EP0236309A1 - Couche protectrice en ceramique - Google Patents

Couche protectrice en ceramique

Info

Publication number
EP0236309A1
EP0236309A1 EP85904794A EP85904794A EP0236309A1 EP 0236309 A1 EP0236309 A1 EP 0236309A1 EP 85904794 A EP85904794 A EP 85904794A EP 85904794 A EP85904794 A EP 85904794A EP 0236309 A1 EP0236309 A1 EP 0236309A1
Authority
EP
European Patent Office
Prior art keywords
oxide
protective layer
base material
aluminum oxide
ceramic protective
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
EP85904794A
Other languages
German (de)
English (en)
Inventor
Friedrich Harbach
Andrew R. Nicoll
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.)
BBC Brown Boveri AG Switzerland
Original Assignee
BBC Brown Boveri AG Switzerland
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 BBC Brown Boveri AG Switzerland filed Critical BBC Brown Boveri AG Switzerland
Publication of EP0236309A1 publication Critical patent/EP0236309A1/fr
Pending legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12Blades
    • F01D5/28Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
    • 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
    • C23C4/00Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge
    • C23C4/04Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge characterised by the coating material
    • C23C4/10Oxides, borides, carbides, nitrides or silicides; Mixtures thereof
    • C23C4/11Oxides

Definitions

  • the invention relates to a ceramic protective layer based on aluminum oxide according to the preamble of claim 1.
  • Oxidation-resistant components for hot gas turbines and jet engines which have a ceramic protective layer, which by means of flame or By applying these protective layers, the metallic components are protected against corrosive influences at high temperatures.
  • the protection consists in reducing undesired chemical attacks on the component and / or in lowering the temperature in the surface area of the component in relation to the temperature on the surface of the protective layer.
  • Replacement sheet ⁇ more or less slowly. In doing so, they go through all possible phase transformations of the ceramic material. Under certain circumstances, additional conversions even occur if the ceramic particles of the protective layer are not in the thermodynamically stable state immediately after they have solidified.
  • the aluminum oxide first forms the * * ? -Aluminium oxide, which is similar to the ⁇ * -Aluminiumoxid, because this like the ⁇ ⁇ -Aluminiumoxid has a lower surface energy than the only thermodynamically stable alumina modification, the o -Aluminiumoxid, also called Korund.
  • the invention is therefore based on the object of a ceramic protective layer based on aluminum oxide to create, which has a very high temperature change resistance and at the same time is very corrosion-resistant.
  • a gas turbine component to be coated (not shown here) is made of an austenitic material, in particular a nickel superalloy. Before the coating, the component is first chemically cleaned and then roughened with a sandblast. This component is coated in air or under reduced pressure using the known plasma spraying process. If required, the component to be coated can first be coated with a NiCrAlY layer before the ceramic protective layer is applied. The protection described below
  • Spare sheet Layer has pure aluminum oxide powder as the base material.
  • this base material is chromium oxide in an amount of 0.1 to 15 mass? added.
  • magnesium oxide in an amount of 0.03 to 4 mass? added to reduce the grain growth of the aluminum oxide.
  • gallium oxide, vanadium oxide or iron oxide can of course also be used as an additive. It is of course also possible to dispense with the four metal oxides described above and to add only magnesium oxide to the base material, which at the same time promotes the formation of the round structure in the case of the aluminum oxide and reduces the grain growth thereof.
  • the component mentioned above made of a nickel superalloy can also be coated with a ceramic protective layer, the base material of which consists of a mixture of aluminum oxide and titanium oxide.
  • the titanium oxide content in such a protective layer is between 10 and 45% by weight.
  • Chromium oxide is added to the base material according to the invention.
  • the chromium oxide content varies between 0.1 and 15 percent by mass based on the amount of aluminum oxide contained in the base material.

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Plasma & Fusion (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Coating By Spraying Or Casting (AREA)
  • Other Surface Treatments For Metallic Materials (AREA)

Abstract

Le matériau de base de la couche ci-décrite est constitué d'oxyde d'aluminium pur ou principalement d'oxyde d'aluminium. Pour améliorer cette couche protectrice, on ajoute à son matériau de base, avant d'appliquer ladite couche, des oxydes des métaux des groupes IIA, IIIA, IIIB, VB, VIB, VIIB ou VIII de la classification périodique. On obtient ainsi dans le cas de l'oxyde d'aluminium la formation d'une structure de corindon, pour laquelle sont particulièrement indiqués l'oxyde de gallium, l'oxyde de vanadium, l'oxyde de chrome ou l'oxyde de fer. La formation de la structure de corindon augmente la résistance de la couche protectrice à l'action corrosive du pentoxyde de vanadium et du sulfate de sodium. L'addition d'une quantité définie d'oxyde de magnésium permet non seulement de stimuler la formation du corindon mais également de réduire la croissance des grains dans le cas de l'oxyde d'aluminium. Les autres oxydes métalliques stimulent surtout la formation de la structure de corindon, de sorte qu'on ajoute à ces oxydes métalliques de préférence de l'oxyde de magnésium pour réduire la croissance des grains.
EP85904794A 1985-09-14 1985-09-14 Couche protectrice en ceramique Pending EP0236309A1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
PCT/DE1985/000320 WO1987001736A1 (fr) 1985-09-14 1985-09-14 Couche protectrice en ceramique

Publications (1)

Publication Number Publication Date
EP0236309A1 true EP0236309A1 (fr) 1987-09-16

Family

ID=6776141

Family Applications (1)

Application Number Title Priority Date Filing Date
EP85904794A Pending EP0236309A1 (fr) 1985-09-14 1985-09-14 Couche protectrice en ceramique

Country Status (2)

Country Link
EP (1) EP0236309A1 (fr)
WO (1) WO1987001736A1 (fr)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US11697879B2 (en) * 2019-06-14 2023-07-11 Applied Materials, Inc. Methods for depositing sacrificial coatings on aerospace components

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2904449A (en) * 1955-07-26 1959-09-15 Armour Res Found Method and compositions for flame spraying
US3625717A (en) * 1968-04-29 1971-12-07 Avco Corp Spray coating compositions
US4077637A (en) * 1977-01-17 1978-03-07 Koppers Company, Inc. Ceramic coated piston rings
JPS57120871A (en) * 1981-01-20 1982-07-28 Toshihiko Yoshino Magnetic field measuring device
CS233501B1 (en) * 1982-06-11 1985-03-14 Karel Zverina Spray material namely for plasma spraying
DE3427456A1 (de) * 1984-07-25 1986-01-30 Brown, Boveri & Cie Ag, 6800 Mannheim Keramische schutzschicht

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
See references of WO8701736A1 *

Also Published As

Publication number Publication date
WO1987001736A1 (fr) 1987-03-26

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Legal Events

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

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Inventor name: HARBACH, FRIEDRICH

Inventor name: NICOLL, ANDREW, R.