US20130071284A1 - Titanium alloy complex powder containing copper powder, chromium powder or iron powder, titanium alloy material consisting of this powder, and process for production thereof - Google Patents

Titanium alloy complex powder containing copper powder, chromium powder or iron powder, titanium alloy material consisting of this powder, and process for production thereof Download PDF

Info

Publication number
US20130071284A1
US20130071284A1 US13/701,159 US201113701159A US2013071284A1 US 20130071284 A1 US20130071284 A1 US 20130071284A1 US 201113701159 A US201113701159 A US 201113701159A US 2013071284 A1 US2013071284 A1 US 2013071284A1
Authority
US
United States
Prior art keywords
powder
titanium alloy
chromium
iron
hip
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.)
Abandoned
Application number
US13/701,159
Other languages
English (en)
Inventor
Osamu Kano
Hideo Takatori
Satoshi Sugawara
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.)
Toho Titanium Co Ltd
Original Assignee
Individual
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 Individual filed Critical Individual
Assigned to TOHO TITANIUM CO., LTD. reassignment TOHO TITANIUM CO., LTD. ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: KANO, OSAMU, SUGAWARA, SATOSHI, TAKATORI, HIDEO
Publication of US20130071284A1 publication Critical patent/US20130071284A1/en
Abandoned legal-status Critical Current

Links

Images

Classifications

    • B22F1/0003—
    • 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
    • B22F8/00—Manufacture of articles from scrap or waste metal particles
    • 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
    • B22F1/00—Metallic powder; Treatment of metallic powder, e.g. to facilitate working or to improve properties
    • B22F1/09—Mixtures of metallic powders
    • 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
    • B22F9/02—Making metallic powder or suspensions thereof using physical processes
    • B22F9/023—Hydrogen absorption
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C1/00—Making non-ferrous alloys
    • C22C1/04—Making non-ferrous alloys by powder metallurgy
    • C22C1/045—Alloys based on refractory metals
    • C22C1/0458—Alloys based on titanium, zirconium or hafnium
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C14/00—Alloys based on 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
    • B22F2998/00—Supplementary information concerning processes or compositions relating to powder metallurgy
    • B22F2998/10—Processes characterised by the sequence of their steps
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02P—CLIMATE CHANGE MITIGATION TECHNOLOGIES IN THE PRODUCTION OR PROCESSING OF GOODS
    • Y02P10/00—Technologies related to metal processing
    • Y02P10/20—Recycling
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02W—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO WASTEWATER TREATMENT OR WASTE MANAGEMENT
    • Y02W30/00—Technologies for solid waste management
    • Y02W30/50—Reuse, recycling or recovery technologies

Definitions

  • the present invention relates to titanium alloy complex powder containing copper powder, chromium powder or iron powder, titanium alloy material consisting of the powder and a process for production thereof, and in particular, relates to titanium alloy material having superior mechanical properties and relates to a process for production thereof.
  • Titanium alloy in particular, Ti-6Al-4V alloy has been well known as a material for airplanes.
  • the titanium alloy is produced by a vacuum arc remelting method or an electron beam remelting method.
  • the vacuum arc remelting method is a process in which Al—V master alloy is added to titanium material at an appropriate amount, this is pressed into briquettes, the briquettes are mutually bonded to form an electrode for remelting, the electrode for remelting is set in the vacuum arc remelting furnace, and the electrode is remelted in the vacuum to produce alloy ingots.
  • the electron beam remelting method is a process in which material for remelting consisting of titanium material and Al—V master alloy is supplied to a hearth, an electron beam is irradiated on the material to remelt it, and the melted metal is poured into a mold arranged downstream of the hearth to produce alloy ingots.
  • the alloy produced with powder material is greatly advantageous from the viewpoint of segregation compared to an alloy produced by the remelting method in which an ingot is solidified from the lower side to the upper side progressively.
  • the alloy is not produced via a step of being melted metal, there is no problem of evaporation of a low-melting point component. In this way, the powder method process for production of titanium alloy has several advantages compared to the remelting method.
  • the titanium alloy powder used in the powder method has inferior workability and formability, as a result, there is another problem that sintering density is difficult to increase.
  • Ti-6Al-4V alloy has small plastic deformability, it is known that sintering density is difficult increase by an ordinary method in the powder method (See Reference 1 below).
  • CIP Cold Isostatic Press
  • HIP Hot Isostatic Press
  • an upper limit of remaining pores in titanium alloy after sintering is controlled to be not more than 50 ⁇ m in the Reference 2.
  • a dense alloy having further fine pores or having no pores substantially is required as a material to which further higher strength is required compared to conventional titanium alloy.
  • An object of the present invention is to provide titanium alloy powder having superior quality by the powder method using titanium alloy scrap or titanium alloy ingot as a raw material, titanium alloy material, and a process for production thereof.
  • titanium alloy complex powder having uniform composition can be produced, by using the titanium alloy scrap or titanium alloy ingot as a raw material, hydrogenating it to generate hydrogenated titanium alloy, dehydrogenating it to generate titanium alloy powder, and further adding copper powder, chromium powder or iron powder, and thus the present invention has been completed.
  • titanium alloy complex powder having copper powder, chromium powder or iron powder can be consolidated to not less than 99% of theoretical density by CIP process and subsequent HIP process or by HIP process after filling the titanium alloy complex powder into a capsule, and thus, the present invention has been completed.
  • titanium alloy complex powder of the present invention has titanium alloy powder, and at least one kind of metallic powder selected from copper powder, chromium powder and iron powder added to the titanium alloy powder, wherein the added amount of the metallic powder is in a range from 1 to 10 wt % in the case in which one metallic powder is added, and the added amount of the metallic powder is in a range from 1 to 20 wt % in the case in which two or more metallic powders are added.
  • the titanium alloy powder contain aluminum and vanadium, or contain at least one kind selected from zirconium, tin, molybdenum, iron and chromium in addition to aluminum and vanadium.
  • the average particle size of the copper powder, chromium powder or iron powder be in a range from 1 to 300 ⁇ m.
  • a process for production of titanium alloy complex powder of the present invention has steps of hydrogenating titanium alloy raw material to generate hydrogenated titanium alloy powder, dehydrogenating the hydrogenated titanium alloy powder to generate titanium alloy powder, and adding at least one of copper powder, chromium powder or iron powder.
  • a process for production of titanium alloy material of the present invention has steps of consolidating the titanium alloy complex powder by CIP process and subsequent HIP process, or by HIP process after filling into a capsule.
  • a titanium alloy material of the present invention is produced by using titanium alloy powder as a raw material which is produced by the process having steps of hydrogenating titanium alloy raw material to generate hydrogenated titanium alloy powder, dehydrogenating the hydrogenated titanium alloy powder to generate titanium alloy powder, and adding at least one of copper powder, chromium powder or iron powder.
  • a true density of the titanium alloy material produced by the above process be not less than 99% of theoretical density.
  • titanium alloy material of the present invention is produced not via remelting and solidifying, segregation of copper, chromium or iron does not occur, and as a result, although it has been conventionally regarded as difficult to disperse or solid solve by the remelting method, copper, chromium or iron can be added at high concentration. Furthermore, since reactions between titanium alloy powder and copper powder, chromium powder or iron powder occur in consolidating processes, and no special technique such as mechanical alloying or the like is necessary in the mixing step.
  • FIG. 1 is a flow chart diagram showing the process for production of titanium alloy material of the present invention.
  • FIG. 2 is a SEM photograph of Ti-6Al-4V alloy powder produced by the hydrogenating and dehydrogenating processes.
  • FIG. 3 is a SEM photograph of titanium alloy complex powder in which copper powder is added to titanium alloy powder.
  • FIG. 4 is a result of EPMA analysis of 5% Cu containing Ti-6Al-4V alloy material in width direction.
  • FIG. 1 shows a desirable embodiment for production of titanium alloy material of the present invention.
  • a raw material of titanium alloy a mixture consisting of a master alloy powder having desired components produced in another process and pure titanium powder can be used; however, since the master alloy powder is expensive, it is desirable to use an alloy scrap or titanium alloy ingot originally having desired components such as titanium alloy chips, titanium alloy forged chips, edge material of titanium alloy rods or the like as the raw material in the present invention from the viewpoint of cost reduction.
  • titanium alloy raw material titanium alloy scraps or titanium alloy ingots
  • block shaped alloy scrap such as the forged chips
  • the alloy raw material is titanium alloy ingot, it is desirable to treat it so as to be cut chips.
  • the titanium alloy raw material treated and controlled as mentioned above is brought into the hydrogenating process under a hydrogen atmosphere.
  • the hydrogenating process is desirably performed in a temperature range from 500 to 650° C. Since hydrogenating process reaction of alloy raw material is an exothermic reaction, any heating operation by a heating furnace is not necessary accompanied by promotion of hydrogenating reaction, and thus hydrogenating reaction can be promoted automatically.
  • the titanium alloy raw material which is hydrogenation treated (hereinafter simply referred to as “hydrogenated titanium alloy”) is then cooled to room temperature, and it is desirably ground and sifted until hydrogenated titanium powder has a predetermined particle size under an inert atmosphere such as argon gas or the like.
  • hydrogenated titanium alloy powder that is ground and sifted is desirably heated until it reaches a high temperature range in an atmosphere held at reduced pressure.
  • the temperature of dehydrogenating process is desirably performed in a range from 500 to 800° C. Since the dehydrogenation reaction is an endothermic reaction, in contrast to the above-mentioned hydrogenation reaction, heating operation is necessary until hydrogen is completely generated from hydrogenated titanium alloy powder. By the operation, titanium alloy powder of the present invention can be obtained.
  • titanium alloy powder of the present invention be controlled in a range from 1 to 300 ⁇ m.
  • Titanium alloy powder obtained by the above-mentioned dehydrogenating process is sometimes sintered together, and in this case, it is desirable that the grinding and sifting processes be performed again.
  • the titanium alloy complex powder of the present invention After dehydrogenating process, by adding copper powder, chromium powder or iron powder which is a third component used in the present invention to the titanium alloy powder ground and sifted, the titanium alloy complex powder of the present invention can be obtained. It is desirable that the titanium alloy complex powder of which grinding and sifting processes be performed and copper powder, chromium powder or iron powder be added controlled in a range from 1 to 300 ⁇ m.
  • the consolidating process be performed by combining CIP and HIP appropriately.
  • titanium alloy complex powder obtained in the above-mentioned method be filled in a CIP rubber, treated at 100 to 200 MPa, then filled in a HIP capsule, and HIP treated at a temperature not more than ⁇ transformation point at 50 to 200 MPa for 1 to 5 hours. After such CIP process and subsequent HIP process, consolidated titanium alloy material can be obtained.
  • titanium alloy complex powder obtained in the above-mentioned method be filled in a HIP capsule and HIP treated at a temperature not higher than ⁇ transformation point at pressure from 50 to 200 MPa for 1 to 5 hours without CIP process.
  • Consolidated titanium alloy material can also be obtained by only the HIP process.
  • the ratio of adding be 1 to 10% of titanium alloy powder weight in the case in which one kind of these metallic powders is added.
  • the total ratio of adding be 1 to 20% of titanium alloy powder weight in the case in which two kinds or more of these metallic powders are added.
  • iron or chromium is originally contained in titanium alloy powder
  • addition ratio of copper powder, chromium powder or iron powder which is the third component and is alone added to titanium alloy powder is not more than 1%, effect of the consolidation cannot be exhibited sufficiently in the consolidating process in the sintering process.
  • addition ratio of copper powder, chromium powder or iron powder is more than 10%, strength of titanium alloy is undesirably deteriorated.
  • copper powder, chromium powder or iron powder used in the present invention has a purity of 2N5 to 4N5.
  • chromium powder or iron powder added to titanium alloy powder commercially available powder sample can be used.
  • powder sample powder that is obtained by grinding a block sample and then sifting can be used.
  • Titanium alloy powder to which copper powder, chromium powder or iron powder is added is consolidated by performing CIP process and subsequent HIP process, or by performing HIP process after filling titanium alloy powder into a capsule.
  • CIP process in the case of an alloy in which copper powder, chromium powder or iron powder is added to Ti-6Al-4V alloy, it is desirable to perform CIP process at 900° C. which is not higher than ⁇ transformation point and at hydrostatic pressure of 100 to 200 MPa and then to perform HIP process at a hydrostatic pressure of 100 MPa for 1 hour.
  • Titanium alloy material having a density not less than 99% can be obtained by such consolidating process.
  • Copper powder, chromium powder or iron powder added in titanium alloy powder is dispersed in titanium of alloy material matrix during a consolidating process, and as a result, alloy in which atoms of copper, chromium or iron are uniformly solid solved in titanium alloy can be produced.
  • titanium alloy copper, chromium or iron that is solid solved in titanium alloy can be solid solved at high ratio compared to a conventional remelting method, that is, 1 to 10 wt % in single powder addition and 1 to 20 wt % in plural powder addition. As a result, mechanical properties of titanium alloy material can be effectively controlled.
  • titanium alloy such as Ti-6Al-4V alloy, Ti-3Al-2.5V alloy, Ti-6Al-2Sn-4Zr-6Mo alloy, Ti-6Al-6V-2Sn alloy, Ti-10V-2Fe-3A1 alloy (10-2-3), Ti-5Al-4V-0.6Mo-0.4Fe alloy (Ti metal 54M), Ti-4.5Al-3V-2Fe-2Mo alloy (SP700), Ti-15V-3Cr-3Al-3Sn alloy (15-3-3-3), Ti-4Al-2.5V-1.5Fe alloy (ATI425), Ti-5Al-5V-5Mo-3Cr alloy (Ti-5553) can be used as the above mentioned raw material of titanium alloy powder.
  • Ti-6Al-4V alloy Ti-3Al-2.5V alloy
  • Ti-6Al-2Sn-4Zr-6Mo alloy Ti-6Al-6V-2Sn alloy
  • Ti-10V-2Fe-3A1 alloy 10-2-3
  • Ti-5Al-4V-0.6Mo-0.4Fe alloy Ti-4.5Al-3V-2Fe
  • Mechanical properties of titanium alloy material containing copper, chromium or iron and being consolidated by the above-mentioned method can be further controlled by subsequent processing such as rolling, extrusion or drawing and heat process.
  • Scrap cut chips of Ti-6Al-4V alloy were cut into chips having lengths not greater than 10 mm.
  • the chips were inserted into a container and the container was set in a furnace. After vacuum evacuation inside the furnace, heating was started, hydrogen was induced into the furnace after the temperature inside the furnace reached 300° C., and heating was continued until 650° C. while maintaining the inside of the furnace in a slightly pressurized condition by hydrogen. During this process, since Ti-6Al-4V alloy scrap chips and hydrogen are reacted and temperature inside the furnace is increased, heater output was set at 0, and the condition was maintained as it was until the reaction was completed.
  • FIG. 2 shows an SEM photograph of titanium alloy powder obtained as above. It was confirmed that alloy powder having relatively even particle size can be obtained by the method of the present invention in the photograph.
  • Electrolytic copper powder (particle size: not greater than 45 ⁇ m, produced by JX Nippon Mining & Metals Corporation) was added to titanium alloy powder of Example 1 at 5 wt % of titanium alloy powder, and they were mixed with a V-type mixing machine.
  • FIG. 3 shows an SEM photograph of titanium alloy complex powder obtained as above. It was confirmed that titanium alloy complex powder having relatively even particle size can be obtained by the method of the present invention in the photograph. Maximal particle size of obtained mixture powder was 300 ⁇ m, and average particle size was 60 ⁇ m.
  • Cu-added titanium alloy powder of Example 2 was filled in a CIP rubber, and CIP treated at 100 MPa. Density of the CIP compact was 65%. It has strength sufficient to be self-supported, and it was never broken during handling.
  • the CIP compact was encapsulated in a soft steel capsule and HIP treated. Conditions of HIP were 900° C., 100 MPa and 1 hr. After HIP process, titanium material was taken out and its density was measured, and it was not less than 99%. Density mentioned here means the ratio of apparent density against the theoretical density.
  • Cu-added titanium alloy powder of Example 2 was encapsulated in a soft steel capsule and HIP treated. Conditions of HIP were 900° C., 100 MPa and 1 hr. After HIP process, titanium alloy material was taken out and its density was measured, and it was not less than 99%. Density mentioned here means the ratio of apparent density against the theoretical density.
  • Titanium alloy material of Example 3 was analyzed by EPMA along a range of 10.5 mm to confirm variation of each component of Ti, Al, V and Cu, and the results are shown in FIG. 4 . It is confirmed that concentration of Cu is almost uniform around 5% along the analyzed range of 10.5 mm.
  • Chromium powder was added to titanium alloy powder of Example 1 at 5 wt % of titanium alloy powder to obtain Cr containing titanium alloy powder.
  • Cr powder was prepared by crushing electrolytic chromium powder produced by Japan Metals & Chemicals Co., Ltd., and sifting it by using a sifter of 50 mesh.
  • Cr containing titanium alloy material was obtained by CIP process and subsequent HIP process in a similar conditions of Example 3. Density of the material was not less than 99%.
  • Chromium added titanium alloy powder of Example 5 was encapsulated in a soft steel capsule and HIP process was performed.
  • HIP condition was 900° C., 100 MPa, and 1 hour. After HIP process, titanium alloy material was taken out and the density was measured, and the density was not less than 99%.
  • Iron powder was added to titanium alloy powder of Example 1 at 5 wt % of titanium alloy powder to obtain Fe containing titanium alloy powder.
  • Fe powder was commercially available atomized iron powder, and its average particle diameter was 4 ⁇ m.
  • Fe containing titanium alloy material was obtained by CIP process and subsequent HIP process in a similar conditions of Example 3. Density of the material was not less than 99%.
  • Iron added titanium alloy powder of Example 6 was encapsulated in a soft steel capsule and HIP process was performed. HIP conditions were 900° C., 100 MPa, and 1 hour. After HIP process, titanium alloy material was taken out and the density was measured, and the density was not less than 99%.
  • Cu powder and Fe powder were added to titanium alloy powder of Example 1 at 5 wt % (each powder), 10 wt % (total powders of Cu+Fe) of titanium alloy powder to obtain Cu—Fe containing titanium alloy powder.
  • Cu powder and Fe powder were the same powders as in Examples 2 and 6 respectively.
  • Cu—Fe containing titanium alloy material was obtained by CIP process and subsequent HIP process in the similar conditions of Example 3. Density of the material was not less than 99%.
  • HIP process Cu powder and Fe powder added titanium alloy powder of Example 7 was encapsulated in a soft steel capsule and HIP process was performed. HIP conditions were 900° C., 100 MPa, and 1 hour. After HIP process, titanium alloy material was taken out and the density was measured, and the density was not less than 99%.
  • Cu powder and Cr powder were added to titanium alloy powder of Example 1 at 5 wt % (each powder), 10 wt % (total powders of Cu+Cr) of titanium alloy powder to obtain Cu—Cr containing titanium alloy powder.
  • Cu powder and Cr powder were the same powders as in Examples 2 and 5 respectively.
  • Cu—Cr containing titanium alloy material was obtained by CIP process and subsequent HIP process in the similar conditions of Example 3. Density of the material was not less than 99%.
  • HIP condition was 900° C., 100 MPa, and 1 hour. After HIP process, titanium alloy material was taken out and the density was measured, and the density was not less than 99%.
  • Cr powder and Fe powder were added to titanium alloy powder of Example 1 at 5 wt % (each powder), 10 wt % (total powders of Cr+Fe) of titanium alloy powder to obtain Cr—Fe containing titanium alloy powder.
  • Cr powder and Fe powder were the same powders as in Examples 5 and 6 respectively.
  • Cr—Fe containing titanium alloy material was obtained by CIP process and subsequent HIP process in the similar conditions of Example 3. Density of the material was not less than 99%.
  • HIP process Cr powder and Fe powder added titanium alloy powder of Example 9 was encapsulated in a soft steel capsule and HIP process was performed. HIP conditions were 900° C., 100 MPa, and 1 hour. After HIP process, titanium alloy material was taken out and the density was measured, and the density was not less than 99%.
  • Cu powder, Cr powder and Fe powder were added to titanium alloy powder of Example 1 at 4 wt % (each powder), 12 wt % (total powders of Cu+Cr+Fe) of titanium alloy powder to obtain Cu—Cr—Fe containing titanium alloy powder.
  • Cu powder, Cr powder and Fe powder were the same powders as in Examples 2, 5 and 6 respectively.
  • Cu—Cr—Fe containing titanium alloy material was obtained by CIP process and subsequent HIP process in the similar conditions of Example 3. Density of the material was not less than 99%.
  • HIP process was performed. HIP conditions was 900° C., 100 MPa, and 1 hour. After HIP process, titanium alloy material was taken out and the density was measured, and the density was not less than 99%.
  • Cu powder was each added at 1%, 3%, 8% and 10% in a way completely similar to that of Example 2 to obtain four samples of Cu containing titanium alloy powder.
  • Cu containing titanium alloy material was obtained by CIP process and subsequent HIP process in similar conditions of Example 3. Densities of all the materials were not less than 99%. Vickers hardnesses thereof were measured, and the results are shown in Table 1. In Table 1, the result of 5 wt % containing alloy of Example 4 is also shown.
  • Titanium alloy powder the as same as in Example 1 was CIP treated in a manner similar to that of Example 3 without adding Cu, Cr and Fe powder.
  • a CIP compact does not have sufficient strength, and a corner part was broken right after removal. Although the part was broken, an attempt was made to handle the CIP compact so as to be encapsulated into a HIP container. Then, the compact broke at a central part into two pieces, and HIP process could not be performed.
  • CIP process was performed similarly at 200 MPa of hydrostatic pressure, and the compact could be completed. The compact was carefully handled to be encapsulated in a HIP container, and HIP was performed in conditions similar to that of Example 3. The compact was taken out of the HIP container and density was measured, and the density was 98%.
  • the present invention provides titanium alloy complex powder, consolidated titanium alloy material and process for production thereof, using titanium alloy scrap or ingot as a raw material and by a hydrogenation and dehydrogenation method.

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Manufacturing & Machinery (AREA)
  • Powder Metallurgy (AREA)
  • Manufacture Of Metal Powder And Suspensions Thereof (AREA)
US13/701,159 2010-05-31 2011-05-31 Titanium alloy complex powder containing copper powder, chromium powder or iron powder, titanium alloy material consisting of this powder, and process for production thereof Abandoned US20130071284A1 (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
JP2010124455 2010-05-31
JP2010-124455 2010-05-31
PCT/JP2011/062873 WO2011152553A1 (ja) 2010-05-31 2011-05-31 銅粉、クロム粉または鉄粉を配合したチタン合金複合粉、これを原料としたチタン合金材及びその製造方法

Publications (1)

Publication Number Publication Date
US20130071284A1 true US20130071284A1 (en) 2013-03-21

Family

ID=45066907

Family Applications (1)

Application Number Title Priority Date Filing Date
US13/701,159 Abandoned US20130071284A1 (en) 2010-05-31 2011-05-31 Titanium alloy complex powder containing copper powder, chromium powder or iron powder, titanium alloy material consisting of this powder, and process for production thereof

Country Status (6)

Country Link
US (1) US20130071284A1 (de)
EP (1) EP2578336A4 (de)
JP (1) JP5889786B2 (de)
CN (1) CN102905822B (de)
RU (1) RU2572928C2 (de)
WO (1) WO2011152553A1 (de)

Cited By (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20160354976A1 (en) * 2015-06-08 2016-12-08 The Boeing Company Additive Manufacturing Methods
WO2019118991A1 (en) * 2017-12-14 2019-06-20 Csir A process and method for producing titanium and titanium alloy billets, spherical and non-spherical powder
US10422018B2 (en) 2013-05-17 2019-09-24 G. Rau Gmbh & Co. Kg Method and device for remelting and/or remelt-alloying metallic materials, in particular Nitinol
US10639712B2 (en) 2018-06-19 2020-05-05 Amastan Technologies Inc. Process for producing spheroidized powder from feedstock materials
US10987735B2 (en) 2015-12-16 2021-04-27 6K Inc. Spheroidal titanium metallic powders with custom microstructures
US11148202B2 (en) * 2015-12-16 2021-10-19 6K Inc. Spheroidal dehydrogenated metals and metal alloy particles
GB2599237A (en) * 2020-09-24 2022-03-30 Bae Systems Plc Powder hot isostatic pressing cycle
US11311938B2 (en) 2019-04-30 2022-04-26 6K Inc. Mechanically alloyed powder feedstock
US11583923B2 (en) 2016-12-07 2023-02-21 Mitsubishi Heavy Industries Aero Engines, Ltd. Hydrogenation-dehydrogenation method for TiAl alloy and method for producing TiAl alloy powder
US11590568B2 (en) 2019-12-19 2023-02-28 6K Inc. Process for producing spheroidized powder from feedstock materials
US11611130B2 (en) 2019-04-30 2023-03-21 6K Inc. Lithium lanthanum zirconium oxide (LLZO) powder
US11717886B2 (en) 2019-11-18 2023-08-08 6K Inc. Unique feedstocks for spherical powders and methods of manufacturing
US11855278B2 (en) 2020-06-25 2023-12-26 6K, Inc. Microcomposite alloy structure
US11919071B2 (en) 2020-10-30 2024-03-05 6K Inc. Systems and methods for synthesis of spheroidized metal powders
US11963287B2 (en) 2020-09-24 2024-04-16 6K Inc. Systems, devices, and methods for starting plasma
US12040162B2 (en) 2023-06-07 2024-07-16 6K Inc. Plasma apparatus and methods for processing feed material utilizing an upstream swirl module and composite gas flows

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP5759426B2 (ja) * 2012-07-24 2015-08-05 東邦チタニウム株式会社 チタン合金及びその製造方法
CN104416156B (zh) * 2013-09-11 2016-08-17 安泰科技股份有限公司 铬铝合金靶材及其制备方法
CN104827022A (zh) * 2015-04-27 2015-08-12 苏州统明机械有限公司 一种用于陶瓷的镍铬合金涂层及其制备方法
CN105855745B (zh) * 2016-05-10 2018-07-17 武汉工程大学 一种铜基焊料及其制备方法和应用方法
US10357822B2 (en) * 2017-03-29 2019-07-23 The Boeing Company Titanium-copper-iron alloy and associated thixoforming method
CN107739887B (zh) * 2017-10-24 2019-08-20 宝鸡市永盛泰钛业有限公司 一种钛合金锻件及其制备工艺
CN107999752B (zh) * 2017-11-29 2020-07-28 吉林云亭石墨烯技术股份有限公司 一种石墨烯3d打印合金材料的制备方法
RU2754672C1 (ru) * 2020-10-26 2021-09-06 Федеральное государственное бюджетное образовательное учреждение высшего образования "Московский авиационный институт (национальный исследовательский университет)" Способ обработки порошкового титанового материала
CN113817933B (zh) * 2021-09-16 2022-05-06 湖南金天铝业高科技股份有限公司 陶瓷增强钛基复合材料、其制备方法及应用

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH05239570A (ja) * 1992-01-09 1993-09-17 Nippon Steel Corp 焼結チタン合金の製造方法
US5922452A (en) * 1996-03-21 1999-07-13 Honda Giken Kogyo Kabushiki Kaisha Titanium and/or titanium alloy sintered friction material

Family Cites Families (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2464112A1 (fr) * 1979-08-27 1981-03-06 Commissariat Energie Atomique Procede de fabrication de pieces en alliage a base de titane par metallurgie des poudres
JPS63183145A (ja) * 1987-01-22 1988-07-28 Sumitomo Electric Ind Ltd 高硬度チタン−アルミニウム−バナジウム系合金およびその製造方法
JPH0250172A (ja) 1988-08-11 1990-02-20 Tokai Rubber Ind Ltd 導電性ロール
JPH0711041B2 (ja) * 1989-04-10 1995-02-08 東京窯業株式会社 セラミックス粒子強化チタン複合材料
JPH03243741A (ja) * 1990-02-21 1991-10-30 Nippon Tungsten Co Ltd Ｔｉ―Ａｌ系焼結体およびその製造方法
JP3223538B2 (ja) 1990-11-09 2001-10-29 株式会社豊田中央研究所 焼結チタン合金およびその製造方法
RU2026154C1 (ru) * 1991-06-26 1995-01-09 Всероссийский научно-исследовательский институт авиационных материалов Способ изготовления спеченных пористых изделий из титана или циркония
JP2737487B2 (ja) * 1991-11-25 1998-04-08 日本鋼管株式会社 高密度粉末焼結用チタン合金の製造方法
JP2551285B2 (ja) * 1991-11-25 1996-11-06 日本鋼管株式会社 高密度粉末焼結用チタン合金
JP2737498B2 (ja) * 1991-12-24 1998-04-08 日本鋼管株式会社 高密度粉末焼結用チタン合金
JPH05345937A (ja) * 1992-04-17 1993-12-27 Nippon Steel Corp Ｔｉ−Ｆｅ−Ａｌ系焼結チタン合金の製造方法
JPH0754021A (ja) * 1993-08-19 1995-02-28 Nippon Steel Corp チタン粉末の製造方法およびその装置
JPH0776705A (ja) * 1993-09-07 1995-03-20 Nippon Steel Corp チタン粉末製造の脱水素化処理における冷却方法および装置
JP3593414B2 (ja) * 1996-04-08 2004-11-24 啓太 平井 チタン合金複組成刃物
JP2002332531A (ja) * 1999-06-11 2002-11-22 Toyota Central Res & Dev Lab Inc チタン合金およびその製造方法
KR100417943B1 (ko) * 1999-06-11 2004-02-11 가부시키가이샤 도요다 쥬오 겐큐쇼 티탄 합금 및 이의 제조방법
JP2002206124A (ja) * 2001-01-04 2002-07-26 Sumitomo Metal Mining Co Ltd Ｔｉ合金焼結体の製造方法
UA70366C2 (uk) * 2001-11-23 2004-10-15 Orest Mykhailovych I Ivasyshyn Спосіб отримання виробів з титанових сплавів
CN101713043B (zh) * 2009-12-21 2012-07-25 中南大学 一种颗粒增强钛基复合材料及制备方法

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH05239570A (ja) * 1992-01-09 1993-09-17 Nippon Steel Corp 焼結チタン合金の製造方法
US5922452A (en) * 1996-03-21 1999-07-13 Honda Giken Kogyo Kabushiki Kaisha Titanium and/or titanium alloy sintered friction material

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
C.R.F. Azevedo, D. Rodrigues, F. Beneduce Neto, Ti-Al-V powder metallurgy (PM) via the hydrogenation-dehydrogenation (HDH) process, Journal of Alloys and Compounds, Volume 353, Issues 1-2, 7 April 2003, Pages 217-227, ISSN 0925-8388. *

Cited By (24)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10422018B2 (en) 2013-05-17 2019-09-24 G. Rau Gmbh & Co. Kg Method and device for remelting and/or remelt-alloying metallic materials, in particular Nitinol
US9796137B2 (en) * 2015-06-08 2017-10-24 The Boeing Company Additive manufacturing methods
US20160354976A1 (en) * 2015-06-08 2016-12-08 The Boeing Company Additive Manufacturing Methods
US11577314B2 (en) 2015-12-16 2023-02-14 6K Inc. Spheroidal titanium metallic powders with custom microstructures
US10987735B2 (en) 2015-12-16 2021-04-27 6K Inc. Spheroidal titanium metallic powders with custom microstructures
US11148202B2 (en) * 2015-12-16 2021-10-19 6K Inc. Spheroidal dehydrogenated metals and metal alloy particles
US11839919B2 (en) 2015-12-16 2023-12-12 6K Inc. Spheroidal dehydrogenated metals and metal alloy particles
US11583923B2 (en) 2016-12-07 2023-02-21 Mitsubishi Heavy Industries Aero Engines, Ltd. Hydrogenation-dehydrogenation method for TiAl alloy and method for producing TiAl alloy powder
WO2019118991A1 (en) * 2017-12-14 2019-06-20 Csir A process and method for producing titanium and titanium alloy billets, spherical and non-spherical powder
US11273491B2 (en) 2018-06-19 2022-03-15 6K Inc. Process for producing spheroidized powder from feedstock materials
US11465201B2 (en) 2018-06-19 2022-10-11 6K Inc. Process for producing spheroidized powder from feedstock materials
US11471941B2 (en) 2018-06-19 2022-10-18 6K Inc. Process for producing spheroidized powder from feedstock materials
US10639712B2 (en) 2018-06-19 2020-05-05 Amastan Technologies Inc. Process for producing spheroidized powder from feedstock materials
US11311938B2 (en) 2019-04-30 2022-04-26 6K Inc. Mechanically alloyed powder feedstock
US11611130B2 (en) 2019-04-30 2023-03-21 6K Inc. Lithium lanthanum zirconium oxide (LLZO) powder
US11633785B2 (en) 2019-04-30 2023-04-25 6K Inc. Mechanically alloyed powder feedstock
US11717886B2 (en) 2019-11-18 2023-08-08 6K Inc. Unique feedstocks for spherical powders and methods of manufacturing
US11590568B2 (en) 2019-12-19 2023-02-28 6K Inc. Process for producing spheroidized powder from feedstock materials
US11855278B2 (en) 2020-06-25 2023-12-26 6K, Inc. Microcomposite alloy structure
GB2599237A (en) * 2020-09-24 2022-03-30 Bae Systems Plc Powder hot isostatic pressing cycle
GB2599237B (en) * 2020-09-24 2024-01-10 Bae Systems Plc Powder hot isostatic pressing cycle
US11963287B2 (en) 2020-09-24 2024-04-16 6K Inc. Systems, devices, and methods for starting plasma
US11919071B2 (en) 2020-10-30 2024-03-05 6K Inc. Systems and methods for synthesis of spheroidized metal powders
US12040162B2 (en) 2023-06-07 2024-07-16 6K Inc. Plasma apparatus and methods for processing feed material utilizing an upstream swirl module and composite gas flows

Also Published As

Publication number Publication date
JP5889786B2 (ja) 2016-03-22
CN102905822B (zh) 2016-01-20
JPWO2011152553A1 (ja) 2013-08-01
CN102905822A (zh) 2013-01-30
RU2572928C2 (ru) 2016-01-20
EP2578336A4 (de) 2014-05-14
EP2578336A1 (de) 2013-04-10
WO2011152553A1 (ja) 2011-12-08
RU2012156888A (ru) 2014-07-20

Similar Documents

Publication Publication Date Title
US20130071284A1 (en) Titanium alloy complex powder containing copper powder, chromium powder or iron powder, titanium alloy material consisting of this powder, and process for production thereof
Ivasishin et al. Low-cost titanium hydride powder metallurgy
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
JP4894008B2 (ja) ＭｏＮｂ系焼結スパッタリングターゲット材の製造方法
JP5837407B2 (ja) チタン合金およびその製造方法
CN103443311B (zh) 用于生产钛合金焊丝的方法
Duz et al. Industrial application of titanium hydride powder
US9969004B2 (en) α+β or β titanium alloy and method for producing same
KR20120064687A (ko) 티타늄 합금의 미세구조 정련 방법 및 티타늄 합금의 고온-고변형률 초가소성 성형방법
US20180105897A1 (en) Alpha + beta or beta TITANIUM ALLOY AND METHOD FOR PRODUCTION THEREOF
US11008639B2 (en) Powder metallurgy titanium alloys
Qian et al. Sintering of titanium and its alloys
JP2014019945A (ja) チタン合金及びその製造方法
Zhang et al. The microstructure and mechanical properties of extra low interstitials (ELI) Ti-6Al-4V alloys manufactured from hydride–dehydride (HDH) powder
JP5837406B2 (ja) チタン合金およびその製造方法
EP0801138A2 (de) Herstellung einer Titan-Molybdän-Vorlegierung
Abakumov et al. High performance titanium powder metallurgy components produced from hydrogenated titanium powder by low cost blended elemental approach
JP2003055747A (ja) 焼結工具鋼及びその製造方法
RU2647424C1 (ru) СПОСОБ ПОЛУЧЕНИЯ ЖАРОПРОЧНЫХ СПЛАВОВ НА ОСНОВЕ ИНТЕРМЕТАЛЛИДА Nb3Al (Варианты)
Raynova Study on low-cost alternatives for synthesising powder metallurgy titanium and titanium alloys
JPH0688153A (ja) 焼結チタン合金の製造方法
Jia et al. Powder Consolidation of Titanium and Titanium Alloys by a Powder Compact Forging Process
Duz et al. Pressing and Sintering of Titanium Powders
El-Soudani Properties and Selection of Powder Metallurgy Titanium and Its Alloys
Zhao et al. Effect of Isothermal Forging on the Microstructure and Properties of Ti‐17 Titanium Alloy Prepared by Different Powder Compaction Methods

Legal Events

Date Code Title Description
AS Assignment

Owner name: TOHO TITANIUM CO., LTD., JAPAN

Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNORS:KANO, OSAMU;TAKATORI, HIDEO;SUGAWARA, SATOSHI;REEL/FRAME:029382/0466

Effective date: 20121026

STCB Information on status: application discontinuation

Free format text: ABANDONED -- FAILURE TO RESPOND TO AN OFFICE ACTION