JPS5569250A - Manufacture of high-temperature gas turbine blade - Google Patents

Manufacture of high-temperature gas turbine blade

Info

Publication number
JPS5569250A
JPS5569250A JP14180178A JP14180178A JPS5569250A JP S5569250 A JPS5569250 A JP S5569250A JP 14180178 A JP14180178 A JP 14180178A JP 14180178 A JP14180178 A JP 14180178A JP S5569250 A JPS5569250 A JP S5569250A
Authority
JP
Japan
Prior art keywords
turbine blade
temp
gas turbine
superalloy
manufacture
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.)
Pending
Application number
JP14180178A
Other languages
Japanese (ja)
Inventor
Kazuo Suzuki
Tetsuo Fujiwara
Kazunori Yoshimoto
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.)
Toshiba Corp
Original Assignee
Toshiba Corp
Tokyo Shibaura Electric 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 Toshiba Corp, Tokyo Shibaura Electric Co Ltd filed Critical Toshiba Corp
Priority to JP14180178A priority Critical patent/JPS5569250A/en
Publication of JPS5569250A publication Critical patent/JPS5569250A/en
Pending legal-status Critical Current

Links

Classifications

    • 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
    • C23C10/34—Embedding in a powder mixture, i.e. pack cementation
    • C23C10/36—Embedding in a powder mixture, i.e. pack cementation only one element being diffused
    • 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
    • C23C10/34—Embedding in a powder mixture, i.e. pack cementation
    • C23C10/52—Embedding in a powder mixture, i.e. pack cementation more than one element being diffused in one step
    • 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
    • C23C12/00—Solid state diffusion of at least one non-metal element other than silicon and at least one metal element or silicon into metallic material surfaces
    • 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
    • C23C8/00—Solid 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
    • C23C8/06—Solid 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
    • C23C8/34—Solid 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 more than one step

Landscapes

  • Chemical & Material Sciences (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Preventing Corrosion Or Incrustation Of Metals (AREA)

Abstract

PURPOSE:To make it possible to use high-temp. gas turbine blade at a high temp. near 1,500 deg.C for a long time, by making Ti, Zr, V, Al, Mg, Ce, B etc. diffuse and permeate into the high-temp. gas turbine blade made of superalloy, then by the heat treanment of the turbine blade. CONSTITUTION:Gas turbine blade is made from Ni or Co base superalloy such as Inconel, Hastelloy. At least one metal selected from the group consisting of Ti, Zr, V, Al, Mg, Ce, and B or their alloy is made to diffuse and permeate into the surface of the turbine blade. Then the turbine blade is heated at a temp. about 1,000 deg.C to oxidize the permeated metal, thereby the bonding strength of the oxide layer to the turbine blade material through the diffused layer is increased. The shearing thermal stress caused by the difference in thermal expansion between the superalloy material and the oxide layer is reduced, so that the turbine blade is used for a long time without peeling of oxide of excellent heat resistance even at a high temp. atout 1,500 deg.C.
JP14180178A 1978-11-17 1978-11-17 Manufacture of high-temperature gas turbine blade Pending JPS5569250A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP14180178A JPS5569250A (en) 1978-11-17 1978-11-17 Manufacture of high-temperature gas turbine blade

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP14180178A JPS5569250A (en) 1978-11-17 1978-11-17 Manufacture of high-temperature gas turbine blade

Publications (1)

Publication Number Publication Date
JPS5569250A true JPS5569250A (en) 1980-05-24

Family

ID=15300443

Family Applications (1)

Application Number Title Priority Date Filing Date
JP14180178A Pending JPS5569250A (en) 1978-11-17 1978-11-17 Manufacture of high-temperature gas turbine blade

Country Status (1)

Country Link
JP (1) JPS5569250A (en)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5963305A (en) * 1982-04-07 1984-04-11 Hitachi Ltd Member of steam turbine
FR2553436A1 (en) * 1983-10-12 1985-04-19 Creusot Loire Process for chemical coating, with titanium nickelide, of nickel-based metal objects.
EP0140889A1 (en) * 1983-04-22 1985-05-15 Sri International Process for applying thermal barrier coatings to metals and resulting product
JPS60190554A (en) * 1984-03-08 1985-09-28 Hitachi Ltd Structural member made of zirconium base alloy and its manufacture
WO1998003698A1 (en) * 1996-07-19 1998-01-29 Abb Patent Gmbh Method of improving the resistance to cracking in components composed of nickel-based and iron-based materials
EP2240213A2 (en) * 2008-01-04 2010-10-20 Smith & Nephew, Inc. Surface alloyed medical implant

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5963305A (en) * 1982-04-07 1984-04-11 Hitachi Ltd Member of steam turbine
JPS6259205B2 (en) * 1982-04-07 1987-12-10 Hitachi Ltd
EP0140889A1 (en) * 1983-04-22 1985-05-15 Sri International Process for applying thermal barrier coatings to metals and resulting product
FR2553436A1 (en) * 1983-10-12 1985-04-19 Creusot Loire Process for chemical coating, with titanium nickelide, of nickel-based metal objects.
JPS60190554A (en) * 1984-03-08 1985-09-28 Hitachi Ltd Structural member made of zirconium base alloy and its manufacture
JPH0371507B2 (en) * 1984-03-08 1991-11-13 Hitachi Ltd
WO1998003698A1 (en) * 1996-07-19 1998-01-29 Abb Patent Gmbh Method of improving the resistance to cracking in components composed of nickel-based and iron-based materials
EP2240213A2 (en) * 2008-01-04 2010-10-20 Smith & Nephew, Inc. Surface alloyed medical implant
EP2240213A4 (en) * 2008-01-04 2013-06-05 Smith & Nephew Inc Surface alloyed medical implant
US10675384B2 (en) 2008-01-04 2020-06-09 Smith & Nephew Inc. Surface alloyed medical implant
US11717597B2 (en) 2008-01-04 2023-08-08 Smith & Nephew, Inc. Surface alloyed medical implant

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