Classifications

• • C—CHEMISTRY; METALLURGY
  • C25—ELECTROLYTIC OR ELECTROPHORETIC PROCESSES; APPARATUS THEREFOR
  • C25C—PROCESSES FOR THE ELECTROLYTIC PRODUCTION, RECOVERY OR REFINING OF METALS; APPARATUS THEREFOR
  • C25C5/00—Electrolytic production, recovery or refining of metal powders or porous metal masses
  • C25C5/04—Electrolytic production, recovery or refining of metal powders or porous metal masses from melts
• • B—PERFORMING OPERATIONS; TRANSPORTING
  • B22—CASTING; POWDER METALLURGY
  • B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
  • B22F9/00—Making metallic powder or suspensions thereof
  • B22F9/16—Making metallic powder or suspensions thereof using chemical processes
  • B22F9/18—Making metallic powder or suspensions thereof using chemical processes with reduction of metal compounds
  • B22F9/20—Making metallic powder or suspensions thereof using chemical processes with reduction of metal compounds starting from solid metal compounds
• • C—CHEMISTRY; METALLURGY
  • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
  • C22B—PRODUCTION AND REFINING OF METALS; PRETREATMENT OF RAW MATERIALS
  • C22B34/00—Obtaining refractory metals
  • C22B34/10—Obtaining titanium, zirconium or hafnium
  • C22B34/12—Obtaining titanium or titanium compounds from ores or scrap by metallurgical processing; preparation of titanium compounds from other titanium compounds see C01G23/00 - C01G23/08
  • C22B34/1263—Obtaining titanium or titanium compounds from ores or scrap by metallurgical processing; preparation of titanium compounds from other titanium compounds see C01G23/00 - C01G23/08 obtaining metallic titanium from titanium compounds, e.g. by reduction
• • C—CHEMISTRY; METALLURGY
  • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
  • C22B—PRODUCTION AND REFINING OF METALS; PRETREATMENT OF RAW MATERIALS
  • C22B34/00—Obtaining refractory metals
  • C22B34/10—Obtaining titanium, zirconium or hafnium
  • C22B34/12—Obtaining titanium or titanium compounds from ores or scrap by metallurgical processing; preparation of titanium compounds from other titanium compounds see C01G23/00 - C01G23/08
  • C22B34/129—Obtaining titanium or titanium compounds from ores or scrap by metallurgical processing; preparation of titanium compounds from other titanium compounds see C01G23/00 - C01G23/08 obtaining metallic titanium from titanium compounds by dissociation, e.g. thermic dissociation of titanium tetraiodide, or by electrolysis or with the use of an electric arc
• • C—CHEMISTRY; METALLURGY
  • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
  • C22B—PRODUCTION AND REFINING OF METALS; PRETREATMENT OF RAW MATERIALS
  • C22B5/00—General methods of reducing to metals
• • C—CHEMISTRY; METALLURGY
  • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
  • C22B—PRODUCTION AND REFINING OF METALS; PRETREATMENT OF RAW MATERIALS
  • C22B5/00—General methods of reducing to metals
  • C22B5/02—Dry methods smelting of sulfides or formation of mattes
• • C—CHEMISTRY; METALLURGY
  • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
  • C22C—ALLOYS
  • C22C47/00—Making alloys containing metallic or non-metallic fibres or filaments
  • C22C47/02—Pretreatment of the fibres or filaments
  • C22C47/04—Pretreatment of the fibres or filaments by coating, e.g. with a protective or activated covering
• • C—CHEMISTRY; METALLURGY
  • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
  • C22C—ALLOYS
  • C22C47/00—Making alloys containing metallic or non-metallic fibres or filaments
  • C22C47/14—Making alloys containing metallic or non-metallic fibres or filaments by powder metallurgy, i.e. by processing mixtures of metal powder and fibres or filaments
• • C—CHEMISTRY; METALLURGY
  • C25—ELECTROLYTIC OR ELECTROPHORETIC PROCESSES; APPARATUS THEREFOR
  • C25C—PROCESSES FOR THE ELECTROLYTIC PRODUCTION, RECOVERY OR REFINING OF METALS; APPARATUS THEREFOR
  • C25C3/00—Electrolytic production, recovery or refining of metals by electrolysis of melts
• • C—CHEMISTRY; METALLURGY
  • C25—ELECTROLYTIC OR ELECTROPHORETIC PROCESSES; APPARATUS THEREFOR
  • C25C—PROCESSES FOR THE ELECTROLYTIC PRODUCTION, RECOVERY OR REFINING OF METALS; APPARATUS THEREFOR
  • C25C3/00—Electrolytic production, recovery or refining of metals by electrolysis of melts
  • C25C3/26—Electrolytic production, recovery or refining of metals by electrolysis of melts of titanium, zirconium, hafnium, tantalum or vanadium
  • C25C3/28—Electrolytic production, recovery or refining of metals by electrolysis of melts of titanium, zirconium, hafnium, tantalum or vanadium of titanium
• • B—PERFORMING OPERATIONS; TRANSPORTING
  • B22—CASTING; POWDER METALLURGY
  • B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
  • B22F2999/00—Aspects linked to processes or compositions used in powder metallurgy
• • C—CHEMISTRY; METALLURGY
  • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
  • C22B—PRODUCTION AND REFINING OF METALS; PRETREATMENT OF RAW MATERIALS
  • C22B4/00—Electrothermal treatment of ores or metallurgical products for obtaining metals or alloys
  • C22B4/06—Alloys

Definitions

• This invention relates to methods for the manufacture of metal foams and to novel applications for these technologies.
• the invention is more particularly directed to, but not limited to manufacture of titanium and titanium alloy foams.
• Certain embodiments of these methods involve the electrolysis of metal oxides or other compounds (M 1 X) in a cell containing a liquid (fused salt M 2 Y) electrolyte and an anode, the metal oxide or other compound forming the cathode. Conditions are controlled so as to bring about the selective dissolution of the oxygen or other contaminant of the cathode in preference to deposition of the metal cation. Improved efficiency of this process can be achieved by various methods as described in GB 0003971.9 and GB 0010873.8 some of which are summarised below.
• titanium dioxide in the form of an amorphous slurry undergoes calcining.
• the titanium dioxide slurry can be used as the principle feedstock in the above described electrolytic method.
• a small percentage of calcined material is mixed with amorphous material and a binder to obtain the most satisfactory results after sintering.
• the calcined material should constitute at least about 5% by weight of the mixture.
• Metal foams are attractive for a number of applications such as filters, medical implants and structural fillers.
• the fabrication of a sponge-like sintered oxide pre-form from the starting material M 1 X can be converted into a solid metal/alloy foam via the electrolytic method previously described.
• Various established methods may be used to make the foam like material from the mixture of oxide powders.
• the foam preform desirably has open porosity that is, porosity which is interconnected and open to the exterior.
• a natural or synthetic polymeric foam is infiltrated with a metal (eg titanium) oxide slip, then dried and fired to remove the polymeric foam, leaving an open “foam” which is an inversion of the original polymeric foam.
• the sintered preform is then electrolytically reduced in accordance with the previously described method to convert it into a titanium/titanium alloy foam.
• the foam is then washed or vacuum distilled to remove the salt.
• the metal oxide powder may be mixed with organic foaming agents. These materials are typically two liquids which when mixed, react to evolve a foaming gas, and then cure to give a solidified foam with either an open or closed structure.
• the metal powder is mixed with one or both of the precursor liquids prior to production of the foam.
• the foam is then fired to remove the organic material, leaving the ceramic foam which is then electrolytically reduced in accordance with the previously described method.
• a near net shape component may be made using the previously described electrolytic method by reducing a ceramic facsimile of the component made from a mixture of a metal oxide or mixture of metal oxide and the oxides of other alloying elements. Again this method is particularly suited to the manufacture of titanium metal and alloy components.
• the ceramic facsimile may be produced using any of a variety of well known production methods for ceramic articles which include; pressing, injection moulding, extrusion and slip casting, followed by firing (sintering). Full density of the metallic component can be achieved by sintering with or without the application of pressure, either in the electrochemical cell, or in a subsequent operation. Shrinkage of the component during the conversion to metal or alloy should be allowed for by making the ceramic facsimile proportionally larger than the desired component.
• the electrolysis is performed on a preformed sintered mass comprising a mixture of metal oxide made up of a proportion of particles of size generally greater than 20 microns and a proportion of finer particles of less than 7 microns.
• the finer particles make up between 10 and 55% by weight of the sintered block.
• High density granules of approximately the size required for the powder are manufactured and then are mixed with very fine unsintered metal oxide (e.g., titanium dioxide), binder and water in the appropriate ratios and formed into the required shape of feedstock.
• This feedstock is then sintered to achieve the required strength for the reduction process.
• the resulting feedstock after sintering but before reduction, consists of high density granules in a lower density (porous) matrix.
• the feedstock can be reduced in block form using the previously described electrolytic method and the result is a friable block which can easily be broken up into powder.
• the calcine discharge used can be replaced by cheaper amorphous TiO 2 .
• the key requirement for this “matrix” material is that it sinters easily with significant shrinkage during the sintering process. Any oxide or mixture of oxides which fulfil these criteria would be usable. In the case of TiO 2 this means the particle size must be less than about 1 ⁇ m. It is estimated that at least 5% of the matrix material should be present in order to give any significant strength to the sintered product.
• the starting granules for this method need not be rutile sand but could be manufactured by a sintering and crushing process, and in principle there is no reason to suppose that alloy powders could not be made by this route.
• X may be a metalloid such as oxygen, sulphur, carbon or nitrogen, preferably, X is oxygen.
• M 1 may be a Group IVA element such as Ti, SI, Ge, Zr, Hf, Sm, Nd, Mo, Cr, Nb or an alloy of any of the preceding metals, preferably, M 1 comprises titanium.
• a preferred electrolyte, M 2 Y, is calcium chloride (CaCl 2 ).
• suitable electrolytes include but are not limited to the molten chlorides of all common alkali and alkaline earth metals.
• Other preferred metals for M 2 are barium, caesium, lithium, strontium and yttrium.
• the anode of the cell is preferably of a relatively inert material.
• One suitable anode material is graphite.
• Processing conditions suitable for the favourable dissolution of the contaminant X require that the potential of the cell preferably be maintained at a potential which is less than the decomposition potential of the molten electrolyte M 2 Y during the process. Allowing for polarisation and resistive losses in the cell, it will be understood that the cell potential may be maintained at a level equal to, or marginally higher than, the decomposition potential of M 2 Y and still achieve the desired result. Potentiostatic methods may be used to control the potential.
• the temperature of the cell is maintained at an elevated temperature which is significantly above the melting point of M 2 Y but below the boiling point of M 2 Y.
• suitable processing parameters include a potential of up to about 3.3V and a processing temperature of between about 825 and 1050° C.
• the present invention provides a method for the manufacture of a foamed metal or alloy article including the steps of:
• the binder is water.
• the preform in step C is subjected to foaming by the blowing of a gas through the slurry. As well as removing some of the water from the preform and assisting in the drying process, this step results in the formation of bubbles in the preform which are retained as cells in the foam.
• foaming agents may be introduced into the slurry to form gas bubbles within the body of the preform.
• the preform in step C may be provided by packing the slurry into the open cells of a foam article which is provided in the desired net shape of the preform.
• This foam template should comprise a material with a vaporisation point significantly lower than the melting point of the contaminated metal or alloy to be foamed. The foam template can then subsequently be burnt off leaving a network of open cells within the resulting metal article.
• a quantity of crushed titanium oxide feedstock is mixed with around 300 ml of water per kilo of the feedstock and placed in a mould of the desired foamed article.
• the article has dimensions of the order of a few centimetres. Air is blown through the mould to assist in foaming the preform. The preform is then left to dry at room temperature and pressure for about 5 days. Once dried, the article is sintered in an oven at between about 1100° C. to 1300° C. for around 2 hours.
• the sintered article is then introduced to an electrochemical cell comprising a molten calcium chloride bath and carbon graphite anode and electrolysis performed in accordance with methods previously described to remove the contaminant oxygen. Once the desired quantity of oxygen has been removed by this method, the purified foamed titanium article is reclaimed from the cell.
• One application may include the manufacture of armour.
• a foamed titanium alloy such as Ti-6Al-4V alloy may be preformed into the net shape of the armour in accordance with the invention.
• the foamed alloy is considerably lighter than full density armour for similar high strength, high stiffness and high temperature properties.
• the foaming provides the additional advantage that the foamed structure begins to collapse on impact thereby absorbing energy from the projectile penetrating the armour and considerably reducing the risk or extent of injury to the protected persons.
• Titanium alloys are widely recognised as good bio-materials as they are relatively inert in the environment provided by a human body.
• Recent developments on orthopaedic research suggest that the life of an implant and the health of tissue surrounding the implant can be greatly improved where the implant is provided with a knurled or otherwise pitted surface. Tissues, in particular bone tissue surrounding the pitted surface of the implant, grow into the pits providing anchorage for the implant and resulting in more even distribution of load from the implant to the bone. It is widely accepted that bone strength and health is compromised by prolonged periods of under loading, hence bone health may be improved by the provision of pits or channels within an orthopaedic implant.
• foamed titanium alloy implants may be provided by forming the preform in the near net shape of the implant. Since the foam structure provides channels passing in varying directions through the implant, exceptional anchorage and load transfer to the bone can be predicted. Where the impact loads of the implant are particularly high, it may be desirable to retain a fully dense alloy core to the implant with an outer foamed layer. This can easily be accommodated by planting a fully dense core at the centre of the preform and coating with the slurry to be foamed.
• metal foams made in accordance with the invention include, the manufacture of filters, sound proofing applications, particularly in high temperature or highly corrosive environments and any structural applications requiring high strength and stiffness with low weight.
• Such structural applications might include aircraft components, windmill propellers and the like.

Landscapes

• Chemical & Material Sciences (AREA)
• Engineering & Computer Science (AREA)
• Materials Engineering (AREA)
• Metallurgy (AREA)
• Organic Chemistry (AREA)
• Mechanical Engineering (AREA)
• Chemical Kinetics & Catalysis (AREA)
• Manufacturing & Machinery (AREA)
• Electrochemistry (AREA)
• Life Sciences & Earth Sciences (AREA)
• Environmental & Geological Engineering (AREA)
• General Life Sciences & Earth Sciences (AREA)
• Geology (AREA)
• General Chemical & Material Sciences (AREA)
• Electrolytic Production Of Metals (AREA)
• Powder Metallurgy (AREA)
• Manufacture And Refinement Of Metals (AREA)
• Inorganic Compounds Of Heavy Metals (AREA)
• Superconductors And Manufacturing Methods Therefor (AREA)
• Oxygen, Ozone, And Oxides In General (AREA)

Applications Claiming Priority (4)

Publications (1)

Family

ID=26243686

Family Applications (5)

Family Applications After (4)

Country Status (15)

Cited By (12)

Families Citing this family (64)

Citations (9)

Family Cites Families (39)

• 2001
  • 2001-02-19 AT AT01905907T patent/ATE372395T1/de not_active IP Right Cessation
  • 2001-02-19 WO PCT/GB2001/000653 patent/WO2001062994A1/fr not_active Ceased
  • 2001-02-19 GB GB0218516A patent/GB2376241B/en not_active Expired - Fee Related
  • 2001-02-19 AU AU3387601A patent/AU3387601A/xx active Pending
  • 2001-02-19 US US10/204,460 patent/US20030057101A1/en not_active Abandoned
  • 2001-02-19 DE DE60130322T patent/DE60130322T2/de not_active Expired - Lifetime
  • 2001-02-19 AU AU2001233876A patent/AU2001233876B2/en not_active Ceased
  • 2001-02-19 AU AU2001233871A patent/AU2001233871A1/en not_active Abandoned
  • 2001-02-19 EP EP01905901A patent/EP1257677A1/fr not_active Withdrawn
  • 2001-02-19 EP EP01905907A patent/EP1257678B1/fr not_active Expired - Lifetime
  • 2001-02-19 US US10/204,465 patent/US20030047462A1/en not_active Abandoned
  • 2001-02-19 WO PCT/GB2001/000661 patent/WO2001062995A1/fr not_active Ceased
  • 2001-02-19 JP JP2001561803A patent/JP4703931B2/ja not_active Expired - Fee Related
  • 2001-02-20 CA CA2401034A patent/CA2401034C/fr not_active Expired - Lifetime
  • 2001-02-20 DK DK08075215.7T patent/DK1956102T3/da active
  • 2001-02-20 AU AU3389001A patent/AU3389001A/xx active Pending
  • 2001-02-20 EA EA200401129A patent/EA008264B1/ru not_active IP Right Cessation
  • 2001-02-20 CN CNB018054552A patent/CN1279194C/zh not_active Expired - Fee Related
  • 2001-02-20 AU AU2001233890A patent/AU2001233890B2/en not_active Ceased
  • 2001-02-20 AT AT01905924T patent/ATE286150T1/de not_active IP Right Cessation
  • 2001-02-20 KR KR1020027010919A patent/KR100767981B1/ko not_active Expired - Fee Related
  • 2001-02-20 EA EA200200895A patent/EA005348B1/ru unknown
  • 2001-02-20 EP EP08075215A patent/EP1956102B1/fr not_active Expired - Lifetime
  • 2001-02-20 ES ES01905924T patent/ES2231443T3/es not_active Expired - Lifetime
  • 2001-02-20 EP EP04022898A patent/EP1489192A1/fr not_active Withdrawn
  • 2001-02-20 JP JP2001561804A patent/JP4995392B2/ja not_active Expired - Fee Related
  • 2001-02-20 WO PCT/GB2001/000683 patent/WO2001062996A1/fr not_active Ceased
  • 2001-02-20 DE DE60108081T patent/DE60108081T2/de not_active Expired - Fee Related
  • 2001-02-20 EP EP01905924A patent/EP1257679B1/fr not_active Expired - Lifetime
  • 2001-02-20 UA UA2002097584A patent/UA74179C2/uk unknown
  • 2001-02-20 EA EA200601812A patent/EA013138B1/ru not_active IP Right Cessation
  • 2001-02-20 US US10/204,547 patent/US6921473B2/en not_active Expired - Fee Related
• 2005
  • 2005-06-10 US US11/149,588 patent/US20060110277A1/en not_active Abandoned
• 2011
  • 2011-03-01 US US12/929,993 patent/US20110158843A1/en not_active Abandoned

Patent Citations (9)

Also Published As

Similar Documents

Legal Events