US20080011035A1 - Method of forging a titanium alloy - Google Patents

Method of forging a titanium alloy Download PDF

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Publication number
US20080011035A1
US20080011035A1 US11/176,382 US17638205A US2008011035A1 US 20080011035 A1 US20080011035 A1 US 20080011035A1 US 17638205 A US17638205 A US 17638205A US 2008011035 A1 US2008011035 A1 US 2008011035A1
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coating
titanium alloy
forging
vanadium
protective coating
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US11/176,382
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US7320238B1 (en
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Wayne E. Voice
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Rolls Royce PLC
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Rolls Royce PLC
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    • C—CHEMISTRY; METALLURGY
    • C23—COATING 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
    • C23C—COATING 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
    • C23C10/00—Solid state diffusion of only metal elements or silicon into metallic material surfaces
    • C23C10/60—After-treatment
    • 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
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22F—CHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
    • C22F1/00—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
    • C22F1/16—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of other metals or alloys based thereon
    • C22F1/18—High-melting or refractory metals or alloys based thereon
    • C—CHEMISTRY; METALLURGY
    • C23—COATING 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
    • C23C—COATING 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
    • C23C10/00—Solid state diffusion of only metal elements or silicon into metallic material surfaces
    • C23C10/18—Solid state diffusion of only metal elements or silicon into metallic material surfaces using liquids, e.g. salt baths, liquid suspensions
    • C—CHEMISTRY; METALLURGY
    • C23—COATING 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
    • C23C—COATING 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
    • C23C10/00—Solid state diffusion of only metal elements or silicon into metallic material surfaces
    • C23C10/28—Solid state diffusion of only metal elements or silicon into metallic material surfaces using solids, e.g. powders, pastes
    • C23C10/30—Solid state diffusion of only metal elements or silicon into metallic material surfaces using solids, e.g. powders, pastes using a layer of powder or paste on the surface

Definitions

  • the present invention relates to a method of forging a titanium alloy and in particular to a method of forging titanium alloys with high levels of vanadium.
  • alloys are coated with a high temperature borosilicate glass lubricant coating and are then forged at a high temperature.
  • liquid and vapour metal oxide e.g. vanadium pentoxide
  • borosilicate glass lubricant produces decohesion or decomposition of the borosilicate glass which produces an unacceptable forging process and makes the surface quality of forged high vanadium and chromium titanium alloy unsatisfactory.
  • the present invention seeks to provide a novel method of forging a titanium alloy, which reduces or overcomes the above-mentioned problem.
  • the present invention provides a method of forging a titanium alloy comprising applying a protective coating onto the titanium alloy, applying a glass lubricant coating onto the protective coating and forging the titanium alloy at a high temperature.
  • the glass lubricant coating comprises a borosilicate glass lubricant coating.
  • Preferably applying the protective coating comprises applying an aluminide coating, a silicon modified aluminide coating, a platinum aluminide coating, an aluminium coating or a platinum coating.
  • Preferably applying the protective coating comprises pack aluminising, vapour phase aluminising, slurry aluminising, spraying, heat-treating or plating.
  • the titanium alloy consists of vanadium and chromium.
  • the titanium alloy consists of 20 wt % to 40 wt % vanadium and 10 to 20 wt % chromium.
  • the titanium alloy consists of 20 wt % to 30 wt % vanadium, 13 wt % to 17 wt % chromium, 1.0 wt % to 3.0 wt % aluminium, 0.1 wt % to 0.4 wt % carbon and up to 0.2 wt % oxygen and balance titanium and incidental impurities.
  • the titanium alloy consists of 25 wt % vanadium, 15 wt % chromium, 2 wt % aluminium, up to 0.15 wt % oxygen, 0.1 wt % to 0.3 wt % carbon and the balance titanium plus incidental impurities.
  • the titanium alloy consists of 35 wt % vanadium and 15 wt % chromium.
  • the titanium alloy is forged into a compressor blade or a compressor vane.
  • FIG. 1 shows a titanium alloy component with a protective coating to be used in a method of forging according to the present invention.
  • a method of forging a titanium alloy component 10 comprises applying a protective coating 14 onto the surface 12 of the titanium alloy component 10 .
  • a glass lubricant coating 16 is applied onto the protective coating 14 and then the titanium alloy component 10 is forged at a high temperature, for example about 1050° C.
  • the titanium alloy component 10 comprises a titanium alloy consisting of vanadium and chromium and other elements, for example a titanium alloy consisting of 20 wt % to 40 wt % vanadium and 10 to 20 wt % chromium.
  • the titanium alloy preferably consisting of 20 wt % to 30 wt % vanadium, 13 wt % to 17 wt % chromium, 1.0 wt % to 3.0 wt % aluminium, 0.1 wt % to 0.4 wt % carbon and up to 0.2 wt % oxygen and balance titanium and incidental impurities.
  • a particular titanium alloy consists of 25 wt % vanadium, 15 wt % chromium, 2 wt % aluminium, up to 0.15 wt % oxygen, 0.1 wt % to 0.3 wt % carbon and the balance titanium plus incidental impurities.
  • Another particular titanium alloy consists of 35 wt % vanadium and 15 wt % chromium.
  • a suitable glass lubricant coating comprises a borosilicate glass lubricant coating.
  • the preferred protective coating comprises an aluminide coating, a silicon modified aluminide coating, a platinum aluminide coating, an aluminium coating or a platinum coating.
  • the protective coating is applied by pack aluminising, vapour phase aluminising, slurry aluminising, spraying, heat-treating or plating.
  • One particular protective coating is a silicon-modified aluminide produced by slurry aluminising.
  • Such protective coatings are available as IPAL IP1041 from Indestructible Paints Ltd of 23-25 Pentos Drive, Sparkhill, Birmingham, B11 3TA or Sermaloy J (RTM) from Sermatech (UK) Ltd of High Holborn Road, Codnor Gate Business Park, Ripley, DE5 3NW.
  • Another particular protective coating is an aluminium water base inorganic acid coating is sprayed onto the titanium alloy component and then cured at a temperature of 540° C. to 560° C.
  • Such protective coatings are available as IPCOTE IP9183, or IPCOTE IP9183R1, from Indestructible Paints Ltd of 23-25 Pentos Drive, Sparkhill, Birmingham, B11 3TA or Sermetal W from Sermatech (UK) Ltd of High Holborn Road, Codnor Gate Business Park, Ripley, DE5 3NW.
  • the protective coating of an aluminide coating is produced by aluminising and the platinum aluminide coating is produced by platinum aluminising.
  • Such protective coatings are available as CN32/1 or CN32/2 and as CN22 or CN22LT from Chromalloy (UK) Ltd of Bramble Way, Clover Nook Industrial Estate, Somercotes, Alfreton, Derbsyshire, DE55 4RH.
  • the protective coating 12 prevents the formation of metal oxides, e.g. vanadium pentoxide, under the glass lubricant coating 14 and hence the glass lubricant coating 14 is not decomposed during the forging process and thus the forging process produces an acceptable surface quality of the forged titanium alloy component 10 .
  • metal oxides e.g. vanadium pentoxide
  • the titanium alloy components may for example be compressor blades, or compressor vanes, of a high-pressure compressor of a gas turbine engine.
  • the present invention is also applicable to titanium alloys consisting of about 15 wt % vanadium.

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  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Crystallography & Structural Chemistry (AREA)
  • Forging (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

A method of forging a titanium alloy component comprises applying a protective coating onto the surface of the titanium alloy component. A glass lubricant coating is applied onto the protective coating and the titanium alloy component is forged at a high temperature. The glass lubricant coating comprises a borosilicate glass lubricant coating. The protective coating comprises an aluminide coating, a silicon modified aluminide coating, a platinum aluminide coating, an aluminium coating or a platinum coating. The titanium alloy component may be a compressor blade, or a compressor vane, of a high-pressure compressor of a gas turbine engine.

Description

  • The present invention relates to a method of forging a titanium alloy and in particular to a method of forging titanium alloys with high levels of vanadium.
  • Conventionally alloys are coated with a high temperature borosilicate glass lubricant coating and are then forged at a high temperature.
  • It has been found that the high temperature borosilicate glass lubricant decomposes on the surface of titanium alloys with high levels of vanadium and chromium and this makes the surface quality of forged high vanadium and chromium titanium alloys unsatisfactory.
  • It has been found that liquid and vapour metal oxide, e.g. vanadium pentoxide, formed underneath the borosilicate glass lubricant produces decohesion or decomposition of the borosilicate glass which produces an unacceptable forging process and makes the surface quality of forged high vanadium and chromium titanium alloy unsatisfactory.
  • Accordingly the present invention seeks to provide a novel method of forging a titanium alloy, which reduces or overcomes the above-mentioned problem.
  • Accordingly the present invention provides a method of forging a titanium alloy comprising applying a protective coating onto the titanium alloy, applying a glass lubricant coating onto the protective coating and forging the titanium alloy at a high temperature.
  • Preferably the glass lubricant coating comprises a borosilicate glass lubricant coating.
  • Preferably applying the protective coating comprises applying an aluminide coating, a silicon modified aluminide coating, a platinum aluminide coating, an aluminium coating or a platinum coating.
  • Preferably applying the protective coating comprises pack aluminising, vapour phase aluminising, slurry aluminising, spraying, heat-treating or plating.
  • Preferably the titanium alloy consists of vanadium and chromium.
  • Preferably the titanium alloy consists of 20 wt % to 40 wt % vanadium and 10 to 20 wt % chromium.
  • Preferably the titanium alloy consists of 20 wt % to 30 wt % vanadium, 13 wt % to 17 wt % chromium, 1.0 wt % to 3.0 wt % aluminium, 0.1 wt % to 0.4 wt % carbon and up to 0.2 wt % oxygen and balance titanium and incidental impurities.
  • Preferably the titanium alloy consists of 25 wt % vanadium, 15 wt % chromium, 2 wt % aluminium, up to 0.15 wt % oxygen, 0.1 wt % to 0.3 wt % carbon and the balance titanium plus incidental impurities.
  • Preferably the titanium alloy consists of 35 wt % vanadium and 15 wt % chromium.
  • Preferably the titanium alloy is forged into a compressor blade or a compressor vane.
  • The present invention will be more fully described by way of example with reference to the accompanying drawings in which:
  • FIG. 1 shows a titanium alloy component with a protective coating to be used in a method of forging according to the present invention.
    •
  • A method of forging a titanium alloy component 10 comprises applying a protective coating 14 onto the surface 12 of the titanium alloy component 10. A glass lubricant coating 16 is applied onto the protective coating 14 and then the titanium alloy component 10 is forged at a high temperature, for example about 1050° C.
  • The titanium alloy component 10 comprises a titanium alloy consisting of vanadium and chromium and other elements, for example a titanium alloy consisting of 20 wt % to 40 wt % vanadium and 10 to 20 wt % chromium. The titanium alloy preferably consisting of 20 wt % to 30 wt % vanadium, 13 wt % to 17 wt % chromium, 1.0 wt % to 3.0 wt % aluminium, 0.1 wt % to 0.4 wt % carbon and up to 0.2 wt % oxygen and balance titanium and incidental impurities. A particular titanium alloy consists of 25 wt % vanadium, 15 wt % chromium, 2 wt % aluminium, up to 0.15 wt % oxygen, 0.1 wt % to 0.3 wt % carbon and the balance titanium plus incidental impurities. Another particular titanium alloy consists of 35 wt % vanadium and 15 wt % chromium.
  • A suitable glass lubricant coating comprises a borosilicate glass lubricant coating.
  • The preferred protective coating comprises an aluminide coating, a silicon modified aluminide coating, a platinum aluminide coating, an aluminium coating or a platinum coating. The protective coating is applied by pack aluminising, vapour phase aluminising, slurry aluminising, spraying, heat-treating or plating.
  • One particular protective coating is a silicon-modified aluminide produced by slurry aluminising. Such protective coatings are available as IPAL IP1041 from Indestructible Paints Ltd of 23-25 Pentos Drive, Sparkhill, Birmingham, B11 3TA or Sermaloy J (RTM) from Sermatech (UK) Ltd of High Holborn Road, Codnor Gate Business Park, Ripley, DE5 3NW.
  • Another particular protective coating is an aluminium water base inorganic acid coating is sprayed onto the titanium alloy component and then cured at a temperature of 540° C. to 560° C. Such protective coatings are available as IPCOTE IP9183, or IPCOTE IP9183R1, from Indestructible Paints Ltd of 23-25 Pentos Drive, Sparkhill, Birmingham, B11 3TA or Sermetal W from Sermatech (UK) Ltd of High Holborn Road, Codnor Gate Business Park, Ripley, DE5 3NW.
  • The protective coating of an aluminide coating is produced by aluminising and the platinum aluminide coating is produced by platinum aluminising. Such protective coatings are available as CN32/1 or CN32/2 and as CN22 or CN22LT from Chromalloy (UK) Ltd of Bramble Way, Clover Nook Industrial Estate, Somercotes, Alfreton, Derbsyshire, DE55 4RH.
  • In use the protective coating 12 prevents the formation of metal oxides, e.g. vanadium pentoxide, under the glass lubricant coating 14 and hence the glass lubricant coating 14 is not decomposed during the forging process and thus the forging process produces an acceptable surface quality of the forged titanium alloy component 10.
  • Other suitable protective coatings may be used.
  • The titanium alloy components may for example be compressor blades, or compressor vanes, of a high-pressure compressor of a gas turbine engine.
  • The present invention is also applicable to titanium alloys consisting of about 15 wt % vanadium.

Claims (13)

1. A method of forging a titanium alloy including vanadium, the method comprising:
applying a protective coating onto the titanium alloy; and
applying a glass lubricant coating onto the protective coating and forging the titanium alloy at a high temperature, the protective coating being selected from a group consisting of an aluminide coating, a silicon modified aluminide coating, a platinum aluminide coating, an aluminum coating and a platinum coating.
2. A method of forging as claimed in claim 1 wherein the glass lubricant coating comprises a borosilicate glass lubricant coating.
3. A method of forging as claimed in claim 1 further comprising applying the protective coating by a method selected from group consisting of pack aluminizing, vapor phase aluminizing, slurry aluminizing, spraying, heat treating and plating.
4. A method of forging as claimed in claim 1 wherein the titanium alloy includes vanadium and chromium.
5. A method of forging as claimed in claim 4 wherein the titanium alloy includes 20 wt % to 40 wt % vanadium and 10 to 20 wt % chromium.
6. A method of forging as claimed in claim 5 wherein the titanium alloy consists of 20 wt % to 30 wt % vanadium, 13 wt % to 17 wt % chromium, 1.0 wt % to 3.0 wt % aluminum, 0.1 wt % to 0.4 wt % carbon and up to 0.2 wt % oxygen and balance titanium and incidental impurities.
7. A method of forging as claimed in claim 6 wherein the titanium alloy consists of 25 wt % vanadium, 15 wt % chromium, 2 wt % aluminum, up to 0.15 wt % oxygen, 0.1 wt % to 0.3 wt % carbon and the balance titanium plus incidental impurities.
8. A method of forging as claimed in claim 5 wherein the titanium alloy includes 35 wt % vanadium and 15 wt % chromium.
9. A method of forging as claimed in claim 1 comprising forging the titanium alloy into a compressor blade.
10. A method of forging as claimed in claim 1 comprising forging the titanium alloy into a compressor vane.
11. A method of forging a titanium alloy including vanadium, the method comprising:
applying a protective coating onto the titanium alloy; and
applying a glass lubricant coating onto the protective coating and forging the titanium alloy at a high temperature, the protective coating being selected from group consisting of an aluminide coating, a silicon modified aluminide coating, a platinum aluminide coating and a platinum coating.
12. A method of forging a titanium alloy including vanadium, the method comprising:
applying a protective coating onto the titanium alloy;
applying a glass lubricant coating onto the protective coating and forging the titanium alloy at a high temperature, the protective coating being selected from a group consisting of an aluminide coating, a silicon modified aluminide coating, a platinum aluminide coating, an aluminum coating and a platinum coating; and
applying the protective coating by a method selected from the group comprising pack aluminizing, vapor phase aluminizing, slurry aluminizing, spraying, heat treating and plating.
13. A method of forging as claimed in claim 1 wherein the titanium alloy includes 15 wt % to 40 wt % vanadium.
US11/176,382 2004-07-28 2005-07-08 Method of forging a titanium alloy Expired - Fee Related US7320238B1 (en)

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GBGB0416764.9A GB0416764D0 (en) 2004-07-28 2004-07-28 A method of forging a titanium alloy
GB0416764.9 2004-07-28

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US20080011035A1 true US20080011035A1 (en) 2008-01-17
US7320238B1 US7320238B1 (en) 2008-01-22

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9909200B2 (en) 2014-09-29 2018-03-06 Hitachi Metals, Ltd. Method of manufacturing Ni-base superalloy

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102007060254A1 (en) 2007-12-14 2009-06-18 Deutsches Zentrum für Luft- und Raumfahrt e.V. Platinum-based high-temperature protective coating on aluminum-rich titanium alloys and titanium aluminides
EP2703454A1 (en) * 2012-08-29 2014-03-05 Pemco Brugge BVBA Coating compositions
CN112496215B (en) * 2020-11-16 2023-06-23 遵义航天新力精密铸锻有限公司 Forging method of titanium alloy thin-wall component

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US4055975A (en) * 1977-04-01 1977-11-01 Lockheed Aircraft Corporation Precision forging of titanium
US4183236A (en) * 1978-01-30 1980-01-15 Trw Inc. Method of isothermal forging
US4318792A (en) * 1980-07-07 1982-03-09 Trw Inc. Process for depositing forging lubricant on titanium workpiece
US4595473A (en) * 1984-08-28 1986-06-17 Trw Inc. Forging lubricant
US5300159A (en) * 1987-12-23 1994-04-05 Mcdonnell Douglas Corporation Method for manufacturing superplastic forming/diffusion bonding tools from titanium
US5743121A (en) * 1996-05-31 1998-04-28 General Electric Company Reducible glass lubricants for metalworking

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US2903785A (en) * 1957-02-11 1959-09-15 Gen Motors Corp Method of hot working titanium
US4055975A (en) * 1977-04-01 1977-11-01 Lockheed Aircraft Corporation Precision forging of titanium
US4183236A (en) * 1978-01-30 1980-01-15 Trw Inc. Method of isothermal forging
US4318792A (en) * 1980-07-07 1982-03-09 Trw Inc. Process for depositing forging lubricant on titanium workpiece
US4595473A (en) * 1984-08-28 1986-06-17 Trw Inc. Forging lubricant
US5300159A (en) * 1987-12-23 1994-04-05 Mcdonnell Douglas Corporation Method for manufacturing superplastic forming/diffusion bonding tools from titanium
US5743121A (en) * 1996-05-31 1998-04-28 General Electric Company Reducible glass lubricants for metalworking

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9909200B2 (en) 2014-09-29 2018-03-06 Hitachi Metals, Ltd. Method of manufacturing Ni-base superalloy

Also Published As

Publication number Publication date
EP1624084B1 (en) 2006-08-23
DE602005000087D1 (en) 2006-10-05
GB0416764D0 (en) 2004-09-01
DE602005000087T2 (en) 2007-01-11
US7320238B1 (en) 2008-01-22
EP1624084A1 (en) 2006-02-08

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