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WO1996005331A1 - Procede de remise en etat de surfaces de pieces en acier - Google Patents

Procede de remise en etat de surfaces de pieces en acier Download PDF

Info

Publication number
WO1996005331A1
WO1996005331A1 PCT/FI1995/000421 FI9500421W WO9605331A1 WO 1996005331 A1 WO1996005331 A1 WO 1996005331A1 FI 9500421 W FI9500421 W FI 9500421W WO 9605331 A1 WO9605331 A1 WO 9605331A1
Authority
WO
WIPO (PCT)
Prior art keywords
coating
reconditioning
weight
coating material
chromium
Prior art date
Application number
PCT/FI1995/000421
Other languages
English (en)
Inventor
Jaakko Tenkula
Original Assignee
Telatek Oy
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 Telatek Oy filed Critical Telatek Oy
Publication of WO1996005331A1 publication Critical patent/WO1996005331A1/fr

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
    • C23C4/00—Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge
    • C23C4/18—After-treatment
    • 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
    • C23C4/00—Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge
    • C23C4/04—Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge characterised by the coating material
    • C23C4/06—Metallic material
    • C23C4/08—Metallic material containing only metal elements
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/005—Repairing methods or devices

Definitions

  • the invention relates to a method for the reconditioning of rotor axle labyrinth sealings and bearing surfaces in a steam turbine so as to restore the said surfaces to their original dimensions.
  • the labyrinth sealing grooves in a steam turbine rotor may in certain cases wear out entirely.
  • the depth of the groove is usually 3-5 mm. In certain cases the bottom of the groove also becomes worn, and therefore 4-7 mm of new material must be introduced onto the surface in the reconditioning of the seal ⁇ ing groove, if restoring of the original dimensions is desired.
  • thick coating layers are not necessary for the bearing surfaces of a turbine rotor in connection with recon ⁇ ditioning.
  • grooves several millimeters deep may form in the bearing surfaces, and thus thick coating layers may be necessary also for their recon ⁇ ditioning.
  • New grooves are machined in the rotor axle. Thereby the axle diameter is reduced.
  • the thickness of the coating must be at minimum 10 mm
  • the coating must be capable of being applied at the power plant
  • the coating must be machinable by lathing the coating must be sufficiently strong and adhere well to the base material
  • the coating must be resistant to erosive and corrosive wear caused by moist steam
  • the coating must not cause corrosive problems between the different parts of the turbine or in the steam pipe system and the heat exchangers
  • the thermal expansion of the coating must be close to the thermal expansion of carbon steels.
  • thick coatings can be formed by spraying martensitic stainless steels or aluminum bronze or tin bronze.
  • Martensitic stainless steel is very difficult to machine, and therefore it is not usable for the present purpose.
  • the thermal expansion of bronzes is so great that a thick coating may detach from the axle during the start-up of the turbine, and therefore they cannot be used.
  • the primary object of the present invention is to provide a method for the reconditioning of the labyrinth sealings and bearing surfaces of the rotor in a steam turbine in such a manner that there is obtained a reliable coating which is suitable for the operating conditions concerned and by means of which the dimensions of the sealing and bearing surfaces can be restored to their original dimensions, and that the coating and related machining can be carried out on site rapidly and economically.
  • the surface to be recon ⁇ ditioned is first preliminarily machined, for example by using a rotary lathe on site. Thereafter, thermal spraying is carried out using a NiCr-alloyed coating material. Finally the coated area is lathed to the desired shape and dimension.
  • the bearing surfaces can additionally be ground on site to the desired surface quality.
  • the coating material used is pref ⁇ erably a metal alloy containing nickel 20-60 % by weight and chromium 15-30 % by weight, in particular nickel 40-60 % by weight and chromium 15-20 % by weight.
  • the balance of the coating material may be steel.
  • the coating material may be in the form of wire or powder. Commercial materials may be used as coating materials in accordance with the invention.
  • Coating materials according to the invention enable a coating over 10 mm thick to be sprayed. This is an essential prerequi ⁇ site for the reconditioning work, as stated above.
  • a single-layer coating having a pos -machining thickness of approx. 0.3-10 mm is formed.
  • Coatings according to the invention are characterized in that there are large amounts of chromium oxides within the coatings, and that on the surface of the coating there is formed a dense and strong oxide film, which prevents erosive and corrosive wear caused by moist steam.
  • the thermal expansion of the coatings according to the inven ⁇ tion is the same as that of carbon steels, and thus the start ⁇ ups and shut-downs of the turbine will not cause problems.
  • the coating can be prepared by using flame, arc, plasma, and/or supersonic spraying, primarily, however, arc, plasma and/or supersonic spraying, in order to achieve a good adhesion of the coating to the base material and in order that the coating should have sufficient intrinsic strength against loads parallel to the axle.
  • the labyrinth sealings and bearing surfaces of a rotor can be reconditioned rapidly on site at a power plant. Thus the down time will be short and production losses will be small.
  • the coatings used in the reconditioning technique will lengthen the useful life of the labyrinth sealings and at the same time the useful life of the rotor, and will lengthen the maintenance interval caased by sealing surfaces.

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Mechanical Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Plasma & Fusion (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Materials Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Coating By Spraying Or Casting (AREA)

Abstract

L'invention concerne un procédé permettant de remettre en état et de recouvrir les surfaces d'appui et d'étanchéité du rotor d'une turbine à vapeur et d'autres pièces en acier qui, dans une turbine, sont exposées à une usure par corrosion et/ou érosion due à la chaleur ou à la vapeur, ou bien à un endommagement mécanique. Selon ledit procédé, la surface à remettre en état et à recouvrir est recouverte par pulvérisation à chaud d'un alliage contenant une grande quantité de nickel et de chrome, que l'on usine ensuite pour donner à la pièce la forme, les dimensions et la qualité de surface désirées.
PCT/FI1995/000421 1994-08-09 1995-08-09 Procede de remise en etat de surfaces de pieces en acier WO1996005331A1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FI943685A FI96970C (fi) 1994-08-09 1994-08-09 Menetelmä teräspintojen kunnostamiseksi
FI943685 1994-08-09

Publications (1)

Publication Number Publication Date
WO1996005331A1 true WO1996005331A1 (fr) 1996-02-22

Family

ID=8541180

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/FI1995/000421 WO1996005331A1 (fr) 1994-08-09 1995-08-09 Procede de remise en etat de surfaces de pieces en acier

Country Status (2)

Country Link
FI (1) FI96970C (fr)
WO (1) WO1996005331A1 (fr)

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1999047723A1 (fr) * 1998-03-14 1999-09-23 Dana Corporation Formation d'un revetement de palier lisse
EP1013786A1 (fr) * 1998-12-22 2000-06-28 GE Aviation Services Operation (Pte) Ltd. Procédé de réparation d'un composant de turbine à base d'un superalliage
EP1123987A1 (fr) * 2000-02-11 2001-08-16 General Electric Company Revêtements réparables d'aluminures à diffusion
RU2173731C1 (ru) * 2000-04-24 2001-09-20 Мордовский государственный университет им. Н.П. Огарева Способ восстановления отверстий деталей из чугунов
WO2002020212A3 (fr) * 2000-09-08 2002-09-12 Mtu Aero Engines Gmbh Procede de tournage et de controle de qualite
EP1798302A4 (fr) * 2004-08-23 2009-12-02 Toshiba Kk Procédé et équipement de réparation d'un rotor
EP2256226A1 (fr) * 2004-08-23 2010-12-01 Kabushiki Kaisha Toshiba Procédé et dispositif pour répararer un rotor
WO2013025384A1 (fr) * 2011-08-17 2013-02-21 General Electric Company Réparation de rainure de joint d'étanchéité de rotor
WO2014115162A3 (fr) * 2013-01-28 2014-12-04 Abhay Vishwas Ranade Joint d'étanchéité à labyrinthe présentant un chemisage/bague interne remplaçable
US9003663B2 (en) 2012-08-22 2015-04-14 Caterpillar Inc. Remanufacturing of bearings using isotropic finishing and thin film coatings

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2418607B2 (de) * 1974-04-11 1978-06-08 Brown Boveri-Sulzer Turbomaschinen Ag, Zuerich (Schweiz) Hochtemperaturkorrosionsschutzschicht
JPS5538969A (en) * 1978-09-14 1980-03-18 Toshiba Corp Corrosion resistant carbon steel
EP0031580A1 (fr) * 1979-12-29 1981-07-08 Ebara Corporation Matériau métallique de revêtement, destiné à éviter la corrosion fissurante d'un acier austénitique inoxydable
WO1985000127A1 (fr) * 1983-06-28 1985-01-17 Castolin S.A. Materiau de pulverisation pulverulent a base de nickel-chrome
EP0224724A1 (fr) * 1985-11-05 1987-06-10 The Perkin-Elmer Corporation Alliage amorphe
EP0293695A1 (fr) * 1987-06-01 1988-12-07 General Electric Company Mélange de poudre d'alliage pour le traitement d'alliages
WO1992004480A1 (fr) * 1990-09-04 1992-03-19 Tampella Telatek Oy Revetement, procede de revetement pour turbine a vapeur et surfaces d'acier contigues

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2418607B2 (de) * 1974-04-11 1978-06-08 Brown Boveri-Sulzer Turbomaschinen Ag, Zuerich (Schweiz) Hochtemperaturkorrosionsschutzschicht
JPS5538969A (en) * 1978-09-14 1980-03-18 Toshiba Corp Corrosion resistant carbon steel
EP0031580A1 (fr) * 1979-12-29 1981-07-08 Ebara Corporation Matériau métallique de revêtement, destiné à éviter la corrosion fissurante d'un acier austénitique inoxydable
WO1985000127A1 (fr) * 1983-06-28 1985-01-17 Castolin S.A. Materiau de pulverisation pulverulent a base de nickel-chrome
EP0224724A1 (fr) * 1985-11-05 1987-06-10 The Perkin-Elmer Corporation Alliage amorphe
EP0293695A1 (fr) * 1987-06-01 1988-12-07 General Electric Company Mélange de poudre d'alliage pour le traitement d'alliages
WO1992004480A1 (fr) * 1990-09-04 1992-03-19 Tampella Telatek Oy Revetement, procede de revetement pour turbine a vapeur et surfaces d'acier contigues

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
PATENT ABSTRACTS OF JAPAN, Vol. 4, No. 73, C-12; & JP,A,55 038 969 (TOKYO SHIBAURA DENKI K.K.), 18 March 1980. *

Cited By (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1999047723A1 (fr) * 1998-03-14 1999-09-23 Dana Corporation Formation d'un revetement de palier lisse
EP1013786A1 (fr) * 1998-12-22 2000-06-28 GE Aviation Services Operation (Pte) Ltd. Procédé de réparation d'un composant de turbine à base d'un superalliage
US6228510B1 (en) 1998-12-22 2001-05-08 General Electric Company Coating and method for minimizing consumption of base material during high temperature service
EP1123987A1 (fr) * 2000-02-11 2001-08-16 General Electric Company Revêtements réparables d'aluminures à diffusion
RU2173731C1 (ru) * 2000-04-24 2001-09-20 Мордовский государственный университет им. Н.П. Огарева Способ восстановления отверстий деталей из чугунов
US6886435B2 (en) 2000-09-08 2005-05-03 Mtu Aero Engines Gmbh Turning and quality assurance process for thermally sprayed turbomachine linings
WO2002020212A3 (fr) * 2000-09-08 2002-09-12 Mtu Aero Engines Gmbh Procede de tournage et de controle de qualite
EP1798302A4 (fr) * 2004-08-23 2009-12-02 Toshiba Kk Procédé et équipement de réparation d'un rotor
EP2256226A1 (fr) * 2004-08-23 2010-12-01 Kabushiki Kaisha Toshiba Procédé et dispositif pour répararer un rotor
WO2013025384A1 (fr) * 2011-08-17 2013-02-21 General Electric Company Réparation de rainure de joint d'étanchéité de rotor
US8893381B2 (en) 2011-08-17 2014-11-25 General Electric Company Rotor seal wire groove repair
EP2753799B1 (fr) 2011-08-17 2018-06-06 General Electric Company Réparation de rainure de joint d'étanchéité de rotor
EP2753799B2 (fr) † 2011-08-17 2024-01-10 General Electric Company Réparation de rainure de joint d'étanchéité de rotor
US9003663B2 (en) 2012-08-22 2015-04-14 Caterpillar Inc. Remanufacturing of bearings using isotropic finishing and thin film coatings
WO2014115162A3 (fr) * 2013-01-28 2014-12-04 Abhay Vishwas Ranade Joint d'étanchéité à labyrinthe présentant un chemisage/bague interne remplaçable

Also Published As

Publication number Publication date
FI96970C (fi) 1996-09-25
FI943685A0 (fi) 1994-08-09
FI96970B (fi) 1996-06-14
FI943685L (fi) 1996-02-10

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