EP1288328A1 - Method for surface hardening a Ti alloy - Google Patents

Method for surface hardening a Ti alloy Download PDF

Info

Publication number
EP1288328A1
EP1288328A1 EP02290753A EP02290753A EP1288328A1 EP 1288328 A1 EP1288328 A1 EP 1288328A1 EP 02290753 A EP02290753 A EP 02290753A EP 02290753 A EP02290753 A EP 02290753A EP 1288328 A1 EP1288328 A1 EP 1288328A1
Authority
EP
European Patent Office
Prior art keywords
alloy
atoms
wear
hardness
carried out
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.)
Withdrawn
Application number
EP02290753A
Other languages
German (de)
French (fr)
Inventor
Masahito Hirose
Hiroaki Asanuma
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.)
Fuji Oozx Inc
Original Assignee
Fuji Oozx Inc
Fuji Valve Co Ltd
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 Fuji Oozx Inc, Fuji Valve Co Ltd filed Critical Fuji Oozx Inc
Publication of EP1288328A1 publication Critical patent/EP1288328A1/en
Withdrawn legal-status Critical Current

Links

Images

Classifications

    • CCHEMISTRY; METALLURGY
    • C23COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23CCOATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C8/00Solid state diffusion of only non-metal elements into metallic material surfaces; Chemical surface treatment of metallic material by reaction of the surface with a reactive gas, leaving reaction products of surface material in the coating, e.g. conversion coatings, passivation of metals
    • C23C8/06Solid state diffusion of only non-metal elements into metallic material surfaces; Chemical surface treatment of metallic material by reaction of the surface with a reactive gas, leaving reaction products of surface material in the coating, e.g. conversion coatings, passivation of metals using gases
    • C23C8/28Solid state diffusion of only non-metal elements into metallic material surfaces; Chemical surface treatment of metallic material by reaction of the surface with a reactive gas, leaving reaction products of surface material in the coating, e.g. conversion coatings, passivation of metals using gases more than one element being applied in one step

Definitions

  • This invention relates to a method of strengthening Ti alloy to improve wear resistance.
  • poppet valves and other valve-operating parts are made of Ti alloy that provides high strength and low specific gravity. Poppet valves require wear resistance and scuff resistance at portion which is engaged with different valve-operating parts.
  • oxides are formed on the surface of Ti alloy in Japanese Patent Pub. No.62-256956.
  • Nitrides are formed on the surface in Japanese Patent Pub. No.61-81505.
  • Carburizing is carried out to diffuse carbon atoms into Ti alloy in Japanese Patent No.2,909,361.
  • Wear resistance and scuff resistance in the foregoing methods are improved in Ti alloy material, but the surface is so hard that different parts to be engaged are likely to be attacked.
  • Japanese Patent Application No.2001-25415 discloses a Ti alloy poppet valve in which Ti-O and Ti-C solid solutions are formed, and a method of manufacturing a Ti alloy poppet valve, comprising the steps of heating the Ti alloy valve at temperature lower than beta transformation point in a plasma vacuum finance which contains oxygen less than stoichiometric amount for forming Ti oxides to diffuse O and C atoms to form O and C diffusion layer which comprises Ti-O and Ti-C solid solutions to strengthen a valve body.
  • Oxygen/carbon diffusion layer thus obtained not only improves wear and scuff resistance, but also decreases attacking property to other members.
  • a method of strengthening Ti alloy comprising the step of heating the Ti alloy in an atmosphere of CO 2 at 600 to 900°C in a heating furnace to diffuse C and O atoms into the Ti alloy.
  • Ti alloys include alpha alloys such as Ti-5Al-2.5Sn; near-alpha alloys such as Ti-6Al-2Sn-4Zr-2Mo(hereinafter refer to "Ti6242") and Ti-8Al-Mo-V; alpha-beta alloys such as Ti-6Al-4V, Ti-6Al-6V-2Sn and Ti-6Al-2Sn-4Zr-6Mo; and beta alloys such as Ti-13V-11Cr-3Al and Ti-15Mo-5Zr-3Al.
  • Ti6242 may be preferably used.
  • Ti alloy is put in a heating furnace, and air in the furnace is purged by CO 2 . It is heated in an atmosphere of CO 2 at 600 to 900°C, preferably 800 to 850°C.
  • Feeding rate may be 0.5 to 3.0 l /min, preferably 1.0 to 2.5 l /min,
  • Time for treatment in CO 2 affects wear resistance or hardness, and may be preferably 1 to 3 hours.
  • O and C atoms are diffused at depth of 25 to 50 ⁇ m from the surface, and surface hardness is HV 550 to 1000.
  • a poppet valve in an internal combustion engine of an automobile is made of Ti alloy
  • suitable Vickers hardness is HV 700 to 850.
  • the valve treated by the method of the present Invention not only provides wear and scuff resistance, but also improves attacking property to the other member.
  • a poppet valve made of Ti6242 was put as sample and CO 2 was introduced to purge air. CO 2 was fed into the furnace at the flow rate of 1 1 /min and the sample was heated till 800°C and maintained at the temperature for two hours. Then, the valve was cooled to room temperature without contacting air. After cooling, the sample was taken out of the furnace and various tests were carried out.
  • Fig. 1 illustrates a micrograph of a section of the sample. As illustrated in the micrograph, O and C atoms were introduced at the depth.
  • Fig. 2 is a graph which shows averages of concentrations of O and C atoms measured at each depth by an electric-field-radiation-type Auger electronic spectrometer.
  • an axis of abscissa denotes depth ( ⁇ m) from the surface of the sample
  • an axis of ordinate denotes concentration (atomic %) of O and C atoms.
  • concentration "atomic %" means rate of O and C atoms with respect to analyzed total atoms.
  • the graph shows oxygen and carbon atoms in the diffusion layer of the sample.
  • X-ray diffraction in X-ray microdiffraction device identifies TiC, but does not find titanium oxide. From the result, oxygen atoms do not combine with titanium, but remain as atoms. Carbon atoms partially combine with titanium to form TiC, but the remaining is diffused as carbon atoms.
  • Section hardness of the sample thus obtained was measured by a Micro-Vickers hardness tester of Shimazu Corp.
  • Fig. 3 shows distribution of hardness.
  • An axis of abscissa means depth ( ⁇ m) from the surface, and an axis of ordinate means hardness (HV) under 100gf. It shows improvement in hardness up to depth of 50 ⁇ m according to the method of the present invention.
  • Figs. 2 and 3 prove that existence of oxygen and carbon atoms contributes improvement in hardness of Ti alloy.
  • Ti6242 was heated at 710 to 850°C for 0.5 to 50 hours, so that O and C atoms were introduced into Ti alloy without forming oxide.
  • Fig. 4 illustrates a microgragh of a Ti alloy poppet valve treated in the Example 3, and O and C diffusion layer was formed.
  • a poppet valve is used in an internal combustion engine of an automobile and is subjected to severe condition such as high temperature. Such a valve requires hardness of HV 700 to 850. In Examples 1, 5 and 6, a sample requires to be subject to the conditions of time for 1 to 2 hours at 800°C.
  • the temperature 850°C was the same as those in Examples 8 and 9, but it took 55 hours to attain HV 1030. But it was so long that an oxide layer was formed on the surface. Deformation is large and it is not suitable.
  • Fig. 5 shows a micrograph of a poppet valve in Comparative Example 2, in which an oxide layer was formed on an O and C diffusion layer.
  • Fig. 6 illustrates results of wear tests of Ti6242 in Examples 1 and 3, Comparative Example 2, untreated Ti alloy and tuftriding-treated heat-resistant steel.
  • a test piece 2 is engaged in a valve guide 1 made of Fe-sintered material.
  • Vertical weight "W” for 6kgf was loaded and the test piece 2 was reciprocally slid for 50 hours while lubricating oil was supplied between them.
  • Example 1 is equivalent to the heat-resistant steel in wear. Owing to difference in surface hardness, Example 3 is larger than Example 1 in wear.
  • the minimum wear in Comparative Example 2 seems to be due to an oxide layer on the surface. Comparative Example 2 was too rigid, so that wear of the valve guide 1 engaged therewith was the maximum.

Abstract

Ti alloy is heated in an atmosphere of CO2 in a heating furnace. O and C atoms are introduced into the Ti alloy to harden it without forming Ti oxide, thereby increasing hardness by Ti-O and Ti-C solid solutions thus formed.

Description

    BACKGROUND OF THE INVENTION
  • This invention relates to a method of strengthening Ti alloy to improve wear resistance.
  • In automobile industries, poppet valves and other valve-operating parts are made of Ti alloy that provides high strength and low specific gravity. Poppet valves require wear resistance and scuff resistance at portion which is engaged with different valve-operating parts.
  • In order to strengthen Ti alloy material to provide wear resistance and scuff resistance, various methods have been developed. For example, oxides are formed on the surface of Ti alloy in Japanese Patent Pub. No.62-256956. Nitrides are formed on the surface in Japanese Patent Pub. No.61-81505. Carburizing is carried out to diffuse carbon atoms into Ti alloy in Japanese Patent No.2,909,361.
  • Wear resistance and scuff resistance in the foregoing methods are improved in Ti alloy material, but the surface is so hard that different parts to be engaged are likely to be attacked.
  • Japanese Patent Application No.2001-25415 discloses a Ti alloy poppet valve in which Ti-O and Ti-C solid solutions are formed, and a method of manufacturing a Ti alloy poppet valve, comprising the steps of heating the Ti alloy valve at temperature lower than beta transformation point in a plasma vacuum finance which contains oxygen less than stoichiometric amount for forming Ti oxides to diffuse O and C atoms to form O and C diffusion layer which comprises Ti-O and Ti-C solid solutions to strengthen a valve body.
  • To diffuse O and C atoms, in the presence of O2 less than stoichiometric amount for forming titanium oxides, heat treatment is carried out at about 800°C. Glow discharge is made in the presence of a gas for ionized carburizing, or plasma carburizing is carried out while oxygen less than stoichiometric amount for forming titanium oxide is supplied. Oxygen/carbon diffusion layer thus obtained not only improves wear and scuff resistance, but also decreases attacking property to other members.
  • However, as mentioned above, heat treatment is carried out in the presence of oxygen in a plasma vacuum finance and ionizing carburizing is carried out by glow discharge, which is complicate. Furthermore, it is necessary to employ a vacuum discharge device and plasma power source in a plasma vacuum finance to increase cost.
  • SUMMARY OF THE INVENTION
  • In view of the disadvantages in the prior art, it is an object of the present invention to provide a method of strengthening Ti alloy to diffuse oxygen and carbon atoms without forming titanium oxide.
  • According to the present invention, there is provided a method of strengthening Ti alloy, comprising the step of heating the Ti alloy in an atmosphere of CO2 at 600 to 900°C in a heating furnace to diffuse C and O atoms into the Ti alloy.
  • BRIEF DESRIPTION OF THE DRAWINGS
  • The features and advantages of the present invention will become more apparent from the following description with respect to appended drawings wherein:
  • Fig. 1 is a micrograph of Ti alloy treated by Example 1 of the present invention;
  • Fig. 2 is a graph that shows oxygen and carbon atom concentration of the Ti alloy material in Fig. 1;
  • Fig. 3 is a graph of hardness to depth of Ti alloy material in Fig. 1;
  • Fig. 4 is a micrograph of Ti alloy treated in Example 3 of the present invention;
  • Fig. 5 is a micrograph of Ti alloy treated in Comparative Example 2;
  • Fig. 6 is a graph of the results of wear test to Ti alloy materials; and
  • Fig. 7 is a schematic view of a device for the wear test.
  • DETAILED DESCRIPTION OF PREFERRED EMBODIMENTS
  • Heat treatment of the present invention will be described as below.
  • Ti alloys include alpha alloys such as Ti-5Al-2.5Sn; near-alpha alloys such as Ti-6Al-2Sn-4Zr-2Mo(hereinafter refer to "Ti6242") and Ti-8Al-Mo-V; alpha-beta alloys such as Ti-6Al-4V, Ti-6Al-6V-2Sn and Ti-6Al-2Sn-4Zr-6Mo; and beta alloys such as Ti-13V-11Cr-3Al and Ti-15Mo-5Zr-3Al. Ti6242 may be preferably used.
  • In heat treatment, Ti alloy is put in a heating furnace, and air in the furnace is purged by CO2. It is heated in an atmosphere of CO2 at 600 to 900°C, preferably 800 to 850°C.
  • Below 600°C, diffusion speed of carbon atoms is too slow, which is disadvantageous in cost. Above 900°C, oxide layer is formed and the temperature exceeds beta transformation point of Ti to change its configuration, which is not preferable.
  • In heat treatment, to supplement CO2 consumed by introduction of C and O into Ti alloy and to maintain CO2 atmosphere in the furnace, CO2 may be always fed into the heating furnace. Feeding rate may be 0.5 to 3.0 l /min, preferably 1.0 to 2.5 l /min,
  • Time for treatment in CO2 affects wear resistance or hardness, and may be preferably 1 to 3 hours. By the heat treatment, O and C atoms are diffused at depth of 25 to 50µ m from the surface, and surface hardness is HV 550 to 1000.
  • When a poppet valve in an internal combustion engine of an automobile is made of Ti alloy, suitable Vickers hardness is HV 700 to 850. The valve treated by the method of the present Invention not only provides wear and scuff resistance, but also improves attacking property to the other member.
  • Example 1
  • In a muffle furnace which has volume of 24 1, a poppet valve made of Ti6242 was put as sample and CO2 was introduced to purge air. CO2 was fed into the furnace at the flow rate of 1 1 /min and the sample was heated till 800°C and maintained at the temperature for two hours. Then, the valve was cooled to room temperature without contacting air. After cooling, the sample was taken out of the furnace and various tests were carried out.
  • Fig. 1 illustrates a micrograph of a section of the sample. As illustrated in the micrograph, O and C atoms were introduced at the depth.
  • Fig. 2 is a graph which shows averages of concentrations of O and C atoms measured at each depth by an electric-field-radiation-type Auger electronic spectrometer. In the graph, an axis of abscissa denotes depth (µ m) from the surface of the sample, and an axis of ordinate denotes concentration (atomic %) of O and C atoms. The unit of concentration "atomic %" means rate of O and C atoms with respect to analyzed total atoms. The graph shows oxygen and carbon atoms in the diffusion layer of the sample.
  • X-ray diffraction in X-ray microdiffraction device identifies TiC, but does not find titanium oxide. From the result, oxygen atoms do not combine with titanium, but remain as atoms. Carbon atoms partially combine with titanium to form TiC, but the remaining is diffused as carbon atoms.
  • Section hardness of the sample thus obtained was measured by a Micro-Vickers hardness tester of Shimazu Corp. Fig. 3 shows distribution of hardness. An axis of abscissa means depth (µ m) from the surface, and an axis of ordinate means hardness (HV) under 100gf. It shows improvement in hardness up to depth of 50 µm according to the method of the present invention.
  • Figs. 2 and 3 prove that existence of oxygen and carbon atoms contributes improvement in hardness of Ti alloy.
  • As shown in Fig. 3, surface hardness was HV 830.
  • Examples 2 to 9 and Comparative Examples 1 to 3
  • Surface treatment was carried out under different temperatures and time with respect to Ti6242, and the following Table shows the results.
    Temperature
    (°C)
    Time
    (h)
    Surface
    Hardness
    (HV)
    Oxide
    Layer
    Example 2 750 3 570 none
    3 800 0.5 630 none
    4 710 50 680 none
    5 800 1 710 none
    6 800 1.5 790 none
    7 800 3 870 none
    8 850 1 930 none
    9 850 2 960 none
    Comparative
    Example 1
    850 55 1030 formed
    2 900 1 980 formed
    3 1000 0.5 1030 formed
  • In an atmosphere of CO2, Ti6242 was heated at 710 to 850°C for 0.5 to 50 hours, so that O and C atoms were introduced into Ti alloy without forming oxide.
  • Fig. 4 illustrates a microgragh of a Ti alloy poppet valve treated in the Example 3, and O and C diffusion layer was formed.
  • A poppet valve is used in an internal combustion engine of an automobile and is subjected to severe condition such as high temperature. Such a valve requires hardness of HV 700 to 850. In Examples 1, 5 and 6, a sample requires to be subject to the conditions of time for 1 to 2 hours at 800°C.
  • As clarified in Comparative Example 1, the temperature 850°C was the same as those in Examples 8 and 9, but it took 55 hours to attain HV 1030. But it was so long that an oxide layer was formed on the surface. Deformation is large and it is not suitable.
  • In Comparative Examples 2 and 3, when the temperature was over 900°C, surface hardness was sufficient, but a thick oxide layer was formed to cause large deformation, which was not suitable for actual use.
  • Fig. 5 shows a micrograph of a poppet valve in Comparative Example 2, in which an oxide layer was formed on an O and C diffusion layer.
  • Fig. 6 illustrates results of wear tests of Ti6242 in Examples 1 and 3, Comparative Example 2, untreated Ti alloy and tuftriding-treated heat-resistant steel.
  • To carry out the test, as shown in Fig. 7, a test piece 2 is engaged in a valve guide 1 made of Fe-sintered material. Vertical weight "W" for 6kgf was loaded and the test piece 2 was reciprocally slid for 50 hours while lubricating oil was supplied between them.
  • The test piece made of untreated Ti6242 was the maximum in wear, and wear becomes smaller in order of Example 3, Example 1, heat-resistant steel and Comparative Example 2. Example 1 is equivalent to the heat-resistant steel in wear. Owing to difference in surface hardness, Example 3 is larger than Example 1 in wear. The minimum wear in Comparative Example 2 seems to be due to an oxide layer on the surface. Comparative Example 2 was too rigid, so that wear of the valve guide 1 engaged therewith was the maximum.

Claims (7)

  1. A method of strengthening Ti alloy, comprising the step of:
    heating the Ti alloy in an atmosphere of CO2 at 600 to 900°C in a heating furnace to diffuse C and O atoms into the Ti alloy.
  2. A method as claimed in claim 1 wherein the method is carried out for 0.5 to 50 hours.
  3. A method as claimed in claim 1 wherein the method is carried out at 800 to 850°C.
  4. A method as claimed in claim 3 wherein the method is carried out for 1 to 3 hours.
  5. A method as claimed in claim 1 wherein CO2 is always introduced into the heating furnace.
  6. A method as claimed in claim 1 wherein the method is carried out at about 800°C for 1 to 2 hours.
  7. A method as claimed in claim 6 wherein the Ti alloy is used to make a poppet valve in an internal combustion engine.
EP02290753A 2001-09-03 2002-03-27 Method for surface hardening a Ti alloy Withdrawn EP1288328A1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
JP2001265462 2001-09-03
JP2001265462A JP2003073799A (en) 2001-09-03 2001-09-03 Surface treatment method for titanium-based material

Publications (1)

Publication Number Publication Date
EP1288328A1 true EP1288328A1 (en) 2003-03-05

Family

ID=19091920

Family Applications (1)

Application Number Title Priority Date Filing Date
EP02290753A Withdrawn EP1288328A1 (en) 2001-09-03 2002-03-27 Method for surface hardening a Ti alloy

Country Status (5)

Country Link
US (1) US20030041922A1 (en)
EP (1) EP1288328A1 (en)
JP (1) JP2003073799A (en)
KR (1) KR20030020228A (en)
CN (1) CN1407127A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2005075698A1 (en) * 2004-02-03 2005-08-18 Exxonmobil Research And Engineering Company Metal dusting resistant stable-carbide forming alloy surfaces
CN106337161A (en) * 2016-12-01 2017-01-18 西北有色金属研究院 Method for plasma oxygen-carbon co-permeation of titanium-based or zirconium-based metal surface

Families Citing this family (43)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
ATE503856T1 (en) 2003-12-09 2011-04-15 Central Res Inst Elect MULTIFUNCTIONAL MATERIAL WITH A LAYER OF CARBON-DOPED TITANIUM OXIDE
US7524791B2 (en) * 2003-12-09 2009-04-28 Central Research Institute Of Electric Power Industry Method for producing substrate having carbon-doped titanium oxide layer
US20050211475A1 (en) 2004-04-28 2005-09-29 Mirchandani Prakash K Earth-boring bits
US20080101977A1 (en) * 2005-04-28 2008-05-01 Eason Jimmy W Sintered bodies for earth-boring rotary drill bits and methods of forming the same
US9428822B2 (en) 2004-04-28 2016-08-30 Baker Hughes Incorporated Earth-boring tools and components thereof including material having hard phase in a metallic binder, and metallic binder compositions for use in forming such tools and components
US7513320B2 (en) * 2004-12-16 2009-04-07 Tdy Industries, Inc. Cemented carbide inserts for earth-boring bits
JP5041392B2 (en) * 2005-02-28 2012-10-03 一般財団法人電力中央研究所 Oil treatment equipment
JP4534144B2 (en) * 2005-02-28 2010-09-01 財団法人電力中央研究所 Purification device
JP4692987B2 (en) * 2005-02-28 2011-06-01 財団法人電力中央研究所 Antiseptic equipment
JP4814535B2 (en) * 2005-02-28 2011-11-16 財団法人電力中央研究所 Manufacturing method of steel products
JP4915634B2 (en) * 2005-02-28 2012-04-11 財団法人電力中央研究所 Antifouling buildings
JP4807723B2 (en) * 2005-02-28 2011-11-02 財団法人電力中央研究所 Manufacturing method of heat-resistant member
JP4814536B2 (en) * 2005-02-28 2011-11-16 財団法人電力中央研究所 Manufacturing method of non-ferrous metal products
JP4807722B2 (en) * 2005-02-28 2011-11-02 財団法人電力中央研究所 Manufacturing method for environmentally resistant equipment
JP4814534B2 (en) * 2005-02-28 2011-11-16 財団法人電力中央研究所 Manufacturing method of structural materials
JP4597713B2 (en) * 2005-02-28 2010-12-15 財団法人電力中央研究所 Metal container
JP4807725B2 (en) * 2005-02-28 2011-11-02 財団法人電力中央研究所 Manufacturing method of energy generating equipment
JP4807724B2 (en) * 2005-02-28 2011-11-02 財団法人電力中央研究所 Rail vehicle manufacturing method
JP4756575B2 (en) * 2005-02-28 2011-08-24 財団法人電力中央研究所 Cultivation medium container
US8637127B2 (en) 2005-06-27 2014-01-28 Kennametal Inc. Composite article with coolant channels and tool fabrication method
US7687156B2 (en) 2005-08-18 2010-03-30 Tdy Industries, Inc. Composite cutting inserts and methods of making the same
US7784567B2 (en) * 2005-11-10 2010-08-31 Baker Hughes Incorporated Earth-boring rotary drill bits including bit bodies comprising reinforced titanium or titanium-based alloy matrix materials, and methods for forming such bits
US8312941B2 (en) 2006-04-27 2012-11-20 TDY Industries, LLC Modular fixed cutter earth-boring bits, modular fixed cutter earth-boring bit bodies, and related methods
US8007922B2 (en) 2006-10-25 2011-08-30 Tdy Industries, Inc Articles having improved resistance to thermal cracking
US8512882B2 (en) * 2007-02-19 2013-08-20 TDY Industries, LLC Carbide cutting insert
US7846551B2 (en) 2007-03-16 2010-12-07 Tdy Industries, Inc. Composite articles
CN102112642B (en) * 2008-06-02 2013-11-06 Tdy工业有限责任公司 Cemented carbide-metallic alloy composites
US8790439B2 (en) 2008-06-02 2014-07-29 Kennametal Inc. Composite sintered powder metal articles
US8322465B2 (en) 2008-08-22 2012-12-04 TDY Industries, LLC Earth-boring bit parts including hybrid cemented carbides and methods of making the same
US8025112B2 (en) 2008-08-22 2011-09-27 Tdy Industries, Inc. Earth-boring bits and other parts including cemented carbide
US8272816B2 (en) 2009-05-12 2012-09-25 TDY Industries, LLC Composite cemented carbide rotary cutting tools and rotary cutting tool blanks
US8201610B2 (en) 2009-06-05 2012-06-19 Baker Hughes Incorporated Methods for manufacturing downhole tools and downhole tool parts
US8308096B2 (en) 2009-07-14 2012-11-13 TDY Industries, LLC Reinforced roll and method of making same
US8440314B2 (en) * 2009-08-25 2013-05-14 TDY Industries, LLC Coated cutting tools having a platinum group metal concentration gradient and related processes
US9643236B2 (en) 2009-11-11 2017-05-09 Landis Solutions Llc Thread rolling die and method of making same
WO2011146760A2 (en) 2010-05-20 2011-11-24 Baker Hughes Incorporated Methods of forming at least a portion of earth-boring tools, and articles formed by such methods
CA2799906A1 (en) 2010-05-20 2011-11-24 Baker Hughes Incorporated Methods of forming at least a portion of earth-boring tools, and articles formed by such methods
US8490674B2 (en) 2010-05-20 2013-07-23 Baker Hughes Incorporated Methods of forming at least a portion of earth-boring tools
US8800848B2 (en) 2011-08-31 2014-08-12 Kennametal Inc. Methods of forming wear resistant layers on metallic surfaces
US9016406B2 (en) 2011-09-22 2015-04-28 Kennametal Inc. Cutting inserts for earth-boring bits
CN102703852B (en) * 2012-06-15 2014-03-12 西北有色金属研究院 Method for composite hydrogen-free oxygen-carburizing on surface of two-phase titanium alloy
WO2021037757A1 (en) 2019-08-23 2021-03-04 Danmarks Tekniske Universitet Low temperature titanium hardening
CN114174550A (en) * 2019-08-23 2022-03-11 医乐世医疗技术皮诺公司 Hardfacing for dental implants

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH0797676A (en) * 1993-09-30 1995-04-11 Nkk Corp Surface treating method of titanium-made bolt or nut
JPH08104970A (en) * 1994-10-04 1996-04-23 Nkk Corp Method of surface hardening treatment for titanium material
US6131603A (en) * 1999-08-10 2000-10-17 Fuji Oozx Inc. Ti alloy poppet valve and surface treatment thereof

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3773258D1 (en) * 1986-05-18 1991-10-31 Daido Steel Co Ltd WEAR-RESISTANT ITEMS MADE OF TITANIUM OR TITANIUM ALLOY.

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH0797676A (en) * 1993-09-30 1995-04-11 Nkk Corp Surface treating method of titanium-made bolt or nut
JPH08104970A (en) * 1994-10-04 1996-04-23 Nkk Corp Method of surface hardening treatment for titanium material
US6131603A (en) * 1999-08-10 2000-10-17 Fuji Oozx Inc. Ti alloy poppet valve and surface treatment thereof

Non-Patent Citations (2)

* Cited by examiner, † Cited by third party
Title
PATENT ABSTRACTS OF JAPAN vol. 1995, no. 07 31 August 1995 (1995-08-31) *
PATENT ABSTRACTS OF JAPAN vol. 1996, no. 08 30 August 1996 (1996-08-30) *

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2005075698A1 (en) * 2004-02-03 2005-08-18 Exxonmobil Research And Engineering Company Metal dusting resistant stable-carbide forming alloy surfaces
US7422804B2 (en) 2004-02-03 2008-09-09 Exxonmobil Research And Engineering Company Metal dusting resistant stable-carbide forming alloy surfaces
CN106337161A (en) * 2016-12-01 2017-01-18 西北有色金属研究院 Method for plasma oxygen-carbon co-permeation of titanium-based or zirconium-based metal surface

Also Published As

Publication number Publication date
JP2003073799A (en) 2003-03-12
KR20030020228A (en) 2003-03-08
US20030041922A1 (en) 2003-03-06
CN1407127A (en) 2003-04-02

Similar Documents

Publication Publication Date Title
EP1288328A1 (en) Method for surface hardening a Ti alloy
EP1174593B1 (en) TI alloy poppet valve and a method of manufactoring the same
EP0925381B1 (en) Surface oxidation of a titanium or titanium alloy article
US5051140A (en) Surface treatment method for titanium or titanium alloy
US6592683B2 (en) Ti alloy surface treatment
EP1712658B1 (en) Method for surface treatment of metal material
KR20010020087A (en) Ti alloy poppet valve and surface treatment thereof
WO2019131602A1 (en) Nitrided steel member, and method and apparatus for producing nitrided steel member
EP2154263A1 (en) Case hardening titanium and its alloys
US20060099435A1 (en) Method of case hardening titanium and zirconium alloys
JP2773092B2 (en) Surface coated steel products
JP2007197822A (en) Method for nitriding metal and vane member
EP1849882A1 (en) Method of surface treatment for titanium alloy member of aerospace instrument
WO2020090999A1 (en) Nitrided steel member, and method and apparatus for producing nitrided steel member
KR100302484B1 (en) Bushless locker arm assembly for vehicle and method for manufacturing the same
JPH09256821A (en) Engine valve
JPH05295515A (en) Surface treatment of valve spring retainer made of titanium alloy
KR20220144824A (en) Sliding elements, in particular piston rings, and methods for manufacturing them
Ferguson et al. Integral Preoxidation of Aerospace Gear Steel
JPH03223457A (en) Sulfurization nitriding method by ion implantation
Epler New Duplex Surface Treatment Dramatically Improves Die Life, Part Quality & Cost Savings
KR20080054830A (en) Method for nitrocarburizing heat treatment
JPH06167206A (en) Valve and valve seat assembly
JPH06264706A (en) Manufacture of titanium alloy valve

Legal Events

Date Code Title Description
PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

Free format text: ORIGINAL CODE: 0009012

AK Designated contracting states

Kind code of ref document: A1

Designated state(s): AT BE CH CY DE DK ES FI FR GB GR IE IT LI LU MC NL PT SE TR

Designated state(s): AT BE CH CY DE DK ES FI FR GB GR IE IT LI LU MC NL PT SE TR

AX Request for extension of the european patent

Extension state: AL LT LV MK RO SI

17P Request for examination filed

Effective date: 20030521

17Q First examination report despatched

Effective date: 20030724

AKX Designation fees paid

Designated state(s): DE GB

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: THE APPLICATION IS DEEMED TO BE WITHDRAWN

18D Application deemed to be withdrawn

Effective date: 20031204