ITUB201613701U1 - Tool steel for tools with increased durability - Google Patents
Tool steel for tools with increased durabilityInfo
- Publication number
- ITUB201613701U1 ITUB201613701U1 ITUB2016U013701U ITUB201613701U ITUB201613701U1 IT UB201613701 U1 ITUB201613701 U1 IT UB201613701U1 IT UB2016U013701 U ITUB2016U013701 U IT UB2016U013701U IT UB201613701 U ITUB201613701 U IT UB201613701U IT UB201613701 U1 ITUB201613701 U1 IT UB201613701U1
- Authority
- IT
- Italy
- Prior art keywords
- tool
- surface layer
- tools
- hrc
- hardness
- Prior art date
Links
- 229910001315 Tool steel Inorganic materials 0.000 title claims description 8
- 230000001965 increasing effect Effects 0.000 title claims description 7
- 239000002344 surface layer Substances 0.000 claims description 27
- 239000000463 material Substances 0.000 claims description 21
- 239000010410 layer Substances 0.000 claims description 13
- 238000000034 method Methods 0.000 description 40
- 230000008569 process Effects 0.000 description 21
- 229910000831 Steel Inorganic materials 0.000 description 13
- 239000010959 steel Substances 0.000 description 13
- 238000005121 nitriding Methods 0.000 description 10
- 238000010791 quenching Methods 0.000 description 9
- 230000000171 quenching effect Effects 0.000 description 9
- 238000005516 engineering process Methods 0.000 description 7
- 238000004519 manufacturing process Methods 0.000 description 7
- 238000004381 surface treatment Methods 0.000 description 7
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 6
- 238000000576 coating method Methods 0.000 description 6
- 238000010438 heat treatment Methods 0.000 description 6
- 239000000203 mixture Substances 0.000 description 5
- 238000005299 abrasion Methods 0.000 description 4
- 239000011247 coating layer Substances 0.000 description 4
- 239000007789 gas Substances 0.000 description 4
- 229910000734 martensite Inorganic materials 0.000 description 4
- 239000000126 substance Substances 0.000 description 4
- 230000008901 benefit Effects 0.000 description 3
- 238000005229 chemical vapour deposition Methods 0.000 description 3
- 239000011248 coating agent Substances 0.000 description 3
- 230000000694 effects Effects 0.000 description 3
- 230000006872 improvement Effects 0.000 description 3
- 150000004767 nitrides Chemical group 0.000 description 3
- 229910052757 nitrogen Inorganic materials 0.000 description 3
- 230000002411 adverse Effects 0.000 description 2
- 238000000151 deposition Methods 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 238000005242 forging Methods 0.000 description 2
- 238000005240 physical vapour deposition Methods 0.000 description 2
- 238000012545 processing Methods 0.000 description 2
- 238000012360 testing method Methods 0.000 description 2
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 description 1
- ATJFFYVFTNAWJD-UHFFFAOYSA-N Tin Chemical compound [Sn] ATJFFYVFTNAWJD-UHFFFAOYSA-N 0.000 description 1
- 239000010953 base metal Substances 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 230000015556 catabolic process Effects 0.000 description 1
- 238000005260 corrosion Methods 0.000 description 1
- 230000007797 corrosion Effects 0.000 description 1
- 238000006731 degradation reaction Methods 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 238000009792 diffusion process Methods 0.000 description 1
- 238000009826 distribution Methods 0.000 description 1
- 230000002708 enhancing effect Effects 0.000 description 1
- 230000007613 environmental effect Effects 0.000 description 1
- 230000001747 exhibiting effect Effects 0.000 description 1
- 230000002349 favourable effect Effects 0.000 description 1
- 239000001257 hydrogen Substances 0.000 description 1
- 229910052739 hydrogen Inorganic materials 0.000 description 1
- 230000000977 initiatory effect Effects 0.000 description 1
- 238000002844 melting Methods 0.000 description 1
- 230000008018 melting Effects 0.000 description 1
- 239000002245 particle Substances 0.000 description 1
- 238000003825 pressing Methods 0.000 description 1
- 230000000750 progressive effect Effects 0.000 description 1
- 229920006395 saturated elastomer Polymers 0.000 description 1
- 238000007493 shaping process Methods 0.000 description 1
- 239000002356 single layer Substances 0.000 description 1
- 238000001228 spectrum Methods 0.000 description 1
- 238000012546 transfer Methods 0.000 description 1
- 230000009466 transformation Effects 0.000 description 1
- 230000007704 transition Effects 0.000 description 1
Classifications
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- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C8/00—Solid state diffusion of only non-metal elements into metallic material surfaces; Chemical surface treatment of metallic material by reaction of the surface with a reactive gas, leaving reaction products of surface material in the coating, e.g. conversion coatings, passivation of metals
- C23C8/02—Pretreatment of the material to be coated
-
- 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
- C21D1/00—General methods or devices for heat treatment, e.g. annealing, hardening, quenching or tempering
- C21D1/06—Surface hardening
- C21D1/09—Surface hardening by direct application of electrical or wave energy; by particle radiation
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C8/00—Solid state diffusion of only non-metal elements into metallic material surfaces; Chemical surface treatment of metallic material by reaction of the surface with a reactive gas, leaving reaction products of surface material in the coating, e.g. conversion coatings, passivation of metals
- C23C8/06—Solid state diffusion of only non-metal elements into metallic material surfaces; Chemical surface treatment of metallic material by reaction of the surface with a reactive gas, leaving reaction products of surface material in the coating, e.g. conversion coatings, passivation of metals using gases
- C23C8/36—Solid state diffusion of only non-metal elements into metallic material surfaces; Chemical surface treatment of metallic material by reaction of the surface with a reactive gas, leaving reaction products of surface material in the coating, e.g. conversion coatings, passivation of metals using gases using ionised gases, e.g. ionitriding
- C23C8/38—Treatment of ferrous surfaces
-
- 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
- C21D2221/00—Treating localised areas of an article
-
- 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
- C21D6/00—Heat treatment of ferrous alloys
- C21D6/002—Heat treatment of ferrous alloys containing Cr
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Organic Chemistry (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Crystallography & Structural Chemistry (AREA)
- Solid-Phase Diffusion Into Metallic Material Surfaces (AREA)
- Gripping On Spindles (AREA)
- Heat Treatment Of Articles (AREA)
Description
Description of utilty model Description of utilty model
Tool from tool steel with enhanced durability Tool from tool steel with enhanced durability
Field of the invention Field of the invention
[0001] The invention concerns commonly to tools from tool steel with amended surface layer, particularly those used in the manufacture of forming tools. [0001] The invention concerns commonly to tools from tool steel with amended surface layer, particularly those used in the manufacture of forming tools.
Background of the invention Background of the invention
[0002] Tool steels have assumed an irreplaceable role in the engineering industry. Diverse surface treatment methods can be used with the aim to influence both the performance and the life properties of various tools. This particularly applies to forming tools where it is possible to considerably enhance the above properties by means of a suitable surface treatment. In the past, the surface properties of the forming tools used to be enhanced by the application of carbidic surface layers or by the application of deposited coatings based on TiN and/or TiCN. [0002] Tool steels have assumed an irreplaceable role in the engineering industry. Diverse surface treatment methods can be used with the aim to influence both the performance and the life properties of various tools. This particularly applies to forming tools where it is possible to considerably enhance the above properties by means of a suitable surface treatment. In the past, the surface properties of the forming tools used to be enhanced by the application of carbidic surface layers or by the application of deposited coatings based on TiN and / or TiCN.
[0003] There is a plurality of more up-to-date methods, one of them being the so called CVD (Chemical Vapour Deposition). Typically, the chemical vapour deposition is carried out under high temperatures (1,000 – 1,200 ̊C). The advantages achieved by this method include the formation of deposited coatings having high density and thermal stability and featuring an excellent adhesion between the base material and the coating itself, the capability of depositing coatings onto workpieces having complex shapes and the low acquisition and operating costs. The drawbacks of this method include the adverse influence on the structure of base materials (resulting in the degradation of mechanical properties of the same) due to the high process temperature levels, the existence of residual stresses inside the coating layer (due to different thermal expansivity coefficients), high energy and time demands, adverse environmental effects caused by the process gases used and undesirable rounding of sharp edges. [0003] There is a plurality of more up-to-date methods, one of them being the so called CVD (Chemical Vapor Deposition). Typically, the chemical vapor deposition is carried out under high temperatures (1,000 - 1,200 ̊C). The advantages achieved by this method include the formation of deposited coatings having high density and thermal stability and featuring an excellent adhesion between the base material and the coating itself, the capability of depositing coatings onto workpieces having complex shapes and the low acquisition and operating costs. The drawbacks of this method include the adverse influence on the structure of base materials (resulting in the degradation of mechanical properties of the same) due to the high process temperature levels, the existence of residual stresses inside the coating layer (due to different thermal expansivity coefficients), high energy and time demands, adverse environmental effects caused by the process gases used and undesirable rounding of sharp edges.
[0004] Another method, which is known as PVD (Physical Vapour Deposition), is characterized by relatively low process temperatures below 500 ̊C. Herein, the deposited coating layers are formed under reduced pressure (0.1-1.0 Pa). This method is preferably used for depositing coating layers onto sharp edges (having a fillet radius smaller than 20 μm). The typical properties of such coating layers include high durability and low friction coefficients. Besides that, combinations of different coating materials within a single layer can be used and precise thickness settings can be selected. The drawbacks of this methods include a relatively complex vacuum system and the so called shadow effect. Moreover, a coating having an uneven thickness distribution can form on the surfaces that do not lie in the direction of the particles. [0004] Another method, which is known as PVD (Physical Vapor Deposition), is characterized by relatively low process temperatures below 500 ̊C. Herein, the deposited coating layers are formed under reduced pressure (0.1-1.0 Pa). This method is preferably used for depositing coating layers onto sharp edges (having a fillet radius smaller than 20 μm). The typical properties of such coating layers include high durability and low friction coefficients. Besides that, combinations of different coating materials within a single layer can be used and precise thickness settings can be selected. The drawbacks of this methods include a relatively complex vacuum system and the so called shadow effect. Moreover, a coating having an uneven thickness distribution can form on the surfaces that do not lie in the direction of the particles.
[0005] Another up-to-date heat treatment method used for enhancing the surface properties of materials is laser quenching. A laser beam impinges on a surface layer consisting of the material to be quenched. This causes the surface layer to be rapidly heated up in order to reach a certain temperature, typically closely below the respective melting point (900 – 1,400 ̊C). As such temperature is reached, the material structure undergoes austenitic transition. The incident point of the laser beam is being continuously shifted in the feeding direction, thus causing the heated spots to be rapidly cooled down through the heat transfer into the surrounding material. This enables a very fine carbidic structure to form which include short martensite needles and having small grain size. Such structure will cause the hardness of the surface layer to increase without compromising the core toughness and initiating any creation of fissure cracks. The main advantage of the laser quenching method consists in that it enables only those locations to be hardened where an increased durability is required without affecting the original material properties in the remaining portions or sections of the respective workpiece. Besides that, an environmentally friendly process is concerned. [0005] Another up-to-date heat treatment method used for enhancing the surface properties of materials is laser quenching. A laser beam impinges on a surface layer consisting of the material to be quenched. This causes the surface layer to be rapidly heated up in order to reach a certain temperature, typically closely below the respective melting point (900 - 1,400 ̊C). As such temperature is reached, the material structure undergoes austenitic transition. The incident point of the laser beam is being continuously shifted in the feeding direction, thus causing the heated spots to be rapidly cooled down through the heat transfer into the surrounding material. This enables a very fine carbidic structure to form which include short martensite needles and having small grain size. Such structure will cause the hardness of the surface layer to increase without compromising the core toughness and initiating any creation of fissure cracks. The main advantage of the laser quenching method consists in that it enables only those locations to be hardened where an increased durability is required without affecting the original material properties in the remaining portions or sections of the respective workpiece. Besides that, an environmentally friendly process is concerned.
[0006] Surface treatment methods based on the laser quenching technology are described in multiple patent documents. The applicability of the laser quenching method is described, for example, in the documents EP 0130749 B1 or GB 202838. Moreover, the document WO96/28574 describes the use of the laser quenching method for treating complex workpieces, in the present case for treating the inside corners of the workpieces. The drawbacks of the last-mentioned method consists in the related high acquisition and operating costs and in the existence of the problems connected with the treatment of highly reflexive materials. [0006] Surface treatment methods based on the laser quenching technology are described in multiple patent documents. The applicability of the laser quenching method is described, for example, in the documents EP 0130749 B1 or GB 202838. Moreover, the document WO96 / 28574 describes the use of the laser quenching method for treating complex workpieces, in the present case for treating the inside corners of the workpieces. The drawbacks of the last-mentioned method consists in the related high acquisition and operating costs and in the existence of the problems connected with the treatment of highly reflexive materials.
[0007] At the present time, the plasma nitriding technology is considered to be one of the most progressive surface treatment technologies used in the engineering industry. A nitriding atmosphere consists of a mixture of nitrogen and hydrogen and the nitriding process is typically carried out in the temperature range from 500 to 550°C. The quality of the nitrided surface layer depends not only on the process temperature but also on the chemical composition of the steel being treated, on the quality of the surface finish of the respective tool and on the physical parameters of the nitriding process, such as the voltage, duration, pulse length and pressure of the gas mixture. This chemical heat treatment is used for increasing the surface hardness, corrosion resistance and fatigue strength. Further advantages include high levels of process accuracy and stability, reduced consumption of gas as well as the possibility of nitriding tool having final dimensions without necessitating the same to be subsequently machine finished (by grinding or the like). A substantial disadvantage, however, consists in the depth limitation of the nitrided surface layers, which corresponds to 0.3 mm of the base material, and in the related wear rate of such rough nitrided surface layer. The nitrided surface layer remains sufficiently stabile under the temperatures up to about 600 ̊C. After exceeding this temperature limit, the properties of such surface layer, particularly the abrasion resistance thereof, gradually degrade. [0007] At the present time, the plasma nitriding technology is considered to be one of the most progressive surface treatment technologies used in the engineering industry. A nitriding atmosphere consists of a mixture of nitrogen and hydrogen and the nitriding process is typically carried out in the temperature range from 500 to 550 ° C. The quality of the nitrided surface layer depends not only on the process temperature but also on the chemical composition of the steel being treated, on the quality of the surface finish of the respective tool and on the physical parameters of the nitriding process, such as the voltage, duration, pulse length and pressure of the gas mixture. This chemical heat treatment is used for increasing the surface hardness, corrosion resistance and fatigue strength. Further advantages include high levels of process accuracy and stability, reduced consumption of gas as well as the possibility of nitriding tool having final dimensions without necessitating the same to be subsequently machine finished (by grinding or the like). A substantial disadvantage, however, consists in the depth limitation of the nitrided surface layers, which corresponds to 0.3 mm of the base material, and in the related wear rate of such rough nitrided surface layer. The nitrided surface layer remains sufficiently stable under the temperatures up to about 600 ̊C. After exceeding this temperature limit, the properties of such surface layer, particularly the abrasion resistance thereof, gradually degrade.
[0008] The plasma nitriding method is mentioned, for example, in the documents JP2013-234370 or KR100661130 B1. The document US 5536549 B1 discloses the application of this method for treating a special surface of a magnetic recording medium wherein the base metal of the respective disc-type carrier is an austenitic steel. [0008] The plasma nitriding method is mentioned, for example, in the documents JP2013-234370 or KR100661130 B1. The document US 5536549 B1 discloses the application of this method for treating a special surface of a magnetic recording medium wherein the base metal of the respective disc-type carrier is an austenitic steel.
[0009] The object of the invention is to present a tool which would enable an extended service life of the functional surfaces. Such tool should be easily treated and, besides that, it should enable the desired structure and properties of the steel layer under the treated surface. [0009] The object of the invention is to present a tool which would enable an extended service life of the functional surfaces. Such tool should be easily treated and, besides that, it should enable the desired structure and properties of the steel layer under the treated surface.
Disclosure of the invention Disclosure of the invention
[0010] The above drawbacks are largely eliminated by the proposed tool from tool steel with enhanced durability according to the present invention, wherein at least function areas of the tool are provided with a surface layer consisting from laser quenched basic layer part of the surface layer with the hardness 51 HRC with up to the depth of 1,3 mm into the basic material and the upmost surface of this surface layer is created of a plasma nitrided superficial layer part which has the hardeness of at least 56 HRC and the whole surface layer consisting of two mentioned parts is removable and renewable on the basic material again. [0010] The above drawbacks are largely eliminated by the proposed tool from tool steel with enhanced durability according to the present invention, wherein at least function areas of the tool are provided with a surface layer consisting from laser quenched basic layer part of the surface layer with the hardness 51 HRC with up to the depth of 1,3 mm into the basic material and the upmost surface of this surface layer is created of a plasma nitrided superficial layer part which has the hardeness of at least 56 HRC and the whole surface layer consisting of two mentioned parts is removable and renewable on the basic material again.
Overview of the figures on drawings Overview of the figures on drawings
[0011] The present invention will be further explained by means of the accompanying drawings wherein Fig.1 is a front view showing a spin forming tool used for shoulder and neck forming in the manufacture of blanks for steel cylinders, Fig.2 is a sectional view showing the spin forming tool from Fig.1 and Fig.3 is a diagram representing the difference between the service lives of multiple spin forming tools before and after undergoing a combined surface treatment based on the method according to the invention, respectively. Preferred embodiment of the invention [0011] The present invention will be further explained by means of the accompanying drawings wherein Fig.1 is a front view showing a spin forming tool used for shoulder and neck forming in the manufacture of blanks for steel cylinders, Fig.2 is a sectional view showing the spin forming tool from Fig.1 and Fig.3 is a diagram representing the difference between the service lives of multiple spin forming tools before and after undergoing a combined surface treatment based on the method according to the invention, respectively. Preferred embodiment of the invention
[0012] The tool 1 shown in Figs. 1 and 2, namely the spin forming tool, is first machined from a forged piece in order to obtain its final shape and subsequently heat treated in order to obtain the desired hardness within its whole volume. Since the whole-volume heat treatment based on the hardness range according to the respective shop drawing would not be, as such, sufficient for the subsequent use in a hot forming process, such as spin forming one, with respect to the desired abrasion resistance, it is necessary to additionally enhance the surface resistance properties of the blank. [0012] The tool 1 shown in Figs. 1 and 2, namely the spin forming tool, is first machined from a forged piece in order to obtain its final shape and subsequently heat treated in order to obtain the desired hardness within its whole volume. Since the whole-volume heat treatment based on the hardness range according to the respective shop drawing would not be, as such, sufficient for the subsequent use in a hot forming process, such as spin forming one, with respect to the desired abrasion resistance, it is necessary to additionally enhance the surface resistance properties of the blank.
[0013] In the given case, such objective can be achieved by surface layer 2 of the tool 1 according to present invention, namely in that first the functional area 4 is heat treated using the laser quenching technology. Shape of the treated blank 3 is illustrated for information. During this treatment process, the structure of the surface layer as well as that of a thin subsurface layer is transformed into a very fine martensitic structure exhibiting very high hardness values up to 55 HRC. In this way, an overall thickness of the through-hardened layer of up to 1.3 mm can be obtained. By this way a laser quenched basic layer part of the surface layer 2 is created. The laser quenching process is implemented by means of high-power filament focused laser devices. [0013] In the given case, such objective can be achieved by surface layer 2 of the tool 1 according to present invention, namely in that first the functional area 4 is heat treated using the laser quenching technology. Shape of the treated blank 3 is illustrated for information. During this treatment process, the structure of the surface layer as well as that of a thin subsurface layer is transformed into a very fine martensitic structure exhibiting very high hardness values up to 55 HRC. In this way, an overall thickness of the through-hardened layer of up to 1.3 mm can be obtained. By this way a laser quenched basic layer part of the surface layer 2 is created. The laser quenching process is implemented by means of high-power filament focused laser devices.
[0014] The above described surface heat treatment step is followed by the chemical heat treatment one consisting in the application of the plasma nitriding technology. During this subsequent processing step, very fine and hard nitrides form in the surface layer of the steel blank due to the fact that the layer is saturated with nitrogen. This causes an additional thin surface layer to form. The latter layer has at most 0.35 mm in thickness, the hardness of the same reaching up to 62 HRC. This process is carried out in the temperature range of 520 – 540ºC for 24 hours. The respective process atmosphere contains a gas mixture consisting of H2and N2in the ratio of 80:20. The surface, which is highlighted in bold and provided with the reference numeral 2, is in the area 4, which undergoes the treatment and through which the tool is brought into contact with the forged piece, i.e. with the blank of the steel cylinder 3 to be closed in its top portion by means of the process of shoulder and neck forming. During processing, the forged piece is driven in rotation, thus imparting rotational movement to the forming tool that constitutes a driven, freely rotating unit. By this way a plasma nitrided superficial layer part of the surface layer 2 is created. [0014] The above described surface heat treatment step is followed by the chemical heat treatment one consisting in the application of the plasma nitriding technology. During this subsequent processing step, very fine and hard nitrides form in the surface layer of the steel blank due to the fact that the layer is saturated with nitrogen. This causes an additional thin surface layer to form. The latter layer has at most 0.35 mm in thickness, the hardness of the same reaching up to 62 HRC. This process is carried out in the temperature range of 520 - 540ºC for 24 hours. The respective process atmosphere contains a gas mixture consisting of H2and N2in the ratio of 80:20. The surface, which is highlighted in bold and provided with the reference numeral 2, is in the area 4, which undergoes the treatment and through which the tool is brought into contact with the forged piece, i.e. with the blank of the steel cylinder 3 to be closed in its top portion by means of the process of shoulder and neck forming. During processing, the forged piece is driven in rotation, thus imparting rotational movement to the forming tool that constitutes a driven, freely rotating unit. By this way a plasma nitrided superficial layer part of the surface layer 2 is created.
[0015] The surface treatment was applied in the manufacture of a forming tool which is referred to as "spin forming tool". Such a type of forming tool is used for the so called spin forming which is a method used for shoulder and neck forming in the manufacture of backwardly extruded high-pressure steel cylinders 3 (by way of illustration, the method, which is used for all the types of steel cylinders, may be compared with the shoulder and neck forming process used in the manufacture of necked tubes, the latter having one end provided with a necked spherical cap). [0015] The surface treatment was applied in the manufacture of a forming tool which is referred to as "spin forming tool". Such a type of forming tool is used for the so called spin forming which is a method used for shoulder and neck forming in the manufacture of backwardly extruded high-pressure steel cylinders 3 (by way of illustration, the method, which is used for all the types of steel cylinders, may be compared with the shoulder and neck forming process used in the manufacture of necked tubes, the latter having one end provided with a necked spherical cap).
[0016] The forming tool is made of the hot work tool steel QRO 90 Supreme, the most similar equivalent of the latter being the steel X32CrMoV33. Hence, the typical base material used for manufacturing the tool blank is the above mentioned steel QRO 90 Supreme. Before being employed in the manufacturing process, the spin forming tool is preheated to reach a temperature ranging between 180 and 220°C. Such elevated temperature ensures a better adhesion during the initial phase of the forming cycle. Afterwards, the working cycle in itself commences. This main cycle consists of heating up the blank to be formed to reach a temperature ranging between 1,000 and 1,200°C, bringing the hot blank, which is continuously rotating around its centre line, into contact with the spin forming tool and in subsequent pressing the spin forming tool against the blank, thus causing the material of the latter to "flow" in the direction defined by the swinging movement of the spin forming tool. During the forming process, the material being formed is continuously reheated by means of burners in order to be held at the above mentioned forming temperature. After the completion of the forming process, the surface of the spin forming tool is cleaned by means of a highpressure jet. [0016] The forming tool is made of the hot work tool steel QRO 90 Supreme, the most similar equivalent of the latter being the steel X32CrMoV33. Hence, the typical base material used for manufacturing the tool blank is the above mentioned steel QRO 90 Supreme. Before being employed in the manufacturing process, the spin forming tool is preheated to reach a temperature ranging between 180 and 220 ° C. Such elevated temperature ensures a better adhesion during the initial phase of the forming cycle. Afterwards, the working cycle in itself commences. This main cycle consists of heating up the blank to be formed to reach a temperature ranging between 1,000 and 1,200 ° C, bringing the hot blank, which is continuously rotating around its center line, into contact with the spin forming tool and in subsequent pressing the spin forming tool against the blank, thus causing the material of the latter to "flow" in the direction defined by the swinging movement of the spin forming tool. During the forming process, the material being formed is continuously reheated by means of burners in order to be held at the above mentioned forming temperature. After the completion of the forming process, the surface of the spin forming tool is cleaned by means of a highpressure jet.
[0017] Until recently, solely the plasma nitriding method has been applied as a surface treatment technology with the aim to improve the characteristics influencing tool life. This technology by itself, however, was not able to ensure any improvement of the total tool life. Instead, it only enabled a temporary improvement to be achieved. This means that the thickness of the nitrided layer containing highly abrasion resistant nitrides was used up after having shaped 1,800 - 2,000 workpieces, on an average, and afterwards solely the base material of the tool was used for shaping the workpieces which led to the occurrence of local deformations and increased abrasive wear of the base material of the spin forming tool as well as to the development of a "sticking" effect between the latter material and that of the workpiece. By means of the laser quenching step, which has been incorporated into the technological process so as to precede the plasma nitriding one, a very fine martensitic structure can be obtained. The latter structure enables an additional abrasion resistant sublayer to form that remains available even after a complete depletion of the nitride layer due to abrasive wear. Simultaneously, the martensitic transformation taking place during the laser quenching process, ensures a significant grain refinement within the hardened layer which is achievable owing to the typical rapid chilling effect in the course of the process. This grain refinement is also a significant prerequisite for creating more favourable conditions for the subsequent nitriding step because it enables a stronger diffusion of nitrogen into the material to be achieved due to the smaller size and increased number of the grains. [0017] Until recently, solely the plasma nitriding method has been applied as a surface treatment technology with the aim to improve the characteristics influencing tool life. This technology by itself, however, was not able to ensure any improvement of the total tool life. Instead, it only enabled a temporary improvement to be achieved. This means that the thickness of the nitrided layer containing highly abrasion resistant nitrides was used up after having shaped 1,800 - 2,000 workpieces, on an average, and afterwards solely the base material of the tool was used for shaping the workpieces which led to the occurrence of local deformations and increased abrasive wear of the base material of the spin forming tool as well as to the development of a "sticking" effect between the latter material and that of the workpiece. By means of the laser quenching step, which has been incorporated into the technological process so as to precede the plasma nitriding one, a very fine martensitic structure can be obtained. The latter structure enables an additional abrasion resistant sublayer to form that remains available even after a complete depletion of the nitride layer due to abrasive wear. Simultaneously, the martensitic transformation taking place during the laser quenching process, ensures a significant grain refinement within the hardened layer which is achievable owing to the typical rapid chilling effect in the course of the process. This grain refinement is also a significant prerequisite for creating more favorable conditions for the subsequent nitriding step because it enables a stronger diffusion of nitrogen into the material to be achieved due to the smaller size and increased number of the grains.
[0018] Once the contact surface layer 2 of the forming tool 1 with its two parts has been worn out, the remaining surface layer 2 can be removed and the whole technological cycle can be repeated and the tool 1 is useable again. [0018] Once the contact surface layer 2 of the forming tool 1 with its two parts has been worn out, the remaining surface layer 2 can be removed and the whole technological cycle can be repeated and the tool 1 is useable again.
Industrial applicability Industrial applicability
[0019] Tools according to the invention can be used for a wide spectrum of forming tools, in particular for forging dies, pull broaches an forging jaws. Tools are extensively applicable to a wide range of tool steel grades, for which it has been developed, such for the grades 38CrMoV5-1, X40CrMoV5-1, or 56CrNiMoV7, and many other ones. [0019] Tools according to the invention can be used for a wide spectrum of forming tools, in particular for forging dies, pull broaches an forging jaws. Tools are extensively applicable to a wide range of tool steel grades, for which it has been developed, such for the grades 38CrMoV5-1, X40CrMoV5-1, or 56CrNiMoV7, and many other ones.
[0020] The applicant’s enterprise uses an extended range of hot work tool steels having similar chemical compositions and being suitable for diverse steel forming processes. [0020] The applicant's enterprise uses an extended range of hot work tool steels having similar chemical compositions and being suitable for diverse steel forming processes.
[0021] The diagram shown in Fig.3 illustrates the results of the respective field tests wherein an evident improvement of the tool life values has been achieved. Furthermore, other spin forming tools, according to the invention, are undergoing similar tests. [0021] The diagram shown in Fig.3 illustrates the results of the respective field tests wherein an evident improvement of the tool life values has been achieved. Furthermore, other spin forming tools, according to the invention, are undergoing similar tests.
Claims (1)
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EP15153854.3A EP3054026A1 (en) | 2015-02-04 | 2015-02-04 | Method of combined surface treatment of tool steels |
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EP (1) | EP3054026A1 (en) |
CZ (1) | CZ29590U1 (en) |
DE (1) | DE202016000752U1 (en) |
FR (1) | FR3032137B3 (en) |
IT (1) | ITUB201613701U1 (en) |
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CA3044930C (en) | 2019-05-31 | 2023-08-29 | Apollo Machine & Welding Ltd. | Hybrid process for enhanced surface hardening |
CN112210746A (en) * | 2019-07-10 | 2021-01-12 | 上海交通大学 | Die-casting die, surface treatment method and application thereof |
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GB202838A (en) | 1922-08-18 | 1923-08-30 | Robert Walter Hutton | Improvements in and relating to collapsible cardboard or the like boxes or containers |
US4533400A (en) | 1983-06-29 | 1985-08-06 | The Garrett Corporation | Method and apparatus for laser hardening of steel |
US5536549A (en) | 1993-08-02 | 1996-07-16 | Tulip Memory Systems, Inc. | Austenitic stainless steel substrate for magnetic-recording media |
DE19508584C1 (en) | 1995-03-13 | 1996-02-08 | Fraunhofer Ges Forschung | Method and appts. for increasing the degree of absorption during solid-phase surface hardening of workpieces |
DE29622682U1 (en) * | 1996-06-14 | 1997-04-03 | Ferromatik Milacron Maschinenbau GmbH, 79364 Malterdingen | Screw for plasticizing and / or extruding plastic material in injection molding machines and extruders |
KR100661130B1 (en) | 2006-01-20 | 2006-12-22 | 한국생산기술연구원 | Method for nitriding stainless steel by post-plasma |
JP6047712B2 (en) | 2012-05-10 | 2016-12-21 | 山梨県 | Plasma nitriding method of steel |
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DE202016000752U1 (en) | 2016-05-24 |
FR3032137B3 (en) | 2017-03-24 |
EP3054026A1 (en) | 2016-08-10 |
FR3032137A3 (en) | 2016-08-05 |
PL124827U1 (en) | 2016-11-07 |
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