, and the sublimation ofcarbon. These high melting points define most of their applications. All the metals arebody-centered cubic except rhenium which ishexagonal close-packed. The physical properties of the refractory elements vary significantly because they are members of differentgroups of the periodic table.[6][7] The hardness, high melting and boiling points, and highenthalpies of atomization of these metals arise from the partial occupation of the outerd subshell, allowing the d electrons to participate in metallic bonding. This gives stiff, highly stable bonds to neighboring atoms and abody-centered cubic crystal structure that resists deformation. Moving to the right in the periodic table, more d electrons increase this effect, but as the d subshell fills they are pulled by the higher nuclear charge into the atom's inertcore, reducing their ability to delocalize to form bonds with neighbors. These opposing effects result in groups 5 through 7 exhibiting the most refractory properties.[8]

Creep resistance is a key property of the refractory metals. In metals, the starting of creep correlates with the melting point of the material; the creep in aluminium alloys starts at 200 °C, while for refractory metals temperatures above 1500 °C are necessary. This resistance against deformation at high temperatures makes the refractory metals suitable against strong forces at high temperature, for example injet engines, or tools used duringforging.[9][10]

Chemical

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The refractory metals show a wide variety of chemical properties because they are members of three distinct groups in theperiodic table. They are easily oxidized, but this reaction is slowed down in the bulk metal by the formation of stable oxide layers on the surface (passivation). Especially the oxide of rhenium is more volatile than the metal, and therefore at high temperature the stabilization against the attack of oxygen is lost, because the oxide layer evaporates. They all are relatively stable against acids.[6]

Applications

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Refractory metals, and alloys made from them, are used inlighting, tools,lubricants,nuclear reactioncontrol rods, ascatalysts, and for theirchemical or electrical properties. Because of their highmelting points, refractory metal components are never fabricated bycasting. The process ofpowder metallurgy is used: powders of the pure metal are compacted, heated using electric current, and further fabricated by cold working with annealing steps. Refractory metals and their alloys can be worked intowire,ingots,rebars,sheets, orfoil.

Molybdenum alloys

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Main articles:Molybdenum andMolybdenum § Applications

Molybdenum-based alloys are widely used, because they are cheaper than superior tungsten alloys. The most widely used alloy of molybdenum is theTitanium-Zirconium-Molybdenum alloy TZM, composed of 0.5% titanium and 0.08% of zirconium (with molybdenum being the rest). The alloy exhibits a higher creep resistance and strength at high temperatures, making service temperatures of above 1060 °C possible for the material. The high resistivity of Mo-30W, an alloy of 70% molybdenum and 30% tungsten, against the attack of moltenzinc makes it the ideal material for casting zinc. It is also used to construct valves for molten zinc.[11]

Molybdenum is used inmercury-wetted reed relays, because molybdenum does not formamalgams and is therefore resistant to corrosion by liquidmercury.[12][13]

Molybdenum is the most commonly used of the refractory metals. Its most important use is as a strengtheningalloy ofsteel.Structural tubing andpiping often contains molybdenum, as do manystainless steels. Its strength at high temperatures, resistance to wear, and lowcoefficient of friction are all properties which make it invaluable as an alloying compound. Its excellent anti-friction properties lead to its incorporation ingreases andoils where reliability and performance are critical. Automotiveconstant-velocity joints use grease containing molybdenum. The compound sticks readily to metal and forms a very hard, friction-resistant coating. Most of the world's molybdenumore can be found in China, theUSA, Chile, andCanada.[14][15][16][17]

Tungsten and its alloys

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Main articles:Tungsten andTungsten § Applications

Tungsten was discovered in 1781 bySwedish chemistCarl Wilhelm Scheele. Tungsten has the highest melting point of all metals, at 3,410 °C (6,170 °F).

Filament of a 200 watt incandescent lightbulb highly magnified

Up to 22%Rhenium is alloyed with tungsten to improve its high-temperature strength and corrosion resistance.Thorium as an alloying compound is used when electric arcs have to be established: ignition is easier and the arc burns more stably than without the addition of thorium. For powder metallurgy applications, binders have to be used for the sintering process. For the production of tungsten heavy alloys, binder mixtures ofnickel andiron or nickel andcopper are widely used. The tungsten content of the alloy is normally above 90%. The diffusion of the binder elements into the tungsten grains is low even at thesintering temperatures and therefore the interior of the grains are pure tungsten.[18]

Tungsten and its alloys are often used in applications where high temperatures are present but a high strength is still necessary and the high density is not troublesome.[19] Tungsten-wire filaments provide the vast majority of householdincandescent lighting, but are also common in industrial lighting as electrodes in arc lamps. Lamps get more efficient in the conversion of electric energy to light with higher temperatures, so a high melting point is essential for the application as filament in incandescent light.[20]Gas tungsten arc welding (GTAW, also known as tungsten inert gas (TIG) welding) equipment uses a permanent, non-meltingelectrode. The high melting point and the wear resistance against the electric arc makes tungsten a suitable material for the electrode.[21][22]

Tungsten's high density and strength are also key properties for its use in weaponprojectiles, for example as an alternative todepleted uranium for tank gun rounds.[23] Its high melting point makes tungsten a good material for applications likerocket nozzles, for example in theUGM-27 Polaris.[24] Some of the applications of tungsten are not related to its refractory properties but simply to its density. For example, it is used in balance weights for planes and helicopters or for heads ofgolf clubs.[25][26] In these applications, similar dense materials like the more expensiveosmium can also be used.

The most common use for tungsten is as the compoundtungsten carbide indrill bits, machining and cutting tools. The largest reserves of tungsten are inChina, with deposits inKorea,Bolivia,Australia, and other countries.

It also finds itself serving as alubricant,antioxidant, in nozzles and bushings, as a protective coating, and in many other ways. Tungsten can be found in printing inks,x-ray screens, in the processing ofpetroleum products, and flame proofing oftextiles.

Niobium alloys

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Main articles:Niobium § Applications, andNiobium alloy
Image of the Apollo Service Module with the moon in the background
Apollo CSM with the dark rocket nozzle made from niobium-titanium alloy

Niobium is nearly always found together with tantalum, and was named afterNiobe, the daughter of themythicalGreek kingTantalus for whom tantalum was named. Niobium has many uses, some of which it shares with other refractory metals. It is unique in that it can be worked through annealing to achieve a wide range of strength andductility, and is the least dense of the refractory metals. It can also be found inelectrolytic capacitors and in the most practicalsuperconducting alloys. Niobium can be found inaircraftgas turbines,vacuum tubes, andnuclear reactors.

An alloy used forliquid rocket thruster nozzles, such as in the main engine of theApollo Lunar Modules, is C103, which consists of 89% niobium, 10% hafnium and 1% titanium.[27] Anotherniobium alloy was used for the nozzle of theApollo Service Module. As niobium is oxidized at temperatures above 400 °C, a protective coating is necessary for these applications to prevent the alloy from becoming brittle.[27]

Tantalum and its alloys

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Main articles:Tantalum andTantalum § Applications

Tantalum is one of the mostcorrosion-resistant substances available. Many important uses have been found for tantalum owing to this property, particularly in themedical andsurgical fields, and also in harshacidic environments. It is also used to make superior electrolytic capacitors. Tantalum films provide the second mostcapacitance per volume of any substance afterAerogel,[citation needed] and allowminiaturization ofelectronic components andcircuitry. Manycellular phones andcomputers contain tantalum capacitors.

Rhenium alloys

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Main article:Rhenium

Rhenium is the most recently discovered refractory metal. It is found in low concentrations with many other metals, in the ores of other refractory metals,platinum orcopper ores. It is useful as an alloy to other refractory metals, where it addsductility andtensile strength. Rhenium alloys are used in electronic components,gyroscopes andnuclear reactors. Rhenium finds its most important use as a catalyst. It is used as a catalyst in reactions such asalkylation,dealkylation,hydrogenation andoxidation. However, its rarity makes it the most expensive of the refractory metals.[28]

Advantages and shortfalls

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The strength and high-temperature stability of refractory metals make them suitable for hotmetalworking applications and forvacuum furnace technology. Many special applications exploit these properties: for example, tungsten lamp filaments operate at temperatures up to 3073 K, and molybdenum furnace windings withstand 2273 K.

However, poor low-temperature fabricability and extremeoxidability at high temperatures are shortcomings of most refractory metals. Interactions with the environment can significantly influence their high-temperature creep strength. Application of these metals requires a protective atmosphere or coating.

The refractory metal alloys of molybdenum, niobium, tantalum, and tungsten have been applied to space nuclear power systems. These systems were designed to operate at temperatures from 1350 K to approximately 1900 K. An environment must not interact with the material in question. Liquidalkali metals as the heat-transfer fluids are used as well as theultra-high vacuum.

The high-temperaturecreepstrain of alloys must be limited for them to be used. The creep strain should not exceed 1–2%. An additional complication in studying creep behavior of the refractory metals is interactions with environment, which can significantly influence the creep behavior.

See also

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  • Refractory – heat resistance of nonmetallic materials

References

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  1. ^"International Journal of Refractory Metals and Hard Materials". Elsevier. Retrieved7 February 2010.
  2. ^Bauccio, Michael; American Society for Metals (1993)."Refractory metals".ASM metals reference book. ASM International. pp. 120–2.ISBN 978-0-87170-478-8.
  3. ^Metals, Behavior Of; Wilson, J. W (1 June 1965). "General Behaviour of Refractory Metals".Behavior and Properties of Refractory Metals. Stanford University Press. pp. 1–28.ISBN 978-0-8047-0162-4.
  4. ^"Refractory Metal - an overview".ScienceDirect Topics. Elsevier. Retrieved23 November 2020.
  5. ^Davis, Joseph R (2001).Alloying: understanding the basics. ASM International. pp. 308–333.ISBN 978-0-87170-744-4.
  6. ^abBorisenko, V. A. (1963). "Investigation of the temperature dependence of the hardness of molybdenum in the range of 20–2500°C".Soviet Powder Metallurgy and Metal Ceramics.1 (3):182–186.doi:10.1007/BF00775076.S2CID 137686216.
  7. ^Fathi, Habashi (2001). "Historical Introduction to Refractory Metals".Mineral Processing and Extractive Metallurgy Review.22 (1):25–53.Bibcode:2001MPEMR..22...25H.doi:10.1080/08827509808962488.S2CID 100370649.
  8. ^Greenwood, Norman N.; Earnshaw, Alan (1997).Chemistry of the Elements (2nd ed.).Butterworth-Heinemann. pp. 978, 1005, 1043.doi:10.1016/C2009-0-30414-6.ISBN 978-0-08-037941-8.
  9. ^Schmid, Kalpakjian (2006)."Creep".Manufacturing engineering and technology. Pearson Prentice Hall. pp. 86–93.ISBN 978-7-302-12535-8.
  10. ^Weroński, Andrzej; Hejwowski, Tadeusz (1991)."Creep-Resisting Materials".Thermal fatigue of metals. CRC Press. pp. 81–93.ISBN 978-0-8247-7726-5.
  11. ^Smallwood, Robert E. (1984)."TZM Moly Alloy".ASTM special technical publication 849: Refractory metals and their industrial applications: a symposium. ASTM International. p. 9.ISBN 978-0-8031-0203-3.
  12. ^Kozbagarova, G. A.; Musina, A. S.; Mikhaleva, V. A. (2003). "Corrosion Resistance of Molybdenum in Mercury".Protection of Metals.39 (4):374–6.doi:10.1023/A:1024903616630.S2CID 91428385.
  13. ^Gupta, C. K. (1992)."Electric and Electronic Industry".Extractive Metallurgy of Molybdenum. CRC Press. pp. 48–49.ISBN 978-0-8493-4758-0.
  14. ^Magyar, Michael J."Commodity Summary 2009:Molybdenum"(PDF).United States Geological Survey. Retrieved1 April 2010.
  15. ^Ervin, D. R.; Bourell, D. L.; Persad, C.; Rabenberg, L. (1988). "Structure and properties of high energy, high rate consolidated molybdenum alloy TZM".Materials Science and Engineering: A.102:25–30.doi:10.1016/0025-5416(88)90529-0.
  16. ^Oleg D., Neikov (2009)."Properties of Molybdenum and Molybdenum Alloys powder".Handbook of Non-Ferrous Metal Powders: Technologies and Applications. Elsevier. pp. 464–6.ISBN 978-1-85617-422-0.
  17. ^Davis, Joseph R. (1997)."Refractory Metalls and Alloys".ASM specialty handbook: Heat-resistant materials. ASM International. pp. 361–382.ISBN 978-0-87170-596-9.
  18. ^Lassner, Erik; Schubert, Wolf-Dieter (1999).Tungsten: properties, chemistry, technology of the element, alloys, and chemical compounds. Springer. pp. 255–282.ISBN 978-0-306-45053-2.
  19. ^National Research Council (U.S.), Panel on Tungsten, Committee on Technical Aspects of Critical and Strategic Material (1973).Trends in Usage of Tungsten: Report. National Academy of Sciences-National Academy of Engineering. pp. 1–3.
  20. ^Lassner, Erik; Schubert, Wolf-Dieter (1999).Tungsten: properties, chemistry, technology of the element, alloys, and chemical compounds. Springer.ISBN 978-0-306-45053-2.
  21. ^Harris, Michael K. (2002)."Welding Health and Safety".Welding health and safety: a field guide for OEHS professionals. AIHA. p. 28.ISBN 978-1-931504-28-7.
  22. ^Galvery, William L.; Marlow, Frank M. (2001).Welding essentials: questions & answers. Industrial Press. p. 185.ISBN 978-0-8311-3151-7.
  23. ^Lanz, W.; Odermatt, W.; Weihrauch3, G. (7–11 May 2001).KINETIC ENERGY PROJECTILES: DEVELOPMENT HISTORY, STATE OF THE ART, TRENDS(PDF). 19th International Symposium of Ballistics. Interlaken, Switzerland.{{cite conference}}: CS1 maint: numeric names: authors list (link)
  24. ^Ramakrishnan, P. (1 January 2007)."Powder metallurgyfor Aerospace Applications".Powder metallurgy : processing for automotive, electrical/electronic and engineering industry. New Age International. p. 38.ISBN 978-81-224-2030-2.
  25. ^Arora, Arran; Venu Gopal Rao (2004). "Tungsten Heavy Alloy For Defence Applications".Materials Technology.19 (4):210–6.Bibcode:2004MaTec..19..210A.doi:10.1080/10667857.2004.11753087.S2CID 139045633.
  26. ^Moxson, V. S.; (sam) Froes, F. H. (2001). "Fabricating sports equipment components via powder metallurgy".JOM.53 (4): 39.Bibcode:2001JOM....53d..39M.doi:10.1007/s11837-001-0147-z.S2CID 135653323.
  27. ^abHebda, John (2 May 2001)."Niobium alloys and high Temperature Applications"(PDF).Niobium Science & Technology: Proceedings of the International Symposium Niobium 2001 (Orlando, Florida, USA). Companhia Brasileira de Metalurgia e Mineração. Archived fromthe original(PDF) on 17 December 2008.
  28. ^Wilson, J. W. (1965)."Rhenium".Behavior and Properties of Refractory Metals. Stanford University Press.ISBN 978-0-8047-0162-4.

Further reading

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  • Levitin, Valim (2006).High Temperature Strain of Metals and Alloys: Physical Fundamentals. Wiley.ISBN 978-3-527-31338-9.
  • Brunner, T (2000). "Chemical and structural analyses of aerosol and fly-ash particles from fixed-bed biomass combustion plants by electron microscopy".1st World Conference on Biomass for Energy and Industry: proceedings of the conference held in Sevilla, Spain, 5–9 June 2000. London: James & James.ISBN 1-902916-15-8.
  • Spink, Donald (1961). "Reactive Metals. Zirconium, Hafnium, and Titanium".Industrial & Engineering Chemistry.53 (2):97–104.doi:10.1021/ie50614a019.
  • Hayes, Earl (1961). "Chromium and Vanadium".Industrial & Engineering Chemistry.53 (2):105–7.doi:10.1021/ie50614a020.
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