WO1997014820A1 - Method of treating titanium parts - Google Patents

Method of treating titanium parts Download PDF

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Publication number
WO1997014820A1
WO1997014820A1 PCT/US1996/016714 US9616714W WO9714820A1 WO 1997014820 A1 WO1997014820 A1 WO 1997014820A1 US 9616714 W US9616714 W US 9616714W WO 9714820 A1 WO9714820 A1 WO 9714820A1
Authority
WO
WIPO (PCT)
Prior art keywords
titanium
parts
furnace
nitrogen
atmosphere
Prior art date
Application number
PCT/US1996/016714
Other languages
French (fr)
Inventor
Douglas W. Fay, Sr.
Original Assignee
Sturm, Ruger & Company, 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 Sturm, Ruger & Company, Inc. filed Critical Sturm, Ruger & Company, Inc.
Publication of WO1997014820A1 publication Critical patent/WO1997014820A1/en

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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

  • the present invention comprises a method of treating titanium-containing parts having the steps of creating in a furnace at atmospheric pressure mixture of nitrogen, methanol and optionally natural gas or propane, causing such mixture to obtain an equilibrium; then introducing the titanium parts into the furnace and finally reducing the furnace temperature to a range of 1450°F. to 1850F° for a time period of between five (5) and three hundred (300) minutes.
  • the temperature range selected should yield a two phase structure balanced between alpha and beta phases.
  • the surface area of the titanium parts so treated are very hard and gall resistant. It is a feature that a coating caused to form on and at the alloy surface during treatment consists predominantly of titanium oxides with regions of oxynitrides and at times some carbonitrides.
  • the surface treatment results in a complex coating which imparts a smooth and relatively hard gall-resistant surface with an appealing blue-back coloration.
  • This coating consists of a variety of oxides, oxynitrides and carbonitrides not to exclude other possible forms of carbon based surface modification constituents with graphite and/or a reduced frictional surface polymer material such as Teflon-like hydrocarbon polymer.
  • Fig. 1 is a partially sectioned elevational view of the apparatus used to carry out the present inventive method.
  • apparatus 10 includes furnace 11, furnace chamber box 12 and titanium parts basket 14 supported by blocks 15.
  • Chamber 12 has three gaseous conduit inlets 16, 17, and 18.
  • Conduit 16 supplies methanol from methanol tank 21 to sparger 22 with shaft.
  • Conduit 17 supplies natural gas from gas tank 23 and conduit 18 supplies nitrogen from nitrogen tank 24.
  • Fan 27 with shaft provides for mixing and circulation of gases in chamber 12 and exhaust chimney 29 (not shown) conducts exhaust gases from chamber 12.
  • Pressure in furnace 11 is atmospheric or slightly above atmospheric.
  • Sensor 37 measures the temperature, oxygen and gas components in chamber 12.
  • Process monitoring unit 31 controls valves 33, 34, 35 in conduits 16, 17, and 18 respectively to control the mixture in chamber 12.
  • the combination of the gases in chamber box 12 creates a hydrocarbon inert gas mixture which is varied to achieve the metallurgical layer characteristics of the parts desired and is composed of an atmosphere of carbon monoxide between 15- 25%, hydrogen between 30-50% and nitrogen between 30-50% using, as supply, gaseous nitrogen, methanol, and propane or natural gas. Gaseous percentages are by volume.
  • Process control equipment 'employed may include but is not limited to oxygen measuring and control. Atmosphere characterization equipment may be used but is not necessary.
  • the titanium parts are transferred to a vacuum furnace at a temperature in the range of 1200°F-1450°F for 30 to 300 minutes. This subsequent step reduces the hydrogen level in the parts to improve yield strength.
  • the vacuum furnace is at a vacuum of between 10 to 500 micrometers of pressure. One atmosphere of pressure equals 760,000 micrometers.
  • Parts which are treatable using the present invention are 100% titanium or alloys of titanium including:
  • Percentages of the alloys are by weight. Tests run on cast Ti-6AL-4V alloys treated by the present invention and untreated produced the following results:
  • Tensile ductility is measured by the percent of elongation or the percent change in cross-sectional area of the tensile specimen when the specimen is tested to failure in a conventional tensile testing situation.
  • the titanium portion be an alpha-beta composition in which a significant percentage of both alpha and beta crystalline structure phases coexist.
  • the alpha plus beta region of the phase diagram is a solid phase.
  • the reaction taking place in the furnace is solid state diffusion of the furnace atmosphere including nitrogen.
  • Example A batch of firearm triggers made of Alloy A were placed in a furnace in which nitrogen, methanol and natural gas are introduced in proportions of nitrogen: 40% (gas) ; methanol: 58-60% (liquid) ; and propane: 0-2% (gas) to create in the furnace a gaseous atmosphere of:
  • the gaseous atmosphere was at or near atmospheric pressure.
  • the treatment atmosphere is a complex mixture of: nitrogen
  • a principle of control of the process is controlling the proportions of gases flowing into the furnace.

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  • Chemical & Material Sciences (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Solid-Phase Diffusion Into Metallic Material Surfaces (AREA)

Abstract

A method of treating titanium-containing parts and the parts so-treated, which treatment includes placing the parts in a furnace chamber (12) having a gaseous atmosphere of 15-25 % carbon monoxide, 30-50 % nitrogen and 30-50 % hydrogen, are disclosed, The atmosphere is at a temperature of between 1450-1850 °F and the treatment lasts for 5-300 minutes. Parts experience improved hardness, strength and wear resistance.

Description

METHOD OF TREATING TITANIUM PARTS
Background Of The Invention
It has been proposed to heat treat metals in hydrogen and nitrogen atmospheres (U.S. Patent No. 3,211,590) or in an ammonia and methane atmosphere (U.S. Patent No. 3,891,473). The treatment of titanium in a neutral atmosphere of helium has also been suggested (U.S. Patent No. 4,098,623).
No prior method has included titanium parts treatment in an atmosphere of nitrogen, hydrogen and carbon monoxide.
Low carbon steels and iron have been treated in atmospheres of 20% carbon monoxide, 40% hydrogen, and 40% nitrogen and gas. Treatment of titanium alloy specimens using propane-argon mixtures or methane-argon mixtures has been reported for improving resistance to galling fTransactions of the ASM Vol. 46, pp. 257, 267-70 (1953).
Summary Of The Invention
Broadly, the present invention comprises a method of treating titanium-containing parts having the steps of creating in a furnace at atmospheric pressure mixture of nitrogen, methanol and optionally natural gas or propane, causing such mixture to obtain an equilibrium; then introducing the titanium parts into the furnace and finally reducing the furnace temperature to a range of 1450°F. to 1850F° for a time period of between five (5) and three hundred (300) minutes. The temperature range selected should yield a two phase structure balanced between alpha and beta phases.
It is a feature of the method that the surface area of the titanium parts so treated are very hard and gall resistant. It is a feature that a coating caused to form on and at the alloy surface during treatment consists predominantly of titanium oxides with regions of oxynitrides and at times some carbonitrides.
It is a feature that the surface treatment results in a complex coating which imparts a smooth and relatively hard gall-resistant surface with an appealing blue-back coloration. This coating consists of a variety of oxides, oxynitrides and carbonitrides not to exclude other possible forms of carbon based surface modification constituents with graphite and/or a reduced frictional surface polymer material such as Teflon-like hydrocarbon polymer.
Related Applications
This application is a continuation-in-part of U. S. Patent Application Serial No. 08/436,686 filed May 8, 1995 which in turn was a continuation application of U.S. Patent Application Serial No. 08/232,890 filed April 25, 1994.
Brief Description Of The Drawings
Fig. 1 is a partially sectioned elevational view of the apparatus used to carry out the present inventive method.
Description Of The Preferred Embodiment
In Fig. 1, apparatus 10 includes furnace 11, furnace chamber box 12 and titanium parts basket 14 supported by blocks 15. Chamber 12 has three gaseous conduit inlets 16, 17, and 18. Conduit 16 supplies methanol from methanol tank 21 to sparger 22 with shaft. Conduit 17 supplies natural gas from gas tank 23 and conduit 18 supplies nitrogen from nitrogen tank 24. Fan 27 with shaft provides for mixing and circulation of gases in chamber 12 and exhaust chimney 29 (not shown) conducts exhaust gases from chamber 12. Pressure in furnace 11 is atmospheric or slightly above atmospheric. Sensor 37 measures the temperature, oxygen and gas components in chamber 12. Process monitoring unit 31 controls valves 33, 34, 35 in conduits 16, 17, and 18 respectively to control the mixture in chamber 12.
The combination of the gases in chamber box 12 creates a hydrocarbon inert gas mixture which is varied to achieve the metallurgical layer characteristics of the parts desired and is composed of an atmosphere of carbon monoxide between 15- 25%, hydrogen between 30-50% and nitrogen between 30-50% using, as supply, gaseous nitrogen, methanol, and propane or natural gas. Gaseous percentages are by volume. Process control equipment 'employed may include but is not limited to oxygen measuring and control. Atmosphere characterization equipment may be used but is not necessary.
After completion of the treatment in furnace 11, the titanium parts are transferred to a vacuum furnace at a temperature in the range of 1200°F-1450°F for 30 to 300 minutes. This subsequent step reduces the hydrogen level in the parts to improve yield strength. The vacuum furnace is at a vacuum of between 10 to 500 micrometers of pressure. One atmosphere of pressure equals 760,000 micrometers.
Parts which are treatable using the present invention are 100% titanium or alloys of titanium including:
Alloy A Component Percent
Titanium 90
Aluminum 6
Vanadium 4
Alloy B
Component Percent Titanium 94.5 Aluminum 3 Vanadium 2.5 Alloy C
Component Percent
Titanium 82
Zirconium 4
Tin 2
Molybdenum 6
Aluminum 6
Percentages of the alloys are by weight. Tests run on cast Ti-6AL-4V alloys treated by the present invention and untreated produced the following results:
1. Mechanical Properties
Surface Tensile Strength Condition Hardness . Hk25 UTS KSI YS,KSl %EL
Untreated 350 - 380 132.7 114.3 10.2
Treated 980 - 1300 137.2 121.7 12.2
The surface hardness of treated samples was significantly higher than that of the untreated samples with the balance of properties essentially similar. Tensile ductility is measured by the percent of elongation or the percent change in cross-sectional area of the tensile specimen when the specimen is tested to failure in a conventional tensile testing situation.
2. Wear Resistance
Abrasive testing using a #10 grit aluminum oxide media indicated the treated samples wore less than untreated samples.
Condition % Wear
Treated .3774
Untreated .4533 When 100% titanium or titanium alloys are used, it is preferred that the titanium portion be an alpha-beta composition in which a significant percentage of both alpha and beta crystalline structure phases coexist. The alpha plus beta region of the phase diagram is a solid phase. The reaction taking place in the furnace is solid state diffusion of the furnace atmosphere including nitrogen.
Example A batch of firearm triggers made of Alloy A were placed in a furnace in which nitrogen, methanol and natural gas are introduced in proportions of nitrogen: 40% (gas) ; methanol: 58-60% (liquid) ; and propane: 0-2% (gas) to create in the furnace a gaseous atmosphere of:
Constituent Percent Carbon monoxide 15-25 Hydrogen 30-50
Nitrogen 30-50
The gaseous atmosphere was at or near atmospheric pressure. The treatment atmosphere is a complex mixture of: nitrogen
C02 CO hydrogen oxygen methane and water. This mixture should exist in equilibrium in the furnace. Methane dissociates to form hydrogen and carbon dioxide and carbon monoxide to accomplish the parts treatment including carburizing of the parts surfaces. Equilibrium is obtained upon completion of reactions of the mixture in the furnace. An equilibrium reaction equation is 2N2+CH3OH *=► 2N2+2H2+CO. Equilibrium determination is accomplished by indirect means such as the analysis of the implanted or diffused carbon level in the material surface treated. Other methods include the measurement of the carbon potential by the oxygen probe located in the furnace which indicates the carbon potential by an algorithm assuming a consistent level of CO gas in the furnace atmosphere. Carbon potential is largely equivalent to a function of the oxygen content assuming a constant CO content. If the CO content changes, the same oxygen % will yield a different carbon potential. Again, an algorithm is used to put all the variables in perspective. The control of carbon by maintaining a consistent atmosphere and then using oxygen % as a control parameter is very important.
A principle of control of the process is controlling the proportions of gases flowing into the furnace.

Claims

I CLAIM :
1. A method for treating titanium-containing parts comprising 1) introducing into the furnace box a mixture of component gases in turn comprising a) 30-50% nitrogen; b) 30-50% hydrogen; and c) 15-25% carbon oxygen compound 2) introducing titanium parts into a furnace box having air therein;
3) sealing the box from the outside atmosphere; and
4) monitoring and controlling the temperature in the box at between 1450F0 and 1850F0.
2. The method of claim 1 in which the carbon oxygen compound is carbon monoxide.
3. The method of claim 1 in which the titanium- containing parts include a significant percentage of both alpha and beta crystalline structure phases.
4. The method of claim 1 in which the introduction of component gases is controlled so that the furnace atmosphere comprises by volume: i) 30-50% nitrogen; ii) 30-50% hydrogen; and iii) 15-25% carbon monoxide.
5. The method of claim 1 in which the titanium parts are treated in a vacuum chamber following treatment in the furnace at temperatures of 1200°F-1450°F for thirty (30) to three hundred (300) minutes.
6. A titanium-containing part treated by the method of claim 1.
PCT/US1996/016714 1995-10-18 1996-10-17 Method of treating titanium parts WO1997014820A1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US54452095A 1995-10-18 1995-10-18
US544,520 1995-10-18

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Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2154263A1 (en) * 2008-07-25 2010-02-17 The BOC Group Limited Case hardening titanium and its alloys
WO2017207794A1 (en) * 2016-06-02 2017-12-07 Danmarks Tekniske Universitet A case hardened component of titanium
WO2021037757A1 (en) 2019-08-23 2021-03-04 Danmarks Tekniske Universitet Low temperature titanium hardening

Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3553038A (en) * 1968-10-21 1971-01-05 Stephanois Rech Mec Method for formation of a titanium carbide surface layer on titanium and titanium alloy parts
US4322255A (en) * 1979-01-15 1982-03-30 L'air Liquide, Societe Anonyme Pour L'etude Et L'exploitation Des Procedes Georges Claude Heat treatment of steel and method for monitoring the treatment
US4450205A (en) * 1979-10-26 1984-05-22 Mitsubishi Kinzoku Kabushiki Kaisha Surface-coated blade member of super hard alloy for cutting tools and process for producing same
US4505764A (en) * 1983-03-08 1985-03-19 Howmet Turbine Components Corporation Microstructural refinement of cast titanium
JPH059703A (en) * 1991-06-28 1993-01-19 Nkk Corp Surface hardening treatment of titanium material
US5192323A (en) * 1990-11-05 1993-03-09 Zimmer, Inc. Method of surface hardening orthopedic implant devices
US5372655A (en) * 1991-12-04 1994-12-13 Leybold Durferrit Gmbh Method for the treatment of alloy steels and refractory metals
US5415704A (en) * 1992-02-07 1995-05-16 Smith & Nephew Richards Inc. Surface hardened biocompatible metallic medical implants
WO1995029270A1 (en) * 1994-04-25 1995-11-02 Sturm, Ruger & Company, Inc. Method of treating titanium parts

Patent Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3553038A (en) * 1968-10-21 1971-01-05 Stephanois Rech Mec Method for formation of a titanium carbide surface layer on titanium and titanium alloy parts
US4322255A (en) * 1979-01-15 1982-03-30 L'air Liquide, Societe Anonyme Pour L'etude Et L'exploitation Des Procedes Georges Claude Heat treatment of steel and method for monitoring the treatment
US4450205A (en) * 1979-10-26 1984-05-22 Mitsubishi Kinzoku Kabushiki Kaisha Surface-coated blade member of super hard alloy for cutting tools and process for producing same
US4505764A (en) * 1983-03-08 1985-03-19 Howmet Turbine Components Corporation Microstructural refinement of cast titanium
US5192323A (en) * 1990-11-05 1993-03-09 Zimmer, Inc. Method of surface hardening orthopedic implant devices
JPH059703A (en) * 1991-06-28 1993-01-19 Nkk Corp Surface hardening treatment of titanium material
US5372655A (en) * 1991-12-04 1994-12-13 Leybold Durferrit Gmbh Method for the treatment of alloy steels and refractory metals
US5415704A (en) * 1992-02-07 1995-05-16 Smith & Nephew Richards Inc. Surface hardened biocompatible metallic medical implants
WO1995029270A1 (en) * 1994-04-25 1995-11-02 Sturm, Ruger & Company, Inc. Method of treating titanium parts

Non-Patent Citations (2)

* Cited by examiner, † Cited by third party
Title
STEEL, 02 November 1953, "Surface Treatment of Titanium", pages 130-132. *
TRAITEMENT THERMIQUE, Mar. 1983, 172, PHILLIPPE QUEILLE, "Influence et Limite du Rapport Azote/Methanol Sur l'Equilibre et la Cinetique en Cementation", pages 31-35. *

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2154263A1 (en) * 2008-07-25 2010-02-17 The BOC Group Limited Case hardening titanium and its alloys
WO2017207794A1 (en) * 2016-06-02 2017-12-07 Danmarks Tekniske Universitet A case hardened component of titanium
US11060175B2 (en) 2016-06-02 2021-07-13 Danmarks Tekniske Universitet Case hardened component of titanium
EP3878999A1 (en) 2016-06-02 2021-09-15 Danmarks Tekniske Universitet A method of oxidising titanium
WO2021037757A1 (en) 2019-08-23 2021-03-04 Danmarks Tekniske Universitet Low temperature titanium hardening

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