EP0348380B2 - Utilisation d'un alliage à base de fer pour la fabrication de pièces frittées, présentant une haute résistance à la corrosion, une haute résistance à l'usure ainsi qu'une haute tenacité et résistance à la compression et destinées, en particulier, au travail des matières synthétiques - Google Patents
Utilisation d'un alliage à base de fer pour la fabrication de pièces frittées, présentant une haute résistance à la corrosion, une haute résistance à l'usure ainsi qu'une haute tenacité et résistance à la compression et destinées, en particulier, au travail des matières synthétiques Download PDFInfo
- Publication number
- EP0348380B2 EP0348380B2 EP89890163A EP89890163A EP0348380B2 EP 0348380 B2 EP0348380 B2 EP 0348380B2 EP 89890163 A EP89890163 A EP 89890163A EP 89890163 A EP89890163 A EP 89890163A EP 0348380 B2 EP0348380 B2 EP 0348380B2
- Authority
- EP
- European Patent Office
- Prior art keywords
- iron
- max
- content
- weight
- carbides
- 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
- 239000000956 alloy Substances 0.000 title claims abstract description 26
- 229910045601 alloy Inorganic materials 0.000 title claims abstract description 26
- 238000005260 corrosion Methods 0.000 title claims abstract description 14
- 230000007797 corrosion Effects 0.000 title claims abstract description 14
- 238000004519 manufacturing process Methods 0.000 title claims abstract description 11
- 230000006835 compression Effects 0.000 title description 2
- 238000007906 compression Methods 0.000 title description 2
- 229920002994 synthetic fiber Polymers 0.000 title 1
- 239000011651 chromium Substances 0.000 claims abstract description 34
- 229910052804 chromium Inorganic materials 0.000 claims abstract description 31
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 claims abstract description 27
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 claims abstract description 23
- 239000010936 titanium Substances 0.000 claims abstract description 22
- 239000010955 niobium Substances 0.000 claims abstract description 21
- 229910052720 vanadium Inorganic materials 0.000 claims abstract description 19
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 claims abstract description 18
- 229910052758 niobium Inorganic materials 0.000 claims abstract description 18
- 229910052719 titanium Inorganic materials 0.000 claims abstract description 18
- 229910052799 carbon Inorganic materials 0.000 claims abstract description 17
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims abstract description 16
- 150000001247 metal acetylides Chemical class 0.000 claims abstract description 16
- 229910052742 iron Inorganic materials 0.000 claims abstract description 13
- 229910052750 molybdenum Inorganic materials 0.000 claims abstract description 13
- 239000000203 mixture Substances 0.000 claims abstract description 10
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 claims abstract description 9
- 239000011159 matrix material Substances 0.000 claims abstract description 9
- 229910052757 nitrogen Inorganic materials 0.000 claims abstract description 9
- 239000004033 plastic Substances 0.000 claims abstract description 9
- 229920003023 plastic Polymers 0.000 claims abstract description 9
- ZOKXTWBITQBERF-UHFFFAOYSA-N Molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 claims abstract description 8
- GUCVJGMIXFAOAE-UHFFFAOYSA-N niobium atom Chemical compound [Nb] GUCVJGMIXFAOAE-UHFFFAOYSA-N 0.000 claims abstract description 8
- WFKWXMTUELFFGS-UHFFFAOYSA-N tungsten Chemical compound [W] WFKWXMTUELFFGS-UHFFFAOYSA-N 0.000 claims abstract description 8
- LEONUFNNVUYDNQ-UHFFFAOYSA-N vanadium atom Chemical compound [V] LEONUFNNVUYDNQ-UHFFFAOYSA-N 0.000 claims abstract description 8
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims abstract description 7
- 229910052782 aluminium Inorganic materials 0.000 claims abstract description 7
- ZOXJGFHDIHLPTG-UHFFFAOYSA-N Boron Chemical compound [B] ZOXJGFHDIHLPTG-UHFFFAOYSA-N 0.000 claims abstract description 6
- 239000011733 molybdenum Substances 0.000 claims abstract description 6
- 229910052721 tungsten Inorganic materials 0.000 claims abstract description 6
- 239000010937 tungsten Substances 0.000 claims abstract description 6
- 229910052796 boron Inorganic materials 0.000 claims abstract description 5
- 239000004411 aluminium Substances 0.000 claims abstract description 4
- 239000012535 impurity Substances 0.000 claims abstract description 4
- 238000002360 preparation method Methods 0.000 claims abstract 2
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 claims description 10
- NINIDFKCEFEMDL-UHFFFAOYSA-N Sulfur Chemical compound [S] NINIDFKCEFEMDL-UHFFFAOYSA-N 0.000 claims description 7
- PWHULOQIROXLJO-UHFFFAOYSA-N Manganese Chemical compound [Mn] PWHULOQIROXLJO-UHFFFAOYSA-N 0.000 claims description 6
- OAICVXFJPJFONN-UHFFFAOYSA-N Phosphorus Chemical compound [P] OAICVXFJPJFONN-UHFFFAOYSA-N 0.000 claims description 6
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 claims description 6
- 229910052710 silicon Inorganic materials 0.000 claims description 6
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 claims description 5
- GUTLYIVDDKVIGB-UHFFFAOYSA-N cobalt atom Chemical compound [Co] GUTLYIVDDKVIGB-UHFFFAOYSA-N 0.000 claims description 5
- 229910052759 nickel Inorganic materials 0.000 claims description 5
- 229910052748 manganese Inorganic materials 0.000 claims description 4
- 239000011572 manganese Substances 0.000 claims description 4
- 229910052698 phosphorus Inorganic materials 0.000 claims description 4
- 239000011574 phosphorus Substances 0.000 claims description 4
- 238000007493 shaping process Methods 0.000 claims description 4
- 239000010703 silicon Substances 0.000 claims description 4
- 238000005496 tempering Methods 0.000 claims description 4
- 239000010941 cobalt Substances 0.000 claims description 3
- 229910017052 cobalt Inorganic materials 0.000 claims description 3
- 239000010949 copper Substances 0.000 claims description 3
- 229910052802 copper Inorganic materials 0.000 claims description 3
- 238000005520 cutting process Methods 0.000 claims description 3
- 239000005864 Sulphur Substances 0.000 claims 1
- 238000000137 annealing Methods 0.000 abstract description 3
- 239000000463 material Substances 0.000 description 24
- 229910000831 Steel Inorganic materials 0.000 description 10
- 239000010959 steel Substances 0.000 description 10
- 230000000694 effects Effects 0.000 description 8
- 239000000843 powder Substances 0.000 description 7
- 238000000227 grinding Methods 0.000 description 6
- 230000015572 biosynthetic process Effects 0.000 description 4
- 238000010438 heat treatment Methods 0.000 description 4
- 238000000034 method Methods 0.000 description 4
- 239000000523 sample Substances 0.000 description 4
- 229910052717 sulfur Inorganic materials 0.000 description 4
- 239000011593 sulfur Substances 0.000 description 4
- QTBSBXVTEAMEQO-UHFFFAOYSA-N Acetic acid Chemical compound CC(O)=O QTBSBXVTEAMEQO-UHFFFAOYSA-N 0.000 description 3
- 238000005275 alloying Methods 0.000 description 2
- PNEYBMLMFCGWSK-UHFFFAOYSA-N aluminium oxide Inorganic materials [O-2].[O-2].[O-2].[Al+3].[Al+3] PNEYBMLMFCGWSK-UHFFFAOYSA-N 0.000 description 2
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 2
- 238000005452 bending Methods 0.000 description 2
- 239000002775 capsule Substances 0.000 description 2
- 238000006243 chemical reaction Methods 0.000 description 2
- 229910052593 corundum Inorganic materials 0.000 description 2
- 238000009689 gas atomisation Methods 0.000 description 2
- 229910052760 oxygen Inorganic materials 0.000 description 2
- 239000001301 oxygen Substances 0.000 description 2
- 238000003825 pressing Methods 0.000 description 2
- 239000000126 substance Substances 0.000 description 2
- 229910001845 yogo sapphire Inorganic materials 0.000 description 2
- UCKMPCXJQFINFW-UHFFFAOYSA-N Sulphide Chemical compound [S-2] UCKMPCXJQFINFW-UHFFFAOYSA-N 0.000 description 1
- 230000002411 adverse Effects 0.000 description 1
- 239000003795 chemical substances by application Substances 0.000 description 1
- 238000005352 clarification Methods 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 238000001816 cooling Methods 0.000 description 1
- 239000000945 filler Substances 0.000 description 1
- 238000005242 forging Methods 0.000 description 1
- 238000001513 hot isostatic pressing Methods 0.000 description 1
- 239000000155 melt Substances 0.000 description 1
- 150000004767 nitrides Chemical class 0.000 description 1
- 238000004663 powder metallurgy Methods 0.000 description 1
- 239000002244 precipitate Substances 0.000 description 1
- 238000007670 refining Methods 0.000 description 1
- 150000003839 salts Chemical class 0.000 description 1
- 238000010583 slow cooling Methods 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 238000007711 solidification Methods 0.000 description 1
- 230000008023 solidification Effects 0.000 description 1
- 239000007921 spray Substances 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
Classifications
-
- 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
- C22C33/0278—Making ferrous alloys by powder metallurgy characterised by the range of the alloying elements with at least one alloying element having a minimum content above 5%
- C22C33/0285—Making ferrous alloys by powder metallurgy characterised by the range of the alloying elements with at least one alloying element having a minimum content above 5% with Cr, Co, or Ni having a minimum content higher than 5%
Definitions
- the invention relates to the use of an iron-based alloy with a special composition as a material for the powder metallurgical production of parts with high corrosion resistance, high wear resistance and high toughness and pressure resistance, preferably for plastic molds, machine parts and tools for non-cutting shaping.
- a material for the powder metallurgical production of parts with high corrosion resistance, high wear resistance and high toughness and pressure resistance preferably for plastic molds, machine parts and tools for non-cutting shaping.
- shaping parts are exposed to chemical and abrasive stresses at the same time, whereby these parts must have high material toughness, high pressure resistance and special material homogeneity due to the mechanical stresses.
- Such requirements are placed, for example, on materials that are used in devices for pressing fiber-reinforced or filler-containing plastics. Austenitic steels or chromium steels with a chromium content of approx.
- alloys according to DIN material no. are used for mechanical components such as screws etc. and also for forming and pressing tools, which are particularly exposed to corrosive stresses. 1.4528. Although such materials have sufficient corrosion resistance, the wear behavior is usually unsatisfactory in practical operation. In order to improve or increase the wear resistance and the hardness of the steel, attempts have also been made to increase the carbide content of the alloy by means of higher carbon contents. These steels, for example alloys according to DIN material no. 1.2080 and material no. 1.2379, with a carbon content of approx. 2% and a chromium content of approx.
- the object of the invention is to avoid the above disadvantages and, in particular, to create materials which can be used advantageously for the plastics processing industry and which, due to a special composition when using certain manufacturing processes, provide high corrosion resistance, high wear resistance and high pressure resistance have good toughness properties.
- the material has a niobium content of 0.2 to 3.0 and / or a titanium content of 0.2 to 3.5 and / or a boron content of 0.001 to 0.002. It is particularly preferred if the value is formed from (% Cr - 13) + 4.4x (% V - 3) + 2x (% Nb) + 4.2x (Ti) is at least 10.0.
- the parts which are produced from the alloy used according to the invention by a powder metallurgy manufacturing process must have a chromium concentration in all parts of the matrix of at least 13% after hardening and tempering.
- the alloy according to the invention from a minimum value, which takes into account the concentrations and the respective effect with the mutual influence of the carbide-forming elements chromium, vanadium, niobium and titanium, and which determines the wear resistance of the material in particular, in certain cases Limits set carbon contents and when using powder metallurgical manufacturing processes, materials that have high corrosion resistance, high wear resistance, high pressure resistance and high toughness at the same time and are advantageous, especially for the construction of plastic molds, can be used, the hardened and tempered state of the Chromium content in all areas of the matrix and the proportion as well as the composition and the grain size of the carbides can be adjusted according to the invention.
- chromium is a carbide former that can form M23C6 carbides with carbon in certain carbon activities and in the presence of molybdenum and vanadium in addition to M7C3 carbides. It is therefore important that the steel contains at least 16% by weight of chromium, but at most contains 29% by weight of chromium, because higher chromium concentrations lead to embrittlement of the material. Molybdenum in contents of 0.4 to 2.5% by weight and tungsten in Levels of 0.3 to 2.0% by weight cause an increase in secondary hardness in the heat treatment due to the formation of fine carbides and are important for adjusting the carbon activity of the alloy.
- Aluminum can be alloyed as an element with a high affinity for oxygen and a high affinity for nitrogen in concentrations of up to 1% by weight to adjust the low oxygen content of the steel and to avoid grain growth, whereby advantageous effects on the conversion behavior and the toughness of the material can also be achieved. It was also found that a minimum value of the alloy, formed from the concentrations of the carbide- and nitride-forming elements chromium, tungsten, niobium, titanium and certain action factors of these elements is required for the setting of the desired mechanical properties of the part, by increasing this Worth an improvement in wear resistance and compressive strength with a slight decrease in toughness.
- the carbon content is set within narrow limits depending on the contents and on certain operating parameters of the carbide-forming elements in the steel in order to obtain the desired properties of the parts.
- Powder-metallurgical production of the parts is essential because this significantly improves their isotropic properties of the material and the grain size of the precipitates or intermetallic phases can be kept small. Carbides with grain sizes over 14 ⁇ m significantly impair the mechanical properties, in particular the bending strength of the parts.
- the powder can be produced using all suitable processes, in particular using gas atomization processes, after which, if appropriate, compacting is carried out by hot isostatic pressing and / or by hot-working the powder in suitable casings.
- Iron and manufacturing-related impurities as the rest an alloy powder was produced in the gas atomization process. After the powder had been poured into a capsule with a diameter of 250 mm and the capsule had been evacuated and sealed gas-tight, it was thermoformed at 1110 ° C. using a 6-fold degree of deformation. After soft annealing at 880 to 900 ° C and slow cooling, plastic molds were made from the forging rod. The hardness of the material was around 280 HB. The parts were hardened after heating to a temperature of 1140 ° C. by cooling in a warm bath, whereupon a hardness value of 61 HRC was measured. After tempering at 540 ° C the material hardness was 59 HRC.
- the 0.2% compression limit was used to determine the compressive strength, the value being 2015 N / mm.
- the wear behavior of the part was tested in the grinding wheel test, in which a steel disc rotates in a corundum-water mixture, against which the sample is pressed.
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Powder Metallurgy (AREA)
- Moulds For Moulding Plastics Or The Like (AREA)
- Mounting, Exchange, And Manufacturing Of Dies (AREA)
- Laminated Bodies (AREA)
- Compositions Of Macromolecular Compounds (AREA)
- Manufacture Of Metal Powder And Suspensions Thereof (AREA)
Claims (6)
- Utilisation d'un alliage à base de fer, dont la composition en % de poids est la suivante :Silicium 0.6 max.Manganèse 0.6 max.Soufre 0.015 max.Phosphore 0.02 max.Chrome 18.0 - 25.0Molybdène 0,6 - 1,7Tungstène 0,5 - 1,5Vanadium 3,5 - 5,6Titane jusqu'à 5,0Aluminium jusqu'à 1,0Nickel 0,5 max.Cobalt 0,5 max.Cuivre 0,4 max.Bore jusqu'à 0,03Azote 0,03 jusqu'à 0,1Niobium jusqu'à 5,0Fer et impuretés dues à la fabrication pour le reste, la valeur représentée par
étant supérieure à 8,8 et la teneur en carbone de l'alliage s'élevant pour le minimum à la relation : et pour le maximum à la relation : cet alliage servant à la fabrication de pièces frittées présentant une haute résistance à la corrosion et une haute résistance à l'usure,ainsi qu'une haute ténacité et résistance à la compression, destinées, en particulier, à des moules pour matières synthétiques, à des pièces de machines et à des outillages pour formage, sous réserve qu'après le durcissement et le revenu, la matrice présente une teneur en chrome d'au moins 13% et que la teneur en carbure s'élève en volume au minimum à 25%, dans au moins 5% en volume de carbure-MC, la grosseur de grain du carbure étant inférieure à 14 µm. - Utilisation d'un alliage à base de fer selon l'une des revendications 1 ou 2, présentant une teneur en niobium s'élevant, quant au % en poids, de 0,2 à 3,0.
- Utilisation d'un alliage à base de fer selon l'une des revendications; 1 à 3, dont la teneur en titane s'élève de 0, 2 à 3, 5,
- Utilisation d'un alliage à base de fer selon l'une des revendications 1 à 4, dont la teneur en bore s'élève de 0,001 à 0,002.
- Utilisation d'un alliage à base de fer selon les revendications 1 à 5, dont la teneur en carbone s'élève, quant au % en poids au minimum à 1,8, mais au plus, cependant,à 6,2.
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| AT0159988A AT393642B (de) | 1988-06-21 | 1988-06-21 | Verwendung einer eisenbasislegierung zur pulvermetallurgischen herstellung von teilen mit hoher korrosionsbestaendigkeit, hoher verschleissfestigkeit sowie hoher zaehigkeit und druckfestigkeit, insbesondere fuer die kunststoffverarbeitung |
| AT1599/88 | 1988-06-21 |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| EP0348380A1 EP0348380A1 (fr) | 1989-12-27 |
| EP0348380B1 EP0348380B1 (fr) | 1992-11-19 |
| EP0348380B2 true EP0348380B2 (fr) | 1996-04-17 |
Family
ID=3516903
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| EP89890163A Expired - Lifetime EP0348380B2 (fr) | 1988-06-21 | 1989-06-14 | Utilisation d'un alliage à base de fer pour la fabrication de pièces frittées, présentant une haute résistance à la corrosion, une haute résistance à l'usure ainsi qu'une haute tenacité et résistance à la compression et destinées, en particulier, au travail des matières synthétiques |
Country Status (8)
| Country | Link |
|---|---|
| EP (1) | EP0348380B2 (fr) |
| JP (1) | JP2583451B2 (fr) |
| AT (2) | AT393642B (fr) |
| AU (1) | AU615756B2 (fr) |
| DE (1) | DE58902742D1 (fr) |
| ES (1) | ES2052971T5 (fr) |
| PT (1) | PT90925B (fr) |
| ZA (1) | ZA894703B (fr) |
Families Citing this family (18)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2684736B2 (ja) * | 1988-12-27 | 1997-12-03 | 大同特殊鋼株式会社 | 粉末冷間工具鋼 |
| AT405193B (de) * | 1995-01-16 | 1999-06-25 | Boehler Edelstahl | Verwendung einer chromhältigen, martensitischen eisenbasislegierung für kunststofformen |
| GB2298869B (en) * | 1995-03-10 | 1999-03-03 | Powdrex Ltd | Stainless steel powders and articles produced therefrom by powder metallurgy |
| US5679908A (en) * | 1995-11-08 | 1997-10-21 | Crucible Materials Corporation | Corrosion resistant, high vanadium, powder metallurgy tool steel articles with improved metal to metal wear resistance and a method for producing the same |
| US5900560A (en) * | 1995-11-08 | 1999-05-04 | Crucible Materials Corporation | Corrosion resistant, high vanadium, powder metallurgy tool steel articles with improved metal to metal wear resistance and method for producing the same |
| DE19924515A1 (de) * | 1999-05-28 | 2000-11-30 | Edelstahl Witten Krefeld Gmbh | Sprühkompaktierter Stahl, Verfahren zu seiner Herstellung und Verbundwerkstoff |
| ATE291645T1 (de) * | 2001-11-13 | 2005-04-15 | Fundacion Inasmet | Verfahren zur herstellung von produkten aus carbidverstärkten baumetallmaterialien |
| RU2283888C2 (ru) * | 2001-11-13 | 2006-09-20 | Фундасьон Инасмет | Изготовление продукта из конструкционных металлических материалов, армированных карбидами |
| SE0200429D0 (sv) * | 2002-02-15 | 2002-02-15 | Uddeholm Tooling Ab | Stållegering och verktyg tillverkat av stållegeringen |
| US20060231167A1 (en) * | 2005-04-18 | 2006-10-19 | Hillstrom Marshall D | Durable, wear-resistant punches and dies |
| AT501794B1 (de) * | 2005-04-26 | 2008-06-15 | Boehler Edelstahl | Kunststoffform |
| SE535090C2 (sv) * | 2010-03-17 | 2012-04-10 | Uddeholms Ab | Förfarande för framställning av en slitplatta för en bandsågsbladstyrning, en sådan slitplatta, samt användning av ett stålmaterial för tillverkning av slitplattan |
| CN103060700B (zh) * | 2013-01-07 | 2014-12-31 | 北京工业大学 | 硼化物颗粒强化Fe-Cr-Al复合材料及其制造方法 |
| CN104878298B (zh) * | 2015-05-15 | 2017-05-03 | 安泰科技股份有限公司 | 粉末冶金耐磨损耐腐蚀合金 |
| DE102017115396A1 (de) * | 2017-07-10 | 2019-01-10 | Saar-Pulvermetall GmbH | Rolle für eine Mahl- oder/und Pressvorrichtung, insbesondere Kollerrolle für eine Presse zur Herstellung von Pellets, und Verfahren zur Herstellung der Rolle |
| JP7572384B2 (ja) | 2019-07-09 | 2024-10-23 | エリコン メテコ(ユーエス)インコーポレイテッド | 耐摩耗性と耐食性のために設計された鉄ベースの合金 |
| CN111850427A (zh) * | 2020-06-07 | 2020-10-30 | 江苏钢银智能制造有限公司 | 一种合金钢材料及其钢板材加工铸造工艺 |
| JP2022182485A (ja) * | 2021-05-28 | 2022-12-08 | 山陽特殊製鋼株式会社 | 耐食性に優れた工具鋼 |
Family Cites Families (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CA953540A (en) * | 1970-08-28 | 1974-08-27 | Hoganas Ab | High alloy steel powders and their consolidation into homogeneous tool steel |
| DE2204886C3 (de) * | 1972-02-02 | 1979-11-22 | Gfe Gesellschaft Fuer Elektrometallurgie Mbh, 4000 Duesseldorf | Verfahren zur pulvermetallurgischen Herstellung von Schnellarbeitsstahl-Formkörpern |
| US4249945A (en) * | 1978-09-20 | 1981-02-10 | Crucible Inc. | Powder-metallurgy steel article with high vanadium-carbide content |
| SE446277B (sv) * | 1985-01-16 | 1986-08-25 | Kloster Speedsteel Ab | Vanadinhaltigt verktygsstal framstellt av metallpulver och sett vid dess framstellning |
| US4765836A (en) * | 1986-12-11 | 1988-08-23 | Crucible Materials Corporation | Wear and corrosion resistant articles made from pm alloyed irons |
-
1988
- 1988-06-21 AT AT0159988A patent/AT393642B/de not_active IP Right Cessation
-
1989
- 1989-06-08 JP JP1144323A patent/JP2583451B2/ja not_active Expired - Lifetime
- 1989-06-14 ES ES89890163T patent/ES2052971T5/es not_active Expired - Lifetime
- 1989-06-14 DE DE8989890163T patent/DE58902742D1/de not_active Expired - Lifetime
- 1989-06-14 EP EP89890163A patent/EP0348380B2/fr not_active Expired - Lifetime
- 1989-06-14 AT AT89890163T patent/ATE82595T1/de not_active IP Right Cessation
- 1989-06-20 AU AU36662/89A patent/AU615756B2/en not_active Ceased
- 1989-06-21 ZA ZA894703A patent/ZA894703B/xx unknown
- 1989-06-21 PT PT90925A patent/PT90925B/pt not_active IP Right Cessation
Also Published As
| Publication number | Publication date |
|---|---|
| AT393642B (de) | 1991-11-25 |
| ATA159988A (de) | 1991-05-15 |
| ES2052971T5 (es) | 1996-10-01 |
| PT90925B (pt) | 1997-10-31 |
| JP2583451B2 (ja) | 1997-02-19 |
| ATE82595T1 (de) | 1992-12-15 |
| EP0348380A1 (fr) | 1989-12-27 |
| PT90925A (pt) | 1989-12-29 |
| ES2052971T3 (es) | 1994-07-16 |
| EP0348380B1 (fr) | 1992-11-19 |
| AU3666289A (en) | 1990-01-25 |
| ZA894703B (en) | 1992-01-29 |
| AU615756B2 (en) | 1991-10-10 |
| DE58902742D1 (de) | 1992-12-24 |
| JPH0277556A (ja) | 1990-03-16 |
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