EP0227001B1 - Verfahren zum Herstellen von Werkzeugen - Google Patents
Verfahren zum Herstellen von Werkzeugen Download PDFInfo
- Publication number
- EP0227001B1 EP0227001B1 EP86117455A EP86117455A EP0227001B1 EP 0227001 B1 EP0227001 B1 EP 0227001B1 EP 86117455 A EP86117455 A EP 86117455A EP 86117455 A EP86117455 A EP 86117455A EP 0227001 B1 EP0227001 B1 EP 0227001B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- process according
- phase
- grain size
- grain
- deformation
- 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
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Classifications
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D8/00—Modifying the physical properties by deformation combined with, or followed by, heat treatment
- C21D8/005—Modifying the physical properties by deformation combined with, or followed by, heat treatment of ferrous alloys
-
- 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
- B22F3/12—Both compacting and sintering
- B22F3/16—Both compacting and sintering in successive or repeated 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
- C22C1/10—Alloys containing non-metals
Definitions
- the invention relates to a method for producing tools from alloyed steels or stellites by thermoforming.
- Tool steels and stellites or hard metals are generally characterized by high levels of carbon, chromium, cobalt, molybdenum, vanadium and tungsten. Together with the corresponding carbides, these elements give the material the necessary strength, in particular wear resistance and hardness. However, this is usually at the expense of toughness and is associated with a corresponding increase in the resistance to deformation.
- a method is known from US Pat. No. 3,951,697 is known in which steels with a very high carbon content are set after a heat treatment at at least 500 ° C by deformation on an equiaxed basic structure with a finely dispersed spherulitic cementite.
- This process is also suitable for the use of powders as the starting material. This is done in such a way that a starting powder with a carbon content of more than 1%, the carbon of which is predominantly in the form of spherulitic cementite, is mixed with an iron powder with a grain size of less than 10 ⁇ m, then compacted and then sintered at 600 to 700 ° C.
- the structure of the sintered compact mainly consists of a coaxial grain with an average grain size of less than 10 ⁇ m and an evenly distributed, mainly spherulitic cementite in the temperature range from 723 to 900 ° C. Apart from powder compaction, no deformation takes place in the known method. In addition, the process only affects iron-carbon materials with a carbon content of over 1.0% and otherwise only impurities such as 0.4 to 0.5% manganese and 0.1 to 0.2% silicon.
- the invention has for its object to provide a method which avoids the aforementioned disadvantages and allows the production of finished parts from alloys, which due to their high deformation resistance normally cannot be deformed or at most can be deformed into a blank which requires machining.
- a stellitic preform with an equiaxial structure and over 30 vol.% Carbidic and / or boridic precipitation phase is thermoformed at 700 to 1000.degree. C., thereby forming a matrix with a grain size of 1 to 3 ⁇ m and one Elimination phase set with a grain size of 0.2 to 1.0 ⁇ m and finally superplastically shaped.
- the small grain size set in the process according to the invention ensures a low yield stress due to grain boundary sliding and thus reduces the required forming force and tool wear.
- the method according to the invention therefore runs in two stages;
- the first stage of the process is to use the powder-metallurgically produced, due to the high cooling rate of, for example, 104 to 105 SchmelzK / s during melt atomization, already fine crystalline, preferably already equiaxial, multi-phase structure of the alloy powder both with regard to the matrix and also with regard to the carbidic and / or boridic precipitation phase to further refine the consolidated state and thereby a thermally stable microstructure during the subsequent thermomechanical processing as a result of hot forming in the second process stage, with a grain size of 1 to 3 ⁇ m or 0.2 to 1.0, which is preferably fine both for the matrix and for the precipitation phase ⁇ m.
- the material structure in the first process stage can be conditioned by thermomechanical processing, which is the case with steel alloys in austenitic Condition, for example, begins at about 900 o C and the ⁇ / ⁇ phase conversion in the range from 750 to 820 o C to a final rolling temperature of 650 o C goes through.
- thermomechanical processing which is the case with steel alloys in austenitic Condition, for example, begins at about 900 o C and the ⁇ / ⁇ phase conversion in the range from 750 to 820 o C to a final rolling temperature of 650 o C goes through.
- the material to be deformed cools down continuously and, in addition to the phase change, the carbides and / or borides are eliminated.
- the carbides and / or borides are eliminated in the hot forming of stellites in the temperature range from 1000 to 700 ° C. during the shaping and the associated continuous cooling.
- thermomechanical conditioning there is a refinement of the matrix grain, which is then equiaxial at the latest, as well as a finer dispersion of the carbide and boride particles as a result of the favorable conditions for nucleation during the phase change. Both have an impact in the direction of higher material strength.
- the conditioning of the starting material produced by powder metallurgy can also be carried out by isothermal shaping with the aim of recrystallizing the structure and setting a fine-grained structure as a prerequisite for the superplastic state.
- the isothermal deformation takes place at temperatures below the transformation temperature, for example at 450 ° C., preferably with a low degree of deformation, for example with a cross-sectional decrease of about 10%, and should include a cyclic ⁇ / ⁇ phase transformation which, owing to the different volumes of the ⁇ and ⁇ phase to internal tensions and thus to internal internal tensions induced deformation of the matrix grain.
- This can be followed by a short primary recrystallization annealing, for example 20 to 60 seconds, to refine the matrix grain size of the hot isostatically pressed blank, which leads to a further grain refinement.
- the aim of the conditioning of the starting material is to establish a structure which is equiaxial for superplastic shaping in the second process stage and which is characterized by a fine structure grain which favors the forming behavior.
- the resistance to deformation is reduced and, at the same time, the rate of deformation can be increased.
- the formed material which is adjusted to a specific multiphase structure, is shaped at a temperature in the order of 50 to 70% of the melting temperature of, for example, 650 to 780 o C, which allows high degrees of deformation at low flow stresses and therefore also manufacture Complicated finished parts made of alloys, the composition of which does not allow shaping by forming without the special pretreatment of the first stage of the method according to the invention.
- the forming speed is preferably 10 ⁇ 3 to 5.10 ⁇ 1 s ⁇ 1.
- the forming temperature is below the temperature of the beginning secondary crystallization or grain coarsening, since each grain growth increases the resistance to deformation and therefore requires higher deformation forces.
- the method according to the invention is particularly suitable for high-carbon cold work steels such as X 178 Cr V 5 2 9 X 155 Cr VW Co 4 5 12 5 X 135 Cr VW Mo 4 4 6 4 X 220 Cr V 17 6 X 245 Cr V 5 10 These have carbon contents from 1.0 to 2.5% and high alloy contents of chromium, vanadium, tungsten, molybdenum and cobalt from 4 to 17%.
- the following alloys are also suitable: X 375 Cr Mo Fe 25 10 60 X 220 Cr W Co 30 12 56 X 120 Cr Mo Co 27 4 60 X 100 Cr W Co NB 15 15 52 3.
- the Stellite are iron and cobalt-based stellite with high boron and carbon contents of 1 to 4%, and contents of the alloying elements chromium, molybdenum, tungsten, 15 to 30%, which can be transformed at a relatively low temperature of 650-720 o C.
- the superplastic shape can be followed by coarse grain annealing in order to increase the creep resistance or heat resistance.
- the round blank 1 shown in FIG. 1 consists of the high-strength cold work steel X 245 Cr V 5 10, which was produced by powder metallurgy by hot isostatic pressing and was set to a structure with a matrix grain size of 1 to 3 ⁇ m. It serves to manufacture the disk-shaped rotary knife shown in FIG. 2 with a cone angle ⁇ of 150 to 160 ° , a thickness of 1.0 to 1.5 mm and an inner diameter of 50 mm and an outer diameter of 100 mm.
- the circular blank 1 was produced by punching from a powder metallurgy and then rolled out at a temperature of 1150 to 1250 ° C. to a thickness of 2.5 mm and measuring 100 ⁇ 200 ⁇ 8 mm. In order to create a sufficient material reserve for the formation of the cutting edges 2 of the rotary knife, the thickness of the board exceeded the finished thickness of the rotary knife by 1 mm.
- the low forming temperature saves energy, ensures minimal scaling and prevents harmful grain growth.
- superplastic forming results in a higher density because pores and cracks weld, as well as higher strength and toughness. Because there is no machining, there are no fatigue cracks in the machining grooves, which increases the tool life by 25 to 30%.
- the method according to the invention is suitable for producing cut bells and tools, shape cutting tools, knives, for example disc, filter and tobacco knives with a thickness of less than 3 mm, embossing dies, jam and pressure rings for extruders, sintering compression tools, extrusion tools and dies, molding tools for the wobble extrusion and multi-hole plates each made of cold work steels, for the production of profile milling cutters, form turning steels and profile countersunk heads from high speed steels as well as for the production of glass blow molding tools, profile rods, nozzles, impellers, turbine disks and valve seats made of stellites. It is characterized by low forming temperatures and a low power requirement.
- the finely dispersed, equiaxial and texture-free microstructure guarantees constant and reproducible mechanical properties, in particular high strength with excellent ductility and good fatigue behavior.
- the dimensional accuracy and surface quality are so good that reworking is not necessary.
- the surface roughness is usually less than 1 ⁇ m.
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Materials Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Crystallography & Structural Chemistry (AREA)
- Thermal Sciences (AREA)
- Physics & Mathematics (AREA)
- Manufacturing & Machinery (AREA)
- Forging (AREA)
- Powder Metallurgy (AREA)
- Treatment Of Steel In Its Molten State (AREA)
- Turning (AREA)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| AT86117455T ATE90899T1 (de) | 1985-12-18 | 1986-12-16 | Verfahren zum herstellen von werkzeugen. |
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE19853544759 DE3544759A1 (de) | 1985-12-18 | 1985-12-18 | Verfahren zum herstellen von werkzeugen |
| DE3544759 | 1985-12-18 |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| EP0227001A2 EP0227001A2 (de) | 1987-07-01 |
| EP0227001A3 EP0227001A3 (en) | 1988-05-04 |
| EP0227001B1 true EP0227001B1 (de) | 1993-06-23 |
Family
ID=6288747
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| EP86117455A Expired - Lifetime EP0227001B1 (de) | 1985-12-18 | 1986-12-16 | Verfahren zum Herstellen von Werkzeugen |
Country Status (6)
| Country | Link |
|---|---|
| US (1) | US5028386A (enrdf_load_stackoverflow) |
| EP (1) | EP0227001B1 (enrdf_load_stackoverflow) |
| JP (1) | JPS62156203A (enrdf_load_stackoverflow) |
| AT (1) | ATE90899T1 (enrdf_load_stackoverflow) |
| DE (1) | DE3544759A1 (enrdf_load_stackoverflow) |
| ES (1) | ES2041242T3 (enrdf_load_stackoverflow) |
Families Citing this family (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4969099A (en) * | 1986-03-11 | 1990-11-06 | Toyota Jidosha Kabushiki Kaisha | Double-detecting, trouble-judging and failsafe devices in system for integrally controlling automatic transmission and engine |
| US4945481A (en) * | 1986-05-08 | 1990-07-31 | Toyota Jidosha Kabushiki Kaisha | System for integrally controlling automatic transmission and engine |
| US4838124A (en) * | 1986-06-30 | 1989-06-13 | Toyota Jidosha Kabushiki Kaisha | System for integrally controlling automatic transmission and engine |
| JPH0712809B2 (ja) * | 1986-07-07 | 1995-02-15 | トヨタ自動車株式会社 | 自動変速機及びエンジンの一体制御装置 |
| US8186561B2 (en) * | 2004-03-24 | 2012-05-29 | Megastir Technologies, LLC | Solid state processing of hand-held knife blades to improve blade performance |
Family Cites Families (12)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2127082A5 (enrdf_load_stackoverflow) * | 1971-02-22 | 1972-10-13 | Charbonnages De France | |
| JPS5510642B2 (enrdf_load_stackoverflow) * | 1973-10-31 | 1980-03-18 | ||
| US4073648A (en) * | 1974-06-10 | 1978-02-14 | The International Nickel Company, Inc. | Thermoplastic prealloyed powder |
| US3976482A (en) * | 1975-01-31 | 1976-08-24 | The International Nickel Company, Inc. | Method of making prealloyed thermoplastic powder and consolidated article |
| US3951697A (en) * | 1975-02-24 | 1976-04-20 | The Board Of Trustees Of Leland Stanford Junior University | Superplastic ultra high carbon steel |
| JPS5485106A (en) * | 1977-12-20 | 1979-07-06 | Seiko Epson Corp | Magnet made from inter-rare-earth-metallic compound |
| JPS5887204A (ja) * | 1981-11-17 | 1983-05-25 | Kobe Steel Ltd | 急冷凝固粉末を用いた超合金の恒温鍛造方法 |
| JPS5893802A (ja) * | 1981-11-30 | 1983-06-03 | Sumitomo Electric Ind Ltd | 難加工性合金線材の製造方法 |
| US4533390A (en) * | 1983-09-30 | 1985-08-06 | Board Of Trustees Of The Leland Stanford Junior University | Ultra high carbon steel alloy and processing thereof |
| DE3346089A1 (de) * | 1983-12-21 | 1985-07-18 | Dr. Weusthoff GmbH, 4000 Düsseldorf | Verfahren zum herstellen hochfester, duktiler koerper aus kohlenstoffreichen eisenbasislegierungen |
| US4582536A (en) * | 1984-12-07 | 1986-04-15 | Allied Corporation | Production of increased ductility in articles consolidated from rapidly solidified alloy |
| JPS62134130A (ja) * | 1985-12-05 | 1987-06-17 | Agency Of Ind Science & Technol | 高強度・難加工材の超塑性ウオ−ムダイ・パツク鍛造法 |
-
1985
- 1985-12-18 DE DE19853544759 patent/DE3544759A1/de active Granted
-
1986
- 1986-12-16 ES ES198686117455T patent/ES2041242T3/es not_active Expired - Lifetime
- 1986-12-16 AT AT86117455T patent/ATE90899T1/de not_active IP Right Cessation
- 1986-12-16 EP EP86117455A patent/EP0227001B1/de not_active Expired - Lifetime
- 1986-12-18 JP JP61302756A patent/JPS62156203A/ja active Pending
-
1990
- 1990-10-17 US US07/600,135 patent/US5028386A/en not_active Expired - Fee Related
Also Published As
| Publication number | Publication date |
|---|---|
| ES2041242T3 (es) | 1993-11-16 |
| DE3544759A1 (de) | 1987-06-19 |
| DE3544759C2 (enrdf_load_stackoverflow) | 1989-08-03 |
| JPS62156203A (ja) | 1987-07-11 |
| EP0227001A2 (de) | 1987-07-01 |
| US5028386A (en) | 1991-07-02 |
| ATE90899T1 (de) | 1993-07-15 |
| EP0227001A3 (en) | 1988-05-04 |
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