EP1667808A2 - Method for manufacturing components with a nickel base alloy as well as components manufactured therewith - Google Patents

Method for manufacturing components with a nickel base alloy as well as components manufactured therewith

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Publication number
EP1667808A2
EP1667808A2 EP04765692A EP04765692A EP1667808A2 EP 1667808 A2 EP1667808 A2 EP 1667808A2 EP 04765692 A EP04765692 A EP 04765692A EP 04765692 A EP04765692 A EP 04765692A EP 1667808 A2 EP1667808 A2 EP 1667808A2
Authority
EP
European Patent Office
Prior art keywords
nickel
substrate core
coated
metal powder
foam body
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.)
Granted
Application number
EP04765692A
Other languages
German (de)
French (fr)
Other versions
EP1667808B1 (en
Inventor
Dirk Naumann
Gunnar Walther
Alexander BÖHM
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.)
Fraunhofer Gesellschaft zur Foerderung der Angewandten Forschung eV
Alantum Corp
Original Assignee
Vale Canada Ltd
Fraunhofer Gesellschaft zur Foerderung der Angewandten Forschung eV
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 Vale Canada Ltd, Fraunhofer Gesellschaft zur Foerderung der Angewandten Forschung eV filed Critical Vale Canada Ltd
Publication of EP1667808A2 publication Critical patent/EP1667808A2/en
Application granted granted Critical
Publication of EP1667808B1 publication Critical patent/EP1667808B1/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B22—CASTING; POWDER METALLURGY
    • B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F7/00—Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B22—CASTING; POWDER METALLURGY
    • B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F7/00—Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression
    • B22F7/002—Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression of porous nature
    • B22F7/004—Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression of porous nature comprising at least one non-porous part
    • B22F7/006—Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression of porous nature comprising at least one non-porous part the porous part being obtained by foaming
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B22—CASTING; POWDER METALLURGY
    • B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F9/00—Making metallic powder or suspensions thereof
    • B22F9/02—Making metallic powder or suspensions thereof using physical processes
    • B22F9/04—Making metallic powder or suspensions thereof using physical processes starting from solid material, e.g. by crushing, grinding or milling
    • B22F2009/041—Making metallic powder or suspensions thereof using physical processes starting from solid material, e.g. by crushing, grinding or milling by mechanical alloying, e.g. blending, milling
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B22—CASTING; POWDER METALLURGY
    • B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F2998/00—Supplementary information concerning processes or compositions relating to powder metallurgy
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B22—CASTING; POWDER METALLURGY
    • B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F2998/00—Supplementary information concerning processes or compositions relating to powder metallurgy
    • B22F2998/10—Processes characterised by the sequence of their steps
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B22—CASTING; POWDER METALLURGY
    • B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F7/00—Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression
    • B22F7/02—Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression of composite layers

Definitions

  • the invention relates to a method for manufacturing components with a nickel base alloy as well as to components manufactured with this method. With this solution, manufacturing the most differently shaped components in various three-dimensional geometries is possible.
  • the components, thus manufactured may also represent porous structures or may comprise such porous structures.
  • a substrate core consisting of pure nickel or a nickel base alloy will be provided with a surface coating at least in areas.
  • the surface coating is formed from a binding agent as well as from a metal powder.
  • the metal powder to be employed according to the invention includes additional alloy forming elements which are still to be referred to subsequently, in addition to a content of at least 20 wt% of nickel.
  • a substrate core consisting of a nickel base alloy should include nickel of at least 20 wt%.
  • the metal powder to be employed according to the invention may be a powder of the respective nickel base alloy but also a powder mixture of the respective alloy forming elements with the nickel which has been preferably subjected to high energy grinding.
  • the substrate core provided with the surface coating is subsequently subjected to a stepped thermal treatment.
  • the binding agent is expelled from the surface coating.
  • Subsequent to expelling of binder agent sintering of metal powder is then achieved.
  • sinter-fusing of a nickel substrate core and/or a solid surface coating formed of a nickel base alloy is developed.
  • the content of nickel which is included in the metal powder should be smaller than the nickel content in the substrate core material.
  • the thermal treatment should be carried out at temperatures of above 1000 °C and in a reducing or inert atmosphere, but preferably in a hydrogen atmosphere.
  • the substrate cores such one can be employed which have already substantially the geometric form of the components to be finally manufactured such that they are allowed to be completely refrained from final shaping re-machining or merely minimum re-machining of the shape is correspondingly required.
  • substrate cores can also be employed in the form of porous semi-finished products having a preferably porous structure which one may denote as foam bodies as well.
  • the surface coating should be developed with a suspension/ dispersion which is made of the binding agent, metal powder and an additional solvent, as the case may be, or is made of a liquid.
  • Such substrate cores having a porous structure are allowed to be fully immersed into such a suspension/ dispersion, and subsequently such a substrate core charged with suspension/ dispersion is allowed to be compressed in order to remove the suspension/ dispersion from the pores such that merely the webs remain wetted.
  • the stepped thermal treatment can then be carried out.
  • a binding agent which has an appropriate viscosity by means of a solvent, as the case may be, will be employed for wetting the surfaces of the porous structure of such a substrate core wherein grouting can be also carried out herein for removing excess binding agent from the pores.
  • the respective metal powder is then allowed to be deposited upon the wetted surfaces, wherein a more uniform distribution of the metal powder can be achieved by vibration. Subsequent to this, the stepped thermal treatment takes place then again.
  • bending can be carried out under compliance of defined minimum bending radii.
  • this surface area is allowed to be brought into touching contact with at least another substrate core, wherein on that occasion the adhesive effect of the binding agent can be used advantageously. Subsequent to this, the thermal treatment takes place during which a closure by adhesive force type connection of the respective substrate cores is then formed.
  • composite members can be manufactured with complex geometries, which, for example, comprise undercuts or cavities, without shaping is required to occur subsequently.
  • composite members which are formed from a substrate core having a dense structure and a substrate core having a porous structure.
  • the metal powders to be employed according to the invention may also include preferably at least 50 wt% of carbon, molybdenum, iron, cobalt, niobium, titanium, aluminium, boron, zircon, manganese, silicon and/or lanthanum in addition to nickel having a minimum content of 20 wt%.
  • the properties of the components manufactured according to the invention can also be changed in that the surface coating will be developed in a different form on defined surface areas of substrate cores.
  • This relates to the respective thickness of the surface coating which can also be carried out by means of a repeated application in a different form, on the one hand, wherein a locally different consistency of the surface coating with different contents of metal powder, compositions of metal powder and granularity of metal powder can also be provided, on the other hand.
  • the graduated alloy compositions can also be developed in the joining area which has been formed by means of the closure by adhesive force type connections.
  • Components manufactured according to the invention have a higher ductility, creep resistance and strength compared with components which have been manufactured from nickel only, wherein this circumstance also applies in comparison with nickel aluminide.
  • the tendency of oxidation compared with nickel components can be reduced as well.
  • the components achieve a thermal stability of up to 1000 ° C, wherein components manufactured according to the invention with porous structures, in particular, present such extended possibilities of application themselves, which e. g. exclude the use of foams of nickel aluminide due to the brittleness thereof.
  • the components manufactured according to the invention in particular, can be employed at higher dynamic loads.
  • a substrate core made of nickel and having the size of 300 mm * 150 mm * 1.9 mm, and having a porosity of 94 % has been immersed in an aqueous 1% solution of polyvinylpyrrolidone with a volume of 50 ml. Subsequently, pressing out on an absorbent pad has been carried out to remove the binding agent from the cavities of the pores such that merely the webs of the porous structure have been wetted.
  • the porous substrate core wetted with the binding agent has been fixed in a vibration device and has been strewed with metal powder.
  • a uniform distribution of the metal powder on the surfaces of the substrate core wetted with the binding agent could be achieved, wherein the open porosity of the structure has been maintained.
  • the metal powder comprised a composition of 0.1 wt% of carbon, 22.4 wt% of chromium, 10.0 wt% of molybdenum, 4.8 wt% of iron, 0.3 wt% of cobalt, 3.8 wt% of niobium and 58.6 wt% of nickel.
  • Such a metal powder is commercially available under the trade name of "Inconel 625".
  • the substrate core surface coated with the metal powder and binding agent has been rolled to a cylinder shaped body. On that occasion, the adhesion of the metal powder has been ensured by means of the binding agent.
  • stepped thermal treatment has been carried out wherein it has been worked in a first step inside a drying oven in a water atmosphere.
  • the temperature has been increased, while a heating rate of 5 K/min was maintained.
  • Expelling the binding agent starts at around 300° C and has been completed at 600 ° C.
  • a detention time of around 30 min should be adhered in order to ensure a complete release from the binding agent.
  • the component thus manufactured consisted of a nickel base alloy wherein the composition thereof at the surface is at least approximately equivalent to the composition of the employed metal powder.
  • the porosity is equal to 91 %.
  • the component has been oxidation-resistant at temperatures of up to 1000 ° C, comprised a high strength, creep resistance and toughness as well. After sintering, a limited deformability of the porous foam body structure was still possible considering particular minimum bending radii.
  • a corrugated sheet of pure nickel with the size of 200 mm * 200 mm * 0.15 mm has been employed as a substrate core.
  • the suspension manufactured from the metal powder and binding agent after intensive stirring has been atomized by means of compressed air, and sprayed upon the substrate core from both sides.
  • the surface coating comprised a thickness of 150 ⁇ m. After drying over a time period of 1 min, approximately, the layer comprised a sufficiently great green strength such that the stepped thermal treatment could be carried out analogous to the embodiment 1.
  • the final component comprised a nickel base alloy, wherein the alloy composition thereof at the surface was approximately equivalent to the alloy composition of the used metal powder. In the air, it was oxidation-resistant at temperatures up to 1000 ° C. The high strength, creep resistance and toughness were increased in comparison with the substrate core made of pure nickel.

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  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Composite Materials (AREA)
  • Manufacturing & Machinery (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Powder Metallurgy (AREA)

Abstract

The invention relates to a method for manufacturing components with a nickel base alloy as well as to components manufactured therewith. The respective components, in particular, are to have improved mechanical properties in comparison with the conventional solutions, and are to be producible in the most differently shaped form. During the production, proceeding takes place then such that a substrate core made of nickel or a nickel base alloy, in which nickel is included with a content of at least 20 wt%, will be coated on the surface with a binding agent as well as a metal powder in which nickel is included with a content of at least 20 wt% in addition to further alloy forming elements. Subsequently, a stepped thermal treatment is carried out in which the binding agent is expelled at first, and subsequent to this sintering of the mezai powder is performed which results in alloying up a nickel substrate core and/or which develops a solid surface coating made of nickel base alloy.

Description

Method for manufacturing components with a nickel base alloy as well as components manufactured therewith
The invention relates to a method for manufacturing components with a nickel base alloy as well as to components manufactured with this method. With this solution, manufacturing the most differently shaped components in various three-dimensional geometries is possible. The components, thus manufactured, may also represent porous structures or may comprise such porous structures.
With the nickel base alloys which are known per se, different components are allowed to be manufactured of course, wherein this can be primarily achieved with the known shaping methods. Thus, such components are allowed to be manufactured as cast parts which can be subsequently cold-worked or warm-worκed again, as the case may be. In particular during such a cutting shaping treatment, however, problems arise due to the mechanical properties of such nickel base alloys.
Furthermore, it has been proposed to modify components made of nickel by means of sintering methods, wherein the formation of solid solution or the formation of intermetallic phases ( preferentially of NiAl) should be achieved by sintering in order to achieve an improvement of the properties of such components. However, particularly in this form, the thermal properties of such components could be merely improved, and as a result the mechanical properties have not been improved in the desired form.
Therefore, it is an object of the invention to predetermine ways by means of which most differently shaped components are producible with nickel base alloys which comprise improved mechanical properties.
According to the invention, this object is solved with a method which comprises the features of claim 1. The components, thus manufactured have the features mentioned in the claims 17 and 18.
Advantageous embodiments and improvements of the invention can be achieved with the features described in the subordinate claims.
For the production of components with a nickel base alloy, the proceeding in accordance with the invention takes place such that a substrate core consisting of pure nickel or a nickel base alloy will be provided with a surface coating at least in areas. The surface coating is formed from a binding agent as well as from a metal powder. The metal powder to be employed according to the invention includes additional alloy forming elements which are still to be referred to subsequently, in addition to a content of at least 20 wt% of nickel.
A substrate core consisting of a nickel base alloy should include nickel of at least 20 wt%.
The metal powder to be employed according to the invention may be a powder of the respective nickel base alloy but also a powder mixture of the respective alloy forming elements with the nickel which has been preferably subjected to high energy grinding.
According to the invention, the substrate core provided with the surface coating is subsequently subjected to a stepped thermal treatment. On that occasion, in a first step the binding agent is expelled from the surface coating. Subsequent to expelling of binder agent sintering of metal powder is then achieved. During sintering, sinter-fusing of a nickel substrate core and/or a solid surface coating formed of a nickel base alloy is developed.
In case if a substrate core made of nickel base alloy has been employed as a semi-finished product, the content of nickel which is included in the metal powder should be smaller than the nickel content in the substrate core material.
The thermal treatment, however, at least such sintering should be carried out at temperatures of above 1000 °C and in a reducing or inert atmosphere, but preferably in a hydrogen atmosphere.
As the substrate cores such one can be employed which have already substantially the geometric form of the components to be finally manufactured such that they are allowed to be completely refrained from final shaping re-machining or merely minimum re-machining of the shape is correspondingly required.
However, with the solution according to the invention, substrate cores can also be employed in the form of porous semi-finished products having a preferably porous structure which one may denote as foam bodies as well.
In particular, with the production of such porous foam body structures the surface coating should be developed with a suspension/ dispersion which is made of the binding agent, metal powder and an additional solvent, as the case may be, or is made of a liquid.
Of course, it is also possible to deposit such suspensions/ dispersions upon non-porous substrate cores.
Such substrate cores having a porous structure are allowed to be fully immersed into such a suspension/ dispersion, and subsequently such a substrate core charged with suspension/ dispersion is allowed to be compressed in order to remove the suspension/ dispersion from the pores such that merely the webs remain wetted.
In the following, the stepped thermal treatment can then be carried out.
However, during the production of components in the form of porous foam bodies proceeding is also allowed to be such that a binding agent which has an appropriate viscosity by means of a solvent, as the case may be, will be employed for wetting the surfaces of the porous structure of such a substrate core wherein grouting can be also carried out herein for removing excess binding agent from the pores. Subsequently, the respective metal powder is then allowed to be deposited upon the wetted surfaces, wherein a more uniform distribution of the metal powder can be achieved by vibration. Subsequent to this, the stepped thermal treatment takes place then again.
It is also possible to deform substrate cores, preferentially such ones with a porous structure, after the development of surface coating and before the stepped thermal treatment.
Thus, for example, bending can be carried out under compliance of defined minimum bending radii. Thus, it is possible to manufacture hollow-cylinder shaped components or rather components shaped in a helical form.
With the solution according to the invention, however, it is also possible to readily manufacture composite members. On that occasion, proceeding is allowed to be such that at least one surface area of a substrate core will be provided with a surface coating as previously set forth.
Then, this surface area is allowed to be brought into touching contact with at least another substrate core, wherein on that occasion the adhesive effect of the binding agent can be used advantageously. Subsequent to this, the thermal treatment takes place during which a closure by adhesive force type connection of the respective substrate cores is then formed.
However, it is also possible to provide surface areas of two or several substrate cores to be connected together with closure by adhesive force with a surface coating and to bring those inro touching contact, and then to connect with closure by adhesive force by means of the thermal treatment. In this manner, composite members can be manufactured with complex geometries, which, for example, comprise undercuts or cavities, without shaping is required to occur subsequently.
However, it is also possible to manufacture composite members which are formed from a substrate core having a dense structure and a substrate core having a porous structure.
The metal powders to be employed according to the invention may also include preferably at least 50 wt% of carbon, molybdenum, iron, cobalt, niobium, titanium, aluminium, boron, zircon, manganese, silicon and/or lanthanum in addition to nickel having a minimum content of 20 wt%.
However, in addition to the respective powder composition, the properties of the components manufactured according to the invention can also be changed in that the surface coating will be developed in a different form on defined surface areas of substrate cores.
This relates to the respective thickness of the surface coating which can also be carried out by means of a repeated application in a different form, on the one hand, wherein a locally different consistency of the surface coating with different contents of metal powder, compositions of metal powder and granularity of metal powder can also be provided, on the other hand.
As a result, locally different properties on such a component manufactured according to the invention can be achieved.
With the solution according to the invention it is possible to manufacture components which comprise a graduated alloy composition starting from the surface. * Thus, for example, it is possible with the use of a substrate core made of pure nickel to manufacture a component which still has a core area of pure nickel after sintering, wherein the content of additional alloy elements changes/ increases successively towards the respective surfaces.
With the production of composite members as already mentioned, the graduated alloy compositions can also be developed in the joining area which has been formed by means of the closure by adhesive force type connections.
Components manufactured according to the invention have a higher ductility, creep resistance and strength compared with components which have been manufactured from nickel only, wherein this circumstance also applies in comparison with nickel aluminide.
The tendency of oxidation compared with nickel components can be reduced as well.
The components achieve a thermal stability of up to 1000 ° C, wherein components manufactured according to the invention with porous structures, in particular, present such extended possibilities of application themselves, which e. g. exclude the use of foams of nickel aluminide due to the brittleness thereof.
The components manufactured according to the invention, in particular, can be employed at higher dynamic loads.
In the following, the invention shall be explained by way of example. Embodiment 1
A substrate core made of nickel and having the size of 300 mm * 150 mm * 1.9 mm, and having a porosity of 94 % has been immersed in an aqueous 1% solution of polyvinylpyrrolidone with a volume of 50 ml. Subsequently, pressing out on an absorbent pad has been carried out to remove the binding agent from the cavities of the pores such that merely the webs of the porous structure have been wetted.
Subsequent to this, the porous substrate core wetted with the binding agent has been fixed in a vibration device and has been strewed with metal powder. As a result of the vibration, a uniform distribution of the metal powder on the surfaces of the substrate core wetted with the binding agent could be achieved, wherein the open porosity of the structure has been maintained.
The metal powder comprised a composition of 0.1 wt% of carbon, 22.4 wt% of chromium, 10.0 wt% of molybdenum, 4.8 wt% of iron, 0.3 wt% of cobalt, 3.8 wt% of niobium and 58.6 wt% of nickel. Such a metal powder is commercially available under the trade name of "Inconel 625".
The substrate core surface coated with the metal powder and binding agent has been rolled to a cylinder shaped body. On that occasion, the adhesion of the metal powder has been ensured by means of the binding agent.
Subsequent to this, stepped thermal treatment has been carried out wherein it has been worked in a first step inside a drying oven in a water atmosphere. The temperature has been increased, while a heating rate of 5 K/min was maintained. Expelling the binding agent starts at around 300° C and has been completed at 600 ° C. A detention time of around 30 min should be adhered in order to ensure a complete release from the binding agent.
Subsequently, sintering has been carried out in a temperature range of 1150 °C and 1250 °C with adhering detention time of around 30 min.
The component thus manufactured consisted of a nickel base alloy wherein the composition thereof at the surface is at least approximately equivalent to the composition of the employed metal powder. The porosity is equal to 91 %. In the air, the component has been oxidation-resistant at temperatures of up to 1000 ° C, comprised a high strength, creep resistance and toughness as well. After sintering, a limited deformability of the porous foam body structure was still possible considering particular minimum bending radii.
Embodiment 2
A corrugated sheet of pure nickel with the size of 200 mm * 200 mm * 0.15 mm has been employed as a substrate core.
Surface coating for this substrate core has been developed from 18 milliliters of an aqueous 6% solution of polyvinyl- pyrrolidone and a metal powder the composition thereof is equivalent to the metal powder used in the embodiment 1.
The suspension manufactured from the metal powder and binding agent after intensive stirring has been atomized by means of compressed air, and sprayed upon the substrate core from both sides. The surface coating comprised a thickness of 150 μm. After drying over a time period of 1 min, approximately, the layer comprised a sufficiently great green strength such that the stepped thermal treatment could be carried out analogous to the embodiment 1.
The final component comprised a nickel base alloy, wherein the alloy composition thereof at the surface was approximately equivalent to the alloy composition of the used metal powder. In the air, it was oxidation-resistant at temperatures up to 1000 ° C. The high strength, creep resistance and toughness were increased in comparison with the substrate core made of pure nickel.

Claims

Claims
1. A method for manufacturing components with a nickel base alloy, wherein a surface coating is deposited on a substrate core made of nickel or a nickel base alloy in which said nickel is included with a content of at least 20 wt%; with a binding agent as well as a metal powder, in which nickel is included with a content of at least 20 wt% in addition to further alloy forming elements; and said coated substrate core is subjected to a stepped thermal treatment, wherein at first said binding agent is expelled, and subsequent to this, sintering said metal powder is carried out during which alloying up said nickel substrate core and/or a solid surface coating formed of said nickel base alloy is developed.
2. A method according to claim 1, characterized in that a metal powder is used, in which the content of said nickel is smaller than the content of said nickel in a substrate core formed of said nickel base alloy.
3. A method according to claim 1 or claim 2, characterized in that a metal powder is used, in which carbon, chromium, molybdenum, iron, cobalt, niobium, titanium, aluminium, boron, zircon, manganese, silicon, and/or lanthanum is/ are included in addition to said nickel.
4. A method according to any one of the preceding claims, characterized in that a porous foam body is used as said substrate core.
5. A method according to claim 4, characterized in that said foam body is coated with a suspension/ dispersion formed of said binding agent and said metal powder, and subsequently said stepped thermal treatment is carried out.
6. A method according to claim 5, characterized in that said coated foam body is pressed for removing said suspension/ dispersion from pores of said foam body.
7. A method according to claim 4, characterized in that said foam body is coated with said binding agent, and said coated foam body is pressed- for removing said binding agent from pores of said foam body, said metal powder is deposited on said foam body wetted with said binding agent, and subsequently said stepped thermal treatment is carried out.
8. A method according to claim 7, characterized in that said foam body is vibrated during and/ or after depositing said metal powder.
9. A method according to any one of claims 4 to 8, characterized in that said coated substrate core or said foam body is deformed before said thermal treatment.
0. A method according to any one of the preceding claims, characterized in that a surface of at least said one substrate core is coated with a suspension/ dispersion, said coated surface is brought into touching contact with a surface of at least said one second substrate core, and an adhesive force type connection of said substrate cores is developed by means of said thermal treatment.
11. A method according to claim 7, characterized in that said respective surface of said second or another substrate core is coated as well.
12. A method according to any one of the preceding claims, characterized in that multiple coating is carried out on said surfaces of said substrate cores.
13. A method according to any one of the preceding claims, characterized in that areas of said substrate core are coated in a different form
14. A method according to claim 9 or claim 10, characterized in that said coating is carried out with said suspensions/ dispersions of different consistencies and/ or of a different layer thickness.
15. A method according to any one of the preceding claims, characterized in that a powder mixture is used with said nickel and powders of another alloy forming elements which have been subjected to high energy grinding.
16. A method according to any one of the preceding claims, characterized in that sintering is carried out at temperatures of above 1000 ° C, and in a reducing or inert atmosphere.
17. A component manufactured with a method according to any one of claims 1 to 16, characterized in that a graduated alloy composition starting from said surface is developed.
18. A component manufactured with a method according to any one of claims 1 to 16, characterized in that a graduated alloy composition is developed at least inside a joining area of a closure by adhesive force type connection.
EP04765692.1A 2003-09-30 2004-09-29 Method for manufacturing components with a nickel base alloy as well as components manufactured therewith Expired - Lifetime EP1667808B1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE10346281A DE10346281B4 (en) 2003-09-30 2003-09-30 Method for producing components with a nickel-based alloy and components produced therewith
PCT/EP2004/010894 WO2005037467A2 (en) 2003-09-30 2004-09-29 Method for manufacturing components with a nickel base alloy as well as components manufactured therewith

Publications (2)

Publication Number Publication Date
EP1667808A2 true EP1667808A2 (en) 2006-06-14
EP1667808B1 EP1667808B1 (en) 2016-11-09

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Country Status (9)

Country Link
US (1) US20060280637A1 (en)
EP (1) EP1667808B1 (en)
JP (1) JP4647604B2 (en)
KR (1) KR100741613B1 (en)
CN (2) CN102653001A (en)
CA (1) CA2533118C (en)
DE (1) DE10346281B4 (en)
ES (1) ES2612730T3 (en)
WO (1) WO2005037467A2 (en)

Families Citing this family (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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DE10346281B4 (en) 2006-06-22
JP4647604B2 (en) 2011-03-09
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CA2533118A1 (en) 2005-04-28
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CN1842387A (en) 2006-10-04
WO2005037467A3 (en) 2005-10-27
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