WO2003062482A2 - Stabilized grain size refractory metal powder metallurgy mill products - Google Patents

Stabilized grain size refractory metal powder metallurgy mill products Download PDF

Info

Publication number
WO2003062482A2
WO2003062482A2 PCT/US2003/001823 US0301823W WO03062482A2 WO 2003062482 A2 WO2003062482 A2 WO 2003062482A2 US 0301823 W US0301823 W US 0301823W WO 03062482 A2 WO03062482 A2 WO 03062482A2
Authority
WO
WIPO (PCT)
Prior art keywords
powder
niobium
mill product
ppm
refractory metal
Prior art date
Application number
PCT/US2003/001823
Other languages
English (en)
French (fr)
Other versions
WO2003062482A3 (en
Inventor
Paul R. Aimone
Howard V. Goldberg
Richard Malen
Thomas A. Morse
Prabhat Kumar
Henning Ulenhut
Original Assignee
H. C. Starck Inc.
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 H. C. Starck Inc. filed Critical H. C. Starck Inc.
Priority to US10/502,281 priority Critical patent/US20050118052A1/en
Priority to CA002473493A priority patent/CA2473493A1/en
Priority to IL16290403A priority patent/IL162904A0/xx
Priority to JP2003562348A priority patent/JP2005516116A/ja
Priority to BR0307073-5A priority patent/BR0307073A/pt
Priority to MXPA04007104A priority patent/MXPA04007104A/es
Priority to KR10-2004-7011314A priority patent/KR20040091627A/ko
Priority to NZ534212A priority patent/NZ534212A/en
Priority to YU64904A priority patent/RS64904A/sr
Priority to EP03705856A priority patent/EP1506322A2/en
Publication of WO2003062482A2 publication Critical patent/WO2003062482A2/en
Publication of WO2003062482A3 publication Critical patent/WO2003062482A3/en

Links

Classifications

    • 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
    • B22F3/00Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces
    • B22F3/10Sintering only
    • B22F3/1003Use of special medium during sintering, e.g. sintering aid
    • 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
    • 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
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C32/00Non-ferrous alloys containing at least 5% by weight but less than 50% by weight of oxides, carbides, borides, nitrides, silicides or other metal compounds, e.g. oxynitrides, sulfides, whether added as such or formed in situ
    • C22C32/001Non-ferrous alloys containing at least 5% by weight but less than 50% by weight of oxides, carbides, borides, nitrides, silicides or other metal compounds, e.g. oxynitrides, sulfides, whether added as such or formed in situ with only oxides
    • C22C32/0015Non-ferrous alloys containing at least 5% by weight but less than 50% by weight of oxides, carbides, borides, nitrides, silicides or other metal compounds, e.g. oxynitrides, sulfides, whether added as such or formed in situ with only oxides with only single oxides as main non-metallic constituents
    • C22C32/0031Matrix based on refractory metals, W, Mo, Nb, Hf, Ta, Zr, Ti, V or alloys thereof
    • 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
    • B22F3/00Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces
    • B22F3/10Sintering only
    • B22F2003/1032Sintering only comprising a grain growth inhibitor
    • 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
    • B22F5/00Manufacture of workpieces or articles from metallic powder characterised by the special shape of the product
    • B22F2005/002Tools other than cutting tools
    • 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
    • B22F2998/00Supplementary information concerning processes or compositions relating to powder metallurgy
    • 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
    • B22F2998/00Supplementary information concerning processes or compositions relating to powder metallurgy
    • B22F2998/10Processes characterised by the sequence of their steps

Definitions

  • the invention relates generally to metal mill products (and fabricated parts) made from powders of refractory metals including the elemental metals and their alloys and, more particularly to the use of oxide dopants for grain size stabilization in mill products and fabricated parts to be subjected to high temperature application usage and/or high temperature fabrication processes.
  • furnace parts As used for manufacturing synthetic diamonds. These products require material with small grain size. Furnace parts particularly require the material to have slow grain growth during service in order to prevent premature deterioration of the mechanical properties.
  • tantalum material with stabilized grain size due to alloying additions or other artifacts, is used for wire or sheet.
  • Si0 2 is used as a grain stabilizer.
  • the disadvantage of such a manufacturing method (resistance-sintering) for grain size stabilized tantalum powder metallurgy (P/M) material is that it is limited to a lot size of 30 pounds for tantalum and approximately 15 pounds for niobium. It is desirable to make lot sizes of up to 1000 pounds of tantalum and 500 pounds of niobium respectively.
  • P/M powder metallurgy
  • the invention relates to a process for making a metal mill product from a refractory metal powder comprising (a) providing a low oxygen refractory metal powder; (b) adding to the powder a grain growth inhibitor to the low oxygen refractory metal powder before consolidating the powder, (c) consolidating the powder by either hot isostatic pressing, extrusion or another thermomechanical working process; and (d) subjecting the consolidated powder to subsequent thermomechanical processing, and thereby forming the mill product.
  • the invention also relates to products made from such a process.
  • Grain growth inhibitors are added to niobium powder by blending inhibitors such as Si0 2 and Y 2 0 3 prior to consolidation or as a residue of a de-oxidation process where magnesium is added to capture the oxygen from the niobium powder and form magnesium oxide during the de- oxidation process.
  • the powder is consolidated either by hot isostatic pressing (HIPing), extrusion or other thermomechanical working.
  • HIPing hot isostatic pressing
  • Such methods of consolidation are capable of providing suitable P/M sheet bars with a weight of up to several hundred pounds, e.g., five hundred pounds, one thousand pounds or more.
  • Subsequent thermomechanical processing of the P/M sheet bar is applied similarly to then P/M derived refractory metals as to metals from ingot sources.
  • the present invention inhibits grain growth in niobium P/M sheets during high temperature exposure.
  • a low oxygen niobium powder ( ⁇ about 400 ppm, preferably ⁇ about 200 ppm) is needed as a starting material. Powders with a higher content in oxygen cannot be consolidated to full density and/or will not yield good mechanical properties.
  • Fig. 1 is a flow chart showing a process of the present invention to create stabilized grain size powder
  • Figs. 2-4 are flow charts showing examples of consolidating steps to create products made of stabilized grain size powder. DETAILED DESCRIPTION OF PREFERRED EMBODIMENTS
  • the invention relates to a process for making a metal mill product from a refractory metal powder comprising (a) providing a low oxygen refractory metal powder; (b) adding to the powder a grain growth inhibitor to the low oxygen refractory metal powder before consolidating the powder, (c) consolidating the powder by either hot isostatic pressing, extrusion or another thermomechanical working process; and (d) subjecting the consolidated powder to subsequent thermomechanical processing, and thereby forming the mill product.
  • the invention also relates to products made from such a process.
  • the low oxygen niobium powder can be any powder, which when used in accordance to the invention, enables user to meet an object of the invention.
  • the metal powders with stabilized grain size of the present invention are preferably produced via the following procedure as discussed in U.S. Patent 6,261 ,337, incorporated herein in its entirety. Niobium alloys can also be used.
  • niobium powders instead of using niobium powders, powders made from a refractory metal selected from hafnium, molybdenum, niobium, rhenium, tantalum, tungsten, vanadium, and zirconium metals can be used. Also, alloys of these metals can also be used.
  • low oxygen niobium and grain growth inhibitor powders (for example Si0 2 or Y 2 0 3 ) are blended to form low oxygen powder with grain size inhibitors.
  • Figs. 2-4 illustrate the consolidation steps with the master blend. The physical processes of blending and consolidating achieve a uniform distribution of grain growth inhibiting particles in the powder metal sheet bars. The powders are made by the process described in US 6,261 ,337 and as described herein.
  • the powders are blended to produce the desired alloy composition.
  • the powders are then sealed in an evacuated can, heated to a desired temperature, and extruded such that the extrusion ratio is at least 8:1. This is done to completely consolidate the niobium powders and the included inhibitors.
  • the can may be removed either just before or just after the rolling operation.
  • the above process can afford advantages of more stable grain size in the final material, more uniform material properties (such as ultimate tensile strength and hardness), lower manufacturing costs, better control of fiber size, and greater flexibility for alloy modifications and control of properties.
  • P/M sheet with grain growth inhibitors, preferably silicon, of 0, 150, and 300 ppm were thermomechanical processed to a thickness of 0.015 inches and annealed at 1065°C for 90 minutes to produce grain sizes of approximately ASTM 9.5.
  • Niobium sheet produced from ingot metallurgy (l/M) a grain size of approximately ASTM 5.5 under the same anneal heat treat conditions.
  • the P/M and l/M test samples were subjected to addi- tional annealing heat treatments at 1150°C for 180 minutes and 1300 °C for 180 minutes.
  • the P/M test samples yielded grain sizes greater than ASTM 7.0 compared to l/M test samples that yielded grain sizes coarser than ASTM 1.
  • the higher P/M Ultimate Tensile Strength of 49.3 KSl, 50.3 KS!, and 49.5 KSl and hardness of 114 VHN, 117 VHN, and 125 VHN are significant improvements over typical l/M material of Ultimate Tensile Strength of 32 KSl and hardness of 72 VHN.
  • the fine grain sizes and improved tensile strength and hardness after heat treatment of the P/M material is a significant advantage, compared to l/M material, in applications where large amounts of deformation are required during fabrication, such as deep drawn diamond cups, or capacitor cans.
  • the blended powders may be isostatically pressed into a bar prior to canning and extrusion, as illustrated in Fig. 2.
  • the advan- tage of this method would be to put a higher weight into the compact prior to extrusion to aid in consolidation and increase yield per extrusion.
  • niobium hydride powder is placed into a vacuum chamber, which also contains a metal having a higher affinity for oxygen, such as calcium or magnesium, preferably the latter.
  • the starting hydride powder has oxygen content less than about 1000 ppm.
  • the chamber is heated to the dehydration temperature to remove the hydrogen, then heated to the deoxidation temperature to produce a powder of niobium or alloy of niobium having a target reduced oxygen content of less than about 400 ppm preferably below 200 ppm and more preferably below 100 ppm.
  • the magnesium, containing the oxygen is then removed from the metal powder by evaporation and subsequently by selective chemical leaching or dissolution of the powder.
  • a niobium powder with less than 400 ppm oxygen can be produced by the deoxidization of niobium hydride under partial pressure of argon.
  • Niobium hydride powder would be blended with 0.3 wt.-% magnesium and placed in a vacuum furnace retort, which is evacuated, and backfilled with argon. The pressure in the furnace would be set at about 100 microns with Argon flowing and the vacuum pump running.
  • the furnace temperature would be ramped to about 650°C in approximately 50°C increments, held until temperature equalized, then ramped up to 950°C in approximately 50°C increments. When the temperature equalized at 950°C it would be held for about two hours. After such hold, the furnace is shut down. Once the furnace cools its powder content is removed from the retort.
  • the metal hydride powder is deoxidized to an oxygen content of less than about 400 ppm.
  • the powder is consolidated to form a niobium or alloy product, having an oxygen content below about about 400 ppm, or below about 300 ppm or below about 200 ppm or below about 100 ppm, but for many powder metallurgy purposes between about 100 ppm and 150 ppm.
  • a formed refractory metal product (niobium product), having a stabilized grain size, may be produced from metal hydride powder, as treated as described above, by any known powder metallurgy techniques.
  • Exemplary of these powder metallurgy techniques used for forming the products are the following, in which the steps are listed in order of performance. Any of the following single techniques or sequences of techniques may be utilized in the present invention: cold isostatic pressing, sintering, encapsulating, hot isostatic pressing and thermomechanical processing; cold isostatic pressing, sintering, hot isostatic pressing thermomechanical processing; cold isostatic pressing, encapsulating, hot isostatic pressing and thermomechanical processing; cold isostatic pressing, encapsulating and hot isostatic pressing; encapsulating and hot isostatic pressing; cold isostatic pressing, sintering, encapsulating, extruding and thermomechanical processing; cold isostatic pressing, sintering, extruding, and thermomechanical processing; cold isostatic pressing, sintering, and extruding; cold isostatic pressing, encapsulating, extruding and thermomechanical processing; cold isostatic pressing, sintering, and extruding; cold isostatic pressing, en
  • niobium powder with grain size inhibitors would be cold isostatically pressed at 60,000 pounds/sq. in. and room temperature, into a compact with rectangular or, preferably, round cross section, then hermetically encapsulated and hot isostatically pressed (HPed) at 40,000 Ibs.lsq. in. and 1300°C for four hours.
  • the HIPed compact would be unencapsulated and converted to sheet or foil by thermomechanical processing steps.
  • a similar process, as illustrated in Fig. 4, of just cold isostatic pressing, sintering and thermomechanical processing using niobium powder having an oxygen content of less than 300 ppm can be conducted by cold isostatically pressing at 60,000 Ibs./sq. in. into a bar shape preform.
  • This preform would be sintered at 1500°C for two hours in a vacuum of less than about 0.001 Torr to yield a preform having a density of about 95% theoretical density (Th) and less than 400 ppm oxygen.
  • the sintered preform would be converted into sheet and foil by thermomechanical processing steps.
  • Production of a formed niobium sheet or foil having a stable grain size by hot extrusion and thermomechanical processing can be made, using niobium powder having an oxygen content of less than 400 ppm as the starting powder.
  • This powder can be hermetically encapsulated then extruded through a rectangular or, preferably, round die at 1000°C to produce an extruded product having oxygen content of less than 400 ppm.
  • the extruded product can be converted to sheet or foil by the thermomechanical processing.
  • Niobium sheet or foil with oxygen content of less than 400 ppm can be produced by cold isostatic pressing, hot extrusion and thermomechanical processing. This compact made by cold isostatically pressing could be hermetically encapsulated then extruded at 1000°C to produce an extruded product with an oxygen content of about 300 ppm which can be converted into sheet and foil by thermomechanical processing steps.
  • Niobium products having stable grain size can be prepared by mechanical pressing, sintering, repressing and resintering.
  • Niobium powder blend having oxygen content of less than 400 ppm can be utilized as the starting powder. It is placed in a die and mechanically pressed, using uniaxial pressure. The pressed tablet should be then sintered at 1500°C for two hours in a vacuum evacuated to less than about 0.001 Torr. The sintered tablet would then be repressed and resintered at 1500°C for two hours in a vacuum evacuated to less than about 0.001 Torr.
  • the resintered tablet will have oxygen content of less than about 400 ppm and be suitable for thermomechanical processing to produce a formed niobium product.
  • a copper or steel container is filled with niobium powder, evacuated, hermetically sealed, and extruded through a die to give a 10:1 extrusion ratio.
  • the copper container is removed by acid treatment and the extruded bar is thermo-mechanically processed into a sheet form flat.
  • a steel container is filled with the niobium powder, evacuated, hermetically sealed and HIPed. The steel container is removed by machining and the HIPed piece is thermo mechanically processed into a sheet form flat.
  • Anneals may be used to improve workability of the material in between two deformation steps or to adjust grain size and texture through recrystallization although a final anneal may not be necessary.
  • the powder is canned during the consolidation (usually to protect it from the environment at high temperature), the can will bond to the niobium.
  • the process provides P/M sheets of large size (>100 pounds) having good mechanical properties and small stable grain size, capable of a higher yield than conventional P/M processes for sheet manufacture, typically 50 pounds or less.
  • Low oxygen niobium powder of less than 400 ppm, preferably less than 150 ppm, of non-spherical particles and sizing less than 250 microns FAPD (Fisher Average Particle Diameter), is provided per processes described herein. Powders with a higher content in oxygen cannot be consolidated to full density and/or will not yield good mechanical properties.
  • the powder is consolidated to full density either by HIPing (hot isostatic pressing) or by extrusion. Both methods of consolidation are capable of providing suitable P/M sheet bars with a weight of up to several hundred pounds.
  • Thermomechancial processing of the P/M sheet bar is similar to standard processes.

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • General Chemical & Material Sciences (AREA)
  • Manufacturing & Machinery (AREA)
  • Materials Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Powder Metallurgy (AREA)
  • Ceramic Products (AREA)
  • Manufacture Of Metal Powder And Suspensions Thereof (AREA)
PCT/US2003/001823 2002-01-23 2003-01-21 Stabilized grain size refractory metal powder metallurgy mill products WO2003062482A2 (en)

Priority Applications (10)

Application Number Priority Date Filing Date Title
US10/502,281 US20050118052A1 (en) 2002-01-23 2003-01-21 Stabilized grain size refractory metal powder metallurgy mill products
CA002473493A CA2473493A1 (en) 2002-01-23 2003-01-21 Stabilized grain size refractory metal powder metallurgy mill products
IL16290403A IL162904A0 (en) 2002-01-23 2003-01-21 Stabilized grain size refractory metal powder metallurgy mill products
JP2003562348A JP2005516116A (ja) 2002-01-23 2003-01-21 安定化した結晶粒度の耐火金属粉末冶金による延伸材
BR0307073-5A BR0307073A (pt) 2002-01-23 2003-01-21 Produtos de moinho de metalurgia de pulverizado de metal refratário de tamanho de grão estabilizado
MXPA04007104A MXPA04007104A (es) 2002-01-23 2003-01-21 Productos laminados de pulvimetalurgia de metal refractario de tamano de grano estabilizado.
KR10-2004-7011314A KR20040091627A (ko) 2002-01-23 2003-01-21 안정화된 입자 크기의 난융 금속 분말 야금 밀 제품
NZ534212A NZ534212A (en) 2002-01-23 2003-01-21 Process for making stabilized grain size refractory metal powder metallurgy mill products
YU64904A RS64904A (en) 2002-01-23 2003-01-21 Stabilized grain size refractory metal powder metallurgy mill products
EP03705856A EP1506322A2 (en) 2002-01-23 2003-01-21 Stabilized grain size refractory metal powder metallurgy mill products

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US35114602P 2002-01-23 2002-01-23
US60/351,146 2002-01-23

Publications (2)

Publication Number Publication Date
WO2003062482A2 true WO2003062482A2 (en) 2003-07-31
WO2003062482A3 WO2003062482A3 (en) 2004-02-26

Family

ID=27613465

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/US2003/001823 WO2003062482A2 (en) 2002-01-23 2003-01-21 Stabilized grain size refractory metal powder metallurgy mill products

Country Status (16)

Country Link
US (1) US20050118052A1 (ko)
EP (1) EP1506322A2 (ko)
JP (1) JP2005516116A (ko)
KR (1) KR20040091627A (ko)
CN (1) CN1623005A (ko)
BR (1) BR0307073A (ko)
CA (1) CA2473493A1 (ko)
IL (1) IL162904A0 (ko)
MX (1) MXPA04007104A (ko)
NZ (1) NZ534212A (ko)
PL (1) PL371625A1 (ko)
RS (1) RS64904A (ko)
RU (1) RU2004125856A (ko)
TW (1) TWI262109B (ko)
WO (1) WO2003062482A2 (ko)
ZA (1) ZA200405764B (ko)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2004069453A2 (en) * 2003-01-31 2004-08-19 H.C. Starck, Inc. Refractory metal annealing bands
CN106567048A (zh) * 2016-11-10 2017-04-19 洛阳科威钨钼有限公司 一种大型高纯钼合金旋转靶材的制造方法

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2214853A4 (en) * 2007-10-15 2013-05-22 Hi Temp Specialty Metals Inc PROCESS FOR PREPARING TANTALUM POWDER USING RECYCLED AGENTS AS AN EXISTING MATERIAL
KR101364607B1 (ko) * 2013-09-11 2014-02-20 한국지질자원연구원 금속 몰리브덴 분말의 산소 저감에 의한 소결체의 결정립 미세화 방법
US9238852B2 (en) * 2013-09-13 2016-01-19 Ametek, Inc. Process for making molybdenum or molybdenum-containing strip
US11274363B2 (en) * 2019-04-22 2022-03-15 Nxp Usa, Inc. Method of forming a sputtering target

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4950327A (en) * 1987-01-28 1990-08-21 Schwarzkopf Development Corporation Creep-resistant alloy of high-melting metal and process for producing the same
US6261337B1 (en) * 1999-08-19 2001-07-17 Prabhat Kumar Low oxygen refractory metal powder for powder metallurgy

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4950327A (en) * 1987-01-28 1990-08-21 Schwarzkopf Development Corporation Creep-resistant alloy of high-melting metal and process for producing the same
US6261337B1 (en) * 1999-08-19 2001-07-17 Prabhat Kumar Low oxygen refractory metal powder for powder metallurgy

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
R.F.CHENEY: "Sintering of refractory metals" , METALS HANDBOOK, ASM, 9TH ED. VOL. 7, 1984, PAGES 389-393 , METALS PARK, OHIO, US XP002245862 page 391, column 2, line 51 - line 60 *

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2004069453A2 (en) * 2003-01-31 2004-08-19 H.C. Starck, Inc. Refractory metal annealing bands
WO2004069453A3 (en) * 2003-01-31 2004-12-09 Starck H C Inc Refractory metal annealing bands
CN106567048A (zh) * 2016-11-10 2017-04-19 洛阳科威钨钼有限公司 一种大型高纯钼合金旋转靶材的制造方法

Also Published As

Publication number Publication date
KR20040091627A (ko) 2004-10-28
TWI262109B (en) 2006-09-21
WO2003062482A3 (en) 2004-02-26
CN1623005A (zh) 2005-06-01
MXPA04007104A (es) 2004-10-29
TW200307583A (en) 2003-12-16
RS64904A (en) 2006-10-27
US20050118052A1 (en) 2005-06-02
EP1506322A2 (en) 2005-02-16
IL162904A0 (en) 2005-11-20
BR0307073A (pt) 2004-12-28
CA2473493A1 (en) 2003-07-31
PL371625A1 (en) 2005-06-27
RU2004125856A (ru) 2005-06-10
NZ534212A (en) 2006-04-28
JP2005516116A (ja) 2005-06-02
ZA200405764B (en) 2005-07-20

Similar Documents

Publication Publication Date Title
KR100236429B1 (ko) 실리콘과 도펀트화합물을 갖는정제된 탄탈륨 또는 니오븀합금
US7311874B2 (en) Sputter target and method for fabricating sputter target including a plurality of materials
AU766574B2 (en) Low oxygen refractory metal powder for powder metallurgy
CN106062235B (zh) 用于制备钼或含钼的带材的方法
JP5855565B2 (ja) セラミックスを含有したチタン合金混合粉、これを用いた緻密化されたチタン合金材およびその製造方法
EP2804711B1 (en) Mixture of powders for preparing a sintered nickel-titanium-rare earth metal (ni-ti-re) alloy
WO2012148471A1 (en) Powder metallurgy methods for the production of fine and ultrafine grain ti, and ti alloys
JP2002371301A (ja) タングステン焼結体およびその製造方法
US20050118052A1 (en) Stabilized grain size refractory metal powder metallurgy mill products
CN110449580B (zh) 一种粉末冶金高强韧性含硼高熵合金材料及其制备方法和应用
US11084093B2 (en) Ti—Fe-based sintered alloy material and method for producing same
JP2005520055A (ja) 増大した引張強さ及び硬さを有するキャパシタ−グレードのリードワイヤ
JP2005520055A5 (ko)
JP5070617B2 (ja) タンタル−ケイ素合金およびそれを含む製品およびそれを製造する方法
AU2003207637A1 (en) Stabilized grain size refractory metal powder metallurgy mill products
JP2737487B2 (ja) 高密度粉末焼結用チタン合金の製造方法
JP3551355B2 (ja) Ruターゲットおよびその製造方法
JPS63199843A (ja) モリブデンまたはその合金とジルコニアの複合成形体およびその製造法
JPH06271901A (ja) 焼結性に優れたTi−Al系金属間化合物粉末およびその焼結体
JPS63171847A (ja) モリブデンルツボとその製造方法
JP2803455B2 (ja) 高密度粉末焼結チタン合金の製造方法
JP3385552B2 (ja) モリブデン材料およびその製造方法
JPH06128604A (ja) 金属材料の製造方法
JP2684477B2 (ja) 高炭素鋼材の製造方法
JPH06306513A (ja) 高疲労強度焼結チタン合金の製造方法

Legal Events

Date Code Title Description
WWE Wipo information: entry into national phase

Ref document number: P-649/04

Country of ref document: YU

AK Designated states

Kind code of ref document: A2

Designated state(s): AE AG AL AM AT AU AZ BA BB BG BR BY BZ CA CH CN CO CR CU CZ DE DK DM DZ EC EE ES FI GB GD GE GH GM HR HU ID IL IN IS JP KE KG KP KR KZ LC LK LR LS LT LU LV MA MD MG MK MN MW MX MZ NO NZ OM PH PL PT RO RU SC SD SE SG SK SL TJ TM TN TR TT TZ UA UG US UZ VC VN YU ZA ZM ZW

AL Designated countries for regional patents

Kind code of ref document: A2

Designated state(s): GH GM KE LS MW MZ SD SL SZ TZ UG ZM ZW AM AZ BY KG KZ MD RU TJ TM AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HU IE IT LU MC NL PT SE SI SK TR BF BJ CF CG CI CM GA GN GQ GW ML MR NE SN TD TG

DFPE Request for preliminary examination filed prior to expiration of 19th month from priority date (pct application filed before 20040101)
121 Ep: the epo has been informed by wipo that ep was designated in this application
WWE Wipo information: entry into national phase

Ref document number: 2003705856

Country of ref document: EP

WWE Wipo information: entry into national phase

Ref document number: 1984/DELNP/2004

Country of ref document: IN

WWE Wipo information: entry into national phase

Ref document number: 2473493

Country of ref document: CA

WWE Wipo information: entry into national phase

Ref document number: 1-2004-501069

Country of ref document: PH

WWE Wipo information: entry into national phase

Ref document number: 10502281

Country of ref document: US

WWE Wipo information: entry into national phase

Ref document number: 2004/05764

Country of ref document: ZA

Ref document number: 534212

Country of ref document: NZ

Ref document number: 200405764

Country of ref document: ZA

WWE Wipo information: entry into national phase

Ref document number: PA/a/2004/007104

Country of ref document: MX

Ref document number: 2003207637

Country of ref document: AU

Ref document number: 2003562348

Country of ref document: JP

Ref document number: 1020047011314

Country of ref document: KR

WWE Wipo information: entry into national phase

Ref document number: 20038026465

Country of ref document: CN

WWE Wipo information: entry into national phase

Ref document number: 2004125856

Country of ref document: RU

WWP Wipo information: published in national office

Ref document number: 2003705856

Country of ref document: EP

WWP Wipo information: published in national office

Ref document number: 534212

Country of ref document: NZ

WWW Wipo information: withdrawn in national office

Ref document number: 2003705856

Country of ref document: EP