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
  • 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
  • B22F3/00—Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces
  • B22F3/10—Sintering only
  • B22F3/11—Making porous workpieces or articles
  • B22F3/1121—Making porous workpieces or articles by using decomposable, meltable or sublimatable fillers
  • B22F3/1125—Making porous workpieces or articles by using decomposable, meltable or sublimatable fillers involving a foaming process
• • 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
  • B22F5/00—Manufacture of workpieces or articles from metallic powder characterised by the special shape of the product
  • B22F5/10—Manufacture of workpieces or articles from metallic powder characterised by the special shape of the product of articles with cavities or holes, not otherwise provided for in the preceding subgroups
• • C—CHEMISTRY; METALLURGY
  • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
  • C22C—ALLOYS
  • C22C1/00—Making non-ferrous alloys
  • C22C1/04—Making non-ferrous alloys by powder metallurgy
  • C22C1/05—Mixtures of metal powder with non-metallic powder
  • C22C1/051—Making hard metals based on borides, carbides, nitrides, oxides or silicides; Preparation of the powder mixture used as the starting material therefor
• • C—CHEMISTRY; METALLURGY
  • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
  • C22C—ALLOYS
  • C22C1/00—Making non-ferrous alloys
  • C22C1/08—Alloys with open or closed pores
• • 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
  • B22F2203/00—Controlling
  • B22F2203/11—Controlling temperature, temperature profile
• • 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
• • C—CHEMISTRY; METALLURGY
  • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
  • C22C—ALLOYS
  • C22C1/00—Making non-ferrous alloys
  • C22C1/04—Making non-ferrous alloys by powder metallurgy
  • C22C1/0408—Light metal alloys
  • C22C1/0416—Aluminium-based alloys
• • C—CHEMISTRY; METALLURGY
  • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
  • C22C—ALLOYS
  • C22C1/00—Making non-ferrous alloys
  • C22C1/04—Making non-ferrous alloys by powder metallurgy
  • C22C1/045—Alloys based on refractory metals
  • C22C1/0458—Alloys based on titanium, zirconium or hafnium
• • C—CHEMISTRY; METALLURGY
  • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
  • C22C—ALLOYS
  • C22C1/00—Making non-ferrous alloys
  • C22C1/08—Alloys with open or closed pores
  • C22C1/083—Foaming process in molten metal other than by powder metallurgy

Definitions

• the present invention relates to a process for producing a metal foam of at least a first metal comprising the main constituent Mg, Al, Pb, Au, Zn, Ti or Fe in an amount of at least about 80% by weight, based on the Amount of the at least one first metal, comprising the steps of (I) providing a semifinished product comprising a foamable mixture comprising the at least one first metal and at least one propellant, (II) immersing the semifinished product in a heatable bath comprising a liquid, and (III) heating the semifinished product in the bath for frothing the foamable mixture by gas elimination from the at least one propellant to form the metal foam.
• the invention relates to a metal foam and a composite material obtainable by the method and a component comprising the metal foam and / or the composite material.
• Metal foams and composites comprising metal foams such as metal foam sandwiches have been known for years. The latter are of particular interest when the composite is a single-material system, i. when using a certain metal and its alloys, such as in particular of aluminum and its alloys, and the connection between the core and cover layer is produced by means of a metallurgical bond.
• DE 44 26 627 C2 describes a method in which one or more metal powders are mixed with one or more propellant powders, and the powder mixture thus obtained by axial hot pressing, hot hydrostatic pressing or rolling compacted and in a subsequent operation with previously surface-treated metal sheets by roll-plating is assembled into a composite material. After the forming of the resulting semi-finished product by, for example, pressing, deep drawing or bending, this is heated in a final step to a temperature which is in the solidus-liquidus region of the metal powder, but below the melting temperature of the outer layers. Since the propellant powder is selected such that in this temperature range at the same time Gas splitting takes place, thereby forming bubbles within the viscous core layer, accompanied by a corresponding increase in volume.
• EP 1 000 690 A2 describes the production of such a composite material on the basis of a powder compact initially produced with open pores, which does not react with the subsequent roll cladding the outer layers is closed pores.
• the remaining process steps are identical.
• the original open porosity is to prevent that lead during storage of the powder compact possible gas splits of the propellant to geometry changes of the compact and thus to problems in the subsequent production of the composite with the outer layers.
• it is intended to facilitate the opening of the oxide layers forming during the storage of the compact in the production of the composite by the open porosity.
• EP 0 997 215 A2 discloses a method for producing a metallic composite material consisting of solid metallic cover layers and a closed-pore, metallic core, which combines the production of the core layer and the connection with the cover layers in one step, such that the powder mixture in the roll gap between the two outer layers is introduced and thus compressed between them. Furthermore, it is proposed to supply the powder in a protective gas atmosphere, so as to prevent the formation of oxide layers, which could adversely affect the required connection between the outer layers and powder mixture.
• US 5,972,521 A discloses a method for producing a composite blank in which air and moisture are removed by evacuation from the powder. Subsequently, the evacuated air is replaced by a gas which is inert to the core material under elevated pressure, before the powder is compacted and connected to the cover layers.
• EP 1 423 222 a process for producing a composite of cover layers and metal powder is known, in which the entire production process takes place under vacuum. Especially the compaction of the powder bed and the subsequent rolling should be done under vacuum. All of these known from the prior art method except that of EP 1 423 222 has in common that by the production of the foaming core layer air or
• Shielding gas is included in the compaction between the metal powder particles and compacted depending on the Kompat istsgrad.
• the resulting gas pressures which increase even further during the temperature increase during the foaming process, lead during the heating even before reaching the solidus-liquidus region of the
• Metal powder material corresponding temperature to form pores.
• these are open, crack-shaped interconnected and irregular pores.
• shaped pores While, for example, from US 5,564,064 AI a method is known, which specifically seeks such an open porosity by expansion of trapped gases below the melting temperature of the powder material, such a pore formation is not desirable in the methods described above, since only the desired ge - Closed, spherical pores allow optimal load transfer on the intact as possible, surrounding the pores cell walls, and thus contribute significantly to the strength of the core foams and thus the composite material.
• DE 102 15 086 A1 discloses a method for producing foamable metal bodies by compacting and pre-compacting a semifinished product.
• the gas-splitting propellant is formed only after the compaction and pre-compression of the semi-finished product by hydrogenation of the mixture of metal-containing propellant pre-material and the at least one metal.
• the porous metal body is formed by heating the foamable metal body thus obtained to a temperature above the decomposition temperature of the blowing agent, and it is preferable that this takes place immediately after the production of the foamable metal body without intermediate cooling thereof.
• BR 10 201 2 023361 A2 discloses the production of a closed-cell metal foam, in which a semifinished product, which is a metal selected from the group consisting of Al, Zn, Mg, Ti, Fe, Cu and Ni, and a blowing agent, selected from the Group consisting of TiH 2 , CaC0 3 , K 2 C0 3 , MgH 2 , ZrH 2 , CaH 2 , SrH 2 and HfH 2 and others, is foamed in a pre-heated to 780 ° C resistance furnace.
• a semifinished product which is a metal selected from the group consisting of Al, Zn, Mg, Ti, Fe, Cu and Ni
• a blowing agent selected from the Group consisting of TiH 2 , CaC0 3 , K 2 C0 3 , MgH 2 , ZrH 2 , CaH 2 , SrH 2 and HfH 2 and others
• a method for the powder metallurgical production of metal foam in which a pressed semi-finished product is used, which is heated in a pressure-tight sealable chamber to the melting or solidus temperature of the powdered metallic material, wherein after its Reaching the pressure in the chamber is reduced from an initial pressure to a final pressure, so that the semifinished product foams.
• DE 199 33 870 C1 discloses a process for producing a metal composite body using a foamable compact, wherein the compact or semifinished product is produced by compacting a mixture of at least one metal powder and at least one gas-releasing propellant powder. The compact is then thermally treated together with a reinforcement in a foaming mold and thereby foamed.
• US 2004/0081571 A1 relates to a process for producing foamable metal shavings which contain a mixture of a metal alloy powder with a foaming agent powder and which are foamed by heating to a temperature greater than the decomposition temperature of the foaming agent.
• EP 0 945 1 97 A1 discloses a method in which composite sheets or strips produced from slab rolled ingots are shaped from a blowing agent-containing aluminum alloy and then foamed to the ignition temperature of the blowing agent under pressure and temperature increase.
• a method for producing a composite body in which a metal foam is foamed pulschmmelzmetallurgisch under such heat supply to a first body part, that the outer fabric layers melt on the bonding surfaces of a substrate body and thereby with the adjacent fabric layers of the first Part of the body are metallurgically bonded.
• the foaming processes known from the prior art suggest the heating of the respective precursor material (semifinished product) for foaming.
• foamable mixtures of metal and blowing agent in particular in the form of semi-finished products, can be foamed in a suitably heated liquid bath in order to form a metal foam.
• a complete wetting of the outer surface of the area to be foamed but usually, also to simplify the process, complete wetting of the outer surface of the entire semi-finished by the heated liquid take place without the wetting by liquid negative effects on the structure and quality of the semifinished product and the forming metal foam.
• the semi-finished products therefore do not have to be held in a mold and / or press individually and subjected to a certain contact pressure in order to ensure a uniform heat transfer, several semifinished products can be foamed simultaneously in a liquid bath.
• no inert gas is required when carrying out the metal foaming process according to the invention; It can be worked according to the invention at ambient atmosphere or air atmosphere and ambient air pressure.
• the present invention therefore provides:
• the semifinished product comprises at least a first region formed from the foamable mixture and at least a second region formed from the at least one second metal in the form of non-foamable solid material for producing a composite material, wherein the composite material comprises at least a first A region formed of the metal foam of the at least one first metal and at least a second region formed of at least one second metal in the form of non-foamable solid material comprises;
• the term “about” or “substantially” is used with reference to values or ranges of values, or certain values result from the use of these terms (eg, the formulation "the outgassing temperature of A is approximately equal to the solidus temperature B "is to be understood as a certain temperature which results from the material B used by the person skilled in the art), this is to be understood as meaning that the person skilled in the art will regard as expertly usual in the given context.
• deviations of the specified values from +/- 10%, preferably from +/- 5%, more preferably from +/- 2%, most preferably from +/- 1% of the terms "about” and “substantially”.
• the invention thus relates to a method for producing a metal foam or a metallic composite material containing a metal foam.
• the metal foam and the metal foam in the composite material according to the invention comprise or consist of at least one first metal which forms voids in the form of pores, preferably in the form of closed pores containing a gas (gas inclusions) consisting of air, the at least one propellant released gas or mixtures thereof.
• Preference is exactly a first metal.
• the at least one first metal is foamed (foamed) with the aid of a blowing agent. In this case, the volume of the first metal increases due to pore formation or gas inclusions.
• a mixture of the at least one first metal and the at least one blowing agent in the form of a foamable mixture is produced.
• This foamable mixture is preferably in the form or as part of a semifinished product.
• the foamable mixture or the semi-finished product is immersed in a heatable bath (heating bath) for foaming (foaming) the at least one first metal or the foamable mixture. Heating the heating bath leads to the release of a gas (gas separation) from the at least one blowing agent.
• the gas released here foams the at least one first metal by producing pores in the at least one first metal and thus the metal foam.
• the steps (II) of immersion and (III) of heating can be carried out simultaneously in the sense that the immersion of the semifinished product takes place in a heated or heated bath.
• metal herein means both a metal in its commercially pure form ("pure metal” such as pure magnesium, pure aluminum, pure iron, pure gold, etc.) and its alloys. In principle, all foamable (foamable) metals in pure form or as an alloy are suitable as the first metal according to the invention. Metals in pure form (pure metals) contain the respective metal in an amount or with a content of at least 99 wt .-%, based on the respective metal.
• Suitable foamable metals are, in particular, magnesium (Mg), aluminum (Al), lead (Pb), gold (Au), zinc (Zn), titanium (Ti) or iron (Fe).
• the first metal may thus be magnesium (Mg), aluminum (Al), lead (Pb), gold (Au), zinc (Zn), titanium (Ti) or iron (Fe) in pure form, ie pure magnesium, pure aluminum, pure lead, Pure gold, pure zinc, pure titanium or pure iron, wherein a content of the respective metal of at least 99 wt .-%, based on the respective metal, is preferred.
• a metal in which magnesium (Mg), aluminum (Al), lead (Pb), gold (Au), zinc (Zn), titanium (Ti) or iron (Fe) in an amount is also suitable as the first metal of at least about 80% by weight (percent by weight,% by weight), based on the amount of the first metal, forms the main component. Therefore, alloys of the aforementioned metals are also used. Therefore, the term "metal" according to the invention in addition to the pure metal also includes metal alloys or alloys shortly.
• a suitable alloy of magnesium for example, AZ 31 (Mg96AI3Zn).
• Suitable alloys of aluminum are, for example, selected from the group consisting of
• higher-strength aluminum alloys selected from the group consisting of aluminum-magnesium-silicon alloys (6000 series) and aluminum-zinc alloys (7000 series), of which aluminum-zinc alloys (series 7000)
• AIZn4.5Mg (Alloy 7020) is preferred, and
• the aluminum, magnesium and silicon include, more preferably AISi6Cu7,5, AIMg6Si6 and AIMg4 ( ⁇ 1) Si8 ( ⁇ 1), even more preferably AIMg6Si6 and AIMg4 ( ⁇ 1) Si8 ( ⁇ 1), more preferably AIMg4 ( ⁇ 1) Si8 ( ⁇ 1).
• the at least one first metal may be aluminum or pure aluminum (at least
• the at least one first metal may be a higher-strength aluminum alloy.
• the higher strength aluminum alloy may be selected from the group consisting of aluminum-magnesium silicon alloys (6000 series) and aluminum-zinc alloys (7000 series), of which AlZn4.5Mg (7020 alloy) is preferred among the aluminum-zinc alloys (series 7000) ,
• the at least one first metal can therefore be in particular AIZn4.5Mg (alloy 7020).
• the at least one first metal may be a higher strength aluminum alloy having a melting point of about 500 ° C to about 580 ° C; preferred higher strength aluminum alloys are AISi6Cu7.5, AIMg6Si6 and AIMg4 ( ⁇ 1) Si8 ( ⁇ 1).
• the at least one first metal may also be a higher strength aluminum alloy having a melting point of about 500 ° C to about 580 ° C comprising aluminum, magnesium and silicon or composed solely of these chemical elements.
• Preferred higher strength aluminum alloys having a melting point of about 500 ° C to about 580 ° C comprising aluminum, magnesium and silicon are AIMg6Si6 and AIMg4 ( ⁇ 1) Si8 ( ⁇ 1), of which
• AIMg4 ( ⁇ 1) Si8 ( ⁇ 1) is particularly preferred.
• the indication ( ⁇ 1) in the alloying formulas used herein means that the respective chemical element concerned may also have a mass percentage more or less than stated. In general, however, a correlation between two elements provided with such information in a formula applies, that is, if, for example, of the first element in the formula which is provided with ( ⁇ 1) one more mass percent is present, then the second element in the formula also provided with ( ⁇ 1), one percent by mass less present.
• the formula AIMg4 ( ⁇ 1) Si8 ( ⁇ 1) thus includes, among others, the formulas AIMg5Si7 and AIMg3Si9.
• a suitable alloy of the lead is, for example, the lead-copper alloy with about 1% copper, ie PbCul or PbCu.
• Suitable alloys of the gold are, for example, gold-titanium alloys with about 1% titanium, ie AuTil or AuTi.
• Suitable alloys of zinc are, for example, zinc-titanium alloys containing about 1% to 3% titanium, ie, for example, ZnTil, ZnTi 2 or ZnTi 3.
• a suitable alloy of titanium is, for example, ⁇ -6 ⁇ -2Sn-4Zr-6Mo.
• Suitable alloys of iron are mainly steel. According to the invention and according to DIN EN 10020: 2000-07, “steel” refers to a material whose mass fraction of iron is greater than that of any other element whose carbon content is generally less than 2% and which contains other elements. A limited number of chromium steels can contain more than 2% carbon, but 2% is the usual limit between steel and cast iron.
• Semi-finished product according to the present invention is a foamable starting material, which after foaming a metal foam or a composite material comprising such a metal foam results.
• the semifinished product as a precursor for the metal foam comprises a foamable (foamable) mixture or has this exclusively.
• the foamable mixture comprises the metal to be foamed, i. the at least one first metal, at least one propellant and optionally at least one excipient.
• the foamable mixture or the entire semifinished product can be produced by powder metallurgy. Powder metallurgically produced semi-finished products have the foamable mixture as compacted powder in the form of a compact (powder compact) or in such a compacted form that the mixture is rollable, such as rollable ingot
• the foamable mixture may also be present as a solid metal that has absorbed a gaseous propellant, such as hydrogen gas.
• a gaseous propellant such as hydrogen gas.
• Composite material according to the present invention is a metallic material in which two structurally different materials, namely foamed metal (metal foam) and metal in the form of solid, non-foamable solid material combined with each other and are positively and / or materially interconnected.
• the (final) material metallurgical connection between metal foam and solid metal takes place at their adjoining connecting surfaces by melting the same when foaming the foamable mixture with heat.
• the majority of the metallurgical connection between the foamable mixture and the solid material is already present in the semi-finished product.
• oxide-free surfaces can be produced which result in the powder particles of the foamable mixture and the Solid solid material (the top layer (s)) connect, ie there is a kind of welding instead.
• the composite material according to the invention comprises a metal foam and metal in the form of non-foamable, solid solid material.
• the composite material comprises or has at least one first region, which is formed from the metal foam of the at least one first metal or comprises this metal foam, and at least one second region, which is formed from at least one second metal in the form of non-foamable solid material or this includes.
• the at least one second region comprises or has exactly one second metal in the form of non-foamable solid material.
• the at least one second region may in particular be formed as a solid, non-foamable metallic layer, in particular as cover layer or cover layer, on at least part of the surface of the at least one first region.
• two second regions are preferably each as a layer, in particular cover layer or top layer, in the form of non-foamable solid material, so applied two massive layers.
• the two massive (deck) layers are preferably separated from one another by a zone of the first region in such a way that the first region could expand in foaming due to the associated increase in volume due to the formation of the metal foam in this zone.
• the composite material preferably has exactly one first area and exactly one second area.
• the composite preferably has exactly one first region and exactly two second regions.
• the composite material has exactly one first region and exactly two second regions, wherein each of the two second regions forms a layer on the first region.
• the two second regions or layers are separated by a zone in which the first region or the semifinished product could expand during foaming.
• the semifinished product as a precursor for the composite material or for the production of the composite material in the context of the present invention is a foamable starting material which, after foaming, gives rise to the composite material.
• the semifinished product comprises or has at least one first region which is formed from or comprises the foamable mixture, and at least one second region which is formed from or comprises the at least one second metal in the form of non-foamable solid material.
• the at least one second region may in particular be formed as a solid, non-foamable metallic layer, in particular as cover layer or cover layer, on at least part of the surface of the at least one first region.
• two second regions are preferably each applied as a layer, in particular cover layer or cover layer, in the form of non-foamable solid material, ie two solid layers.
• two second regions are each preferably applied as a layer in the form of non-foamable solid material, ie two solid layers which are separated from one another by a zone of the first region such that the first region during foaming due to the resulting associated volume increase by the formation of the metal foam in this zone can expand.
• the semifinished product for the composite material preferably has exactly one first area and exactly one second area.
• the semifinished product for the composite material preferably has exactly one first region and exactly two second regions.
• the semifinished product for the composite material has exactly one first region and exactly two second regions, wherein each of the two second regions forms a layer on the first region.
• the two second regions or layers are separated by a zone in which the first region or the semifinished product can expand during foaming.
• the composite comprises at least a first region formed of the metal foam of the at least one first metal and at least a second region formed of at least one second metal in the form of non-foamable bulk material;
• the semi-finished product comprises at least a first region formed from the foamable mixture and at least one second region formed from the at least one second metal in the form of non-foamable solid material.
• the at least one first region is formed as a foamed core and in the semi-finished product for the production of this composite material, the at least one first region is designed as a foamable core. This core is covered in layers by the second region, ie in the form of at least one cover layer. In this case, sandwich-like structures, ie layered plate-shaped structures, layer structures or layered structures with planes of straight (non-curved) propagation direction are possible.
• Core and cover layer (s) then describe levels straight (non-curved) propagation direction or are plate-shaped.
• spherical layer structures with curved layers or levels possible such as in a layered solid rod or rod, a hose, a tube or a sausage.
• the spherical layer structure may be solid throughout with a solid rod-shaped core or with an innermost hollow core such that the foamable or foamed core has a tubular configuration.
• the metal foams, composite materials and semi-finished products may have any shape as long as an increase in volume or volume expansion of the at least one first region with the foamable mixture is ensured in the semi-finished products.
• the semi-finished products can be plate-shaped, round or square bars and other, regularly or irregularly shaped body.
• the semi-finished products may have a layered structure, but the at least one first and at least one second
• the at least one second region consists of at least one solid, non-foamable second metal and therefore does not expand when the at least one first region is foamed, the at least one second region must not completely cover the at least one first region, i. an "open" zone must remain in the at least one first region, which allows expansion of the at least one first region or the foamable mixture during foaming.
• "open" ends and / or at least one open inner channel are to be provided on or in which the first region can expand during foaming.
• the foamable mixture is present at least at the beginning of the production process in the form of powder comprising powder particles.
• the finished semifinished product can mixture also contained in powder form, preferably the foamable mixture is present in the finished semi-finished but in a compacted form, for example as a compact.
• the compaction of the powder leads to its solidification and can extend as far as a metallurgical connection of the powder particles with each other, ie the individual grains or particles of the powder (powder particles) become partially or completely diffusion and formation of (first) intermetallic phases within the mixture completely interconnected instead of forming a loose powder.
• This (first) metallurgical bonding has the advantage of a more stable and more compact foamable first region or core, which forms almost no defects in the foam during foaming.
• the first metallurgical joining furthermore produces a stable rolling ingot, ie the deformability of the semifinished product, in particular by rolling, bending, deep-drawing and / or hydroforming, is improved.
• the powder particles are partially connected to the at least one second region, in particular if present in the form of at least one layer, for example in the form of at least one cover layer or cover layer.
• the powder of the at least one first metal consists of powder particles, which may have a particle size of about 2 ⁇ to about 250 ⁇ , preferably from about 10 ⁇ to about 150 ⁇ . These particle sizes have the advantage that a particularly homogeneous mixture, i. forms a particularly homogeneous foamable mixture, so that later occurring defects during foaming are avoided.
• the foamable (foamable) mixture comprises at least a first metal and at least one blowing agent.
• the foamable mixture comprises exactly one first metal and at least one blowing agent.
• the foamable mixture preferably comprises exactly one first metal and exactly two blowing agents.
• the foamable mixture comprises exactly one first metal and exactly one blowing agent.
• the foamable mixture may further comprise adjuvants.
• the foamable mixture advantageously comprises no excipient, since is usually disturbed with one or more auxiliaries, the structure of the foamable mixture and the foamable core that the later obtained therefrom foamed (voids) core defects such as inhomogeneities in the foam structure, too large pores or bubbles and / or open pores instead of closed Having pores.
• the foamable mixture contains only exactly one first metal, exactly one blowing agent, optionally one or more derivatives of the blowing agent and no further substances or auxiliaries.
• the foamable mixture may exclusively contain or consist of the aforementioned substances or constituents instead of just comprising them.
• the blowing agent as derivative (s) additionally comprise at least one oxide and / or oxihydride of the metal or metals of the metal hydride (s) used in each case.
• oxides and / or Oxihydride arise in a pretreatment of the propellant and its durability as well as its response during foaming, so improve the timing of the release of the propellant gas, so that the propellant used or the propellant not too early, but not too late release; too early or too late release of the propellant gas can produce oversized cavities and thus defects in the metal foam.
• the inventive at least one propellant releases from a certain temperature, the Ausgastemperatur of the blowing agent, by means of degassing or gas separation, a propellant, which serves to foam the at least one first metal.
• a propellant which serves to foam the at least one first metal.
• a metal hydride as blowing agent is released as propellant hydrogen (H 2 ).
• carbon dioxide (C0 2 ) is released as a propellant gas.
• the at least one blowing agent according to the invention is selected from the blowing agents known to the person skilled in the art for the respective first metal.
• Preferably exactly one driving medium Tel used but it can also be mixtures of blowing agents, in particular mixtures of two different blowing agents are used.
• blowing agents which are selected from the group consisting of metal hydrides and metal carbonates are suitable for the metals explicitly mentioned herein.
• the outgassing temperature of the at least one blowing agent should advantageously be equal to the solidus temperature of the at least one first metal or should be below the solidus temperature of the at least one first metal to later become a closed-cell foam free of defects and a good result in foaming the core.
• the outgassing temperature of the propellant should preferably be no more than about 90 ° C, more preferably no more than about 50 ° C below the solidus temperature of the at least one first metal.
• the outgassing temperature of the at least one propellant should also be less than the solidus temperature of the at least one second metal, since the at least one second metal may not enter its solidus area during foaming of the at least one first metal, thus, it may not begin to melt to prevent mixing with the at least one first metal, as explained elsewhere herein.
• the outflow temperature of the at least one propellant is therefore preferably below, more preferably at least about 5 ° C below the solidus temperature of the at least one second metal.
• the blowing agent according to the invention is preferably selected as follows:
• the at least one blowing agent is preferably selected from the group consisting of metal hydrides and metal carbonates, more preferably selected from Metal hydrides of the group consisting of TiH 2 , ZrH 2 , HfH 2 , MgH 2 , CaH 2 , SrH 2 , LiBH 4 and LiAlH 4 ; and
• Carbonates of the second main group of the Periodic Table of the Elements ie in particular the group consisting of BeC0 3 , MgC0 3 , CaC0 3 , Sr-C0 3 and BaC0 3 .
• the at least one blowing agent is more preferably selected from the group consisting of TiH 2 , ZrH 2 , MgC0 3 and CaC0 3 .
• the propellant is in particular a metal hydride.
• the metal hydride is preferably selected from the group consisting of TiH 2 , ZrH 2 , HfH 2 ,
• the at least one metal hydride is more preferably selected from the group consisting of TiH 2 , ZrH 2 , HfH 2 , LiBH 4 and LiAlH 4 , more preferably selected from the group consisting of TiH 2 , ZrH 2 , LiBH 4 and LiAlH 4 more preferably selected from the group consisting of TiH 2 , LiBH 4 and LiAlH 4 .
• the metal hydride is preferably also selected from the group consisting of TiH 2 , ZrH 2 and HfH 2 , more preferably consisting of TiH 2 and ZrH 2 .
• the metal hydride TiH 2 is particularly preferred.
• a combination of two metal hydrides selected from the group consisting of TiH 2 , ZrH 2 and HfH 2 , preferably the combination of TiH 2 and ZrH 2 is suitable.
• a combination of two metal hydrides is suitable as a blowing agent, wherein from each of the two groups
• each one blowing agent is selected; preferred of these is the combination of TiH 2 with a propellant selected from the group consisting of MgH 2 , CaH 2 , SrH 2 , LiBH 4 and LiAlH 4 ; particularly preferred is the combination of TiH 2 with LiBH 4 or LiAlH 4 .
• a propellant selected from the group consisting of MgH 2 , CaH 2 , SrH 2 , LiBH 4 and LiAlH 4 ; particularly preferred is the combination of TiH 2 with LiBH 4 or LiAlH 4 .
• exactly one propellant is used according to the invention.
• the propellant is in particular an alkaline earth metal carbonate nat, ie in particular selected from the group consisting of MgC0 3 , CaC0 3 , SrC0 3 and BaC0 3 , preferably selected from the group consisting of MgC0 3 , CaC0 3 , SrC0 3 and BaC0 3 , more preferably selected from the group consisting of MgC0 3 , CaC0 3 and SrC0 3 , more preferably selected from the group consisting of MgC0 3 and CaC0 3 .
• the at least one propellant is preferably selected from the group consisting of metal carbonates, more preferably selected from carbonates of the second main group of the Periodic Table of the Elements (alkaline earth metals), ie in particular the group consisting of MgC0 3 , CaC0 3 , SrC0 3 and BaC0 3 , even more preferably selected from the group consisting of MgC0 3 , CaC0 3 and SrC0 3 , more preferably selected from the group consisting of MgC0 3 and SrC0 3 .
• the outgassing temperature is in each case as follows (specification of the outgassing temperature in parentheses): TiH 2 (about 480 ° C.), ZrH 2 (about 640 ° C. to about 750 ° C.), HfH 2 (approx 500 ° C to about 750 ° C), MgH 2 (about 41 5 ° C), CaH 2 (about 475 ° C), SrH 2 (about 510 ° C), LiBH 4 (about 100 ° C) and LiAlH 4 ( about 250 ° C).
• the outgassing temperature is in each case as follows (specification of the outgassing temperature in parentheses): MgC0 3 (about 600 ° C. to about 1300 ° C.), CaC0 3 (about 650 ° C. to about 700 ° C.) ° C), SrC0 3 (about 1290 ° C) and BaC0 3 (about 1 360 ° C to about 1450 ° C).
• the metal hydride may additionally comprise as blowing agent at least one oxide and / or oxihydride of the metal or of the metals of one or more of the metal hydrides used in each case.
• the oxides and / or oxihydrides are formed in the pretreatment of the metal hydride-containing propellant and improve its durability as well as its response during foaming, ie the timing of the release of the propellant gas.
• the improvement of the foaming response with respect to the timing of the release of the propellant gas is mainly a shift in the release of the propellant gas or the outgassing in the late direction to a too-fast outgassing and thus the formation of defects such as bubbles and holes instead ( closed) pores to avoid;
• This is achieved, on the one hand, by the abovementioned oxides and / or oxihydrides, and on the other hand achieved by the at least one propellant, especially in the case of using one or more metal hydrides, in the matrix of the semifinished product, after the metallic joining within the first region and optionally after the metallic joining of the first region to the second region is under high pressure.
• the oxide is in particular an oxide of the formula Ti v O w , where v is from about 1 to about 2 and w is from about 1 to about 2.
• the oxihydride is especially an oxihydride of the formula TiH x O y , where x is from about 1.82 to about 1.99 and y is from about 0.1 to about 0.3.
• the oxide and / or oxihydride of the propellant may form a layer on the grains of the powder of the propellant; the thickness of this layer may be from about 10 nm to about 100 nm.
• the amount of the blowing agent or the total amount of all blowing agents using at least two different blowing agents can be from about 0.1% by weight (wt .-%) to about 1, 9 wt .-%, preferably from about 0.3 wt. % to about 1, 9 wt .-%, each based on the total amount of the foamable mixture.
• the amount of oxide and / or Oxihydride may be from about 0.01% to about 30% by weight, based on the total amount of the at least one blowing agent.
• the at least one second metal may be arbitrarily selected, as long as it is suitable for the solid and permanent connection with the other material component, here the metal foam, which is typical in a composite material.
• the at least one first metal and the at least one second metal are not identical, i. Both metals differ at least in one alloy constituent, the mass or weight fraction of at least one alloying constituent and / or in the nature (powder versus solid solid material), so that the solidus temperature of the at least one second metal is higher than the liquidus temperature of the at least one first metal. In particular, however, the solidus temperature of the at least one second metal is higher than the liquidus temperature of the foamable mixture.
• the at least one second metal as (solid, non-foamable) solid material compared to the at least one first metal as (compacted) powder, this usually has a different melting behavior than that, i.
• the same metal or metal alloy as solid material begins to melt later in time at the same temperature due to a higher enthalpy of fusion than in the form of powder.
• solid material can only begin to melt at a somewhat higher temperature than when it is present as a (compacted) powder, especially if the latter is also mixed with a blowing agent, because this lowers the melting point of the mixture of metal powder and blowing agent, ie the foamable Total mixture.
• the solidus temperature of the at least one second metal is higher than the liquidus temperature of the at least one first metal, in particular higher than the liquidus temperature of the foamable mixture. It is also advantageous if the at least one second metal begins to melt in time so much later (ie, sufficiently late) than the at least one first metal, so that the at least one second region made of the at least one second metal in solid, non-foamable form, which can be formed, for example, as a solid metallic cover layer, does not melt or start to melt during foaming of the foamable mixture. It has been found that otherwise, during the melting of the at least one layer during the foaming process, the latter is unintentionally deformed, in particular under the pressure of the gas released from the blowing agent.
• the at least one second metal begins to melt on foaming of the at least one first metal, it mixes with the at least one first metal beyond the boundary layers and destroys the foam or does not allow its formation at all or is itself foamed, so that the Foaming process is completely uncontrollable.
• the difference required between the solidus temperature of the at least one second metal and the liquidus temperature of the at least one first metal depends on the one hand on the (chemical) nature of the metals or metal alloys selected for the at least one first metal and the at least one second metal, on the other hand conditioned by their melting behavior.
• the at least one second metal has a solidus temperature which is at least about 5 ° C. higher than the liquor temperature of the foamable mixture. This higher solidus temperature and / or the temporally sufficiently early onset of melting of the at least one second metal can be realized according to the invention
• the at least one second metal (as a solid solid material compared to a powder form of the at least one first metal), ie a shape or texture that causes a higher solidus temperature and / or higher enthalpy of fusion (since metal melts earlier in powder form and a lower one Solidus temperature as solid metal in the form of solid material); and or in that the at least one second metal has less alloying constituents than the at least one first metal and / or has (compared with) the at least one first metal at least one identical lower mass fraction alloying component in the alloy (ie the mass fraction of at least one first and at least one second metal identical alloy component is in the at least one second metal lower or smaller than in at least a first metal).
• the different molten, solidus and / or or liquidus temperatures are adjusted by different alloying additives in powder and solid material accordingly.
• the solidus temperature of the at least one second metal is at least about 5 ° C higher than the liquidus temperature of the at least one first metal.
• the solidus temperature of the at least one second metal is more preferably at least about 6 ° C, more preferably at least about 7 ° C, even more preferably at least about 8 ° C, even more preferably at least about 9 ° C, even more preferably at least about 10 ° C, even more preferably at least about 1 1 ° C, even more preferably at least about 1 2 ° C, even more preferably at least about 1 3 ° C, still further preferably at least about 14 ° C, more preferably at least about 15 ° C, even more preferably at least about 1 6 ° C, even more preferably at least about 1 7 ° C, even more preferably at least about 18 ° C, even more preferably at least about 1 9 ° C and even more preferably at least about 20 ° C higher than the liquidus temperature of the at least one first metal.
• the at least one second metal does not soften or melt so much melts or melts that by the propellant gas formation and / or expansion unwanted bulges, bumps, cracks, holes and similar defects in at least a second Area arise and / or the at least one second area with the at least one first area partially or completely merges or mixed.
• the solidus temperature of the at least one second metal should be at least about 5 ° C higher, preferably about 10 ° C higher and most preferably about 1 5 ° C higher than the liquidus temperature of the at least one first metal; in special cases, the solidus temperature of the at least one second metal is at least about 20 ° C higher than the liquidus temperature of the at least one first metal.
• a solidus temperature of the at least one second metal which is about 15 ° C higher than the liquidus temperature of the at least one first metal usually a good compromise between the strength of the metal foam structure and the solid material on the one hand and the quality of Composite structure, so clear phase boundary between metal foam and solid material and no fusion of metal foam and solid material on the other hand, provides.
• the solidus temperature of the at least one second metal is higher than the liquidus temperature of the foamable mixture by the temperature stated above.
• the at least one first and second metal are not identical.
• the at least one second metal has less alloy components than the at least one first metal; the at least one second metal, alternatively or additionally to the at least one first metal, comprises at least one identical lower mass fraction alloying component in the alloy;
• the higher solidus temperature of the at least one second metal specified here relative to the liquidus temperature of the at least one first metal can be achieved.
• the composite material and the semi-finished product for its production preferably contain exactly one second metal as solid (non-foamable) solid material. Under solid material here massive metal that is not foamed, so has no pores, and is not present in powder form, understood.
• the metal can also be a metal alloy.
• the at least one second metal has the main component Mg (magnesium), Al (aluminum), Pb (lead), Au (gold), Zn (zinc), Ti (titanium), Fe (iron), or Pt (platinum) in one Amount of at least about 80 wt .-%, based on the amount of the at least one second metal on.
• the at least one second metal can be selected from those pure metals and alloys, as defined herein for the at least one first metal.
• the at least one first metal and the at least one second metal preferably have the same main constituent Mg, Al, Pb, Au, Zn, Ti or Fe. If the at least one second metal has aluminum as the main constituent, it is in particular selected from the group consisting of
• higher strength aluminum alloys selected from the group consisting of aluminum-magnesium alloys (5000 series), aluminum-magnesium-silicon alloys (6000 series) and aluminum-zinc alloys (7000 series).
• the at least one second metal may be aluminum or pure aluminum (at least 99 weight percent aluminum), with aluminum being preferred in which the aluminum content is from about 85 weight percent to about 99 weight percent, more preferably about 98 Wt .-%, based on the at least one second metal is.
• the at least one second metal may be a higher strength aluminum alloy.
• the higher-strength aluminum alloy may be selected from the group consisting of aluminum-magnesium alloys (series 5000), aluminum-magnesium-silicon alloys (series 6000) and aluminum-zinc alloys (series 7000).
• the at least one second metal may in particular be an aluminum-magnesium alloy (series 5000).
• the at least one second metal can in particular an aluminum-magnesium-silicon alloy (series 6000), preferably Al 6082 (Al Si 1 MgMn).
• the at least one second metal may in particular be an aluminum-zinc alloy (series 7000).
• Suitable combinations of first and second metal include, but are not limited to, alloys having the following metals as a major constituent, ie, in an amount of at least about 80% by weight based on the respective first and second metals, respectively Restriction to this - suitable propellants are given:
• steel may be used as the alloy.
• step (I) preferably step (I)
• step (III) the chronological sequence or sequence of the method steps according to the invention preferably corresponds to the numbering with Roman numerals as indicated in embodiment (1), ie preferably step (I), then step (II) and finally step (III).
• the heat input into the semifinished product during heating in step (III) and optionally preheating in a step (IV) described below takes place according to the invention from the outside into the semifinished product, ie via the outer surface of the semifinished product or a part of the outer surface of the semifinished product.
• step (III) the heat is introduced into the semifinished product when heated in a heatable bath comprising a liquid (heatable liquid bath) with the liquid from the outside into the semifinished product, ie from the liquid to the outside Surface of the semifinished product or a part of the outer surface of the semifinished product.
• a heatable bath comprising a liquid (heatable liquid bath) with the liquid from the outside into the semifinished product, ie from the liquid to the outside Surface of the semifinished product or a part of the outer surface of the semifinished product.
• at least complete wetting or even complete contact of those parts of the outer surface of the semifinished product which are also part of the (at least a first) region of the semifinished product or behind which the (at least a first) region to be foamed is preferably carried out of semifinished product (directly), with the liquid of the heated bath.
• the semifinished product is preferably so immersed in the heatable, preferably already heated bath that at least complete wetting of the above-mentioned parts of the outer
• the heating in step (III) of the process is preferably carried out to a foaming temperature which is within the foamable mixture (a) at least as high as the outgassing temperature of the at least one blowing agent, and / or (b) at least as high as the solidus temperature of the foamable mixture ,
• the foaming temperature is a temperature at which the at least one first metal is in a foamable state and the blowing agent decomposes, thereby releasing a blowing gas which foams the at least one first metal.
• the at least one first metal is in a foamable state when it begins to melt (at its solidus temperature) or is partially or completely melted.
• the heating in step (III) is preferably carried out to a foaming temperature which is lower than the solidus temperature of the at least one second metal within the foamable mixture.
• the foaming temperature in step (III) of the process according to the invention is that temperature at which the foamable mixture foams (foams up) and the metal foam forms.
• the foaming temperature should be equal to or higher than the outgassing temperature of the at least one propellant, at least as high as the solidus temperature of the at least one first metal (more precisely, taking into account a, albeit usually small, melting point depression by mixing with the at least one propellant and optionally one Auxiliaries: at least as high as the solidus temperature of the foamable mixture), and less than the solidus temperature of the at least one second metal in order to achieve the most homogeneous metal foam and preserve the character of the composite material, ie one for a superficial connection between Metal foam and metallic solid material to prevent merging of the two materials.
• the process of the invention may additionally comprise the step (IV) of preheating by heating the semifinished product of step (I) to a temperature which is from about 50 ° C to about 180 ° C, preferably to about 100 ° C, below the foaming temperature the step (IV) is performed prior to the step (II) and / or step (III).
• Step (IV) preferably takes place before step (II), which in turn takes place before step (III).
• step (II) is preferably carried out in a heated or heated bath, so that the heating takes place directly in step (III).
• the preheating / preheating may, for one or more times, also several parts simultaneously and over longer periods of several hours suc- preferably over periods of about 5 minutes to about 8 hours, more preferably over periods of about 10 minutes to about 6 hours.
• the heating in step (III) of the method according to the invention can be carried out at a controlled heating rate to the time of sufficient for foaming the at least one first metal propellant gas development on the time of reaching a frothable state of the at least one first metal, such as its solidus temperature to vote.
• the heat should be supplied in such a way that a sufficiently strong propellant gas development for foaming the at least one first metal and any maximum propellant gas development is present when the at least one first metal has reached its foamable state, such as its solidus temperature.
• the immersion of the semifinished product in the heatable liquid bath is preferably carried out so that a heat input into the regions to be foamed or the at least one first region takes place as short a path as possible.
• a heat input into the regions to be foamed or the at least one first region takes place as short a path as possible.
• the semifinished product is completely immersed in the heatable liquid bath.
• the formation of imperfections in the foam and, in the case of the composite material, also at the interfaces between the at least one first and at least one second region, ie between foam and non-foamable, solid solid material is reduced;
• the at least one second region in the composite material is formed as a layer or cover layer on the at least one first region, in particular if the composite material comprises exactly one first region and exactly two second regions, and each of the two second regions is formed as a layer or cover layer on the exactly one first region, and is particularly true when in these cases, the first region is formed as a core or core layer in the composite material.
• molten salt selected from salts, in particular inorganic salts, or solid particles, in particular sand or aluminum oxide granules, can fulfill these requirements.
• the salt is not present in solution in a chemical compound present at room temperature as a liquid, in particular not in aqueous solution. It is possible to use a mixture of two or more salts.
• the liquid of the heatable bath preferably comprises at least one molten salt, more preferably exactly one molten salt.
• the liquid of the heatable bath preferably comprises at least one molten inorganic salt, more preferably exactly one molten inorganic salt, preferably sodium chloride or potassium chloride.
• the (entire) liquid of the heated bath can be the aforementioned substances or components exclusively contain or consist of these instead of these only include.
• the term "liquid" in the sense of the present invention thus also encompasses, in particular, molten salts and solid particle baths.
• Solid particle baths comprise solid particles mixed with at least one gas and / or air, in particular as gas nitrogen or helium, even in further mixture with air, and are preferably produced in the sense of the present invention by a fluidized bed furnace. Solid particles are flowed through by the at least one gas and / or air, so that they set in motion and behave like a liquid or for the present invention have properties that resemble a liquid. This is also the case with molten salt in the context of the present invention.
• the grain size of the usable solid particles in the heated bath is preferably in a range of about 10 ⁇ to about 200 ⁇ more preferably in a range of about 80 ⁇ to about 1 50 ⁇ .
• the semi-finished product can be immersed in a solid-particle bath, for example of sand, and preheated, in particular to temperatures in a range of about 430 ° C. to about 520 ° C., preferably to temperatures in a range of about 450 ° C. to about 500 ° ° C.
• a solid-particle bath for example of sand
• preheated in particular to temperatures in a range of about 430 ° C. to about 520 ° C., preferably to temperatures in a range of about 450 ° C. to about 500 ° ° C.
• One or more readily several parts may be preheated simultaneously and over extended periods of several hours, preferably over periods of from about 5 minutes to about 8 hours, more preferably over periods of about 10 minutes to about 6 hours.
• the semifinished product in step (II) is preferably immersed in a solid-particle bath, in particular in a fluidized-bed furnace, in particular of aluminum oxide in the form of granules, the bath preferably having a temperature in a range from about 570 ° C. to about 630 ° C. , more preferably, has a temperature in a range of about 580 ° C to about 610 ° C.
• the heating according to step (III) thus takes place directly.
• the residence time in this solid particle bath is preferably about 1 minute to about 10 minutes, more preferably about 1.5 minutes to about 6 minute
• the foamed semifinished product is preferably removed and fed to a quench, for example in the form of a solid-particle bath, in particular of sand, preferably at a temperature in a range from about 10 ° C. to about 40 ° C.
• the residence time in the quenching is preferably in a range of about 30 seconds to about 10 minutes, preferably in a range of about 1 minute to about 3 minutes.
• the foamed semifinished product for example in the form of a composite material as described above, can be stored out warm.
• the steps (I) to (IV) can also be carried out in a continuous operation to increase the production rate. Also in the same bath preheating / preheating and foaming can take place.
• a correspondingly high (specific) heat capacity and / or thermal conductivity of the liquid of the heated bath is desirable.
• a high (specific) heat capacity and / or heat conductivity of the liquid of the heated bath thus surprisingly enables the formation of a particularly homogeneous metal foam, i. with a narrow size distribution of pore sizes.
• the foaming process can be done faster in this way.
• the liquid or the molten salt of the heatable bath is preferred
• Achieving the end point of step (III) may, with a suitable choice of the density of the liquid, in particular the molten salt or the solid particle bath, in comparison to the density
• the metal foam also as a part or region of the composite material, is designed to be closed-pored.
• closed, spherical pores allow optimal load transfer over the intact as possible, surrounding the pores cell walls, and thus contribute significantly to the strength of the metal foam and thus a composite material comprising a metal foam.
• a metal foam is closed-pore, if the individual gas volumes therein, in particular two adjoining gas volumes, by a separating solid phase (wall) are separated or at most by small production-related openings (cracks, holes) whose respective cross-section relative to the cross section of the two Gas volume separating solid phase (wall) is small, interconnected.
• the formation of a substantially closed-cell metal foam is preferably carried out, in particular in method step (III).
• the essentially closed-cell metal foam is distinguished by the fact that the individual gas volumes are interconnected at most by small production-related openings (cracks, holes) whose cross-section is small in relation to the cross-section of the solids phase separating the volumes.
• the porosity of the metal foam thus formed is from about 60% to about 92%, preferably from about 80% to about 92%, more preferably about 89.3%.
• the density of the unfoamed bulk material can be from about 90% to about 100% of the density of the raw material.
• the density of the metal foam formed in step (III) can be from about 0.2 g / cm 3 to about 0.5 g / cm 3 for aluminum foam or, corresponding to the density of the non-foamed solid material, a porosity of about 60%. to reach about 92%.
• the method according to the invention may additionally comprise the step (V) forming of the semifinished product provided in step (I) into a molded part, wherein in step (III) and / or (IV) the heating of the resulting molded part takes place instead of the semifinished product.
• the forming of the semifinished product can be carried out by methods known to the person skilled in the art. According to the invention, however, the forming is preferably carried out by a method selected from the group consisting of bending, deep drawing, hydroforming and hot pressing.
• a component comprising a composite material.
• component designates a component or production part that is used alone or together with other components, for example for a device, a machine, a (water, air) vehicle, a building, for a special purpose or special purpose. Furniture or any other end product can be used.
• the component may have a certain, for example, for the interaction with other components necessary, approximately custom-fit, shaping.
• Such shaping can advantageously already be carried out by the additional process step of reshaping described here (step (V)) on the non-foamed (ie foamable) semifinished product, which can be deformed more easily than the metal foam or composite material.
• Fig. 1 shows a composite material according to the invention as a metal foam sandwich in cross-section, which was prepared according to Example 1 in a salt bath.
• the foamable core began to expand evenly after exceeding the solidus temperature and formed a good pore distribution (see FIG. 1).
• the heating rates of the foaming were, depending on the material thickness, between 0.5 K / s and 50 K / s.
• the density of the semifinished product dropped below the density of the salt bath, causing the metal foam sandwich to swell up and the end of the foaming process being easily recognizable.
• the process was also carried out accordingly with a semi-finished product consisting only of a compressed foamable mixture without cover layers.
• the amount of the blowing agent in% by weight (wt .-%) is based on the total amount of the foamable mixture.
• the same process was carried out in the amounts indicated above instead of TiH 2 with the following blowing agents: ZrH 2 , HfH 2 , MgH 2 , CaH 2 , SrH 2 , LiBH 4 and LiAlH 4 and the combinations of TiH 2 with LiBH 4 and TiH 2 with LiAlH 4 .
• Example 2 The procedure was carried out according to Example 1, wherein the salt bath had a temperature of 400 ° C to 500 ° C and the foaming temperature of 380 ° C to 420 ° C.
• the amount of the blowing agent in% by weight (wt .-%) is based on the total amount of the foamable mixture.
• the same procedure was carried out instead of MgH 2 with TiH 2 as blowing agent in the amounts indicated above.
• Example 2 The procedure was carried out according to Example 1, wherein the salt bath had a temperature of 300 ° C to 400 ° C and the foaming temperature of 310 ° C to 380 ° C was.
• blowing agent in% by weight (wt .-%) is based on the total amount of the foamable mixture.
• the same procedure was carried out instead of ZrH 2 with TiH 2 as blowing agent in the amounts indicated above.
• Example 4
• Example 2 The process was carried out according to Example 1, wherein the salt bath had a temperature of 550 ° C to 650 ° C and the foaming temperature of 580 ° C to 630 ° C was.
• the amount of the blowing agent in% by weight (% by weight) is based on the total amount of the foamable mixture.
• Example 5 The procedure was carried out according to Example 1, wherein the salt bath had a temperature of 1200 ° C to 1450 ° C and the foaming temperature of 1 380 ° C to 1420 ° C was.
• the amount of the blowing agent in% by weight (% by weight) is based on the total amount of the foamable mixture.
• Example 2 The process was carried out according to Example 1, wherein the salt bath had a temperature of 1 300 ° C to 1650 ° C and the foaming temperature of 1500 ° C to 1 680 ° C.
• Ti-6Al-2Sn-4Zr-6Mo SrC0 3 (0.8 wt%) Ti-5Al-2Sn-2Zr-4Mo-4Cr or Ti 6.4
• Ti-6Al-2Sn-4Zr-6Mo SrCO 3 (1, 0 wt%) Ti-5Al-2Sn-2Zr-4Mo-4Cr or Ti
• Example 2 The process was carried out according to Example 1, wherein the salt bath had a temperature of 900 ° C to 1 150 ° C and the foaming temperature of 980 ° C to 1 100 ° C was.
• the amount of the blowing agent in% by weight (wt .-%) is based on the total amount of the foamable mixture.
• Example 2 The process was carried out in accordance with Example 1, in which, instead of a salt bath, a fluidized-bed furnace with alumina granules as solid-state particle bath with a granular large was used in a range of about 80 ⁇ to about ⁇ ⁇ .
• the temperature for heating after step (III) was 600 ° C, the residence time in the fluidized bed oven at 3 min.
• AISi8Mg4 was used as the alloy and 0.8% by weight of TiH 2 , based on the total amount of the foamable mixture, as blowing agent.
• the semi-finished product was preheated / heated in a sand bath at 500 ° C. for 15 minutes.
• the foaming was carried out by immersion in the heated solid particle bath.
• the bath for preheating / preheating and for foaming may also be identical.
• the resulting composite material was closed-pored and had a highly homogeneous metal foam between the two cover layers.

Landscapes

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

Applications Claiming Priority (2)

Publications (1)

Family

ID=63642960

Family Applications (1)

Country Status (7)

Families Citing this family (2)

Family Cites Families (25)

• 2017
  • 2017-09-15 DE DE102017121513.1A patent/DE102017121513A1/de active Pending
• 2018
  • 2018-09-14 KR KR1020227027362A patent/KR102498753B1/ko active IP Right Grant
  • 2018-09-14 EP EP18773122.9A patent/EP3661677A1/de active Pending
  • 2018-09-14 CN CN201880074383.3A patent/CN111511488B/zh active Active
  • 2018-09-14 KR KR1020207010717A patent/KR20200079243A/ko active Application Filing
  • 2018-09-14 US US16/646,770 patent/US11745262B2/en active Active
  • 2018-09-14 WO PCT/EP2018/074869 patent/WO2019053184A1/de unknown
  • 2018-09-14 CA CA3077575A patent/CA3077575A1/en not_active Abandoned

Also Published As

Similar Documents

Legal Events