WO1999002745A1 - Alloy for corrosion-resistant coatings or surface coatings - Google Patents

Alloy for corrosion-resistant coatings or surface coatings Download PDF

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Publication number
WO1999002745A1
WO1999002745A1 PCT/IT1998/000167 IT9800167W WO9902745A1 WO 1999002745 A1 WO1999002745 A1 WO 1999002745A1 IT 9800167 W IT9800167 W IT 9800167W WO 9902745 A1 WO9902745 A1 WO 9902745A1
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WO
WIPO (PCT)
Prior art keywords
metal
yttrium
alloy
main group
cobalt
Prior art date
Application number
PCT/IT1998/000167
Other languages
French (fr)
Inventor
Nelso Antolotti
Original Assignee
Turbocoating S.P.A.
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 Turbocoating S.P.A. filed Critical Turbocoating S.P.A.
Priority to AT98929635T priority Critical patent/ATE217032T1/en
Priority to EP98929635A priority patent/EP0996752B1/en
Priority to US09/462,272 priority patent/US6355212B1/en
Priority to DE69805179T priority patent/DE69805179T2/en
Publication of WO1999002745A1 publication Critical patent/WO1999002745A1/en

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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
    • C23C30/00—Coating with metallic material characterised only by the composition of the metallic material, i.e. not characterised by the coating process
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C19/00—Alloys based on nickel or cobalt
    • C22C19/07—Alloys based on nickel or cobalt based on cobalt

Definitions

  • the present invention relates to an alloy for anti-corrosive coatings or surface coatings which are resistant up to 1100°C.
  • Such surface coatings can be obtained by the following thermal spraying methods: plasma spraying in vacuo, plasma spraying in air, HVOF (High- Velocity Oxygen Fuel) or high-velocity oxygen flame.
  • thermal spraying methods plasma spraying in vacuo, plasma spraying in air, HVOF (High- Velocity Oxygen Fuel) or high-velocity oxygen flame.
  • Said alloy is resistant to corrosion and guarantees a service life of 1000 hours if used for the coating of components which operate in the presence of sodium-, vanadium-, sulphur- and chlorine-containing hydrocarbon combustion products.
  • a first disadvantage is that this alloy does not guarantee sufficient corrosion resistance if employed at temperatures above 700°C.
  • Cobalt (Co) remaining pe is also known.
  • Said second alloy is used for coating components with a superalloy material.
  • the presence of silicon in the coating matrix provides resistance against the formation of oxides and sulphides on the surface layer.
  • this second alloy has a low yttrium content, which is insufficient for ensuring corrosion resistance in the presence of products containing substantial amounts of sulphur, chlorine and vanadium.
  • a third alloy is known from US 4,585,481, which describes an alloy based on cobalt and containing chromium, aluminium, yttrium and silicon in the following proportions:
  • this alloy has a silicon content which is normally above 4.5% and therefore results in a reduction of the plasticity of the coating, making it impossible to use it for the coating of apparatuses or objects which must withstand substantial changes in temperature.
  • a further disadvantage is that, during application of the coating or surface coating by the plasma method, oxidation of yttrium and silicon may take place.
  • This third alloy is unable to guarantee the corrosion resistance required in the presence of combustion products containing substantial amounts of sulphur, chlorine and vanadium.
  • the alloys mentioned above can usually be used at temperatures not exceeding 900 °C, since all of them are based on cobalt.
  • the object of the present invention is to eliminate the abovementioned disadvantages and provide an alloy with excellent performance even at high temperatures, in particular even above 1000°C. Said objects are fully achieved by the alloy, according to the present invention, for corrosion-resistant coatings or surface coatings and which is characterized by the contents of the claims indicated below and in particular in that it comprises:
  • the Applicant has realized that the disadvantages of the known alloys based on cobalt and containing chromium, aluminium, yttrium and silicon can be avoided by adding one of the metals from the second main group (magnesium, calcium, barium, strontium), both in free form and in the form of the oxide, in the abovementioned proportions.
  • the present invention also relates to a subsequently modified alloy in which the components are present in the following proportions:
  • Me remaining percentage in which Me is a metal which can be nickel (Ni) or iron (Fe) or cobalt (Co) or a composition comprising Ni-Fe-Co, Ni-Co, Ni-Fe, Fe-Co.
  • rhenium (Re) may also be present in a percentage of 2.0 - 1 1.0%.
  • the alloy according to the present invention is an alloy for anti-corrosive surface coatings which is based on cobalt and contains chromium, aluminium, yttrium, silicon, and a metal from the second main group, together with the corresponding oxide, in the following proportions: Chromium (Cr) 26.0 - 30.0%
  • Co Cobalt (Co) remaining percentage.
  • the addition of one of the metals from the second main group (magnesium, calcium, barium, strontium), both in free form and in the form of the oxide, in the abovementioned proportions, does indeed avoid the disadvantages of the cobalt-based alloys of the prior art.
  • the second alloy differs from the preceding one mainly by:
  • Metal from the second main group (Mg, Ca, Ba, Sr) 0.1 - 2.0%
  • Me remaining percentage where Me denotes a metal which can be nickel (Ni) or iron (Fe) or cobalt (Co) or a composition comprising Ni-Fe-Co.
  • rhenium (Re) is envisaged as being present in a percentage of 2.0 - 1 1.0.
  • the predominant presence of the metal denoted by Me and the content of chromium and aluminium in the percentages given ensure that the coating obtained exhibits a base and two phases: the ⁇ -phase matrix on top of an Me-Cr base and the free Me-Al ⁇ -phase.
  • the presence of aluminium on the surface of the coating in the abovementioned percentage results in the formation of a protective Al 2 O 3 layer which gives the coating obtained improved corrosion resistance.
  • yttrium (Y) by an yttrium/hafnium (Y/Hf) composition having the same percentage (0.3 -1.5%), relative to the total of the components, achieves better adhesion of the alumina, Al 2 O 3 , to the surface of the coating.
  • Y/Hf yttrium/hafnium
  • the combination of silicon with the metal from the second main group and its oxide makes it possible to maintain the operational capacity of the surface coating obtained when applied by plasma spraying in air or by high-velocity flame spraying.
  • the presence of the metal from the second main group (Mg, Ca, Ba, Sr) in the proportions mentioned prevents the yttrium and silicon from being oxidized during application of the coating or surface coating.
  • a lower content of silicon, of the metal from the second main group and its oxide in the alloy based on nickel, iron and cobalt according to the present invention does not increase the corrosion resistance of the coating.
  • a higher content of silicon, yttrium, metal from the second main group and its oxide in the alloy according to the present invention produces a deterioration in the mechanical characteristics of the coating obtained, increases the fragility, reduces the coefficient of thermal expansion, and thus causes the coating to form cracks and to flake and therefore lowers the protection with respect to corrosion caused by sulpho-oxidation.
  • the addition of tantalum and/or rhenium furthermore results in a significantly improved performance at oxidation temperature levels above temperatures of 1000°C.

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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)
  • Preventing Corrosion Or Incrustation Of Metals (AREA)
  • Physical Vapour Deposition (AREA)
  • Coating By Spraying Or Casting (AREA)
  • Chemically Coating (AREA)
  • Other Surface Treatments For Metallic Materials (AREA)

Abstract

The invention falls within the field of anti-corrosive alloys and relates in particular to an alloy containing cobalt, chromium, aluminium, yttrium, silicon, a metal from the second main group, together with the corresponding oxide, in the following proportions: chromium (Cr) 26.0-30 %; aluminium (A1) 5.5-13.0 %; yttrium (Y) 0.3-1.5 %; silicon (Si) 1.5-4.5 %; metal from the second main group (magnesium, calcium, barium, strontium) 0.1-2.0 %; oxide of the corresponding metal from the second main group 0.1-2.0 %; cobalt (Co) remaining percentage. Preferably, tantalum (Ta) is also added in a proportion of 0.5-4.0 %, and the remaining percentage of cobalt is replaced by a remaining percentage of Me, Me being understood to mean a metal which may be nickel (Ni) or iron (Fe) or cobalt (Co) or a composition comprising Ni-Fe-Co, Ni-Fe, Ni-Co, Co-Fe.

Description

ALLOY FOR CORROSION-RESISTANT COATINGS OR SURFACE COATINGS
DESCRIPTION The present invention relates to an alloy for anti-corrosive coatings or surface coatings which are resistant up to 1100°C.
Such surface coatings can be obtained by the following thermal spraying methods: plasma spraying in vacuo, plasma spraying in air, HVOF (High- Velocity Oxygen Fuel) or high-velocity oxygen flame.
In the field of metallurgy, and in particular in the field of alloys used as coatings for gas turbines against corrosion caused by sulpho-oxidation, an alloy based on cobalt and also containing chromium, aluminium and yttrium in the following proportions: Chromium (Cr) 8.0 - 30.0% Aluminium (Al) 5.0 - 15.0% Yttrium (Y) 0 - 1.0% Cobalt (Co) remaining percentage is already known.
Said alloy is resistant to corrosion and guarantees a service life of 1000 hours if used for the coating of components which operate in the presence of sodium-, vanadium-, sulphur- and chlorine-containing hydrocarbon combustion products.
A first disadvantage is that this alloy does not guarantee sufficient corrosion resistance if employed at temperatures above 700°C.
Furthermore, if said alloy is applied by a thermal spraying method (APS, VPS, HVOF), oxidation of yttrium and aluminium occurs, thus resulting in the loss of the working property of the coating. A second alloy based on cobalt and containing chromium, aluminium, yttrium and silicon in the following proportions:
Chromium (Cr) 12.5 - 20.0%
Aluminium (Al) 2.0 - 8.0%
Yttrium (Y) 0 - 0.25%
Silicon (Si) 2.0 - 6.0%
Cobalt (Co) remaining pe is also known.
Said second alloy is used for coating components with a superalloy material. The presence of silicon in the coating matrix provides resistance against the formation of oxides and sulphides on the surface layer.
However, this second alloy has a low yttrium content, which is insufficient for ensuring corrosion resistance in the presence of products containing substantial amounts of sulphur, chlorine and vanadium.
A third alloy is known from US 4,585,481, which describes an alloy based on cobalt and containing chromium, aluminium, yttrium and silicon in the following proportions:
Chromium (Cr) 5.0 - 40.0%
Aluminium (Al) 8.0 - 35.0%
Yttrium (Y) 0.1 - 2.0%
Silicon (Si) 1.0 - 7.0% C Coobbaalltt ( (CCoo)) remaining percentage.
However, this alloy has a silicon content which is normally above 4.5% and therefore results in a reduction of the plasticity of the coating, making it impossible to use it for the coating of apparatuses or objects which must withstand substantial changes in temperature. A further disadvantage is that, during application of the coating or surface coating by the plasma method, oxidation of yttrium and silicon may take place. This third alloy is unable to guarantee the corrosion resistance required in the presence of combustion products containing substantial amounts of sulphur, chlorine and vanadium. The alloys mentioned above can usually be used at temperatures not exceeding 900 °C, since all of them are based on cobalt.
The object of the present invention is to eliminate the abovementioned disadvantages and provide an alloy with excellent performance even at high temperatures, in particular even above 1000°C. Said objects are fully achieved by the alloy, according to the present invention, for corrosion-resistant coatings or surface coatings and which is characterized by the contents of the claims indicated below and in particular in that it comprises:
Chromium (Cr) 26.0 - 30.0%
Aluminium (Al) 6.0 - 8.0% Y Yttttririuumm ( (YY)) 0.3 - 1.5%
Silicon (Si) 1.5 - 4.5% Metal from the second main group
(magnesium, calcium, barium, strontium) 0.1 - 0.5%
Oxide of the corresponding metal from the second main group 0.1 - 1.0%
Cobalt (Co) remaining percentage.
After numerous studies, the Applicant has realized that the disadvantages of the known alloys based on cobalt and containing chromium, aluminium, yttrium and silicon can be avoided by adding one of the metals from the second main group (magnesium, calcium, barium, strontium), both in free form and in the form of the oxide, in the abovementioned proportions.
The present invention also relates to a subsequently modified alloy in which the components are present in the following proportions:
Chromium (Cr) 22.0 - 30.0%
Aluminium (Al) 5.5 - 13.0%
Yttrium (Y) 0.3 - 1.5%
Silicon (Si) 1.5 - 4.5%
Metal from the second main group
(Mg, Ca, Ba, Sr) 0.1 - 2.0% Oxide of the corresponding metal (Mg,
Ca, Ba, Sr) from the second main group 0.1 - 2.0% with the addition of
Tantalum (Ta) 0.5 - 4.0%
Me remaining percentage in which Me is a metal which can be nickel (Ni) or iron (Fe) or cobalt (Co) or a composition comprising Ni-Fe-Co, Ni-Co, Ni-Fe, Fe-Co.
Together with tantalum or in its place, rhenium (Re) may also be present in a percentage of 2.0 - 1 1.0%.
This characteristic feature, along with others, will become more apparent from the following description of a few preferred embodiments which are described by way of non- limiting examples.
The alloy according to the present invention is an alloy for anti-corrosive surface coatings which is based on cobalt and contains chromium, aluminium, yttrium, silicon, and a metal from the second main group, together with the corresponding oxide, in the following proportions: Chromium (Cr) 26.0 - 30.0%
Aluminium (Al) 6.0 - 8.0%
Yttrium (Y) 0.3 - 1.5%
Silicon (Si) 1.5 - 4.5% Metal from the second main group
(magnesium, calcium, barium, strontium) 0.1 - 0.5%
Oxide of the corresponding metal from the second main group 0.1 - 1.0%
Cobalt (Co) remaining percentage. The addition of one of the metals from the second main group (magnesium, calcium, barium, strontium), both in free form and in the form of the oxide, in the abovementioned proportions, does indeed avoid the disadvantages of the cobalt-based alloys of the prior art.
After numerous tests and studies, the Applicant has furthermore developed a second alloy directly derived from the one described above.
Indeed, the second alloy differs from the preceding one mainly by:
- the addition of a new element, i.e. tantalum,
- the replacement of cobalt by nickel or iron or by cobalt-nickel-iron, nickel-iron, iron- cobalt or nickel-cobalt alloys, - and, to a lesser extent, by different percentages of other elements in the following proportions:
Chromium (Cr) 22.0 - 31.0%
Aluminium (Al) 5.5 - 13.0%
Yttrium (Y) 0.3 - 1.5% Silicon (Si) 1.5 - 10.0% Metal from the second main group (Mg, Ca, Ba, Sr) 0.1 - 2.0%
Oxide of the corresponding metal (Mg, Ca, Ba, Sr) from the second main group 0.1 - 2.0% Tantalum (Ta) 0.5 - 4.0%
Me remaining percentage where Me denotes a metal which can be nickel (Ni) or iron (Fe) or cobalt (Co) or a composition comprising Ni-Fe-Co.
Moreover, according to a second variant, in addition to tantalum or in place of tantalum, rhenium (Re) is envisaged as being present in a percentage of 2.0 - 1 1.0.
The predominant presence of the metal denoted by Me and the content of chromium and aluminium in the percentages given ensure that the coating obtained exhibits a base and two phases: the γ-phase matrix on top of an Me-Cr base and the free Me-Al β-phase. The presence of aluminium on the surface of the coating in the abovementioned percentage results in the formation of a protective Al2O3 layer which gives the coating obtained improved corrosion resistance.
The presence of yttrium in the proportions mentioned prevents the coating from developing cracks and from flaking.
Moreover, the Applicant has found that replacing yttrium (Y) by an yttrium/hafnium (Y/Hf) composition having the same percentage (0.3 -1.5%), relative to the total of the components, achieves better adhesion of the alumina, Al2O3, to the surface of the coating. The presence of silicon and of a metal from the second main group in free form and in the form of the oxide in the proportions mentioned increases the corrosion resistance of the γ-matrix of the surface of the coating obtained on the article which operates in a temperature range of between 700°C and 850°C. The combination of silicon with the metal from the second main group and its oxide makes it possible to maintain the operational capacity of the surface coating obtained when applied by plasma spraying in air or by high-velocity flame spraying. The presence of the metal from the second main group (Mg, Ca, Ba, Sr) in the proportions mentioned prevents the yttrium and silicon from being oxidized during application of the coating or surface coating.
A lower content of silicon, of the metal from the second main group and its oxide in the alloy based on nickel, iron and cobalt according to the present invention does not increase the corrosion resistance of the coating. A higher content of silicon, yttrium, metal from the second main group and its oxide in the alloy according to the present invention produces a deterioration in the mechanical characteristics of the coating obtained, increases the fragility, reduces the coefficient of thermal expansion, and thus causes the coating to form cracks and to flake and therefore lowers the protection with respect to corrosion caused by sulpho-oxidation. Increasing the content of the oxide of the metal from the second main group, relative to the abovementioned percentages, ensures that the effect that the corrosion-promoting components present in the fuel (Na2SO4 and V2O5) have on the coating is diminished owing to the formation of thermodynamically stable sulphates and vanadates. The addition of tantalum and/or rhenium furthermore results in a significantly improved performance at oxidation temperature levels above temperatures of 1000°C.

Claims

CLAIMS Alloy for corrosion-resistant coatings or surface coatings, characterized in that it contains cobalt, chromium, aluminium, yttrium, silicon, and a metal from the second main group, together with the corresponding oxide, in the following proportions:
Chromium (Cr) 26.0 - 30.0%
Aluminium (Al) 5.5 - 13.0%
Yttrium (Y) 0.3 - 1.5%
Silicon (Si) 1.5 - 4.5% Metal from the second main group (magnesium, calcium, barium, strontium) 0.1 -
2.0% Oxide of the corresponding metal from the second main group 0.1 - 2.0%
Cobalt (Co) remaining percentage.
Alloy for corrosion-resistant coatings or surface coatings, characterized in that it contains chromium, aluminium, yttrium, silicon, and a metal from the second main group, together with the corresponding oxide, tantalum and one or more metals from Ni, Fe and Co, in the following proportions:
Chromium (Cr) 22.0 - 31.0%
Aluminium (Al) 5.5 - 13.0%
Yttrium (Y) 0.3 - 1.5%
Silicon (Si) 1.5 - 10.0%
Metal from the second main group (Mg, Ca, Ba, Sr) 0.1 - 2.0%
Oxide of the corresponding metal (Mg, Ca, Ba, Sr) from the second main group 0.1 - 2.0% with the addition of
Tantalum (Ta) 0.5 - 4.0%
Me remaining percentage where Me is a metal which can be nickel (Ni) or iron (Fe) or cobalt (Co) or a composition comprising Ni-Fe-Co, Ni-Fe, Ni-Co, Fe-Co.
3. Alloy according to Claim 2, in which furthermore Rhenium (Re) 2.0 - 11.0% is present.
4. Alloy according to Claim 2, in which tantalum is replaced by Rhenium (Re) 2.0 - 1 1.0%
5. Alloy according to Claim 1 or 2, in which yttrium is replaced by an yttrium (Y) and hafnium (Hf) composition which maintains the percentage of 0.3 - 1.5%, relative to the total composition of the alloy.
6. Protective anti corrosive coating, characterized in that it is prepared by using an alloy according to any one of the preceding claims.
PCT/IT1998/000167 1997-07-10 1998-06-19 Alloy for corrosion-resistant coatings or surface coatings WO1999002745A1 (en)

Priority Applications (4)

Application Number Priority Date Filing Date Title
AT98929635T ATE217032T1 (en) 1997-07-10 1998-06-19 ALLOY FOR CORROSION-RESISTANT COATINGS OR SURFACE COATINGS
EP98929635A EP0996752B1 (en) 1997-07-10 1998-06-19 Alloy for corrosion-resistant coatings or surface coatings
US09/462,272 US6355212B1 (en) 1997-07-10 1998-06-19 Alloy for corrosion-resistant coatings or surface coatings
DE69805179T DE69805179T2 (en) 1997-07-10 1998-06-19 ALLOY FOR CORROSION RESISTANT COATINGS OR SURFACE COATINGS

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
IT97PR000039A IT1294098B1 (en) 1997-07-10 1997-07-10 CORROSION RESISTANT ALLOY OR COATINGS.
ITPR97A000039 1997-07-10

Publications (1)

Publication Number Publication Date
WO1999002745A1 true WO1999002745A1 (en) 1999-01-21

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Application Number Title Priority Date Filing Date
PCT/IT1998/000167 WO1999002745A1 (en) 1997-07-10 1998-06-19 Alloy for corrosion-resistant coatings or surface coatings

Country Status (5)

Country Link
EP (1) EP0996752B1 (en)
AT (1) ATE217032T1 (en)
DE (1) DE69805179T2 (en)
IT (1) IT1294098B1 (en)
WO (1) WO1999002745A1 (en)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1061150A2 (en) * 1999-06-08 2000-12-20 ABB Alstom Power (Schweiz) AG Coating containing NiAl beta Phases
EP1272301A1 (en) * 2000-03-27 2003-01-08 Sulzer Metco (US) Inc. Superalloy hvof powders with improved high temperature oxidation, corrosion and creep resistance
EP1319730A1 (en) * 2001-12-17 2003-06-18 Mitsubishi Heavy Industries, Ltd. High temperature corrosion resistant alloy, thermal barrier coating material with metal bonding layer, and gas turbine using high temperature corrosion resistant alloy
WO2003060194A1 (en) * 2002-01-18 2003-07-24 Alstom Technology Ltd High-temperature protective coating
EP1790746A1 (en) * 2005-11-24 2007-05-30 Siemens Aktiengesellschaft Alloy, protective layer and component
CN107406919A (en) * 2015-08-25 2017-11-28 韩国机械研究院 Machinability, inoxidizability, corrosion resistance and the outstanding Co Cr class dental alloys of taste

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US4503122A (en) * 1982-12-16 1985-03-05 Bbc Aktiengesellschaft Brown, Boveri & Cie High-temperature protection layer
US4585481A (en) * 1981-08-05 1986-04-29 United Technologies Corporation Overlays coating for superalloys
DE3842300A1 (en) * 1988-12-16 1990-06-21 Asea Brown Boveri Protective high-temperature layer
RU2051196C1 (en) * 1993-11-26 1995-12-27 Совместное Российско-Итальянское предприятие "Интеркоут Турбинсервис" Cobalt-based alloy
WO1996012049A1 (en) * 1994-10-14 1996-04-25 Siemens Aktiengesellschaft Protective layer for protecting parts against corrosion, oxidation and excessive thermal stresses, as well as process for producing the same

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US4585481A (en) * 1981-08-05 1986-04-29 United Technologies Corporation Overlays coating for superalloys
US4503122A (en) * 1982-12-16 1985-03-05 Bbc Aktiengesellschaft Brown, Boveri & Cie High-temperature protection layer
DE3842300A1 (en) * 1988-12-16 1990-06-21 Asea Brown Boveri Protective high-temperature layer
RU2051196C1 (en) * 1993-11-26 1995-12-27 Совместное Российско-Итальянское предприятие "Интеркоут Турбинсервис" Cobalt-based alloy
WO1996012049A1 (en) * 1994-10-14 1996-04-25 Siemens Aktiengesellschaft Protective layer for protecting parts against corrosion, oxidation and excessive thermal stresses, as well as process for producing the same

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Cited By (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1589122A1 (en) * 1999-06-08 2005-10-26 Alstom Technology Ltd Coating containing NiAl beta Phases
EP1061150A3 (en) * 1999-06-08 2000-12-27 ABB Alstom Power (Schweiz) AG Coating containing NiAl beta Phases
US6471791B1 (en) 1999-06-08 2002-10-29 Alstom (Switzerland) Ltd Coating containing NiAl-β phase
EP1061150A2 (en) * 1999-06-08 2000-12-20 ABB Alstom Power (Schweiz) AG Coating containing NiAl beta Phases
EP1272301A1 (en) * 2000-03-27 2003-01-08 Sulzer Metco (US) Inc. Superalloy hvof powders with improved high temperature oxidation, corrosion and creep resistance
EP1272301A4 (en) * 2000-03-27 2003-05-28 Sulzer Metco Us Inc Superalloy hvof powders with improved high temperature oxidation, corrosion and creep resistance
EP1319730A1 (en) * 2001-12-17 2003-06-18 Mitsubishi Heavy Industries, Ltd. High temperature corrosion resistant alloy, thermal barrier coating material with metal bonding layer, and gas turbine using high temperature corrosion resistant alloy
US6756131B2 (en) 2001-12-17 2004-06-29 Mitsubishi Heavy Industries, Ltd. High temperature corrosion resistant alloy, thermal barrier coating material, and gas turbine using high temperature corrosion resistant alloy
WO2003060194A1 (en) * 2002-01-18 2003-07-24 Alstom Technology Ltd High-temperature protective coating
US7052782B2 (en) 2002-01-18 2006-05-30 Alstom Technology Ltd. High-temperature protection layer
CN100350075C (en) * 2002-01-18 2007-11-21 阿尔斯托姆科技有限公司 High-temperature protection layer
EP1790746A1 (en) * 2005-11-24 2007-05-30 Siemens Aktiengesellschaft Alloy, protective layer and component
CN107406919A (en) * 2015-08-25 2017-11-28 韩国机械研究院 Machinability, inoxidizability, corrosion resistance and the outstanding Co Cr class dental alloys of taste
CN107406919B (en) * 2015-08-25 2020-05-08 韩国机械研究院 Co-Cr dental alloy having excellent machinability, oxidation resistance, corrosion resistance and aesthetic properties

Also Published As

Publication number Publication date
DE69805179D1 (en) 2002-06-06
ITPR970039A1 (en) 1999-01-10
ATE217032T1 (en) 2002-05-15
EP0996752A1 (en) 2000-05-03
EP0996752B1 (en) 2002-05-02
IT1294098B1 (en) 1999-03-22
ITPR970039A0 (en) 1997-07-10
DE69805179T2 (en) 2002-11-14

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