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US20040154705A1 - Fastening element made of carbon-containing steel and method for the production thereof - Google Patents

Fastening element made of carbon-containing steel and method for the production thereof Download PDF

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Publication number
US20040154705A1
US20040154705A1 US10/480,882 US48088203A US2004154705A1 US 20040154705 A1 US20040154705 A1 US 20040154705A1 US 48088203 A US48088203 A US 48088203A US 2004154705 A1 US2004154705 A1 US 2004154705A1
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United States
Prior art keywords
fixing element
functional tip
martensite
process according
carbon
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.)
Abandoned
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US10/480,882
Inventor
Heinrich Friederich
Reinhard Schmoock
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Ejot GmbH and Co KG
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Individual
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Filing date
Publication date
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Assigned to EJOT VERBINDUNGSTECHNIK GMBH & CO KG reassignment EJOT VERBINDUNGSTECHNIK GMBH & CO KG ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: FRIEDERICH, HEINRICH DR., SCHMOOCK, REINHARD
Assigned to EJOT GMBH & CO. KG reassignment EJOT GMBH & CO. KG MERGER (SEE DOCUMENT FOR DETAILS). Assignors: EJOT VERBINDUNGSTECHNIK GMBH & CO. KG
Publication of US20040154705A1 publication Critical patent/US20040154705A1/en
Priority to US11/404,452 priority Critical patent/US20060185768A1/en
Priority to US11/519,417 priority patent/US20070062620A1/en
Abandoned legal-status Critical Current

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Classifications

    • CCHEMISTRY; METALLURGY
    • C23COATING 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
    • C23CCOATING 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
    • C23C8/00Solid 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
    • C23C8/06Solid 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
    • C23C8/08Solid 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 only one element being applied
    • C23C8/20Carburising
    • C23C8/22Carburising of ferrous surfaces
    • CCHEMISTRY; METALLURGY
    • C21METALLURGY OF IRON
    • C21DMODIFYING 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
    • C21D9/00Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor
    • C21D9/0093Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor for screws; for bolts
    • CCHEMISTRY; METALLURGY
    • C23COATING 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
    • C23CCOATING 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
    • C23C8/00Solid 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
    • C23C8/06Solid 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
    • C23C8/28Solid 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 more than one element being applied in one step
    • C23C8/30Carbo-nitriding
    • C23C8/32Carbo-nitriding of ferrous surfaces
    • CCHEMISTRY; METALLURGY
    • C23COATING 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
    • C23CCOATING 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
    • C23C8/00Solid 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
    • C23C8/80After-treatment
    • CCHEMISTRY; METALLURGY
    • C21METALLURGY OF IRON
    • C21DMODIFYING 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
    • C21D1/00General methods or devices for heat treatment, e.g. annealing, hardening, quenching or tempering
    • C21D1/18Hardening; Quenching with or without subsequent tempering
    • CCHEMISTRY; METALLURGY
    • C21METALLURGY OF IRON
    • C21DMODIFYING 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
    • C21D1/00General methods or devices for heat treatment, e.g. annealing, hardening, quenching or tempering
    • C21D1/34Methods of heating
    • C21D1/42Induction heating
    • CCHEMISTRY; METALLURGY
    • C21METALLURGY OF IRON
    • C21DMODIFYING 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
    • C21D2221/00Treating localised areas of an article
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02PCLIMATE CHANGE MITIGATION TECHNOLOGIES IN THE PRODUCTION OR PROCESSING OF GOODS
    • Y02P10/00Technologies related to metal processing
    • Y02P10/25Process efficiency

Definitions

  • the invention concerns a process for the production of a fixing element which has a hardened functional tip and comprises a carbon-bearing steel which after heating to austenitisation temperature and subsequent quenching forms martensite, wherein the fixing element is heated overall to the austenitisation temperature, held at that temperature and then quenched and is then subjected to an annealing operation. It further concerns a fixing element, in particular a screw having a screwthread-forming and possibly hole-forming shaping zone, the structure thereof comprising in part martensite and in part annealed martensite.
  • Fixing elements which are to be driven into hard materials require a correspondingly hard functional tip.
  • the functional tip can involve preferably in the present case—the shaping zone of a screw, which forms a counterpart thread and possibly pre-bores or flow-shapes the hole which is required beforehand.
  • the functional tip however can also be the driving-in tip of a firing bolt fixed by a bolt-setting gun, or the cutting ring edge of a stamping rivet.
  • screws comprising low-alloyed carbon steel (heat-treatable steel or case-hardening steel)
  • screws of that kind are susceptible to hydrogen-induced delayed brittle fracture formation or stress crack corrosion.
  • DE-AS No 22 11 608 to impart a very high degree of hardness to the screwthread-forming portion of a screw of that kind, such hardness extending only slightly into the screwthread core which in other respects is of a lower degree of hardness (but higher toughness).
  • Induction hardening which is used in that respect admittedly permits the desired limited hardening effect to be achieved, but it requires individual treatment of the screws in an annular coil, which involves the corresponding expenditure of time and cost.
  • disconformities are formed between that edge zone and the core structure, because at that location there is an unintended annealing effect in respect of inductive heating. Those disconformities can penetrate so far in the radial direction that they partially displace the heat-treated structure which is initially present there and in that way produce a torsional rupture-endangered cross-section.
  • the invention seeks to provide simplified production without limitation of the range of uses of the fixing elements and also to afford a simpler structure of such fixing elements.
  • the process aspect of the invention provides that the annealing operation is effected by inductive heating to a temperature above annealing brittleness and is limited to the region of the fixing element, which is outside the functional tip. That is based on the fundamental notion that the hardness of the martensite structure formed by the known austenitisation operation and subsequent quenching is sufficient for the purposes of use in relation to a hard counterpart material; in accordance with a development of the invention that hardness can be still further increased by recarburisation or carbonitriding in the region near the edge.
  • the hardness of the martensite structure is not reduced again (in the interests of higher toughness) by heating the entire fixing element to the annealing temperature, and the functional tip—that is to say for example the screwthread-forming and possibly hole-forming shaping zone of a screw—is also not subjected to more extensive special treatment, but a heat-treated structure consisting of annealed martensite is produced in the remainder of the fixing element (for example the screw), which does not belong to the functional tip or the shaping zone, by virtue of partial short-term annealing by means of inductive heating; that heat-treated structure of annealed martensite, in the fixing condition, can withstand the stresses produced in that situation, without stress crack corrosion and brittle fracture formation.
  • the annealing treatment in the furnace is eliminated and correspondingly reduces the manufacturing expenditure.
  • martensite besides non-annealed martensite, is also used to denote unstressed and low-annealed martensite. That can be afforded if the fixing element is subjected for example to a tempering treatment (about 1800-220° C.) after galvanic coating or a baking/precipitation-hardening treatment (approximately 300° C.) in the context of a dip coating operation. In comparison heating to a temperature above annealing brittleness ( ⁇ 360° C.) results in (highly) annealed martensite.
  • a tempering treatment about 1800-220° C.
  • a baking/precipitation-hardening treatment approximately 300° C.
  • the hardness of the functional tip can be further increased if at least the tip is recarburised or carbonitrided during heating to and holding at the austenitisation temperature.
  • the edge hardness of the functional tip/screwthread-forming zone can thereby be increased to 750-950 HV0.3, with a core hardness of 350-650 HV0.3. If the region of the fixing element, which is outside the functional tip, is also recarburised or carbonitrided, that affords overall four regions of different hardness levels, more specifically two in the axial direction (tip/shank) and two in the radial direction (edge/core).
  • Preferred inductive heating of the fixing elements in a continuous-heating procedure through a line inductor permits a high treatment speed and a correspondingly high output which further reduces the additional costs of such fixing elements, in comparison with conventional fixing elements of the same quality.
  • the functional tip is advantageously cooled—for example in a water bath—in order not to adversely affect its hardness, by virtue of heating to the annealing temperature.
  • the functional tip is formed by an at least screwthread-forming shaping zone.
  • the shaping zone can also be continued to the screw tip in a hole-forming portion, that is to say a boring portion or a flow hole-forming portion.
  • the fixing element can also be a firing bolt fixed by a bolt-setting gun or a rivet, in particular a stamping rivet.
  • a fixing element according to the invention with a hardened functional tip comprising a carbon-bearing steel whose structure is in part martensitic and in part annealed martensitic, wherein the functional tip is martensitic throughout and the remainder of the fixing element comprises a martensite annealed by short-term inductive heating.
  • the functional tip consisting of martensite has the high level of hardness required for driving the fixing element into a hard counterpart material, while the annealed martensite of the remainder of the fixing element (as a consequence of the short-term inductive heating thereof to the annealing temperature) has a notched bar toughness which allows it, even under stress, to withstand being endangered by hydrogen-induced brittle fracture formation or stress crack corrosion.
  • martensite besides non-annealed martensite, is further used to denote unstressed and low-annealed martensite.
  • a wire portion (bar) of low-alloyed carbon steel such as SAE 1018/18B3/16MnCr5 (which can be case-hardened with recarburisation or carbonitriding) or SAE 1022/22MnB4Cr/35B2/34CrMo4 (which can be heat-treated) or a high-alloyed carbon-bearing steel such as for example X20Cr13 or X38CrMoV15 (that is to say stainless steel) is upset at one end to form a screw head.
  • a bore-forming part or flow hole-forming part of the functional tip is formed on the other end by squeezing. Then, a screwthread is rolled on to the shank which is therebetween.
  • the initial threads serve for forming the thread and belong to the shaping zone which forms the functional tip.
  • the rough screw is then heated to austenitisation temperature in the furnace and, depending on the respective material/dimensioning/furnace type, maintained at that temperature for 10 to 60 minutes; in that case, case-hardenable steel can be recarburised or carbonitrided.
  • the screw is then quenched in water or oil.
  • the portions of the screw which lie outside the functional tip are inductively heated to an annealing temperature in a linear inductor for 3 to 60 seconds, while at the same time the functional tip is cooled, for example in a water bath.
  • the screw can be coated for the purposes of corrosion protection.

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  • 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)
  • Heat Treatment Of Articles (AREA)
  • Heat Treatment Of Sheet Steel (AREA)
  • Treatment Of Steel In Its Molten State (AREA)
  • Connection Of Plates (AREA)
  • Gripping Jigs, Holding Jigs, And Positioning Jigs (AREA)

Abstract

A fixing element which comprises carbon-bearing steel and has a hardened functional tip is overall heated to the austenitisation temperature, held at that temperature and then quenched and is then subjected to an annealing operation which is effected by inductive heating and limited to the region of the fixing element, which lies outside the functional tip. In that way the structure of the fixing element comprises in part martensite and in part annealed martensite, wherein the functional tip comprises throughout martensite and the remainder of the fixing element comprises a martensite which is annealed by short-term inductive heating.

Description

  • The invention concerns a process for the production of a fixing element which has a hardened functional tip and comprises a carbon-bearing steel which after heating to austenitisation temperature and subsequent quenching forms martensite, wherein the fixing element is heated overall to the austenitisation temperature, held at that temperature and then quenched and is then subjected to an annealing operation. It further concerns a fixing element, in particular a screw having a screwthread-forming and possibly hole-forming shaping zone, the structure thereof comprising in part martensite and in part annealed martensite. [0001]
  • Fixing elements which are to be driven into hard materials require a correspondingly hard functional tip. The functional tip can involve preferably in the present case—the shaping zone of a screw, which forms a counterpart thread and possibly pre-bores or flow-shapes the hole which is required beforehand. The functional tip however can also be the driving-in tip of a firing bolt fixed by a bolt-setting gun, or the cutting ring edge of a stamping rivet. [0002]
  • In the case of screws comprising low-alloyed carbon steel (heat-treatable steel or case-hardening steel), it is known for them to be hardened and annealed in continuous-heating furnace installations or case-hardened and annealed, with recarburisation or carbonitriding. In particular after subsequent galvanic coating, screws of that kind are susceptible to hydrogen-induced delayed brittle fracture formation or stress crack corrosion. It is also known from DE-AS No 22 11 608 to impart a very high degree of hardness to the screwthread-forming portion of a screw of that kind, such hardness extending only slightly into the screwthread core which in other respects is of a lower degree of hardness (but higher toughness). Induction hardening which is used in that respect admittedly permits the desired limited hardening effect to be achieved, but it requires individual treatment of the screws in an annular coil, which involves the corresponding expenditure of time and cost. [0003]
  • Finally, it is also known for thorough or penetration hardening of a screw consisting of heat-treatable steel (heating it and holding it for a prolonged period of time at the austenitisation temperature and then quenching in water or oil) with subsequent annealing, to be followed by inductive hardening which is limited to the shaping zone, by a procedure whereby the outer edge region of the shaping zone is briefly heated again to the austenitisation temperature and freshly quenched. As a result, in this case also, only that edge region is transformed to hard martensite while the core retains the lattice structure of the annealed martensite produced by the preceding annealing operation. It will be noted however that disconformities are formed between that edge zone and the core structure, because at that location there is an unintended annealing effect in respect of inductive heating. Those disconformities can penetrate so far in the radial direction that they partially displace the heat-treated structure which is initially present there and in that way produce a torsional rupture-endangered cross-section. [0004]
  • In place of the generally multi-stage and at any event complicated and expensive process for the production of a fixing element with a hard functional tip, the invention seeks to provide simplified production without limitation of the range of uses of the fixing elements and also to afford a simpler structure of such fixing elements. [0005]
  • The process aspect of the invention provides that the annealing operation is effected by inductive heating to a temperature above annealing brittleness and is limited to the region of the fixing element, which is outside the functional tip. That is based on the fundamental notion that the hardness of the martensite structure formed by the known austenitisation operation and subsequent quenching is sufficient for the purposes of use in relation to a hard counterpart material; in accordance with a development of the invention that hardness can be still further increased by recarburisation or carbonitriding in the region near the edge. Then the hardness of the martensite structure is not reduced again (in the interests of higher toughness) by heating the entire fixing element to the annealing temperature, and the functional tip—that is to say for example the screwthread-forming and possibly hole-forming shaping zone of a screw—is also not subjected to more extensive special treatment, but a heat-treated structure consisting of annealed martensite is produced in the remainder of the fixing element (for example the screw), which does not belong to the functional tip or the shaping zone, by virtue of partial short-term annealing by means of inductive heating; that heat-treated structure of annealed martensite, in the fixing condition, can withstand the stresses produced in that situation, without stress crack corrosion and brittle fracture formation. The annealing treatment in the furnace is eliminated and correspondingly reduces the manufacturing expenditure. [0006]
  • In this respect, the term martensite, besides non-annealed martensite, is also used to denote unstressed and low-annealed martensite. That can be afforded if the fixing element is subjected for example to a tempering treatment (about 1800-220° C.) after galvanic coating or a baking/precipitation-hardening treatment (approximately 300° C.) in the context of a dip coating operation. In comparison heating to a temperature above annealing brittleness (≧360° C.) results in (highly) annealed martensite. [0007]
  • The hardness of the functional tip can be further increased if at least the tip is recarburised or carbonitrided during heating to and holding at the austenitisation temperature. The edge hardness of the functional tip/screwthread-forming zone can thereby be increased to 750-950 HV0.3, with a core hardness of 350-650 HV0.3. If the region of the fixing element, which is outside the functional tip, is also recarburised or carbonitrided, that affords overall four regions of different hardness levels, more specifically two in the axial direction (tip/shank) and two in the radial direction (edge/core). [0008]
  • Preferred inductive heating of the fixing elements in a continuous-heating procedure through a line inductor permits a high treatment speed and a correspondingly high output which further reduces the additional costs of such fixing elements, in comparison with conventional fixing elements of the same quality. During inductive heating of the remaining length of the fixing element, that is to say all portions thereof which are outside its functional tip, the functional tip is advantageously cooled—for example in a water bath—in order not to adversely affect its hardness, by virtue of heating to the annealing temperature. [0009]
  • If the fixing element is a screw the functional tip is formed by an at least screwthread-forming shaping zone. The shaping zone however can also be continued to the screw tip in a hole-forming portion, that is to say a boring portion or a flow hole-forming portion. In a comparable manner however the fixing element can also be a firing bolt fixed by a bolt-setting gun or a rivet, in particular a stamping rivet. [0010]
  • In a corresponding manner a fixing element according to the invention with a hardened functional tip comprising a carbon-bearing steel whose structure is in part martensitic and in part annealed martensitic, wherein the functional tip is martensitic throughout and the remainder of the fixing element comprises a martensite annealed by short-term inductive heating. The functional tip consisting of martensite has the high level of hardness required for driving the fixing element into a hard counterpart material, while the annealed martensite of the remainder of the fixing element (as a consequence of the short-term inductive heating thereof to the annealing temperature) has a notched bar toughness which allows it, even under stress, to withstand being endangered by hydrogen-induced brittle fracture formation or stress crack corrosion. In this respect in this case also the term martensite, besides non-annealed martensite, is further used to denote unstressed and low-annealed martensite. [0011]
  • EXAMPLE
  • A wire portion (bar) of low-alloyed carbon steel such as SAE 1018/18B3/16MnCr5 (which can be case-hardened with recarburisation or carbonitriding) or SAE 1022/22MnB4Cr/35B2/34CrMo4 (which can be heat-treated) or a high-alloyed carbon-bearing steel such as for example X20Cr13 or X38CrMoV15 (that is to say stainless steel) is upset at one end to form a screw head. A bore-forming part or flow hole-forming part of the functional tip is formed on the other end by squeezing. Then, a screwthread is rolled on to the shank which is therebetween. The initial threads serve for forming the thread and belong to the shaping zone which forms the functional tip. [0012]
  • The rough screw is then heated to austenitisation temperature in the furnace and, depending on the respective material/dimensioning/furnace type, maintained at that temperature for 10 to 60 minutes; in that case, case-hardenable steel can be recarburised or carbonitrided. The screw is then quenched in water or oil. [0013]
  • Thereupon, the portions of the screw which lie outside the functional tip (head, possibly the screwthread-free shank portion, and the holding pitches of the screwthread) are inductively heated to an annealing temperature in a linear inductor for 3 to 60 seconds, while at the same time the functional tip is cooled, for example in a water bath. [0014]
  • Finally the screw can be coated for the purposes of corrosion protection. [0015]

Claims (14)

1. A process for the production of a fixing element which has a hardened functional tip and comprises a carbon-bearing steel which after heating to austenitisation temperature and subsequent quenching forms martensite, wherein the fixing element is heated overall to the austenitisation temperature, held at that temperature and then quenched and is then subjected to an annealing operation, characterised in that the annealing operation is effected by inductive heating to a temperature above annealing brittleness and is restricted to the region of the fixing element, which lies outside the functional tip.
2. A process according to claim 1 characterised in that a low-alloyed carbon steel is used as the carbon-bearing steel.
3. A process according to claim 1 characterised in that a high-alloyed carbon steel is used as the carbon-bearing steel.
4. A process according to claim 2 characterised in that at least the functional tip is recarburised or carbonitrided during the operation of heating to the austenitisation temperature.
5. A process according to one of claims 1 to 4 characterised in that the inductive heating operation is effected in a continuous mode through a line inductor.
6. A process according to one of claims 1 to 5 characterised in that the functional tip is cooled during inductive heating of the rest of the fixing element.
7. A process according to one of claims 1 to 6 characterised in that the fixing element is a screw and the functional tip is a screwthread-forming and possibly hole-forming shaping zone.
8. A process according to one of claims 1 to 6 characterised in that the fixing element is a firing nail or setting bolt.
9. A process according to one of claims 1 to 6 characterised in that the fixing element is a rivet, in particular a stamping rivet.
10. A fixing element which comprises a carbon-bearing steel and has a hardened functional tip and whose structure comprises in part martensite and in part annealed martensite, characterised in that the functional tip comprises martensite throughout and the remainder of the fixing element comprises a martensite annealed by short-term inductive heating to a temperature above annealing brittleness.
11. A fixing element according to claim 8 characterised in that the edge region at least of the functional tip is case-hardened as a result of recarburisation or carbonitriding.
12. A fixing element according to claim 8 or claim 9 characterised in that it is a screw and the functional tip is a screwthread-forming and possibly hole-forming shaping zone.
13. A fixing element according to claim 8 or claim 9 characterised in that it is a firing nail or setting bolt.
14. A fixing element according to claim 8 or claim 9 characterised in that it is a rivet, in particular a stamping rivet.
US10/480,882 2001-11-28 2002-11-19 Fastening element made of carbon-containing steel and method for the production thereof Abandoned US20040154705A1 (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
US11/404,452 US20060185768A1 (en) 2001-11-28 2006-04-14 Fixing element comprising a low-alloyed steel and process for the production thereof
US11/519,417 US20070062620A1 (en) 2001-11-28 2006-09-12 Fixing element comprising a low-alloyed steel and process for the production thereof

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
DE10158197.1 2001-11-28
DE10158197A DE10158197A1 (en) 2001-11-28 2001-11-28 Fastener made from a low alloy carbon steel and process for its manufacture
PCT/EP2002/012943 WO2003046229A1 (en) 2001-11-28 2002-11-19 Fastening element made of a carbon-containing steel and method for the production thereof

Related Child Applications (2)

Application Number Title Priority Date Filing Date
US11/404,452 Division US20060185768A1 (en) 2001-11-28 2006-04-14 Fixing element comprising a low-alloyed steel and process for the production thereof
US11/519,417 Continuation US20070062620A1 (en) 2001-11-28 2006-09-12 Fixing element comprising a low-alloyed steel and process for the production thereof

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US20040154705A1 true US20040154705A1 (en) 2004-08-12

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Application Number Title Priority Date Filing Date
US10/480,882 Abandoned US20040154705A1 (en) 2001-11-28 2002-11-19 Fastening element made of carbon-containing steel and method for the production thereof
US11/404,452 Abandoned US20060185768A1 (en) 2001-11-28 2006-04-14 Fixing element comprising a low-alloyed steel and process for the production thereof
US11/519,417 Abandoned US20070062620A1 (en) 2001-11-28 2006-09-12 Fixing element comprising a low-alloyed steel and process for the production thereof

Family Applications After (2)

Application Number Title Priority Date Filing Date
US11/404,452 Abandoned US20060185768A1 (en) 2001-11-28 2006-04-14 Fixing element comprising a low-alloyed steel and process for the production thereof
US11/519,417 Abandoned US20070062620A1 (en) 2001-11-28 2006-09-12 Fixing element comprising a low-alloyed steel and process for the production thereof

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CN104197127A (en) * 2014-09-17 2014-12-10 平湖市当湖街道飞天人机械图文设计服务部 Connecting bolt of oil circuit of numerical-control lathe and process for thermally treating connecting bolt
CN104191560A (en) * 2014-09-21 2014-12-10 金方明 Injection molding machine base pressing plate and heat processing technology thereof
CN104197128A (en) * 2014-09-17 2014-12-10 平湖市当湖街道飞天人机械图文设计服务部 Bolt of oil circuit of numerical-control lathe and process for thermally treating bolt
CN104196851A (en) * 2014-09-17 2014-12-10 平湖市当湖街道飞天人机械图文设计服务部 Automotive body connector and heat treatment process thereof
CN104212964A (en) * 2014-09-21 2014-12-17 金方明 Injection molding machine pressing plate connecting piece and heat treating process thereof
CN104212962A (en) * 2014-09-17 2014-12-17 平湖市当湖街道飞天人机械图文设计服务部 CNC lathe hoisting system connecting element and heat treatment technology of CNC lathe hoisting system connecting element
CN104229229A (en) * 2014-09-21 2014-12-24 金方明 Connector for lifting mechanism of packing machine and thermal processing technique thereof
CN104227430A (en) * 2014-09-17 2014-12-24 平湖市当湖街道飞天人机械图文设计服务部 Lifting system base of numerical control lathe and thermal treatment technology of lifting system base
CN104227052A (en) * 2014-09-17 2014-12-24 平湖市当湖街道飞天人机械图文设计服务部 Turning tool outer cover of numerical control lathe and thermal treatment technology of turning tool outer cover
US11331703B2 (en) * 2015-09-25 2022-05-17 Nippon Steel Corporation Piercer plug and method of manufacturing the same

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JP2014506287A (en) * 2010-12-20 2014-03-13 エヨット ゲーエムベーハー ウント カンパニー カーゲー Low alloy carbon steel screw and method of manufacturing the screw
US20130302109A1 (en) * 2010-12-20 2013-11-14 Ejot Gmbh & Co. Kg Screw made of low-alloy carbon steel, and method for producing such a screw
US9340848B2 (en) * 2010-12-20 2016-05-17 Ejot Gmbh And Co. Kg Screw made of low-alloy carbon steel, and method for producing such a screw
CN104227430A (en) * 2014-09-17 2014-12-24 平湖市当湖街道飞天人机械图文设计服务部 Lifting system base of numerical control lathe and thermal treatment technology of lifting system base
CN104197127A (en) * 2014-09-17 2014-12-10 平湖市当湖街道飞天人机械图文设计服务部 Connecting bolt of oil circuit of numerical-control lathe and process for thermally treating connecting bolt
CN104197128A (en) * 2014-09-17 2014-12-10 平湖市当湖街道飞天人机械图文设计服务部 Bolt of oil circuit of numerical-control lathe and process for thermally treating bolt
CN104196851A (en) * 2014-09-17 2014-12-10 平湖市当湖街道飞天人机械图文设计服务部 Automotive body connector and heat treatment process thereof
CN104212962A (en) * 2014-09-17 2014-12-17 平湖市当湖街道飞天人机械图文设计服务部 CNC lathe hoisting system connecting element and heat treatment technology of CNC lathe hoisting system connecting element
CN104227052A (en) * 2014-09-17 2014-12-24 平湖市当湖街道飞天人机械图文设计服务部 Turning tool outer cover of numerical control lathe and thermal treatment technology of turning tool outer cover
CN104191560A (en) * 2014-09-21 2014-12-10 金方明 Injection molding machine base pressing plate and heat processing technology thereof
CN104229229A (en) * 2014-09-21 2014-12-24 金方明 Connector for lifting mechanism of packing machine and thermal processing technique thereof
CN104212964A (en) * 2014-09-21 2014-12-17 金方明 Injection molding machine pressing plate connecting piece and heat treating process thereof
US11331703B2 (en) * 2015-09-25 2022-05-17 Nippon Steel Corporation Piercer plug and method of manufacturing the same

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DE10158197A1 (en) 2003-06-12
WO2003046229A1 (en) 2003-06-05
DE50210135D1 (en) 2007-06-21
US20070062620A1 (en) 2007-03-22
AU2002352053A1 (en) 2003-06-10
EP1451378A1 (en) 2004-09-01
ATE361999T1 (en) 2007-06-15
EP1451378B1 (en) 2007-05-09
US20060185768A1 (en) 2006-08-24
ES2286308T3 (en) 2007-12-01

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