EP0187741A4 - Metal a base de metaux de transition de groupe ivb et ses procedes de production. - Google Patents

Metal a base de metaux de transition de groupe ivb et ses procedes de production.

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Publication number
EP0187741A4
EP0187741A4 EP19840902748 EP84902748A EP0187741A4 EP 0187741 A4 EP0187741 A4 EP 0187741A4 EP 19840902748 EP19840902748 EP 19840902748 EP 84902748 A EP84902748 A EP 84902748A EP 0187741 A4 EP0187741 A4 EP 0187741A4
Authority
EP
European Patent Office
Prior art keywords
transition metal
particles
metal
group ivb
zinc alloy
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Ceased
Application number
EP19840902748
Other languages
German (de)
English (en)
Other versions
EP0187741A1 (fr
Inventor
Robert A Hard
Joseph A Megy
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Occidental Research Corp
Original Assignee
Occidental Research Corp
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Occidental Research Corp filed Critical Occidental Research Corp
Publication of EP0187741A1 publication Critical patent/EP0187741A1/fr
Publication of EP0187741A4 publication Critical patent/EP0187741A4/fr
Ceased legal-status Critical Current

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Classifications

    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C1/00Making non-ferrous alloys
    • C22C1/04Making non-ferrous alloys by powder metallurgy
    • C22C1/045Alloys based on refractory metals
    • C22C1/0458Alloys based on titanium, zirconium or hafnium
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F1/00Metallic powder; Treatment of metallic powder, e.g. to facilitate working or to improve properties
    • B22F1/14Treatment of metallic powder
    • B22F1/145Chemical treatment, e.g. passivation or decarburisation
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F1/00Metallic powder; Treatment of metallic powder, e.g. to facilitate working or to improve properties
    • B22F1/14Treatment of metallic powder
    • B22F1/148Agglomerating
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F9/00Making metallic powder or suspensions thereof
    • B22F9/16Making metallic powder or suspensions thereof using chemical processes
    • B22F9/18Making metallic powder or suspensions thereof using chemical processes with reduction of metal compounds
    • B22F9/24Making metallic powder or suspensions thereof using chemical processes with reduction of metal compounds starting from liquid metal compounds, e.g. solutions

Definitions

  • Group IVb transition metals specifically titanium, zirconium and hafnium
  • titanium, zirconium and hafnium are essential to the aerospace, nuclea and the chemical processing industries.
  • the high strength and excellent resistance to chemical attack of metals having titanium, zirconium and hafnium as a base are the principal reasons for their demand.
  • Demand for Group IVb metals has outstripped production capabilities in some countries. Titanium is a strong, light metal that is useful at many temperatures, malleable when heated and ductile when pure. It is used in the pure state or in alloys for aircraft and chemical industry, for surgical instruments, and in cermets, and metal-ceramic braising.
  • Zirconium is a hard metal that is strong and ductile and is used in the nuclear industry and in alloys, pyrotechnics, welding fluxes and explosives. Hafnium, although not as widely used because of its relative expense, is used primarily in the nuclear and chemical process industries. For many uses, alloys which are based on the Group IVb metals have better propertie and wider usage than the pure metals themselves.
  • Impurities outside specification values in the Group IVb metals and alloys based on the Group IVb metals can cause such metals and alloys based thereon to be brittle and hence, of little use.
  • Impurities such as halides, carbon, oxygen, nitrogen and silicon can cause the Group IVb metals and alloy based thereon to be greatly reduced in strength and chemical resistance.
  • Small amounts of silicon and oxygen can be used in Group IVbtransition metal alloys, such as hafnium and zir ⁇ conium alloys.
  • the Group IVb metals and alloys based thereon are also useful in powder metallurgy for the production of articles which would be more expensive or more difficult to produce by machining or forging from massive metal shapes.
  • This invention is directed toward the production of Group IVb metal powders and alloy powders based on Group IVb metals. Articles made by powder metallurgy from such powders can be ground, milled, drilled and welded.
  • This invention relates to the passified Group IVb transition metal-based particles, and alloys based thereon, which are substantially free of halides, and which are suitable for powder metallurgy usage without further par ⁇ ticle size reduction, and processes for the production thereof.
  • particles as used herein is meant to include powders and granules as well as particles.
  • a very important advantage of this invention is the capability of producing metal shapes, i.e., near net shapes, directly from a metal sponge without the necessity of an - expensive arc melting step which is required in conventional technology for consolidation or alloying of the Group IVb transition metals.
  • such passified Group IVb transition metal-based metal particles are produced by heating a Group IVb transi ⁇ tion metal-zinc alloy which is substantially free of halides, at a temperature between about 500°and about 1150°C under conditions which are operative to vaporize and separate the zinc from such alloy and to produce a Group IVb transi ⁇ tion metal sponge or metal based sponge thereon which is substantially free of both zinc and halides.
  • metal sponges have an internal porosity of between about 1% to about 5% by volume.
  • the metal sponges of the present inven ⁇ tion have internal porosities of between about 10% to about 30% by volume.
  • substantially free of zinc herein is meant less than 0.1% by weight.
  • substantially free of halides herein is meant less than 0.02%.
  • no more than about 100 parts per million by weight (PPM) of zinc and about 50 PPM of halides are contained in the Group IVb transition metal-zinc alloy.
  • the Group IVb metal or alloy thereof has less than about 10 PPM metal halide.
  • •5 IVb transition metal-zinc alloy can be comminuted to or formed into particles and the zinc distilled off as des ⁇ cribed herein to produce Group IVb transition metal powder.
  • the transition metal-zinc alloy is brittle.
  • the transition metal-zinc alloy contains no alloying agents
  • the Group IVb transition metal-zinc alloy can be formed into small particles by conventional means known to the art, such as shot tower processing in a non- deleteriously reactive atmosphere, such as a halium or 5 argon atmosphere.
  • Group IVb transition metals prepared by conventional processes such as the Hunter process or Kroll process for titanium, contain halide salts, such as sodium chloride or magnesium chloride. With conventional processes, it is
  • Group IVb transition metals having halide contents of less than 2000 PPM.
  • Halides form fine small holes in Group IVb transition metals which act as crack initiators and make the metal laible to fatigue cracking. In addition, it is very difficult to obtain
  • Group IVb transition metals having a halide content of more than 50 PPM 25 good welds on Group IVb transition metals having a halide content of more than 50 PPM.
  • O PI_ metallurgy processes are capital intensive and energy intensive.
  • Group IVb transition metal-zinc alloy herein is meant a titanium-zinc alloy or zirconium-zinc or hafnium- zinc alloy.
  • produced transition metal or metal based thereon is heated to, or maintained at, a temperature between about 850° and about 1250°C, preferably between about 1020° and about 1060°C, under conditions which are operative to sinter the transition metal. Sintering is necessary in order to reduce the surface area of the Group IVb transition metal-based metal particles and thus reduce the amount of oxygen or nitrogen required for subsequent passification of the transition metal, or alloy based thereon, so that it may be readily and safely stored and used for powder metallurgy at a later time.
  • the particles of Group IVb transi ⁇ tion metal-based metal shrink in size by about 50 to about 85% but in general retain their original shape.
  • Such sintered particles are not fused together although usually there is some sticking or adhering of the particles to each other.
  • adhered particles can be readily separa ⁇ ted by mechanical means.
  • the particles of sintered transition metal values are cooled to a lower temperature between about 300°and 700°C during which time they are simultaneously contacted with hydrogen or a gaseous stream containing hydrogen under conditions which are operative to hydride and em ⁇ brittle the sintered transition metal values.
  • transition metal values herein is meant either a Group IVb transition metal or a Group IVb transition metal-based metal.
  • the hydrided and embrittled transition metal values can now be readily comminuted to a predetermined
  • the hydriding and subsequent embrittlement greatly facilitates controlling the commi ⁇ nution of the Group IVb transition metal values.
  • the improved controllability afforded by the hydriding of the Group IVb transition metal values is a particularly important aspect of this invention because it ultimately enables the production of a passified Group IVb transi ⁇ tion metal-based metal particles of a size distribution readily adaptable and operable for powder metallurgy usage.
  • Such hydrided and embrittled transition metal-based metal particles are comminuted under a nondeleteriously- reactive atmosphere, to a predetermined particle size distribution.
  • the comminuted transition metal values are treated at a temperature between about 400° and about 700°C, preferably between about 600° and about 700°C under conditions operative to remove essentially all hydrogen values from the comminuted transition metal values and to produce Group IVb transition metal-based metal particles.
  • removing essentially all hydrogen values from the comminuted transition metal values is meant that the transition metal values contain no more than about 200 PPM of hydrogen.
  • the dehydrided Group IVb transition metal-based metal particles are then contacted with a small or effec- ' tive amount of a gas selected from the group consisting of oxygen, nitrogen and mixtures thereof, under conditions operative to passify the transition metal particles thereby producing passified transition metal particles.
  • a gas selected from the group consisting of oxygen, nitrogen and mixtures thereof under conditions operative to passify the transition metal particles thereby producing passified transition metal particles.
  • the controlled comminuting of the hydrided and embrittled transition metal values is such that the passified transi ⁇ tion metal-based metal particles ultimately produced have at least a substantial amount by weight of such
  • transition metal-based metal particles which are suitable for powder metallurgy usage without further particle size reduction.
  • a substantial amount is meant at least about 50% by weight of the passified transition metal-based metal particles produced.
  • at least about 95% by weight of the particles produced are suitable for powder metallurgy use without further particle size reduction.
  • particles no greater than about 1/4 inch, preferably from +200 to -30 mesh (U.S. Sieve Series) are suitable for powder metallurgy usage without further particle size reduction. It is to be noted that this embodiment of this invention is particularly useful where extremely fine powder metallurgical particles are required or where a yield of suitable powder is required, or where a highly tailored particle size distribution is required which is not easily or economically obtainable by other means.
  • the heating of the Group IVb transition metal-zinc alloy tc vaporize zinc therefrom, and the subsequent sintering' of the trans ⁇ ition metal values produced thereby is conducted in the same zone or vessel.
  • the hydrid ⁇ ing and embrittle ent of the sintered transition metal values are also conducted in the same zone or vessel as the zinc vaporization and sintering steps.
  • the nondeleteriously-reactive atmosphere used during the comminuting of the embrittled transition metal values and/or sintering of the Group IVb transition metal values is an inert gas, such as argon or helium.
  • the nondeleteriously-reactive atmosphere used during the comminuting step is hydrogen.
  • such heating is conducted under a continuous flow of a nondeleteriously-reactive sweep gas.
  • the sweep gas is selected from the Group consisting of hydrogen, inert gas (such as, argon or helium) , and mixtures thereof.
  • the dehydriding and/or sintering of the particles of transi ⁇ tion metal values is conducted under a partial vacuum.
  • Group IVb transition metal-based metal particles which are substantially free of halides, and which are suitable for powder metallurgy usage, from a Group IVb transition metal- zinc alloy comprises forming a Group IVb transition metal- zinc alloy which is substantially free of halides, into
  • transition metal values will comprise essentially the pure Group IVb transition metal or such metal with minor amounts of other metals desirable in the ultimate final
  • a titanium-based metal alloy may contain, by weight per ⁇ cent, 0 to about 5% tin, 0 to about 10% vanadium, 0 to about 10% aluminum, 0 to about 5% zirconium, 0 to about 5% molybdenum, 0 to about 10% silicon, 0 to about 10% iron, 0 to about 0.5% oxygen and mixtures thereof.
  • a hafnium or zirconium-based metal alloy may contain, by weight percent, 0 to about 3% tin, 0 to about 0.40% iron, 0 to about 0.02% chronium, 0 to about 0.01% nickel, 0 to about 0.5% oxygen and mixtures thereof.
  • a titanium, hafnium or zirconium alloy will normally comprise at least 90% by weight titanium, hafnium or zirconium, respectively; although such alloys can contain less than about 90% by weight titanium, hafnium or zirconium, respectively.
  • the thusly formed particles which are substantially free of zinc and halides are then heated to, or maintained at, a sintering temperature between about 850° and 1250°C under conditions operative to sinter such particles.
  • a sintering temperature between about 850° and 1250°C under conditions operative to sinter such particles.
  • sintering results in a reduction of the surface area of such particles and because of the reduction in surface area, subsequent passification with a passifying gas will require a substantially less amount of such gas and thus reduce the oxygen and/or nitrogen content of the Group IVb transition metal-based metal.
  • the sintered particles are then cooled to a te - perature between about ambient and about 200°C, preferably between about ambient and about 60°C, and then contacted with a small or effective amount of a gas selected from
  • Group IVb passified transition metal-based metal particles which are substantially free of halides.
  • An important feature of this embodiment of this invention is the forming of a transition metal-zinc alloy of a specified and particular particle size distribution such that the Group IVb transition metal-zinc alloy particles will have a particle size distribution of about 90% by weight between about 80 mesh and about 1/4 inch, and the subsequent sintering of such particles at a sintering temperature between about 850° and 1250°C, in combination with the other steps of this process, are operative to cause the passified transition metal-based metal particles ultimately produced to have a particle size distribution such that a significant amount by weight of said passified Group IVb metal-based metal particles are suitable for powder metallurgy usage with- out additional particle size reduction.
  • significant amount by weight suitable for powder metallurgy usage without additional particle size reduction as used herein is meant at least about 5% by weight.
  • This embodiment of this invention is, however, capable of producing particles wherein at least about 80% by weight are suitable for powder metallurgy usage without additional particle size reduction.
  • An advantage of the invention is that the shape or configuration of the feed Group IVb transition metal-zinc alloy particles prior to vaporization of the zinc therefrom, and the subsequent sintering of the particles of Group IVb transition metal values produced from said vaporization of zinc from the metal-zinc alloy, produces particles having about 15 to about 50% of the volume of the feed alloy particles. Thus, it is possible to predetermine the shape of the feed alloy particles and produce pseudomorph parti- cles of the feed alloy particles.
  • the heating or distillation of the particles of transition metal-zinc alloy at a temperature between about 500° and about 1150°C, and the subsequent sintering of the zinc free particles therefrom, are conducted in the same zone or vessel.
  • the cooling and passification of the sintered particles are also conducted in the same zone or vessel as the zinc vaporization and sintering steps.
  • the heating or distillation of the Group IVb transition metal-zinc alloy to vaporize and separate zinc therefrom is conducted under a partial vacuum.
  • the nondeleteriously- reactive sweep gas used in the heating or distillation of the Group IVb transition metal-zinc alloy is an inert gas.
  • such nondeleteriously-reactive sweep gas is hydrogen.
  • hydrogen is used as the sweep gas, it is necessary to remove all hydrogen values from the final Group IVb transition metal-base particles since hydrogen will cause embrittlement of such particles. Hydrogen can be removed during the dehydriding step described herein.
  • the Group IVb transition metal-zinc alloy particles have a particle size distribution of about 90% by weight between about 60 mesh and about 20 mesh before such particles are heated or distilled at a temperature between about 500 and about 1150°C to vaporize the zinc therefrom.
  • the forming of a Group IVb transition metal-zinc alloy into such particles is by comminuting of the alloy.
  • such particles are formed by casting the Group IVb transition metal-zinc alloy into particles; preferably, particles of -1/4 inch mesh.
  • the Group IVb transition metal-zinc alloy is produced by a process com ⁇ prising fluorinating a Group IVb transition metal-bearing ore, which comprises Group IVb transition metal oxides, b contacting with an alkali metal fluosilicate at a temperature of from about 600° to about 1000°C to form a fluorinated ore and to convert the Group IVb transition metal oxides to Group IVb transition metal fluorides; and reducing such fluorides with a zinc reductant metal alloy, such as an aluminum-zinc alloy, to produce the Group IVb transition metal-zinc alloy.
  • the Group IVb transition metal-zinc alloy can be prepared as shown in the process illustrated in Fig. 1.
  • the alloy may be prepared by adding Group IVb transition metal sponge into a molten batch of zinc agitated to form the Group IVb transition metal-zinc alloy substantially free of halide.
  • the metal sponge or scrap contains halide, such as sodium halide, the halide salt separates from the metal and metal-zinc alloy when the metal-zinc alloy is formed.
  • the halide salt is immiscible with the metal zinc alloy and floats to the surface of the molten alloy as a separate phase which can be separated from the alloy by conventional means to produce a Group IVb transition metal alloy substantially free of halide.
  • a solid zinc metal and a solid Group IVb transition metal may be melted together to form the Group IVb transition metal-zinc alloy substan ⁇ tially free of halide.
  • Halide salts present in the Group IVb transition metal are immiscible with the resulting Group IVb transition metal-zinc alloy and float to the top of the alloy as a separate phase which can be separa- ted from the alloy.
  • the alloying agent may be incorporated into the molten zinc batch prior to introduction of the Group IVb transition metal, or added with the Group IVb transition metal to the molten-zinc batch, or co-melted with the solid zinc metal and the solid Group IVb transition metal.
  • the Group IVb transition metal-zinc alloy can be prepared from Group IVb transition metal halide salts as set forth in the process illustrated in Fig. 1 by adding the Group IVb transition metal halide salt with a zinc and a reductant metal, such as and preferably aluminum, by melting and agitating the resulting mixture.
  • a reductant metal such as and preferably aluminum
  • an alkali metal halide salt may be added to the mixture to form a floating phase immiscible with the metal alloy which inhibits the vaporization of the molten zinc.
  • alloying agents may be added to produce a Group IVb transition metal-zinc-alloy containing the desired
  • alloying agents to yield a Group IVb transition metal based metal alloy product as described herein.
  • the various components may be mixed together and melted as a mix or alternatively the various ingredients may be added to molten zinc or the molten batch of zinc and the reductant metal.
  • the Group IVb transition metal salt may be contacted with the zinc and reductant metal to form the Group IVb transition metal-zinc alloy substantially free of halide and separated from the reaction mixture. Alloy agents may then be added to the molten Group IVb transition metal-zinc alloy to incorporate the desired alloying agents.
  • Such Group IVb transition metal- zinc alloy, with or without additional alloying agents may be treated as described herein to produce passified Group IVb transition metal-based metal powders suitable for metallurgy usage which are substantially free of halide and zinc.
  • the entire process is conducted at temperatures which are nc higher than about 1300°C, and in a preferred embodiment, the entire process is conducted at temperatures which are no higher than about 1200°C, and in an especially preferred embodiment, at a temperature no higher than 1150°C to prevent sintering of the Group IVb transition metal particles.
  • the temperatures reached during the conventional high temperature arc melting processes required for consolidation of, and/or alloying of, for example, titanium products produced by conventional processes, such as, the "Kroll Process" are not required. In other words, the high temperatures required for arc melting are simply not required for this process.
  • Arc melting processes generally require temperatures which
  • Some of the advantages of using hydrogen as the sweep gas in the heating or distillation step to vaporize zinc from the Group IVb transition metal-zinc alloy are hydrogen because of its low molecular weight, it facili ⁇ tates the diffusion of zinc out of the Group IVb transition metal sponge pores and by virtue of such improved diffusion improved heat transfer during the distillation is also realized.
  • hydrogen is cheaper than helium and argon and other inert gases.
  • the hydrogen tie bond between hydrogen and the Group IVb transition metal is weak, even the weak hydrogen tie bond will more readily displace zinc as opposed to inert gases where there is no tie bond between the inert gas and the Group IVb transition metal at all.
  • substantially all hydrogen values must be removed from the final metal particle product.
  • Hydrogen can be removed from the metal particles by heating the particles to a temperature at from about 600° to about 700°C, pre ⁇ ferably under a partial vacuum.
  • substantially all hydrogen values being removed from the final metal particle product it is meant that no more than about 200 PPM of hydrogen is permitted in the final metal particles produced, and preferably no more than about 50 PPM of hydrogen is in the final product. This is to be compared with conven ⁇ tional process which produce particles having 200PPM of
  • the metal sponge comprising Group IVb transition
  • metal-based metal, of the present invention is character ⁇ ized in having less than 50 PPM of halides and an internal porosity of at least 10% by volume.
  • the metal has less than about 10 PPM halide and an internal porosity of at least 20% by volume.
  • Angular shaped powder particles are irregular shaped particles with irregular
  • the metal sponge of the present invention is unequaled and no Group IVb transition metal-based metal sponge having the low halide, hydrogen and carbon contamination and high internal porosity described herein have been prepared
  • the powder metal of the present invention is unique and no Group IVb transition metal-based metal powder having the low halide, hydrogen, oxygen, nitrogen
  • the Group IVb transition metal-based metal powder and sponge of the present invention are superior metals for metallurgical use.
  • the low halide content is essen ⁇ tial for maximum metal strength, toughness and durability.
  • the high internal porosity and angular particle shape of the powder permits the fabrication by conventional powder metallurgical processes of strong, durable and defect free shaped Group IVb transition metal-based metal pieces, such as shaped articles, plates, sheets, pipes, rods, beams and billets.
  • the compressibility of the powder and the angular particles of the powder permit the parti ⁇ cles to be closely pressed together and securely interlocked when pressed into the desired shapes yielding a cold pressed article with greater green strength than conventional Group IVb transition metal powders for powder metallurgy usage which have higher amounts of contaminants, very little internal porosity and spherical shaped powder particles.
  • the Group IVb transition metal-zinc alloy can contain any desirable additional alloying agents such as aluminum, vanadium or other beneficial elements, which are desir ⁇ able in the final product particles. Such alloying agents are not required to be added in a high temperature arc melting step. In fact, arc melting is not required in this invention.
  • the alloying agents can be added to the Group IVb transition metal when it is in the form of the Group IVb transition metal-zinc alloy or when such
  • the alloying agent can be added to molten zinc to form a molten zinc alloy.
  • the Group IVb transition metal such as titanium metal sponge, can be added to the molten zinc alloy to form a Group IVb transition metal-based metal zinc alloy.
  • a Group IVb transition metal halide salt such as sodium fluotitanate, can be added to the molten zinc alloy when a reductant metal, such as aluminum, is present to reduce the halide salt and produce the Group IVb transition metal-based metal zinc alloy which is recovered by separa ⁇ ting it from the floating slog, containing the halide salt of the reductant metal, formed during the reduction of the Group IVb transition metal halide salt.
  • Such alloying agents remain with the Group IVb transition metal as the zinc is vaporized and separated therefrom.
  • the heating or distillation of zinc from the alloy is conducted at a temperature between about 900° and about 950°C, sintering is conducted between about 1020 and about 1060°C, embrittlement and hydriding is conducted between about 600° and about 700°C, and passification is conducted at about ambient to about 60°C.
  • a particular advantage of this process is the avoidance of entrapment of halide salts in the passified transition metal-based metal particle product.
  • Another advantage is that heating or distillation to vaporize and separate zinc and sintering may be conducted in the same zone, reactor, or vessel.
  • Fig. 1 is a flow sheet of one embodiment of this invention which comprises hydriding and dehydriding steps.
  • Fig. 2 is an alternate embodiment of this invention which does not require hydriding and dehydriding steps.
  • Fig. 3 is an alternative embodiment of this inven ⁇ tion which does not require the sintering step.
  • Fig. 4 is an alternative embodiment of this invention which does not require a sintering step.
  • Fig. 5 is a further alternate embodiment of this invention which does not require the hydriding and dehy ⁇ driding steps, and, optionally, does not require the sintering step.
  • Fig. 6 is a flow sheet of one embodiment of this invention which comprises preparing a passified Group IVb transition metal-based metal powder from a passified Group IVb transition metal sponge.
  • ilmenite 8 an ore comprising titanium and iron oxides, is ground to a finely divided physical state in zone 10 to make it more susceptible to fluorination, such as between 30 and 400 mesh.
  • the ore is fluorinated in zone 20 with a fluosilicate such as sodium fluosilicate introduced in stream 14.
  • the mixture of sodium fluosilicate and ore is heated to a temperature of at least about 600°C preferably from 750° to 950°C for a time sufficient to change the iron and titanium from oxide form to fluoride form.
  • the addition of carbon by stream 16 to the mixture has been found to have a syner- gistic effect on the fluorination of the ore.
  • the reaction is carried out under an atmosphere of a gaseous fluorinating agent such as silicon tetrafluoride which can be generated in situ, or which can be introduced by stream 18.
  • a gaseous fluorinating agent such as silicon tetrafluoride which can be generated in situ, or which can be introduced by stream 18.
  • the fluorination reaction may be carried out under a partial pressure of from about 0.1 to about 500 psig of silicon tetrafluoride.
  • the husly fluorinated ore is then leached in zone 30 with an aqueous solution of a strong acid such as hydrochloric or sulfuric acid introduced in stream 24.
  • the leaching is conducted under conditions to solubilize as much of the fluorides of titanium as economically possible. Leaching may be enhanced with addition of aqueous hydrogen fluoride solu ⁇ tion.
  • the mixture is passed to zone 40 in stream 32 and filtered to remove silica, residual ilmenite ore and other insoluble material in stream 42.
  • the filtrate in stream 44 comprises soluble fluorides of titanium and as for example sodium fluotitanate.
  • the solution may be evapora ⁇ ted in zone 50 to remove water in stream 52 and concentrate
  • zones 50, 60 and 70 can be all in one zone or vessel.
  • the molten titanium fluoride salts and the zinc-aluminum alloy are essentially immiscible. Reduc ⁇ tion is conducted at a temperature of at least about 650°C up to about 1000°C with agitation.
  • the mixture is separated in separation zone 100, into an upper phase comprising an aluminum fluoride salt which is removed in stream 102, and a lower phase comprising a titanium-zinc alloy which is removed in stream 110.
  • the titanium-zinc alloy is substantially free of halides.
  • a titanium-zinc alloy has been produced by the process described above, a zirconium-zinc alloy or a hafnium-zinc alloy can be produced by a similar sequence of processing steps using zirconium or hafnium ores or values.
  • the amount of titanium in the zinc can be substan ⁇ tially increased by operating zone 90 under a positive pressure.
  • the titanium-zinc alloy removed in stream 110 which is substantially free of halides, is heated or distilled in zone 200 at a temperature between about 900° and 1000°C while simultaneously introducing into zone
  • titanium values are then heated in the same vessel, depicted as zone 210, to a temperature between about 1020° and about 1060°C under conditions operative to sinter such titanium values.
  • the sintered titanium values are cooled to a tempera- ture between about 600° and about 700°C in zone 220 and simultaneously treated, as depicted in zone 230, with hydrogen introduced in stream 224 under conditions operative to hydride and embrittle the sintered titanium values.
  • the hydrided and embrittled titanium values are then crushed in zone 240 under an inert atmosphere, preferably helium introduced through stream 242, to form particles of titanium metal values.
  • the particles of titanium metal values are dehydrided in zone 250 at a temperature between about 600° and about 700°c under conditions operative to remove essen- tially all hydrogen values from the particles of titanium values.
  • the dehydrided particles are cooled in zone 260 to a temperature between ambient and about 60°C and then passified in zone 270 with a relatively small amount of air introduced in stream 264.
  • An effective amount of air is introduced under the passification conditions to passify the particles. Excess air is not required or desirable.
  • At least a substantial part of the passified titanium-based metal particles thusly produced and removed in stream 272 are suitable for powder metallurgy usage without further particle size reduction.
  • a molten stream of a titanium-zinc alloy 110 which can be
  • casting zone 300 wherein it is formed into particles having a particle size distribution between about 60 mesh and about 20 mesh.
  • the 60 to 20 mesh particles are removed in stream 302 and introduced into heating or distillation zone 310 along with a continuous flow of helium sweep gas intro ⁇ cuted through stream 304.
  • heating zone 310 which is operated at atmosphere pressure, the zinc is vaporized
  • Particles of titanium values which are substantially free of zinc and halides, are removed by stream 308 and introduced into sintering zone 320 which is maintained at a sintering temperature between about 1020° and 1060°C
  • cooling zone 330 wherein they are cooled to a temperature between about ambient and about 60°C.
  • the cooled particles are removed through stream 332 and introduced into break ⁇ ing zone 340 wherein the weakly adhered particle masses are broken apart by suitable mechanical means under non- 25 deleteriously-reactive environment.
  • the thusly separated particles removed in stream 342 are introduced into passification zone 350 where they are passified with a relatively small amount of air introduced through stream 352. In some embodiments such breaking is not required.
  • FIG. 3 An alternative embodiment of the process of Fig. 2 is shown in Fig. 3.
  • the sintered particle masses are passed from cooling zone 330 (shown in Fig. 2) through stream 332 to passification zone 350 where they are passified with air introduced through stream 352 as described above.
  • the passified sintered particle masses are passed from zone 350 into breaking zone 340 through stream 354 wherein the weakly adhered particle masses are broken apart by conventional mechanical means under a nondeleteriously-reactive environment as described above.
  • the separated particles are passed from zone 340 into screening zone 360 through stream 342 wherein oversized particles are separated and removed through stream 362 and particles having the desired particle size are removed through stream 364.
  • a titanium-zinc alloy optionally alloyed with other alloying agents, which is substantially free of halides, is passed to heating zone 400 through stream 110 wherein the alloy is heated to distill off the zinc at a temperature between about 900°-1000°C while simultaneously introducing into zone 400 a flow of hydrogen sweep gas from stream 402 under conditions effective for the distillation of the zinc from the alloy to produce titanium values which are substantially free of zinc and halide.
  • the zinc is removed in stream 404.
  • the titanium values are passed to hydriding zone 410 wherein the titanium
  • the hydrided titanium values are treated with hydrogen introduced through stream 412 under conditions operative to hydride and embrittle the titanium values.
  • the hydrided titanium values are comminuted in comminuting zone 420 under an inert atmos- phere, such as argon or helium, introduced in stream 422 to form particles of titanium metal values.
  • the hydrided titanium values may be comminuted with conventional equip ⁇ ment known to the art for crushing metal values. Such equipment may be modified for comminuting under an inert atmosphere.
  • the particles of titanium metal values from zone 420 are passed to dehydriding zone 430 wherein the particles are heated to a temperature between about 600°-700°C under conditions operative to remove essen ⁇ tially all the hydrogen values from the particles.
  • the dehydrided particles are cooled in cooling zone 440 to a temperature between about ambient to about 60°C and then passed to a passification zone 450 and passified with a small or effective amount of air introduced in stream 452.
  • the passified particles of titanium values are passed to screening zone 460 wherein oversized particles are separated and removed through stream 462 and particles having the desired particle size distribution are removed through stream 464.
  • a titanium-zinc alloy which may be optionally alloyed with other alloying agents, is introduced into comminuting zone 500 through stream 110 wherein the alloy is crushed or ground to predetermined particle size, preferably from about 80 mesh to about 1/4 inch, to form particles of the titanium-zinc alloy.
  • the titanium- zinc alloy can be cast into irregular particles of a predetermined particle size in a casting zone (now shown) rather than comminuted as described herein.
  • zinc alloy can also be formed into particles by con ⁇ ventional shot forming techniques (not shown) , such as the shot tower techniques.
  • the particles are preferably deformed into irregular particles by dropping the particles on a hard surface or deforming the par ⁇ ticles in a rod mill or ball mill.
  • the particles are passed to a distillation zone 510, optionally a non ⁇ deleteriously-reactive sweep gas may be introduced through stream 512, wherein the zinc is vaporized from the particles of titanium-zinc alloy and the zinc is removed in stream 514.
  • the resulting particles of titanium values which are substantially free of zinc and halides, are introduced in a stream 516 into sintering zone 520 wherein the titanium values are then heated to a sintering temperature under conditions operative to sinter such titanium values.
  • the sintered titanium values are introduced in stream 522 into cool ⁇ ing zone 530 wherein the sintered titanium values are cooled to a temperature between about ambient and about 60°C.
  • the cooled sintered titanium values are introduced into passification zone 540 wherein titanium values are passified with an effective amount or relatively small amount of air introduced in stream 542 to produce passified titanium-based metal particles suitable for powder metallurgy usage which are removed in stream 544.
  • the sintering step in zone 520 is eliminated and titanium values from distil ⁇ lation zone 510 are introduced into cooling zone 530 through stream 518 wherein the titanium values, sub- stantially free of halides and zinc, are cooled to a temperature between about ambient and about 60°C.
  • the cooled titanium values are introduced into passification
  • zone 540 wherein the titanium values are passified with an effective amount of air introduced in stream 542 to produce passified titanium-based metal particles, substantial portions of which are suitable for powder metallurgy usage without further partifle size reduction.
  • passified titanium-based metal particles may be screened in a screening zone (not shown) to separate oversized particles from the particles of the desired particle size range.
  • the passification step is preferably controlled, to prevent excess contamination of the titanium values with nitrogen and oxygen which are introduced during passi ⁇ fication.
  • FIG. 6 an alternative process is illustrated which employs sintered Group IVb transition metal sponge substantially free of halides and zinc which is produced from a Group IVb transition metal-zinc alloy substantially free of halide by distilling off the zinc to produce a Group IVb transition metal spo ⁇ e sub- stantially free of haldies and zinc, sintering t.he metal sponge at a temperature between about 1020°-1060°C under conditions operative to sinter such metal values, and passifying the sintered metal sponge with an effective amount or small amount of oxygen, nitrogen or air at a temperature between about ambient and about 60°C to produce a passified Group IVb transition metal sponge which is introduced through stream 112 into heating zone 600 to heat the sintered metal sponge to a temperature between about 600°-700°C.
  • the heated passified metal sponge is introduced in hydriding zone 610 wherein the metal sponge is contacted with hydrogen gas introduced in stream 612 under conditions operative to hydride the heated metal
  • the heating step and dehydriding step in zones 600 and 610, respectively, can be carried out in the same vessel.
  • the hydrided metal sponge is passed to comminuting zone 620 wherein the metal sponge is crushed to a desired particle size distribution using conventional metal crushing equipment known to the art.
  • the comminuting performed under an inert atmosphere or gas introduced in stream 622 into zone 620.
  • the metal particles are introduced into dehydriding zone 630 wherein the metal particles are dehydrided at a temperature between about 600°-700°C under conditions operative to remove essentially all of the hydrogen values from the metal particles.
  • the dehydrided metal particles are cooled in cooling zone 640 and passified in passification zone 650 with an effective amount or small amount of air introduced in stream- 652 as described above with respect to Fig. 5.
  • the resulting passified Group IVb transition metal- based metal particles are recovered from stream 654.
  • Substantial portions of the metal particles in stream 654 are suitable for powder metallurgy usage without addi ⁇ tional particle size reduction. These particles may be screened in a screening zone (not shown) to remove the oversized particles from the particles of the desired particle size range.
  • OMPI atmospheric pressure may in some circumstances be bene ⁇ ficially conducted at slightly higher or lower pressure than atmospheric and hence, by atmospheric we mean to include such slight pressure variations.
  • Other elements are to be construed similarly.
  • the invention is equally operative with other Group IVb transition metal values, such as zirconium and hafnium values.

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  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Manufacture Of Metal Powder And Suspensions Thereof (AREA)
  • Powder Metallurgy (AREA)
EP19840902748 1984-07-03 1984-07-03 Metal a base de metaux de transition de groupe ivb et ses procedes de production. Ceased EP0187741A4 (fr)

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US6095679A (en) * 1996-04-22 2000-08-01 Ta Instruments Method and apparatus for performing localized thermal analysis and sub-surface imaging by scanning thermal microscopy
JP5628767B2 (ja) * 2011-09-02 2014-11-19 東邦チタニウム株式会社 チタン合金の水素化方法
CN102560153B (zh) * 2012-01-18 2013-04-10 深圳市新星轻合金材料股份有限公司 一种氟钛酸钾铝热还原制备海绵钛的方法
CN102534263B (zh) * 2012-01-18 2013-06-05 深圳市新星轻合金材料股份有限公司 一种氟钛酸钠铝热还原制备海绵钛的方法

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2522679A (en) * 1945-02-17 1950-09-19 William J Kroll Method of producing titanium alloys
US3119685A (en) * 1959-12-17 1964-01-28 Nat Distillers Chem Corp Method for melting metals
WO1986000550A1 (fr) * 1984-07-02 1986-01-30 Occidental Research Corporation Poudre et eponge metalliques et leurs procedes de fabrication

Family Cites Families (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2782116A (en) * 1946-09-06 1957-02-19 Frank H Spedding Method of preparing metals from their halides
US2903351A (en) * 1949-04-11 1959-09-08 Frank H Spedding Thorium-beryllium alloys and method of producing same
US2837426A (en) * 1955-01-31 1958-06-03 Nat Distillers Chem Corp Cyclic process for the manufacture of titanium-aluminum alloys and regeneration of intermediates thereof
US2905548A (en) * 1957-09-06 1959-09-22 Fansteel Metallurgical Corp Method of recovering tantalum and columbium
GB886002A (en) * 1959-09-16 1962-01-03 Continental Titanium Metals Co A method of dehydrogenating titanium metal powder
US3607012A (en) * 1967-08-18 1971-09-21 Frederick V Schossberger Process for the production of titanium and iron material
JPS5427811B2 (fr) * 1973-02-07 1979-09-12
AU8223375A (en) * 1974-06-21 1976-12-23 Univ Melbourne Benefication of titaniferous ores
US4072506A (en) * 1975-10-17 1978-02-07 Teledyne Industries, Inc. Method of separating hafnium from zirconium
US4141719A (en) * 1977-05-31 1979-02-27 Fansteel Inc. Tantalum metal powder
DE2921593C2 (de) * 1979-05-28 1984-02-02 Gränges Nyby AB, Nybybruk Verfahren und Vorrichtung zum Weiterzerkleinern von hydriertem, grobstückigem Material, insbes. Schrott aus Titan oder dessen Legierungen
US4359449A (en) * 1980-12-15 1982-11-16 Occidental Research Corporation Process for making titanium oxide from titanium ore
US4390365A (en) * 1980-12-15 1983-06-28 Occidental Research Corporation Process for making titanium metal from titanium ore
US4468248A (en) * 1980-12-22 1984-08-28 Occidental Research Corporation Process for making titanium metal from titanium ore

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2522679A (en) * 1945-02-17 1950-09-19 William J Kroll Method of producing titanium alloys
US3119685A (en) * 1959-12-17 1964-01-28 Nat Distillers Chem Corp Method for melting metals
WO1986000550A1 (fr) * 1984-07-02 1986-01-30 Occidental Research Corporation Poudre et eponge metalliques et leurs procedes de fabrication

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
See also references of WO8600610A1 *

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JPS61502615A (ja) 1986-11-13
WO1986000610A1 (fr) 1986-01-30

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