EP0149210B1 - Verfahren zum Herstellen hochfester, duktiler Körper aus Kohlenstoffreichen Eisenbasislegierungen - Google Patents
Verfahren zum Herstellen hochfester, duktiler Körper aus Kohlenstoffreichen Eisenbasislegierungen Download PDFInfo
- Publication number
- EP0149210B1 EP0149210B1 EP84116080A EP84116080A EP0149210B1 EP 0149210 B1 EP0149210 B1 EP 0149210B1 EP 84116080 A EP84116080 A EP 84116080A EP 84116080 A EP84116080 A EP 84116080A EP 0149210 B1 EP0149210 B1 EP 0149210B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- iron
- carbon
- powder
- process step
- less
- 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.)
- Expired - Lifetime
Links
- 238000000034 method Methods 0.000 title claims description 59
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 title claims description 56
- 229910045601 alloy Inorganic materials 0.000 title claims description 46
- 239000000956 alloy Substances 0.000 title claims description 46
- 229910052799 carbon Inorganic materials 0.000 title claims description 29
- 229910052742 iron Inorganic materials 0.000 title claims description 28
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 title claims description 27
- 230000008569 process Effects 0.000 title claims description 22
- 238000004519 manufacturing process Methods 0.000 title claims description 7
- 239000000843 powder Substances 0.000 claims description 24
- 239000002245 particle Substances 0.000 claims description 21
- 239000011651 chromium Substances 0.000 claims description 14
- 230000000930 thermomechanical effect Effects 0.000 claims description 14
- 229910000859 α-Fe Inorganic materials 0.000 claims description 14
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 claims description 11
- 229910052804 chromium Inorganic materials 0.000 claims description 11
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 claims description 10
- 238000010791 quenching Methods 0.000 claims description 10
- 230000000171 quenching effect Effects 0.000 claims description 9
- 238000007596 consolidation process Methods 0.000 claims description 8
- 229910052751 metal Inorganic materials 0.000 claims description 8
- 239000002184 metal Substances 0.000 claims description 8
- 229910052710 silicon Inorganic materials 0.000 claims description 8
- 239000010703 silicon Substances 0.000 claims description 8
- ZOXJGFHDIHLPTG-UHFFFAOYSA-N Boron Chemical compound [B] ZOXJGFHDIHLPTG-UHFFFAOYSA-N 0.000 claims description 7
- 229910052796 boron Inorganic materials 0.000 claims description 7
- 239000011159 matrix material Substances 0.000 claims description 6
- 229910052759 nickel Inorganic materials 0.000 claims description 6
- 239000000654 additive Substances 0.000 claims description 5
- WPBNNNQJVZRUHP-UHFFFAOYSA-L manganese(2+);methyl n-[[2-(methoxycarbonylcarbamothioylamino)phenyl]carbamothioyl]carbamate;n-[2-(sulfidocarbothioylamino)ethyl]carbamodithioate Chemical compound [Mn+2].[S-]C(=S)NCCNC([S-])=S.COC(=O)NC(=S)NC1=CC=CC=C1NC(=S)NC(=O)OC WPBNNNQJVZRUHP-UHFFFAOYSA-L 0.000 claims description 5
- 238000000889 atomisation Methods 0.000 claims description 4
- 229910052748 manganese Inorganic materials 0.000 claims description 4
- 239000011572 manganese Substances 0.000 claims description 4
- PWHULOQIROXLJO-UHFFFAOYSA-N Manganese Chemical compound [Mn] PWHULOQIROXLJO-UHFFFAOYSA-N 0.000 claims description 3
- BUGBHKTXTAQXES-UHFFFAOYSA-N Selenium Chemical compound [Se] BUGBHKTXTAQXES-UHFFFAOYSA-N 0.000 claims description 3
- 229910052787 antimony Inorganic materials 0.000 claims description 3
- WATWJIUSRGPENY-UHFFFAOYSA-N antimony atom Chemical compound [Sb] WATWJIUSRGPENY-UHFFFAOYSA-N 0.000 claims description 3
- 229910052797 bismuth Inorganic materials 0.000 claims description 3
- JCXGWMGPZLAOME-UHFFFAOYSA-N bismuth atom Chemical compound [Bi] JCXGWMGPZLAOME-UHFFFAOYSA-N 0.000 claims description 3
- 238000001513 hot isostatic pressing Methods 0.000 claims description 3
- 229910052711 selenium Inorganic materials 0.000 claims description 3
- 239000011669 selenium Substances 0.000 claims description 3
- 229910052714 tellurium Inorganic materials 0.000 claims description 3
- PORWMNRCUJJQNO-UHFFFAOYSA-N tellurium atom Chemical compound [Te] PORWMNRCUJJQNO-UHFFFAOYSA-N 0.000 claims description 3
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 claims description 2
- OAICVXFJPJFONN-UHFFFAOYSA-N Phosphorus Chemical compound [P] OAICVXFJPJFONN-UHFFFAOYSA-N 0.000 claims description 2
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 claims description 2
- 239000010941 cobalt Substances 0.000 claims description 2
- 229910017052 cobalt Inorganic materials 0.000 claims description 2
- GUTLYIVDDKVIGB-UHFFFAOYSA-N cobalt atom Chemical compound [Co] GUTLYIVDDKVIGB-UHFFFAOYSA-N 0.000 claims description 2
- 238000001125 extrusion Methods 0.000 claims description 2
- 238000005242 forging Methods 0.000 claims description 2
- 229910052749 magnesium Inorganic materials 0.000 claims description 2
- 239000011777 magnesium Substances 0.000 claims description 2
- 229910052758 niobium Inorganic materials 0.000 claims description 2
- 239000010955 niobium Substances 0.000 claims description 2
- GUCVJGMIXFAOAE-UHFFFAOYSA-N niobium atom Chemical compound [Nb] GUCVJGMIXFAOAE-UHFFFAOYSA-N 0.000 claims description 2
- 229910052698 phosphorus Inorganic materials 0.000 claims description 2
- 239000011574 phosphorus Substances 0.000 claims description 2
- 239000010936 titanium Substances 0.000 claims description 2
- 229910052719 titanium Inorganic materials 0.000 claims description 2
- 230000000087 stabilizing effect Effects 0.000 claims 1
- 239000000463 material Substances 0.000 description 11
- 239000012071 phase Substances 0.000 description 11
- 239000000155 melt Substances 0.000 description 9
- 229910000640 Fe alloy Inorganic materials 0.000 description 8
- 229910001566 austenite Inorganic materials 0.000 description 7
- 229910001567 cementite Inorganic materials 0.000 description 7
- 229910002804 graphite Inorganic materials 0.000 description 7
- 239000010439 graphite Substances 0.000 description 7
- KSOKAHYVTMZFBJ-UHFFFAOYSA-N iron;methane Chemical compound C.[Fe].[Fe].[Fe] KSOKAHYVTMZFBJ-UHFFFAOYSA-N 0.000 description 6
- 150000001247 metal acetylides Chemical class 0.000 description 6
- 238000000137 annealing Methods 0.000 description 5
- 230000009466 transformation Effects 0.000 description 5
- 229910001018 Cast iron Inorganic materials 0.000 description 4
- 229910000831 Steel Inorganic materials 0.000 description 4
- 230000015572 biosynthetic process Effects 0.000 description 4
- 238000001816 cooling Methods 0.000 description 4
- 210000001787 dendrite Anatomy 0.000 description 4
- 230000000694 effects Effects 0.000 description 4
- 238000010438 heat treatment Methods 0.000 description 4
- 239000000203 mixture Substances 0.000 description 4
- 239000002244 precipitate Substances 0.000 description 4
- 238000012545 processing Methods 0.000 description 4
- 239000010959 steel Substances 0.000 description 4
- 238000009792 diffusion process Methods 0.000 description 3
- 238000009826 distribution Methods 0.000 description 3
- 230000002349 favourable effect Effects 0.000 description 3
- 229910000734 martensite Inorganic materials 0.000 description 3
- 150000002739 metals Chemical class 0.000 description 3
- 239000000523 sample Substances 0.000 description 3
- 238000005496 tempering Methods 0.000 description 3
- 229910001339 C alloy Inorganic materials 0.000 description 2
- 229910000975 Carbon steel Inorganic materials 0.000 description 2
- 230000008901 benefit Effects 0.000 description 2
- 238000006243 chemical reaction Methods 0.000 description 2
- 238000002425 crystallisation Methods 0.000 description 2
- 230000008025 crystallization Effects 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 230000007246 mechanism Effects 0.000 description 2
- 238000002074 melt spinning Methods 0.000 description 2
- 238000010310 metallurgical process Methods 0.000 description 2
- 238000001000 micrograph Methods 0.000 description 2
- 238000001556 precipitation Methods 0.000 description 2
- 238000005096 rolling process Methods 0.000 description 2
- 238000005204 segregation Methods 0.000 description 2
- 239000007787 solid Substances 0.000 description 2
- 238000004781 supercooling Methods 0.000 description 2
- 238000012360 testing method Methods 0.000 description 2
- TWQHGBJNKVFWIU-UHFFFAOYSA-N 8-[4-(4-quinolin-2-ylpiperazin-1-yl)butyl]-8-azaspiro[4.5]decane-7,9-dione Chemical compound C1C(=O)N(CCCCN2CCN(CC2)C=2N=C3C=CC=CC3=CC=2)C(=O)CC21CCCC2 TWQHGBJNKVFWIU-UHFFFAOYSA-N 0.000 description 1
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 description 1
- 230000004308 accommodation Effects 0.000 description 1
- 238000005275 alloying Methods 0.000 description 1
- 238000004458 analytical method Methods 0.000 description 1
- 238000013459 approach Methods 0.000 description 1
- 244000052616 bacterial pathogen Species 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- 238000001311 chemical methods and process Methods 0.000 description 1
- 239000007795 chemical reaction product Substances 0.000 description 1
- 230000015271 coagulation Effects 0.000 description 1
- 238000005345 coagulation Methods 0.000 description 1
- 230000006835 compression Effects 0.000 description 1
- 238000007906 compression Methods 0.000 description 1
- 239000013078 crystal Substances 0.000 description 1
- 230000001419 dependent effect Effects 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 230000018109 developmental process Effects 0.000 description 1
- 230000035784 germination Effects 0.000 description 1
- 229910052734 helium Inorganic materials 0.000 description 1
- 239000001307 helium Substances 0.000 description 1
- SWQJXJOGLNCZEY-UHFFFAOYSA-N helium atom Chemical compound [He] SWQJXJOGLNCZEY-UHFFFAOYSA-N 0.000 description 1
- 239000012535 impurity Substances 0.000 description 1
- 230000002401 inhibitory effect Effects 0.000 description 1
- 150000002505 iron Chemical class 0.000 description 1
- 238000002844 melting Methods 0.000 description 1
- 230000008018 melting Effects 0.000 description 1
- 238000013508 migration Methods 0.000 description 1
- 230000005012 migration Effects 0.000 description 1
- 238000004881 precipitation hardening Methods 0.000 description 1
- 239000000047 product Substances 0.000 description 1
- 238000007712 rapid solidification Methods 0.000 description 1
- 229920006395 saturated elastomer Polymers 0.000 description 1
- 239000011265 semifinished product Substances 0.000 description 1
- 239000007790 solid phase Substances 0.000 description 1
- 239000006104 solid solution Substances 0.000 description 1
- 238000007711 solidification Methods 0.000 description 1
- 230000008023 solidification Effects 0.000 description 1
- 239000000243 solution Substances 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
- 238000007669 thermal treatment Methods 0.000 description 1
Images
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
- B22F9/00—Making metallic powder or suspensions thereof
- B22F9/02—Making metallic powder or suspensions thereof using physical processes
- B22F9/06—Making metallic powder or suspensions thereof using physical processes starting from liquid material
- B22F9/08—Making metallic powder or suspensions thereof using physical processes starting from liquid material by casting, e.g. through sieves or in water, by atomising or spraying
- B22F9/10—Making metallic powder or suspensions thereof using physical processes starting from liquid material by casting, e.g. through sieves or in water, by atomising or spraying using centrifugal force
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C33/00—Making ferrous alloys
- C22C33/02—Making ferrous alloys by powder metallurgy
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C33/00—Making ferrous alloys
- C22C33/02—Making ferrous alloys by powder metallurgy
- C22C33/0257—Making ferrous alloys by powder metallurgy characterised by the range of the alloying elements
Definitions
- the invention relates to a method for producing high-strength, ductile bodies from carbon-rich iron-based alloys, in which a molten iron-based alloy is quenched, atomized and thermomechanically compressed.
- end products are desired that have a high strength on the one hand, on the other hand, they are also characterized by favorable ductility parameters.
- the heat treatment of the steel or iron or the workpieces made from it i.e. the thermal treatment of the metal in the solid state.
- a grain refinement is achieved by annealing at approx. 800 - 950 ° C and then quenching, which requires a significant increase in strength, but at the same time also increases the brittleness of the workpiece. Subsequent quenching and tempering (for example by so-called tempering) will then cause the workpiece to lose some strength again, but favorable ductility and homogeneity properties can be achieved.
- thermomechanical treatment processes particularly for micro-alloyed structural steels, have recently come to the fore.
- These metals dissolve and, on the other hand, they can be eliminated again specifically, allows the effects of very fine carbonitride particles on the structure and the mechanical properties of the rolled products to be exploited.
- the carbonitrides When the carbonitrides are precipitated in austenite in a relatively fine form during the subsequent austenite transformation, they act as germs and act as a brake against the migration of the phase and grain boundaries.
- thermomechanical technologies as described, for example, by Kaspar et. al. in “Stahl und Eisen” 101 (1981), 721 "Metallurgical processes during preheating and pre-rolling of microalloyed structural steels" all refer to weldable, i.e. low-carbon steels or iron alloys.
- unalloyed and alloyed cast iron ie iron with a carbon content of more than 1.7% by weight
- the plastic deformability of carbon-rich cast iron alloys is only 1 - 2%. The reason for this is in particular the relatively high volume fraction of carbides (V carbide ⁇ 33%) or the amount, shape and distribution of the carbon separated out as graphite.
- a two-stage powder metallurgical process is also known from British Patent Application 2 116 207, in which a melt is atomized at a high cooling rate and the powder is then thermomechanically treated, that is to say hot consolidated.
- a melt or powder comes with it for use, which contains 0.1 to 1.5% boron. Boron improves supercooling and promotes the formation of a homogeneous and metastable crystallized structure when the melt is atomized with a high cooling rate.
- the melt or alloy contains in principle neither manganese, nor silicon and nickel, which can at best be considered impurities.
- the invention has for its object to apply the aforementioned method to another alloy powder and to show a way of producing workpieces from carbon-rich iron-based alloys which have both a particularly high strength and particularly advantageous ductile properties.
- This object is achieved by a method of the type mentioned in the introduction, in which, according to the invention, an alloy with over 1.7% carbon, over 3.0% nickel and / or manganese, up to 15% chromium and / or cobalt and individually or side by side to 1 % Boron, tellurium, bismuth, selenium, antimony, titanium, niobium, magnesium and phosphorus as well as optionally 2 to 4% silicon, the rest iron is atomized to an average particle diameter of less than 30 ⁇ m and then thermomechanically compressed.
- thermomechanical compression either temperatures below 720 ° C., preferably 650 ° C., are to be regarded as particularly advantageous in the sense of the invention, or the thermomechanical treatment can also be carried out at normal annealing temperatures of 850 to 1000 ° C.
- the first stage of the process the quenching and atomization of the molten metal in such a way that powder particles with a diameter of less than 30 ⁇ m are formed, has the effect that the structure structures obtained by normal solidification conditions, such as coarse dendrites and / or acicular carbides, are changed in favor of a fine crystalline structure.
- This process section is preferably carried out according to the so-called "rapid solidification technology", a temperature gradient of, for example, 104 - 104 K / s being selected. With such a quenching rate, extremely high germination rates can be achieved, however, to keep the germ growth very low due to the short crystallization time until the solid phase is reached.
- the quenching rate should be chosen depending on the alloy and the particular process so that particles with an average diameter that is smaller than 30 microns are available for the second process stage and the phases of the structure that forms in the particles unite Have a diameter that is less than 0.1 microns.
- the quenching according to an exemplary embodiment of the invention is particularly advantageous if additives such as tellurium, bismuth, selenium or antimony, in amounts of up to 1% by weight, achieve a higher supercooling of the melt.
- the rapid cooling from the homogeneous melting phase has the further consequence that the crystals formed do not precipitate out in the total weight composition, since the short diffusion times available are not sufficient to bring about complete segregation.
- a preferred method for carrying out the first method step according to the teaching of the invention is the so-called “melt spinning” method known for low-carbon steels.
- the melt which is saturated with carbon due to its high solubility at high temperatures, is atomized and at the same time extremely quenched, which causes the small particles formed to freeze due to the short diffusion times.
- the carbon dissolved in the melt cannot separate out in the form of graphite, but on the other hand, precipitation in carbide form is only fine-grained possible or even completely excluded if suitable additional alloying elements are added.
- a preferred embodiment of the invention provides that after the completion of the first process stage and before the start of the thermomechanical treatment, the powders are pre-compacted in an intermediate stage to form a blank and / or are encased in a metal container. It can also be provided that the powders are sifted to a grain size of less than 30 microns after atomization. Furthermore, it can be provided that the powders are subjected to a reducing annealing before they are compacted, optionally with deoxidizing additives being added.
- the invention teaches in a first embodiment to work in a temperature range below the A 1 temperature.
- the metastable ⁇ phase and the martensite phase in finely disperse cementite with a grain size can be obtained by hot isostatic pressing, forging or extrusion at temperatures between 600 ° C and 720 ° C, preferably in the range around 650 ° C below 0.5 ⁇ m and fine-grained ferrite with a particle size below 2 ⁇ m can be converted.
- the dendritic microstructure is simultaneously molded into a finely crystalline, equiaxial structure made of spherodized, dispersed carbides in the ferrite.
- the volume fraction of the Carbide particles for example, is over 50% and thus forms the matrix of these high-carbon iron-based alloys.
- this iron-based alloy is adjusted by adding up to 1% by weight of boron to the iron-based alloy in such a way that the powders produced therefrom by the first process step according to the invention also at temperatures between 850 ° C. - 1000 ° C, ie at "normal" processing temperatures, can be treated thermomechanically, since the addition of boron reduces the carbon solubility of the austenite. Materials of ferrite and carbide are then produced in such a process.
- the alloy can also be adjusted by adding nickel and / or manganese, in an order of magnitude greater than 3% by weight, so that iron-based materials with a purely austenitic structure are formed. Also leave these iron base materials treat themselves thermomechanically at normal processing temperatures.
- iron-based alloy is that silicon is added in an order of magnitude of 2-4% by weight to the melt, so that a material with a bainitic matrix and carbides is produced, which is also found in the previous examples mentioned temperatures can be treated.
- superplasticity can be achieved in the temperature range between 600 ° C and 720 ° C with deformation values of up to 1,300% with high strength at the same time.
- the structure, structure, hardness and ductility were tested in the strips obtained.
- the samples were produced according to the so-called "melt spinning” process.
- the fracture appearance of tempered samples is different from that of the as-quenched sample.
- the samples with a content of 6% by weight of chromium and 3% by weight of carbon have different properties after an annealing treatment in that the fracture no longer runs along the former dendrite grain boundaries.
- the samples were produced by the powder atomization method, which allows large quantities of rapidly quenched material to be produced, so that further processing by means of powder metallurgical techniques is possible.
- Creep properties in the temperature range between 500 and 720 ° C were investigated on rapidly quenched strips of Fe-Cr-C alloys. This leads to changes during heating in the form of changes in length, which are due to the residual austenite transformation, precipitations, etc. (1st-3rd tempering stage). Such falsifying effects can be eliminated by heating once at 10 K / min.
- the change in length depending on the temperature in the temperature range of 500 - 600 ° C indicates a normal dislocation creep. In the temperature range of 600 to 650 ° C, however, the creep speed drops. This is due on the coagulation of cementite. Above 650 ° C, up to around 720 ° C, effects are obtained which indicate superplasticity.
- the compacting and compacting of the extremely rapidly quenched Fe-C-Cr powder by a combination of powder metallurgical and thermomechanical process techniques, namely hot isostatic pressing and rolling just below the A 1 transformation temperature, causes profound structural changes in the structure. These consist in the transformation of the metastable ⁇ phase and the martensite into finely disperse cementite with a grain size of less than 0.5 ⁇ m and fine-grained ferrite with a grain size of less than 2 ⁇ m.
- the dendritic microstructure is molded into a finely crystalline, equiaxial structure made of spherodized, dispersed carbides in the ferrite.
- FIG. 2 shows a scanning electron microscope micrograph of the equiaxial microstructure of the compacted and thermomechanically treated high-carbide iron alloys.
- the volume fraction of the carbide particles is approximately 56 vol .-% and thus represents the matrix phase of this high-carbon iron-based alloy.
- the yield stresses and compressive strengths of the two alloys produced according to the invention are different from one another.
- the higher strength values of the chromium-rich alloy are due to the structurally more stable, fine-crystalline structure after the thermomechanical treatment.
- the predominant content of chromium is dissolved in the cementite, stabilizes the carbides and prevents undesired carbide growth.
- a strength-increasing contribution due to the solid solution hardening of the ferrite by the chromium dissolved in the ⁇ -iron can be assumed.
- the optimal superplastic deformation temperature is about 650 ° C.
- the diffusion-controlled accommodation mechanisms of grain boundary sliding are sufficiently thermally activated, and at this temperature the microstructure is stable against a stress or strain-induced grain growth of the cementite and ferrite phase. This applies in particular to the chromium-containing alloy.
- Superplastic materials are generally characterized by high amounts of uniform expansion. In the fracture zone, however, local constrictions can often be found, which are caused by the plastomechanical instabilities due to local hardening processes.
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Powder Metallurgy (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE19833346089 DE3346089A1 (de) | 1983-12-21 | 1983-12-21 | Verfahren zum herstellen hochfester, duktiler koerper aus kohlenstoffreichen eisenbasislegierungen |
DE3346089 | 1983-12-21 |
Publications (3)
Publication Number | Publication Date |
---|---|
EP0149210A2 EP0149210A2 (de) | 1985-07-24 |
EP0149210A3 EP0149210A3 (en) | 1987-07-29 |
EP0149210B1 true EP0149210B1 (de) | 1992-04-29 |
Family
ID=6217490
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP84116080A Expired - Lifetime EP0149210B1 (de) | 1983-12-21 | 1984-12-21 | Verfahren zum Herstellen hochfester, duktiler Körper aus Kohlenstoffreichen Eisenbasislegierungen |
Country Status (2)
Country | Link |
---|---|
EP (1) | EP0149210B1 (enrdf_load_stackoverflow) |
DE (2) | DE3346089A1 (enrdf_load_stackoverflow) |
Families Citing this family (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS6033343A (ja) * | 1983-08-03 | 1985-02-20 | Nippon Piston Ring Co Ltd | 耐摩耗性焼結合金 |
JPH0610321B2 (ja) * | 1985-06-17 | 1994-02-09 | 日本ピストンリング株式会社 | 耐摩耗性焼結合金 |
DE3544759A1 (de) * | 1985-12-18 | 1987-06-19 | Zapp Robert Werkstofftech | Verfahren zum herstellen von werkzeugen |
JP3077410B2 (ja) * | 1992-07-29 | 2000-08-14 | アイシン精機株式会社 | ターボチャージャのタービンハウジング |
EP0808681A4 (en) * | 1995-10-18 | 1999-12-29 | Kawasaki Steel Co | IRON POWDER FOR POWDER METALLURGY, METHOD FOR THE PRODUCTION THEREOF, AND IRON-BASED POWDER MIXTURE FOR POWDER METALLURGY |
JP3694732B2 (ja) * | 2000-05-16 | 2005-09-14 | 独立行政法人産業技術総合研究所 | 高硬度高クロム鋳鉄粉末合金の製造方法 |
Family Cites Families (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
SE317522B (enrdf_load_stackoverflow) * | 1968-04-16 | 1969-11-17 | Hoeganaes Ab | |
JPS599615B2 (ja) * | 1974-09-25 | 1984-03-03 | 株式会社リケン | 超塑性を有する強靭球状黒鉛鋳鉄及び熱処理方法 |
US3951697A (en) * | 1975-02-24 | 1976-04-20 | The Board Of Trustees Of Leland Stanford Junior University | Superplastic ultra high carbon steel |
SE7612279L (sv) * | 1976-11-05 | 1978-05-05 | British Steel Corp | Finfordelat glodgat stalpulver, samt sett att framstella detta. |
US4331478A (en) * | 1979-02-09 | 1982-05-25 | Scm Corporation | Corrosion-resistant stainless steel powder and compacts made therefrom |
BR8200106A (pt) * | 1982-01-11 | 1983-09-13 | Metal Leve Sa | Processo para fabricacao de porta-aneis por metalurgia do po,a partir de ligas ferrosas austeniticas |
GB2116207A (en) * | 1982-03-02 | 1983-09-21 | Marko Materials Inc | Improved tool steels which contain boron and have been processed using a rapid solidification process and method |
-
1983
- 1983-12-21 DE DE19833346089 patent/DE3346089A1/de active Granted
-
1984
- 1984-12-21 DE DE8484116080T patent/DE3485689D1/de not_active Expired - Fee Related
- 1984-12-21 EP EP84116080A patent/EP0149210B1/de not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
DE3346089A1 (de) | 1985-07-18 |
DE3346089C2 (enrdf_load_stackoverflow) | 1988-01-14 |
EP0149210A2 (de) | 1985-07-24 |
EP0149210A3 (en) | 1987-07-29 |
DE3485689D1 (de) | 1992-06-04 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
DE2937724C2 (de) | Pulvermetallurgisch hergestelltes Stahlerzeugnis mit hohem Vanadiumcarbid- Anteil | |
DE69226946T2 (de) | Austenitischer manganstahlblech mit hoher verformbarkeit, festichkeit und schweissbarkeit und verfahren | |
DE60002745T2 (de) | Hochfester rostfreier automatenstahl | |
DE3587572T2 (de) | Verfahren zur Erhöhung der Duktilität von verstärkten Gegenständen, gefertigt aus einer rasch erstarrten Legierung. | |
DE69604902T2 (de) | Rostfreier stahlpuder und ihre verwendung zur herstellung formkörper durch pulvermetallurgie | |
DE60019141T2 (de) | Verfahren zum Herstellen von Produkten aus ausscheidungsgehärtetem, martensitischem, nichtrostendem Stahl und Verwendung des Verfahrens | |
DE3043503A1 (de) | Kristalline metallegierung | |
EP2374560A1 (de) | Verschleißbeständiger Werkstoff | |
DE3043290A1 (de) | Stahllegierung mit einem gehalt an bor | |
DE2606632C2 (de) | Verwendung von Kohlenstoff-Stahl als superplastischer Wirkstoff und Verfahren zu dessen Wärmebehandlung | |
EP3591078A1 (de) | Verwendung eines stahls für ein additives fertigungsverfahren, verfahren zur herstellung eines stahlbauteils und stahlbauteil | |
DE69814896T2 (de) | Stahl und wärmebehandeltes werkzeug, hergestellt in einem integrierten pulvermetallurgischem prozess und die nutzung eines solchen stahles für werkzeuge | |
DE1533275B1 (de) | Verfahren zur pulvermetallurgischen Herstellung von Hartlegierungen | |
DE1298293B (de) | Hochverschleissfeste, bearbeitbare und haertbare Sinterstahllegierung und Verfahren zu deren Herstellung | |
EP3638820A1 (de) | Monotektische aluminium-gleitlagerlegierung und verfahren zu seiner herstellung und damit hergestelltes gleitlager | |
WO2021084025A1 (de) | Korrosionsbeständiger und ausscheidungshärtender stahl, verfahren zur herstellung eines stahlbauteils und stahlbauteil | |
DE102018126719A1 (de) | Additives herstellungsverfahren und pulvermaterial dafür | |
DE69902767T2 (de) | Stahlmaterial und verfahren zu dessen herstellung | |
EP1274872B1 (de) | Verfahren zur herstellung eines stickstofflegierten, sprühkompaktierten stahls, verfahren zu seiner herstellung | |
DE69024582T2 (de) | Stahllegierung zum Anwenden in spritzgegossenen pulvermetallurgisch hergestellten gesinterten Formkörpern | |
AT391324B (de) | Pulvermetallurgisch hergestellter schnellarbeitsstahl, daraus hergestellter verschleissteil und verfahren zu seiner herstellung | |
EP4018006A1 (de) | Werkzeugstahl für kaltarbeits- und schnellarbeitsanwendungen | |
DE69417003T2 (de) | Titanfreier, nickelenthaltender, martensitanohärtbarer Stahl für Stempelblöcke und ein Verfahren zu dessen Herstellung | |
EP0149210B1 (de) | Verfahren zum Herstellen hochfester, duktiler Körper aus Kohlenstoffreichen Eisenbasislegierungen | |
DE69218109T2 (de) | Verdichtete und verfestigte Wirkstoffe aus Aluminium-Legierung |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PUAI | Public reference made under article 153(3) epc to a published international application that has entered the european phase |
Free format text: ORIGINAL CODE: 0009012 |
|
AK | Designated contracting states |
Kind code of ref document: A2 Designated state(s): BE CH DE FR GB IT LI LU NL SE Designated state(s): BE CH DE FR GB IT LI LU NL SE |
|
PUAL | Search report despatched |
Free format text: ORIGINAL CODE: 0009013 |
|
AK | Designated contracting states |
Kind code of ref document: A3 Designated state(s): BE CH DE FR GB IT LI LU NL SE |
|
17P | Request for examination filed |
Effective date: 19880129 |
|
17Q | First examination report despatched |
Effective date: 19890908 |
|
DIN1 | Information on inventor provided before grant (deleted) | ||
RAP1 | Party data changed (applicant data changed or rights of an application transferred) |
Owner name: KAINER, KARL-ULRICH Owner name: FROMMEYER, GEORG, DR. Owner name: BERGMANN, HANS WILHELM, DR.-ING. Owner name: MORDIKE, BARRY LESLIE, PROF. DR. |
|
RIN1 | Information on inventor provided before grant (corrected) |
Inventor name: KAINER, KARL-ULRICH Inventor name: FROMMEYER, GEORG, DR. Inventor name: BERGMANN, HANS WILHELM, DR.-ING. Inventor name: MORDIKE, BARRY LESLIE, PROF. DR. |
|
DIN1 | Information on inventor provided before grant (deleted) | ||
RAP1 | Party data changed (applicant data changed or rights of an application transferred) |
Owner name: FROMMEYER, GEORG, PROF. DR.-ING. |
|
RIN1 | Information on inventor provided before grant (corrected) |
Inventor name: KAINER, KARL-ULRICH, DR. Inventor name: FROMMEYER, GEORG, PROF. DR. Inventor name: BERGMANN, HANS WILHELM, DR.-ING. Inventor name: MORDIKE, BARRY LESLIE, PROF. DR. |
|
GRAA | (expected) grant |
Free format text: ORIGINAL CODE: 0009210 |
|
RAP1 | Party data changed (applicant data changed or rights of an application transferred) |
Owner name: ROBERT ZAPP WERKSTOFFTECHNIK GMBH & CO KG |
|
AK | Designated contracting states |
Kind code of ref document: B1 Designated state(s): BE CH DE FR GB IT LI LU NL SE |
|
REF | Corresponds to: |
Ref document number: 3485689 Country of ref document: DE Date of ref document: 19920604 |
|
GBT | Gb: translation of ep patent filed (gb section 77(6)(a)/1977) | ||
ITF | It: translation for a ep patent filed | ||
ET | Fr: translation filed | ||
PLBE | No opposition filed within time limit |
Free format text: ORIGINAL CODE: 0009261 |
|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT |
|
26N | No opposition filed | ||
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: GB Payment date: 19931206 Year of fee payment: 10 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: LU Payment date: 19931216 Year of fee payment: 10 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: FR Payment date: 19931217 Year of fee payment: 10 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: SE Payment date: 19931227 Year of fee payment: 10 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: NL Payment date: 19931231 Year of fee payment: 10 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: BE Payment date: 19940104 Year of fee payment: 10 |
|
EPTA | Lu: last paid annual fee | ||
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: LU Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 19941221 Ref country code: GB Effective date: 19941221 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: SE Effective date: 19941222 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: BE Effective date: 19941231 |
|
EAL | Se: european patent in force in sweden |
Ref document number: 84116080.7 |
|
BERE | Be: lapsed |
Owner name: ROBERT ZAPP WERKSTOFFTECHNIK G.M.B.H. & CO. K.G. Effective date: 19941231 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: NL Effective date: 19950701 |
|
GBPC | Gb: european patent ceased through non-payment of renewal fee |
Effective date: 19941221 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: FR Effective date: 19950831 |
|
NLV4 | Nl: lapsed or anulled due to non-payment of the annual fee |
Effective date: 19950701 |
|
EUG | Se: european patent has lapsed |
Ref document number: 84116080.7 |
|
REG | Reference to a national code |
Ref country code: FR Ref legal event code: ST |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: CH Payment date: 19981229 Year of fee payment: 15 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: DE Payment date: 19990224 Year of fee payment: 15 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: LI Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 19991231 Ref country code: CH Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 19991231 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: DE Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20001003 |