• 专利附录
  • 专利说明
  • 权利要求
  • 类似技术
  • 同族专利
  • 引用文献
  • 法律状态
  • 优先权
    • 专利摘要:
    The invention relates to a method for producing a connection between a first metallic component (2) and a second metallic component (3), wherein at least one of the two metallic components (2, 3) is made of a sintered material by powder metallurgy and the connection in between the two metallic components (2, 3) formed connection area (4) is produced by soldering. The surface (9) of the metallic component (2 or 3) made of the sintered material, which also forms the connection region (4), is compressed to a density of at least 95% of the solid material density before the soldering.
    公开号:AT521546A1
    申请号:T50686/2018
    申请日:2018-08-10
    公开日:2020-02-15
    发明作者:
    申请人:Miba Sinter Austria Gmbh；
    IPC主号:
    专利说明:

    The invention relates to a method for producing a connection between a first metallic component and a second metallic component, wherein at least one of the two metallic components is made of a sintered material by powder metallurgy and the connection is produced in a connection area formed between the two metallic components by soldering.
    The invention further relates to an assembly comprising a first metallic component and a second metallic component, at least one of the two metallic components being made from a sintered material by powder metallurgy, and the two components being soldered to one another in a connection region.
    Joining components made of sintered materials to one another sometimes reaches the limits of the bond strengths that can usually be achieved. This applies in particular to sintered materials that are difficult to process by powder metallurgy, such as, for example, stainless steel powder or hard metal powder. In order to obtain applicable connection strengths, a wide variety of approaches have already been described in the prior art.
    For example, the DD 283 160 A5 hard metal alloy consisting of one or more hard material phases of carbides of the metals of IV., V. and VI. Sub-group of the PSE, preferably made of tungsten carbide, and a binder metal phase made of cobalt, nickel or iron or from alloys of these metals with a proportion of 2.5 to 30% by mass, with the exception of austenitic binder metal alloys, the starting powder mixture or the hard metal batch being 0.5 up to 5% by mass
    N2018 / 18300-AT-00
    2/18
    Contains manganese or manganese oxide. According to the description of this document, this hard metal alloy can be used particularly inexpensively where, on the one hand, oxide-free and non-binding metal-depleted surfaces are necessary and, on the other hand, a high level of mechanical properties such as hardness and fracture toughness are required.
    DE 37 34 002 A1 describes a method for producing a component composed of sintered iron or sintered steel, according to which bores and pegs are formed from iron or steel powder, the molded parts are put together to form a component and the parts are made by applying one Magnetite layer are cohesively connected to each other on their surface. This is to avoid the need to use expensive solders that only wet the surface of the sintered component.
    Exactly the opposite is described in DE 44 04 406 A1, a solder for soldering porous sintered steels, in which alloy components diffuse into the material in the molten state and thereby cause the solder to solidify in the pores. A solder which can be used universally consists of 1 to 6% by weight of silicon, 0.1 to 1.5% by weight of boron, 0 to 25% by weight of iron and 0 to 20% by weight of nickel, the rest being copper.
    The present invention has for its object to provide a way with which components made of sintered materials can be easily soldered under industrial conditions.
    The object of the invention is achieved with the above-mentioned method, according to which the surface of the metallic component made of the sintered material, which also forms the connection area, is compacted prior to soldering.
    The object of the invention is further achieved with the assembly mentioned at the outset, in which the metallic component, which is produced from the sintered material, is surface-densified in the connection area.
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    With the surface compression of the connection area of the sintered component, the pores on the surface of the metallic component are closed. This means that a significantly smaller amount or no solder penetrates into the pores. A significantly smaller amount of solder is therefore consumed, since the solder is not drawn off from the connection area, as a result of which the connection quality would ultimately suffer. In addition, the increase in weight of the component as a result of the connection process can also be avoided, as a result of which an increase in the weight force which acts on the connection point and thus also on the other component can be avoided. It is therefore not necessary to take into account a weight increase as a result of the further processing of the sintered component during the manufacture of the sintered component, as a result of which the material selection for the sintered component can be simplified or more possible sintered powders are available. In addition, the application of the solder can be simplified on an industrial scale, since there is no longer any fear of fluctuations in the quantity of solder in the joint gap.
    The compression of the surface of the component which is made of a sintered material by powder metallurgy and which forms the connecting region is preferably carried out to a density of at least 99.5% of the solid material density, so that the component in this region therefore has at least 99.5% of the solid material density, in order to thus cite the aforementioned To further improve effects or to increase the certainty that the solder does not infiltrate the sintered component or infiltrate in negligibly small amounts.
    The surface of the component, which is made of a sintered material and is powder metallurgically produced, is preferably compacted by means of blasting. It can be used to compress relatively precisely those areas that are required for producing the composite with the other component. The remaining areas of the sintered component, however, can retain their original properties.
    A steel powder made of stainless steel produced by gas atomization is particularly preferably used as the blasting agent for the blasting. It could namely be demonstrated in the evaluation of the invention that with this abrasive
    N2018 / 18300-AT-00
    4/18 compared to other blasting agents, significantly higher densities can be achieved, so that the sintered component can have a density in this area that corresponds to 100% of the full density.
    A copper solder is preferably used as the solder for soldering the two metallic components together. This has proven to be favorable with regard to the industrial processing of sintered components, since it can be applied in paste form and can then be automatically melted into the connection point by simple temperature treatment without manual manipulation being necessary.
    According to another embodiment variant of the invention, it can be provided that the metallic component, which is made of the sintered material, has a compressed layer in the connection area, which has a layer thickness between 50 μm and 350 μm. With such a thick, compact surface layer of the sintered component, the security of avoiding infiltration of the component with the solder can be increased, so that minor damage to the surface of the component due to its manipulation during processing is not a problem for the improved connection formation.
    For the reasons mentioned above, according to another embodiment variant of the assembly, it can be provided that the metallic component, which is produced from the sintered material, has a solder content of at most 0.1% by volume in the connection area.
    For a better understanding of the invention, this will be explained in more detail with reference to the following figures.
    Each show in a highly simplified, schematic representation:
    Figure 1 shows an assembly of two metallic components in section.
    FIG. 2 shows an enlarged detail of the assembly according to FIG. 1.
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    In the introduction, it should be noted that in the differently described embodiments, the same parts are provided with the same reference numerals or the same component names, and the disclosures contained in the entire description can be applied analogously to the same parts with the same reference numbers or the same component names. The location information selected in the description, e.g. above, below, to the side, etc., referring to the figure described and illustrated immediately, and if the position is changed, these are to be applied to the new position.
    1 shows an embodiment variant of an assembly 1, which comprises or consists of a first metallic component 2 and a second metallic component 3. At least one of the two components 2, 3 is made of a sintered material by powder metallurgy. In the embodiment variant shown, this is the first metallic component 2, which is a fastening element for the second metallic component 3, in particular a screw socket, for which purpose this has a continuous bore running in the direction of the longitudinal central axis for receiving a connecting element, in particular a screw. In the embodiment variant shown, the second metallic component 3 is a pipeline, for example a fuel line. Furthermore, the second metallic component 3 or generally the component that is not manufactured by powder metallurgy (unless both metallic components 2, 3 are manufactured by powder metallurgy from a sintered material), for example a cast part, in particular consist of a steel.
    The assembly 1 or its metallic components 2, 3 can also be provided for another application, for example for exhaust systems or lubricant lines in plant construction.
    The first metallic component 2 is connected to the second metallic component 3 by soldering. For this purpose, a connection area 4 (a joining gap) is formed between the two metallic components 2, 3, in which a solder 5, with which the integral connection between the two metallic components 2, 3 is made, is received, as can be better seen in FIG. 2 can be seen, which shows the connection area 4 in a larger representation.
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    It should be mentioned at this point that the first metallic component 2 has a recess for partially accommodating the second metallic component 3, as can be seen from FIGS. 1 and 2. In particular, this recess has a curvature that at least approximately corresponds to the curvature of the second metallic component 3. The connection area 4 can also have a shape other than that shown in FIGS. 1 and 2.
    The first metallic component 2 or generally the component produced by powder metallurgy can be produced by a conventional sintering process. Since this is known per se, it should only be mentioned here so much that this method comprises the steps of powder mixing, powder pressing to form a green compact, single- or multi-stage sintering and, if necessary, mechanical finishing, such as Deburring. The parameters to be used in each case are directed, inter alia, according to the powder used and are known to the person skilled in the art, so that reference is made here to avoid repetition to the relevant prior art.
    In the following, reference is only made to a component produced by powder metallurgy, that is to say a sintered component. This also includes the first metallic component 2.
    Following the sintering, it is now provided that the powder-metallurgically manufactured component is compressed in the connection area 4. In principle, the compression can also be carried out further, so that not only a surface area 6 of the sintered component is compressed in the connection area 4, but also areas adjoining it. However, this is not absolutely necessary for the formation of the connection between the two metallic components 2, 3, since no solder 5 is applied at these points.
    The surface area 6 of the component produced by powder metallurgy can be compressed by various methods, for example by means of pressing or rolling.
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    In the preferred variant of the method, the compaction is carried out by blasting a blasting medium. In addition to compaction, blasting can also increase the hardness of the powder-metallurgically manufactured component in this area by cold working the surface.
    For example, scrap particles, gravel, etc., can be used as the abrasive. The particles of the abrasive can have an elongated shape, an acicular shape, an irregular shape, a polygonal shape, a round shape, an oval shape, etc.
    For the above reasons, however, a steel powder made of stainless steel produced by gas atomization is particularly preferably used as the blasting agent.
    The particles of the abrasive can have a particle diameter which is selected from a range from 0.2 mm to 2 mm. The particle diameter is the diameter of a sphere into which the particle just fits.
    The blasting agent can have particles with a particle size distribution between 0.2 mm and 2 mm. This can be provided, for example, by using one or more sieve line (s).
    By compressing the surface area 6 of the component produced by powder metallurgy, a density in this area can be achieved which is at least 95% of the solid material density, but according to one embodiment variant is at least 99.5% of the solid material density. The solid material density is the density that the component would have in the connection area 4 if it were a void-free cast component, in other words, the density of a non-porous component.
    The surface area 6 particularly preferably has a density of at least 99.9% of the solid material density. In particular, the density of the component produced by powder metallurgy in the surface area 6 which also forms the connection area 4 is 100% of the solid material density. This is indicated in Fig. 2
    N2018 / 18300-AT-00
    8/18 in that the surface area 6 has no pores 7 which only appear below a dashed line 8 which marks the end of the surface area 6.
    The compressed surface area 6 extends from an outer surface 9 of the component produced by powder metallurgy, which also forms the connection area 4, to a depth below this surface 9, which is at least 50 μm. According to one embodiment variant, it is preferably provided that the compressed surface area 6 has a layer thickness 10 which is between 50 μm and 350 μm, in particular between 100 μm and 150 μm. Such a high layer thickness of the compressed area can be achieved in particular by using the above-mentioned steel powder produced by a gas atomization process.
    A known metal powder (mixture) can be used to produce the component produced by powder metallurgy. However, a steel powder is preferably used, in particular a steel powder made of a stainless steel or stainless steel. The steel powder can e.g. the composition comprises 0% by weight to 20% by weight of nickel, 1% by weight to 25% by weight of chromium, 0% by weight to 20% by weight of molybdenum, the rest: iron. For example, the powder made of 18.5% by weight of Cr,
    11.2% by weight of Ni, remainder iron (oxygen at most 0.22% by weight, nitrogen at most 005% by weight, carbon at most 0.02% by weight). The usual processing aids, such as pressing aids, etc., can be added to the powder, as are known per se.
    It is also possible that 5 low-melting alloys, such as tin alloys, are used as the solder. According to a further embodiment variant, however, a copper solder is particularly preferred. The term “copper solder” also includes copper alloys that can be used as solder 5.
    The solder 5 can be applied, for example, as a paste to the first and / or the second metallic component 2, 3. For a higher degree of automation, the solder 5 can be applied at least partially outside the connection area 4 to at least one of the two metallic components 2, 3. By
    N2018 / 18300-AT-00
    9/18 the heating of the solder 5 to at least the melting temperature, for example in a continuous furnace, the solder 5 can flow into the connection area 4 and, after cooling, form the connection between the two metallic components 2, 3. For this purpose, the two metallic components 2, 3 are positioned corresponding to each other with a holding device, in particular before the solder 5 is applied.
    According to a further embodiment variant, it can be provided that the metallic component, which is produced from the sintered material, in the connection area 4 in the surface area 6 has a solder content of at most 0.1% by volume, in particular of 0% by volume.
    The component produced by powder metallurgy is preferably cleaned after compression, in particular jet compression, and before soldering. The cleaning is carried out in particular by means of thermal cleaning in an H2 atmosphere. This cleaning is used to remove oxides from the surface of the component as much as possible. This cleaning can be carried out at a temperature between 800 ° C and 1200 ° C.
    Tests were carried out to evaluate the connection quality. For this purpose, two metallic components 2, 3 connected to one another via a copper solder were clamped in a test device and the breaking force was measured. One of the two components consisted of a cast steel, the other of a steel powder that was processed by powder metallurgy. To measure the breaking force, the force acting on the connection area 4 was increased until the assembly 1 was broken. In all cases, the powder metallurgy component itself is broken and not the connection area 4. Forces of approx. 2,600 N were measured
    The exemplary embodiments show or describe possible design variants, it being noted at this point that combinations of the individual design variants with one another are also possible.
    N2018 / 18300-AT-00
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    For the sake of order, it should finally be pointed out that, for a better understanding of the structure, elements have sometimes been shown to scale and / or enlarged and / or reduced.
    N2018 / 18300-AT-00
    11/18
    Reference list
    Assembly
    Component
    Component
    Connection area
    Lot
    Surface area
    pore
    line
    surface
    Layer thickness
    N2018 / 18300-AT-00
    权利要求:
    Claims (10)
    [1]
    Claims
    1. A method for producing a connection between a first metallic component (2) and a second metallic component (3), wherein at least one of the two metallic components (2, 3) is made of a sintered material by powder metallurgy and the connection in one between the two Metallic components (2, 3) formed connection area (4) is produced by soldering, characterized in that the surface (9) of the metallic component (2 or 3) made of the sintered material, which also forms the connection area (4), in front of the Soldering is compacted.
    [2]
    2. The method according to claim 1, characterized in that the compression of the joint area (4) co-forming surface (9) of the component (2 or 3) made of a sintered material is carried out by powder metallurgy to a density of at least 99.5% of the solid material density.
    [3]
    3. The method according to claim 1 or 2, characterized in that the compression of the connecting area (4) co-forming surface (9) of the component (2 or 3) made of a sintered material is carried out by means of blasting.
    [4]
    4. The method according to claim 3, characterized in that for blasting a powder made of gas from stainless steel is used as the blasting agent.
    [5]
    5. The method according to any one of claims 1 to 4, characterized in that a sintered powder made of a stainless steel is used as the sintered material.
    [6]
    6. The method according to any one of claims 1 to 5, characterized in that a copper solder is used as the solder.
    N2018 / 18300-AT-00
    13/18
    [7]
    7. An assembly (1) comprising a first metallic component (2) and a second metallic component (3), at least one of the two metallic components (2, 3) being made from a sintered material by powder metallurgy, and the two components (2, 3 ) are soldered to one another in a connection area (4) with a solder (5), characterized in that the metallic component which is produced from the sintered material is surface-densified in the connection area (4).
    [8]
    8. The assembly (1) according to claim 7, characterized in that the metallic component (2 or 3), which is made of the sintered material, has a surface density of at least 99.5% of the solid material density in the connection area (4).
    [9]
    9. The assembly (1) according to claim 7 or 8, characterized in that the metallic component (2 or 3), which is made of the sintered material, has a compressed layer in the connection region (4), which has a layer thickness (10) between 50 μm and 350 μm.
    [10]
    10. The assembly (1) according to any one of claims 7 to 9, characterized in that the metallic component (2 or 3), which is made of the sintered material, in the connection area (4) a solder content of at most 0.1 vol .-% having.
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    同族专利:
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    BR102019014461A2|2020-02-11|
    DE102019120906A1|2020-02-13|
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    引用文献:
    公开号 | 申请日 | 公开日 | 申请人 | 专利标题
    DE1187333B|1958-11-05|1965-02-18|Siemens Ag|Electrical contact with high welding reliability, high erosion resistance and good adhesive strength of the contact layer on the contact carrier|
    US3985283A|1974-08-01|1976-10-12|United Aircraft Products, Inc.|Method of joining braze alloy to a parent metal part|
    DE2653650B1|1976-11-25|1978-05-18|Siemens Ag|Process for the surface-like soldering of two metallic bodies|
    US5155326A|1990-12-24|1992-10-13|United Technologies Corporation|Porous materials brazing|
    CN112676577A|2020-12-25|2021-04-20|中北大学|Lattice structure of nickel-based alloy clad material and preparation method thereof|
    法律状态:
    优先权:
    申请号 | 申请日 | 专利标题
    ATA50686/2018A|AT521546B1|2018-08-10|2018-08-10|Process for making a connection between two metallic components|ATA50686/2018A| AT521546B1|2018-08-10|2018-08-10|Process for making a connection between two metallic components|
    US16/452,664| US20200047289A1|2018-08-10|2019-06-26|Method for producing a connection between two metallic components|
    BR102019014461-0A| BR102019014461A2|2018-08-10|2019-07-12|METHOD FOR PRODUCTION OF A CONNECTION BETWEEN A FIRST METALLIC COMPONENT AND A SECOND METALLIC COMPONENT AND A CONSTRUCTIVE GROUP UNDERSTANDING A FIRST METALLIC COMPONENT AND A SECOND METALLIC COMPONENT|
    CN201910670973.9A| CN110814353A|2018-08-10|2019-07-24|Method and structural assembly for establishing a connection between metal components|
    DE102019120906.4A| DE102019120906A1|2018-08-10|2019-08-02|Process for making a connection between two metallic components|
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