WO2016072906A1 - A cast iron article comprising a corrosion resistant layer and a method of producing said article - Google Patents
A cast iron article comprising a corrosion resistant layer and a method of producing said article Download PDFInfo
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- WO2016072906A1 WO2016072906A1 PCT/SE2015/051108 SE2015051108W WO2016072906A1 WO 2016072906 A1 WO2016072906 A1 WO 2016072906A1 SE 2015051108 W SE2015051108 W SE 2015051108W WO 2016072906 A1 WO2016072906 A1 WO 2016072906A1
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- corrosion resistant
- layer
- resistant layer
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- cast iron
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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
- 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
- C23C4/073—Metallic material containing MCrAl or MCrAlY alloys, where M is nickel, cobalt or iron, with or without non-metal elements
-
- 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
- C23C28/00—Coating for obtaining at least two superposed coatings either by methods not provided for in a single one of groups C23C2/00 - C23C26/00 or by combinations of methods provided for in subclasses C23C and C25C or C25D
- C23C28/30—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer
- C23C28/32—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one pure metallic layer
- C23C28/321—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one pure metallic layer with at least one metal alloy layer
- C23C28/3215—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one pure metallic layer with at least one metal alloy layer at least one MCrAlX layer
-
- 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
- C23C28/00—Coating for obtaining at least two superposed coatings either by methods not provided for in a single one of groups C23C2/00 - C23C26/00 or by combinations of methods provided for in subclasses C23C and C25C or C25D
- C23C28/30—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer
- C23C28/34—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one inorganic non-metallic material layer, e.g. metal carbide, nitride, boride, silicide layer and their mixtures, enamels, phosphates and sulphates
- C23C28/345—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one inorganic non-metallic material layer, e.g. metal carbide, nitride, boride, silicide layer and their mixtures, enamels, phosphates and sulphates with at least one oxide layer
- C23C28/3455—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one inorganic non-metallic material layer, e.g. metal carbide, nitride, boride, silicide layer and their mixtures, enamels, phosphates and sulphates with at least one oxide layer with a refractory ceramic layer, e.g. refractory metal oxide, ZrO2, rare earth oxides or a thermal barrier system comprising at least one refractory oxide layer
-
- 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
- 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
- C23C4/10—Oxides, borides, carbides, nitrides or silicides; Mixtures thereof
- C23C4/11—Oxides
-
- 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
- C23C6/00—Coating by casting molten material on the substrate
Definitions
- a cast iron article comprising a corrosion resitant layer and a method of producing said article
- the i nvention relates to an article comprising a cast iron bulk material and having an in ner surface delimiting an internal passage, as well as a method of producing such an article.
- Such articles are commonly used in e.g. exhaust system of a vehicle.
- An example of such an article is an exhaust manifold, which has a complex geometry including internal passages. Exhaust manifolds as well as other components in exhaust systems of internal combustion engines are subjected to a corrosive environment and to elevated temperatures. However, cast iron
- a way to partly overcome the problem with thermal losses in the exhaust system is to apply a ceramic thermal barrier coating to the outer surface of articles such as the exhaust manifold within the exhaust system. I n this way, thermal conduction from the exhaust manifold to surrou ndi ng components is prevented, but the thermal conduction from the exhaust gases to the exhaust manifold itself still leads to thermal losses in the exhaust gases. Fu rthermore, thermal fatigue is not prevented and neither is corrosion of the exhaust manifold .
- this object is achieved by means of an article as initially defined , which is characterized in that said inner surface is coated with a coating comprising a corrosion resistant layer comprising MCrAIX, wherein M is one of Fe and Ni, and wherein X is an active element, and a ceramic layer provided outside of the corrosion resistant layer.
- the article according to the invention has relatively low material costs in comparison with e.g . articles having a bulk material comprising stainless steel or superalloy. However, thanks to the internal coating , it has corrosion properties which are superior to plain cast iron articles and it is therefore suitable for use in corrosive environments such as i n exhaust systems.
- the MCrAIX layer which is preferably in the form of a distinct non-diffused layer, on one hand provides corrosion resistance and on the other hand forms an excellent bond layer for bonding the ceramic layer to the article.
- the ceramic layer is preferably a so called thermal barrier coating, providing good thermal insulation properties.
- the article according to the invention is therefore suitable for use in e.g .
- the corrosion resistant layer comprises FeCrAIX.
- FeCrAIX both the corrosion resistant layer and the bulk material are ferritic, which means that the thermal expansion properties of the bulk material and the corrosion resistant layer are essentially the same. The stability of the coating du ring thermal cycling is thereby increased .
- the corrosion resistant layer comprises between 8-1 5 % Cr by weight, preferably between 1 0- 1 4 % Cr by weig ht.
- the corrosion resistant layer has a thickness in the range 0.05-1 mm, preferably 0.05-0.5 mm , and more preferably 0.1 -0.5 m m. This thickness is sufficient to provide corrosion resistance to the article and the layer is also thin enoug h to keep the material costs low.
- the ceramic layer has a thickness in the range 0.05-1 mm, preferably 0.2-0.5 mm. With a ceramic layer of this thickness, sufficient thermal insulation properties are achieved while the material costs are kept reasonable. A too thick layer may lead to spallation while a too thin layer gives insufficient thermal insulation properties.
- the ceramic layer comprises one of a stabilized zirconiu m oxide, mullite, or forsterite. These materials are all known to have suitable thermal insulation properties.
- the ceramic layer comprises yttria-stabilized zirconia. I n this embodiment, the ceramic layer has excellent thermal i nsulation properties.
- the coating fu rther comprises an alu mina layer formed between the corrosion resistant layer and the cast iron bulk material.
- the alumina layer reduces the risk of formi ng chromium carbides in the interface between the cast iron bulk material and the corrosion resistant layer due to carbon diffusion . Ch romium carbides may otherwise embrittle the corrosion resistant layer material close to the bulk material and thereby reduce the ad hesion of the layer. I n this embodiment, the alumina layer protects the corrosion resistant layer material from embrittlement and the adhesion of the corrosion resistant layer is improved.
- the alumina layer has a thickness of less than 500 nm, preferably less than 200 nm. An alu mina layer of this thickness is sufficient to form an efficient barrier for carbon diffusion.
- the article is an exhaust manifold. Advantages and advantageous featu res of such an exhaust manifold are as listed above. According to a second aspect of the invention , the above mentioned object is achieved by means of a method of producing an article comprising a cast i ron bulk material and havi ng an inner su rface delimiting an internal passage, comprising the steps :
- a corrosion resistant layer comprising MCrAIX onto the ceramic layer, wherein M is one of Fe and Ni, and wherei n X is an active element,
- the corrosion resistant layer has a much hig her melting temperatu re than the cast iron bulk material, typically about 1 500 °C as compared to a pouring temperature of 1 350 °C, and MCrAIX therefore forms a distinct and non-diffused layer on the inner surface of the bulk material.
- cast iron articles of complicated geometry can be formed with a thermally insulating and corrosion resistant coating on an internal su rface of the article.
- the corrosion resistant layer apart from protecting against corrosion , forms an excellent bond layer for bonding the ceramic layer onto the article. Therefore, the application of a corrosion resistant layer is crucial for the quality of the ceramic layer and is a prerequisite for obtaining the thermally insulating properties offered by the ceramic layer. Without the corrosion resistant MCrAIX layer, the adhesion of the ceramic layer to the cast i ron bulk material will be too poor.
- the method fu rther comprises the step :
- thermal spraying is used in the step of applying a ceramic layer.
- Thermal spraying includes e.g . plasma spraying , flame spraying, wire arc spraying, etc.
- Thermal spraying is an efficient way of applying a coati ng in the form of a ceramic layer of a desired thickness on the core, which may be e.g. a sand core or the like.
- thermal spraying is used in the step of applying a corrosion resistant layer. This is an efficient way of applyi ng a coati ng in the form of a corrosion resistant layer of a desired thickness on top of the ceramic layer.
- Fig. 1 schematically shows a cross section of an article according to the invention
- Fig.2 schematically shows a partial cross section of an article according to the invention
- Fig.3 shows a flow chart of a method according to the invention.
- An article 1 according to a first embodiment of the invention is schematically shown in cross section in fig. 1.
- the article 1 is formed with an internal passage 2 and comprises a cast iron bulk material 3, a corrosion resistant layer 4 applied on the cast iron bulk material 3 on its side facing the internal passage 2, and a ceramic layer 5 applied on the corrosion resistant layer 4.
- the corrosion resistant layer 4 is preferably in the form of a ferritic FeCrAIX layer, wherein X is one or more of Hf, Y, Ti, Zr, La, Th, Ce, or one or more other reactive elements known in the art.
- the FeCrAIX corrosion resistant layer 4 on one hand prevents corrosion of the cast iron bulk material 3 and on one hand increases the adhesion of the ceramic layer 5.
- the corrosion resistant layer 4 preferably has a thickness in the range 0.05-1 mm, preferably 0.05-0.5 mm, and more preferably 0.1 -0.5 mm. Since the FeCrAIX corrosion resistant layer 4 is in direct contact with the cast i ron bulk material 3, it is preferable to use a FeCrAIX comprising between 8-1 5 % Cr by weig ht, preferably between 1 0-1 4 % Cr by weig ht. Typically, the FeCrAIX layer may comprise about 1 0 % Cr by weight.
- the ceramic layer 5 has approximately the same thickness as the corrosion resistant layer 4 and is a thermal barrier layer in the form of e.g. a stabilized zirconiu m oxide, preferably yttria-stabilized zirconia, mullite, or forsterite.
- a partial cross section of an article 1 according to a second embodiment is schematically shown i n fig . 2.
- the article 1 comprises a cast iron bulk material 3, a corrosion resistant layer 4 i n the form of a FeCrAIX layer, wherein X is chosen according to above, and a ceramic layer 5 applied on the corrosion resistant layer 4.
- the article 1 in this second embodiment differs from the article 1 according to the first embodiment in that between the corrosion resistant layer 4 and the cast iron bulk material 3, a thin alumina layer 6 is formed .
- the alumina layer 6 acts as a barrier layer against carbon diffusion into the FeCrAIX layer 4 and thereby prevents embrittlement of the FeCrAIX layer 4 close to the bulk material 3.
- the chromiu m content in the corrosion resistant FeCrAIX layer 4 may be increased to arou nd 20-22 % by weight, which i mproves the corrosion resistance of the article 1 .
- the alumina layer 6 has a thickness of less than 500 n m, preferably less than 200 nm.
- an article 1 is formed by means of a casting process.
- the method is schematically illustrated as a flow chart in fig . 3.
- a core for defining an internal passage 2 in the article 1 is formed .
- the core can be e.g . a resin bonded sand core or similar.
- a ceramic layer 5, preferably in the form of an yttria-stabilized zirconia layer, is applied onto the core, e.g . by thermal spraying using any of plasma spraying, flame spraying , wire arc spraying, etc.
- a corrosion resistant layer 4 comprising e.g .
- FeCrAIX wherein X is one or more of Hf, Y, Ti, Zr, La, Th, Ce, or one or more other reactive elements known in the art, is applied by thermal spraying in a step S3.
- X is one or more of Hf, Y, Ti, Zr, La, Th, Ce, or one or more other reactive elements known in the art.
- the corrosion resistant layer 4 is subjected to an oxidization , whereby a thin alu mina layer 6 is formed on top of the corrosion resistant FeCrAIX layer 4.
- the core is assembled into a mold in a step S5, and iron is cast into the mold at a pouring temperatu re of approximately 1 350 °C in a step S6 to form the article 1 .
- the pou ring temperature is lower than the melting temperature of the corrosion resistant layer 4, which for FeCrAIX is typically around 1 500 °C, so the corrosion resistant layer 4 thereby forms a non-diffused distinct layer on the cast iron bulk material 3.
- the core is removed and the internal passage 2 is formed .
- the article 1 formed according to the method comprises a cast iron bulk material 3, and on its inner surface a coating comprising a thin alu mina layer 6, a corrosion resistant layer 4 and a ceramic layer 5 is formed .
- the internal passages in which exhaust gases flow are covered with a ceramic layer acting as a thermal barrier between the exhaust gases and the bulk material, a corrosion resistant layer bonding the ceramic layer to the bulk material and preventi ng corrosion of the bulk material, and optionally an alumina layer preventing formation of chromiu m carbides in the corrosion resistant layer.
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- Chemical Kinetics & Catalysis (AREA)
- Physics & Mathematics (AREA)
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- Coating By Spraying Or Casting (AREA)
Abstract
An article (1 ) comprising a cast iron bulk material (3) and having an inner surface delimiting an internal passage (2), said inner surface being coated with a coating comprising a corrosion resistant layer (4) comprising MCrAlX, wherein M is Fe, and wherein X is an active element, and a ceramic layer (5) provided outside of the corrosion resistant layer. A method of forming such an article comprises forming a core and applying a ceramic layer and a corrosion resistant layer comprising MCrAlX, wherein M is one of Fe and Ni, and wherein X is an active element, onto the core, assembling the core into a mold, casting iron into the mold at a pouring temperature lower than the melting temperature of the corrosion resistant layer to form said article, and removing the core.
Description
A cast iron article comprising a corrosion resitant layer and a method of producing said article
FI ELD OF TH E I NVENTION AN D P RIOR ART
5
The i nvention relates to an article comprising a cast iron bulk material and having an in ner surface delimiting an internal passage, as well as a method of producing such an article. Such articles are commonly used in e.g. exhaust system of a vehicle.
10 An example of such an article is an exhaust manifold, which has a complex geometry including internal passages. Exhaust manifolds as well as other components in exhaust systems of internal combustion engines are subjected to a corrosive environment and to elevated temperatures. However, cast iron
15 articles are sensitive to corrosion , which reduces the service life of the article and impairs the mechanical properties. Cast iron articles also show relatively high thermal conductivity. Hot exhaust gases flowing throug h the i nternal passages of an exhaust manifold made from cast iron therefore lose thermal
20 energy by heat conduction to the exhaust manifold and surrou nding areas. Large thermal losses are thus present in the exhaust system, which reduce the efficiency of the engine. Moreover, the large temperature variations present in the exhaust system may lead to thermal fatigue of the exhaust
25 manifold , reducing its service life. Cast iron is however a relatively inexpensive material in comparison with more corrosion resistant alloys and it is therefore a common choice of material to keep the material costs low.
A way to partly overcome the problem with thermal losses in the exhaust system is to apply a ceramic thermal barrier coating to the outer surface of articles such as the exhaust manifold within the exhaust system. I n this way, thermal conduction from the exhaust manifold to surrou ndi ng components is prevented, but the thermal conduction from the exhaust gases to the exhaust manifold itself still leads to thermal losses in the exhaust gases. Fu rthermore, thermal fatigue is not prevented and neither is corrosion of the exhaust manifold .
Alternative materials such as superalloys and stainless steel are relatively expensive and are therefore not suitable for use in exhaust systems of combustion engines in vehicles such as trucks, buses, cars, etc.
SUMMARY OF TH E I NVENTION
It is an object of the present invention to provide on one hand an article comprising a cast iron bulk material and having an internal passage, and on the other hand a method of producing such an article, which article and method in at least some aspect are improved with respect to known such articles and methods. I n particular, it is an object to provide such an article which has improved corrosion resistance and thermal insulation properties in comparison with standard cast iron articles havi ng an internal passage.
In the case of the article, this object is achieved by means of an article as initially defined , which is characterized in that said
inner surface is coated with a coating comprising a corrosion resistant layer comprising MCrAIX, wherein M is one of Fe and Ni, and wherein X is an active element, and a ceramic layer provided outside of the corrosion resistant layer.
The article according to the invention has relatively low material costs in comparison with e.g . articles having a bulk material comprising stainless steel or superalloy. However, thanks to the internal coating , it has corrosion properties which are superior to plain cast iron articles and it is therefore suitable for use in corrosive environments such as i n exhaust systems. The MCrAIX layer, which is preferably in the form of a distinct non-diffused layer, on one hand provides corrosion resistance and on the other hand forms an excellent bond layer for bonding the ceramic layer to the article. The ceramic layer is preferably a so called thermal barrier coating, providing good thermal insulation properties. The article according to the invention is therefore suitable for use in e.g . exhaust systems of combustion engines, in which exhaust gases of elevated temperature flows throug h the internal passage of the article. The ceramic coating prevents thermal conduction from the exhaust gases to the bulk material of the article. It therefore efficiently minimizes power losses in the exhaust system and thereby increases the efficiency of the engine. It also increases the corrosion resistance of the bulk material, since corrosion is generally promoted at high temperatu res. Thereby, also the mechanical properties of the article are i mproved with respect to plain cast i ron articles.
According to the invention , the corrosion resistant layer comprises FeCrAIX. By using FeCrAIX, both the corrosion
resistant layer and the bulk material are ferritic, which means that the thermal expansion properties of the bulk material and the corrosion resistant layer are essentially the same. The stability of the coating du ring thermal cycling is thereby increased .
According to the invention , the corrosion resistant layer comprises between 8-1 5 % Cr by weight, preferably between 1 0- 1 4 % Cr by weig ht. By keeping the ch romiu m content of the corrosion resistant layer relatively low, the risk of forming chromium carbides in the interface between the cast iron bulk material and the corrosion resistant layer is reduced. This is thus an alternative way to prevent the bulk material from embrittlement and to improve the ad hesion of the corrosion resistant layer. Of course, an alu mina layer may additionally be formed between the bulk material and the corrosion resistant layer to further reduce the risk of forming chromiu m carbides.
According to an embodiment of the invention, the corrosion resistant layer has a thickness in the range 0.05-1 mm, preferably 0.05-0.5 mm , and more preferably 0.1 -0.5 m m. This thickness is sufficient to provide corrosion resistance to the article and the layer is also thin enoug h to keep the material costs low. According to an embodiment of the invention , the ceramic layer has a thickness in the range 0.05-1 mm, preferably 0.2-0.5 mm. With a ceramic layer of this thickness, sufficient thermal insulation properties are achieved while the material costs are kept reasonable. A too thick layer may lead to spallation while a too thin layer gives insufficient thermal insulation properties.
According to an embodiment of the invention , the ceramic layer comprises one of a stabilized zirconiu m oxide, mullite, or forsterite. These materials are all known to have suitable thermal insulation properties.
According to an embodiment of the invention , the ceramic layer comprises yttria-stabilized zirconia. I n this embodiment, the ceramic layer has excellent thermal i nsulation properties.
According to an embodi ment of the i nvention, the coating fu rther comprises an alu mina layer formed between the corrosion resistant layer and the cast iron bulk material. The alumina layer reduces the risk of formi ng chromium carbides in the interface between the cast iron bulk material and the corrosion resistant layer due to carbon diffusion . Ch romium carbides may otherwise embrittle the corrosion resistant layer material close to the bulk material and thereby reduce the ad hesion of the layer. I n this embodiment, the alumina layer protects the corrosion resistant layer material from embrittlement and the adhesion of the corrosion resistant layer is improved.
According to an embodiment of the invention , the alumina layer has a thickness of less than 500 nm, preferably less than 200 nm. An alu mina layer of this thickness is sufficient to form an efficient barrier for carbon diffusion.
According to an embodiment of the invention, the article is an exhaust manifold. Advantages and advantageous featu res of such an exhaust manifold are as listed above.
According to a second aspect of the invention , the above mentioned object is achieved by means of a method of producing an article comprising a cast i ron bulk material and havi ng an inner su rface delimiting an internal passage, comprising the steps :
forming a core for defi ning the internal passage,
applying a ceramic layer onto the core,
applying a corrosion resistant layer comprising MCrAIX onto the ceramic layer, wherein M is one of Fe and Ni, and wherei n X is an active element,
assembling the core into a mold ,
casting iron into the mold to form said article, and
removi ng the core.
The corrosion resistant layer has a much hig her melting temperatu re than the cast iron bulk material, typically about 1 500 °C as compared to a pouring temperature of 1 350 °C, and MCrAIX therefore forms a distinct and non-diffused layer on the inner surface of the bulk material. By means of the inventive method, cast iron articles of complicated geometry can be formed with a thermally insulating and corrosion resistant coating on an internal su rface of the article. The corrosion resistant layer, apart from protecting against corrosion , forms an excellent bond layer for bonding the ceramic layer onto the article. Therefore, the application of a corrosion resistant layer is crucial for the quality of the ceramic layer and is a prerequisite for obtaining the thermally insulating properties offered by the ceramic layer. Without the corrosion resistant MCrAIX layer, the adhesion of the ceramic layer to the cast i ron bulk material will be too poor.
According to an embodiment of this aspect of the i nvention , the method fu rther comprises the step :
oxidizing the corrosion resistant layer before casting iron into the mold , such that an alu mina layer is formed between the corrosion resistant layer and the cast i ron bulk material. I n this way, the risk of forming ch romiu m carbides in the interface between the cast iron bulk material and the corrosion resistant layer is reduced. Thereby, the bulk material is protected from embrittlement and the adhesion of the corrosion resistant layer is improved .
According to an embodiment of this aspect of the invention, thermal spraying is used in the step of applying a ceramic layer. Thermal spraying includes e.g . plasma spraying , flame spraying, wire arc spraying, etc. Thermal spraying is an efficient way of applying a coati ng in the form of a ceramic layer of a desired thickness on the core, which may be e.g. a sand core or the like.
According to an embodiment of this aspect of the invention, thermal spraying is used in the step of applying a corrosion resistant layer. This is an efficient way of applyi ng a coati ng in the form of a corrosion resistant layer of a desired thickness on top of the ceramic layer.
Other advantageous featu res as well as advantages present invention will appear from the following description
BRIEF DESCRIPTION OF THE DRAWINGS
The invention will in the following be further described by means of example with reference to the appended drawings, wherein
Fig. 1 schematically shows a cross section of an article according to the invention,
Fig.2 schematically shows a partial cross section of an article according to the invention, and
Fig.3 shows a flow chart of a method according to the invention.
DETAILED DESCRIPTION OF EMBODIMENTS OF THE INVENTION
An article 1 according to a first embodiment of the invention is schematically shown in cross section in fig. 1. The article 1 is formed with an internal passage 2 and comprises a cast iron bulk material 3, a corrosion resistant layer 4 applied on the cast iron bulk material 3 on its side facing the internal passage 2, and a ceramic layer 5 applied on the corrosion resistant layer 4. In the shown embodiment, the corrosion resistant layer 4 is preferably in the form of a ferritic FeCrAIX layer, wherein X is one or more of Hf, Y, Ti, Zr, La, Th, Ce, or one or more other reactive elements known in the art. The FeCrAIX corrosion resistant layer 4 on one hand prevents corrosion of the cast iron bulk material 3 and on one hand increases the adhesion of the ceramic layer 5. The corrosion resistant layer 4 preferably has a thickness in the range 0.05-1 mm, preferably 0.05-0.5 mm, and more preferably
0.1 -0.5 mm. Since the FeCrAIX corrosion resistant layer 4 is in direct contact with the cast i ron bulk material 3, it is preferable to use a FeCrAIX comprising between 8-1 5 % Cr by weig ht, preferably between 1 0-1 4 % Cr by weig ht. Typically, the FeCrAIX layer may comprise about 1 0 % Cr by weight. With this relatively low ch romiu m content, the risk of forming chromium carbides in the interface between the corrosion resistant layer 4 and the cast iron bulk material 3 is reduced, and thereby also the risk of embrittlement of the corrosion resistant layer 4. The ceramic layer 5 has approximately the same thickness as the corrosion resistant layer 4 and is a thermal barrier layer in the form of e.g. a stabilized zirconiu m oxide, preferably yttria-stabilized zirconia, mullite, or forsterite. A partial cross section of an article 1 according to a second embodiment is schematically shown i n fig . 2. I n this embodiment, the article 1 comprises a cast iron bulk material 3, a corrosion resistant layer 4 i n the form of a FeCrAIX layer, wherein X is chosen according to above, and a ceramic layer 5 applied on the corrosion resistant layer 4. The article 1 in this second embodiment differs from the article 1 according to the first embodiment in that between the corrosion resistant layer 4 and the cast iron bulk material 3, a thin alumina layer 6 is formed . The alumina layer 6 acts as a barrier layer against carbon diffusion into the FeCrAIX layer 4 and thereby prevents embrittlement of the FeCrAIX layer 4 close to the bulk material 3. Thus, in this embodiment, the chromiu m content in the corrosion resistant FeCrAIX layer 4 may be increased to arou nd 20-22 % by weight, which i mproves the corrosion resistance of the article
1 . The alumina layer 6 has a thickness of less than 500 n m, preferably less than 200 nm.
In a method according to the invention, an article 1 is formed by means of a casting process. The method is schematically illustrated as a flow chart in fig . 3. I n a first step S1 , a core for defining an internal passage 2 in the article 1 is formed . The core can be e.g . a resin bonded sand core or similar. In a step S2, a ceramic layer 5, preferably in the form of an yttria-stabilized zirconia layer, is applied onto the core, e.g . by thermal spraying using any of plasma spraying, flame spraying , wire arc spraying, etc. After applyi ng the ceramic layer 5, a corrosion resistant layer 4 comprising e.g . FeCrAIX, wherein X is one or more of Hf, Y, Ti, Zr, La, Th, Ce, or one or more other reactive elements known in the art, is applied by thermal spraying in a step S3. I n an optional step S4, the corrosion resistant layer 4 is subjected to an oxidization , whereby a thin alu mina layer 6 is formed on top of the corrosion resistant FeCrAIX layer 4. Thereafter, the core is assembled into a mold in a step S5, and iron is cast into the mold at a pouring temperatu re of approximately 1 350 °C in a step S6 to form the article 1 . The pou ring temperature is lower than the melting temperature of the corrosion resistant layer 4, which for FeCrAIX is typically around 1 500 °C, so the corrosion resistant layer 4 thereby forms a non-diffused distinct layer on the cast iron bulk material 3. I n a step S7, the core is removed and the internal passage 2 is formed . The article 1 formed according to the method comprises a cast iron bulk material 3, and on its inner surface a coating comprising a thin alu mina layer 6, a corrosion resistant layer 4 and a ceramic layer 5 is formed .
In a cast iron exhaust manifold accordi ng to the invention , the internal passages in which exhaust gases flow are covered with a ceramic layer acting as a thermal barrier between the exhaust gases and the bulk material, a corrosion resistant layer bonding the ceramic layer to the bulk material and preventi ng corrosion of the bulk material, and optionally an alumina layer preventing formation of chromiu m carbides in the corrosion resistant layer.
The invention is of cou rse not in any way restricted to the em- bodiments described above, but many possibilities to modifications thereof would be apparent to a person with skill in the art without departi ng from the scope of the invention as defined in the appended clai ms.
Claims
1 . An article (1 ) comprising a cast iron bulk material (3) and having an in ner su rface deli miting an internal passage (2) , wherein said in ner surface is coated with a coating comprising : a corrosion resistant layer (4) comprising MCrAIX, wherein M is one of Fe and Ni, and wherein X is an active element, and a ceramic layer (5) provided outside of the corrosion resistant layer (4),
characterized in
that the corrosion resistant layer (4) comprises FeCrAIX, and that the corrosion resistant layer (4) comprises between 8-1 5 % Cr by weig ht.
2. The article according to claim 1 , wherein the corrosion resistant layer (4) has a thickness i n the range 0.05-1 mm, preferably 0.05-0.5 mm , and more preferably 0.1 -0.5 mm .
3. The article according to claim 1 or 2, wherein the ceramic layer (5) has a thickness in the range 0.05-1 mm, preferably 0.2-
0.5 mm .
4. The article according to any of the preceding claims, wherein the ceramic layer (5) comprises one of a stabilized zirconium oxide, mullite, or forsterite.
5. The article according to claim 4, wherei n the ceramic layer (5) comprises yttria-stabilized zirconia.
6. The article according to any of the preceding claims, wherein the coating further comprises an alu mina layer (6)
formed between the corrosion resistant layer (4) and the cast iron bulk material (3) .
7. The article according to claim 6, wherei n the alumina layer (6) has a thickness of less than 500 nm, preferably less than 200 nm.
8. The article according to any of the preceding claims, wherein the corrosion resistant layer (4) comprises between 1 0- 1 4 % Cr by weight.
9. An article according to any of the preceding claims, wherein the article is an exhaust manifold.
1 0. A method of producing an article (1 ) comprising a cast iron bulk material (3) and having an inner surface delimiti ng an internal passage (2), comprising the steps :
forming a core for defining the internal passage (2) , applyi ng a ceramic layer (5) onto the core,
applyi ng a corrosion resistant layer (4) comprising MCrAIX onto the ceramic layer (5) , wherein M is one of Fe and Ni, and wherein X is an active element,
assembling the core into a mold,
casting iron into the mold at a pouring temperature lower than the melti ng temperature of the corrosion resistant layer (4) to form said article (1 ) , and
removing the core.
1 1 . The method according to claim 1 0, fu rther comprising the step :
oxidizing the corrosion resistant layer (4) before casting iron into the mold, such that an alu mina layer (6) is formed between the corrosion resistant layer (4) and the cast iron bulk material (3) .
1 2. The method according to any of the claims 1 0-1 1 , wherein thermal spraying is used in the step of applying a ceramic layer (5).
1 3. The method according to any of the claims 1 0-1 2, wherein thermal spraying is used in the step of applying a corrosion resistant layer (4).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE112015004365.9T DE112015004365B4 (en) | 2014-10-27 | 2015-10-19 | Cast iron article having a corrosion resistant layer and method of making the article |
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| SE1451283A SE538682C2 (en) | 2014-10-27 | 2014-10-27 | A cast iron article with a corrosion resistant layer and a method of producing said article |
| SE1451283-4 | 2014-10-27 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| WO2016072906A1 true WO2016072906A1 (en) | 2016-05-12 |
Family
ID=55909490
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| PCT/SE2015/051108 Ceased WO2016072906A1 (en) | 2014-10-27 | 2015-10-19 | A cast iron article comprising a corrosion resistant layer and a method of producing said article |
Country Status (3)
| Country | Link |
|---|---|
| DE (1) | DE112015004365B4 (en) |
| SE (1) | SE538682C2 (en) |
| WO (1) | WO2016072906A1 (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN116848284A (en) * | 2021-01-22 | 2023-10-03 | 欧瑞康美科股份公司,沃伦 | Transplanted Thermal Barrier Coating System |
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| DE59505454D1 (en) * | 1994-10-14 | 1999-04-29 | Siemens Ag | PROTECTIVE LAYER FOR PROTECTING A COMPONENT AGAINST CORROSION, OXIDATION AND THERMAL OVERLOAD AND METHOD FOR THEIR PRODUCTION |
| WO2005108747A1 (en) * | 2004-05-12 | 2005-11-17 | Honeywell International Inc. | Turbocharger with reduced thermal inertia and method of producing the same |
| EP2511394B1 (en) * | 2011-04-15 | 2015-05-27 | Siemens Aktiengesellschaft | Cast iron with niobium and component |
| US9228462B2 (en) * | 2014-02-06 | 2016-01-05 | Caterpillar Inc. | Jacket-cooled exhaust manifold |
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2014
- 2014-10-27 SE SE1451283A patent/SE538682C2/en unknown
-
2015
- 2015-10-19 DE DE112015004365.9T patent/DE112015004365B4/en active Active
- 2015-10-19 WO PCT/SE2015/051108 patent/WO2016072906A1/en not_active Ceased
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| US5384200A (en) * | 1991-12-24 | 1995-01-24 | Detroit Diesel Corporation | Thermal barrier coating and method of depositing the same on combustion chamber component surfaces |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN116848284A (en) * | 2021-01-22 | 2023-10-03 | 欧瑞康美科股份公司,沃伦 | Transplanted Thermal Barrier Coating System |
Also Published As
| Publication number | Publication date |
|---|---|
| DE112015004365B4 (en) | 2020-09-24 |
| DE112015004365T5 (en) | 2017-06-14 |
| SE538682C2 (en) | 2016-10-18 |
| SE1451283A1 (en) | 2016-04-28 |
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