CN107206442A - Hot forming tool - Google Patents
Hot forming tool Download PDFInfo
- Publication number
- CN107206442A CN107206442A CN201580060124.1A CN201580060124A CN107206442A CN 107206442 A CN107206442 A CN 107206442A CN 201580060124 A CN201580060124 A CN 201580060124A CN 107206442 A CN107206442 A CN 107206442A
- Authority
- CN
- China
- Prior art keywords
- matrix
- metal
- protrusion
- instrument
- braid
- 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.)
- Granted
Links
- 229910052751 metal Inorganic materials 0.000 claims abstract description 30
- 239000002184 metal Substances 0.000 claims abstract description 30
- 239000011241 protective layer Substances 0.000 claims abstract description 12
- 239000011159 matrix material Substances 0.000 claims description 33
- 238000000034 method Methods 0.000 claims description 27
- 229910000831 Steel Inorganic materials 0.000 claims description 25
- 239000010959 steel Substances 0.000 claims description 25
- 238000000576 coating method Methods 0.000 claims description 24
- 239000011248 coating agent Substances 0.000 claims description 23
- 239000000463 material Substances 0.000 claims description 22
- 239000010410 layer Substances 0.000 claims description 19
- 238000004519 manufacturing process Methods 0.000 claims description 13
- 238000005242 forging Methods 0.000 claims description 7
- 230000008569 process Effects 0.000 claims description 7
- 239000007921 spray Substances 0.000 claims description 7
- 230000003647 oxidation Effects 0.000 claims description 6
- 238000007254 oxidation reaction Methods 0.000 claims description 6
- 239000000203 mixture Substances 0.000 claims description 4
- 239000000126 substance Substances 0.000 claims description 4
- 238000005240 physical vapour deposition Methods 0.000 claims description 3
- 238000005229 chemical vapour deposition Methods 0.000 claims description 2
- 238000010285 flame spraying Methods 0.000 claims description 2
- PCHJSUWPFVWCPO-UHFFFAOYSA-N gold Chemical group [Au] PCHJSUWPFVWCPO-UHFFFAOYSA-N 0.000 claims description 2
- 239000010931 gold Substances 0.000 claims description 2
- 229910052737 gold Inorganic materials 0.000 claims description 2
- 238000007781 pre-processing Methods 0.000 claims description 2
- 238000000465 moulding Methods 0.000 claims 1
- 238000007751 thermal spraying Methods 0.000 claims 1
- 238000004804 winding Methods 0.000 claims 1
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 16
- 238000007493 shaping process Methods 0.000 description 14
- 229910052742 iron Inorganic materials 0.000 description 8
- 239000007789 gas Substances 0.000 description 7
- 239000002245 particle Substances 0.000 description 6
- 239000012071 phase Substances 0.000 description 6
- 238000006243 chemical reaction Methods 0.000 description 5
- UQSXHKLRYXJYBZ-UHFFFAOYSA-N Iron oxide Chemical compound [Fe]=O UQSXHKLRYXJYBZ-UHFFFAOYSA-N 0.000 description 4
- 239000002131 composite material Substances 0.000 description 4
- 238000005516 engineering process Methods 0.000 description 4
- 238000005507 spraying Methods 0.000 description 4
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 description 3
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 3
- 239000000919 ceramic Substances 0.000 description 3
- 150000001875 compounds Chemical class 0.000 description 3
- 230000000694 effects Effects 0.000 description 3
- 238000009413 insulation Methods 0.000 description 3
- 239000001301 oxygen Substances 0.000 description 3
- 229910052760 oxygen Inorganic materials 0.000 description 3
- 238000005096 rolling process Methods 0.000 description 3
- 238000005299 abrasion Methods 0.000 description 2
- 239000000654 additive Substances 0.000 description 2
- 230000000996 additive effect Effects 0.000 description 2
- 239000000853 adhesive Substances 0.000 description 2
- 230000001070 adhesive effect Effects 0.000 description 2
- 239000000956 alloy Substances 0.000 description 2
- 238000006701 autoxidation reaction Methods 0.000 description 2
- 238000000151 deposition Methods 0.000 description 2
- 238000010891 electric arc Methods 0.000 description 2
- 238000005566 electron beam evaporation Methods 0.000 description 2
- 230000008020 evaporation Effects 0.000 description 2
- 238000001704 evaporation Methods 0.000 description 2
- 239000000446 fuel Substances 0.000 description 2
- 239000011229 interlayer Substances 0.000 description 2
- 150000002500 ions Chemical class 0.000 description 2
- 230000001788 irregular Effects 0.000 description 2
- 238000003754 machining Methods 0.000 description 2
- 238000003801 milling Methods 0.000 description 2
- 230000001681 protective effect Effects 0.000 description 2
- 238000004549 pulsed laser deposition Methods 0.000 description 2
- 239000002994 raw material Substances 0.000 description 2
- 239000007787 solid Substances 0.000 description 2
- 238000003856 thermoforming Methods 0.000 description 2
- 239000002699 waste material Substances 0.000 description 2
- 229910000669 Chrome steel Inorganic materials 0.000 description 1
- ZOKXTWBITQBERF-UHFFFAOYSA-N Molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 description 1
- 230000004913 activation Effects 0.000 description 1
- 229910045601 alloy Inorganic materials 0.000 description 1
- 238000000889 atomisation Methods 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- 238000004140 cleaning Methods 0.000 description 1
- 239000008199 coating composition Substances 0.000 description 1
- 239000011247 coating layer Substances 0.000 description 1
- 239000000470 constituent Substances 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 230000008021 deposition Effects 0.000 description 1
- 238000010574 gas phase reaction Methods 0.000 description 1
- 239000007792 gaseous phase Substances 0.000 description 1
- 238000000227 grinding Methods 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 238000007749 high velocity oxygen fuel spraying Methods 0.000 description 1
- 230000008676 import Effects 0.000 description 1
- 239000000314 lubricant Substances 0.000 description 1
- 239000000289 melt material Substances 0.000 description 1
- 239000007769 metal material Substances 0.000 description 1
- 238000004377 microelectronic Methods 0.000 description 1
- 238000002156 mixing Methods 0.000 description 1
- 229910052750 molybdenum Inorganic materials 0.000 description 1
- 239000011733 molybdenum Substances 0.000 description 1
- 229910000476 molybdenum oxide Inorganic materials 0.000 description 1
- 230000001590 oxidative effect Effects 0.000 description 1
- 229910052574 oxide ceramic Inorganic materials 0.000 description 1
- PQQKPALAQIIWST-UHFFFAOYSA-N oxomolybdenum Chemical compound [Mo]=O PQQKPALAQIIWST-UHFFFAOYSA-N 0.000 description 1
- 238000010422 painting Methods 0.000 description 1
- 238000007750 plasma spraying Methods 0.000 description 1
- 238000012802 pre-warming Methods 0.000 description 1
- 230000009467 reduction Effects 0.000 description 1
- 238000007592 spray painting technique Methods 0.000 description 1
- 238000004544 sputter deposition Methods 0.000 description 1
- 238000009628 steelmaking Methods 0.000 description 1
- 239000000758 substrate Substances 0.000 description 1
- 238000002207 thermal evaporation Methods 0.000 description 1
- 230000032258 transport Effects 0.000 description 1
- 238000003466 welding Methods 0.000 description 1
- 230000036642 wellbeing Effects 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21B—ROLLING OF METAL
- B21B25/00—Mandrels for metal tube rolling mills, e.g. mandrels of the types used in the methods covered by group B21B17/00; Accessories or auxiliary means therefor ; Construction of, or alloys for, mandrels or plugs
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21B—ROLLING OF METAL
- B21B19/00—Tube-rolling by rollers arranged outside the work and having their axes not perpendicular to the axis of the work
- B21B19/02—Tube-rolling by rollers arranged outside the work and having their axes not perpendicular to the axis of the work the axes of the rollers being arranged essentially diagonally to the axis of the work, e.g. "cross" tube-rolling ; Diescher mills, Stiefel disc piercers or Stiefel rotary piercers
- B21B19/04—Rolling basic material of solid, i.e. non-hollow, structure; Piercing, e.g. rotary piercing mills
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Other Surface Treatments For Metallic Materials (AREA)
- Coating By Spraying Or Casting (AREA)
- Forging (AREA)
- Chemical Vapour Deposition (AREA)
Abstract
One kind is proposed by possessing the hot forming tool (1) that the tool base of at least part face coat (4) (2) is constituted, and thus the hot forming tool obtains：Metal bump thing is provided to tool base, it then completely or partially aoxidizes and form protective layer.
Description
Technical field
The invention belongs to manufacture the domain variability of tubular metal thing to be related to shaping jig, particularly possessing improves wearing for durability
Hole top, forging drift and plug.
Background technology
Seamless steel pipe generally goes through three thermoforming stage productions.During the first stage, about 1200 DEG C of steel billet position is heated to
In on Mannesmann piercing mill, by interior shaping jig --- perforating head, it is processed to hollow ingot.Wherein oblique roller rolling transports steel billet
Move to pass through perforating head.During second stage, hollow ingot is in longitudinal operation of rolling in interior shaping jig --- plug it is auxiliary
Help down, diameter and wall thickness are reduced and length increase.During the phase III, rolled piece be processed to needed for length and wall thickness, typically not
Using interior shaping jig.
The interior shaping jig used during the first second stage is subjected to high temperature and high machinery pressure in process of production.Therefore it is many
Shaping jig uses heat-resisting steel making in the case of number.Interior shaping is inevitably produced when being rolled for a long time in production process
The progressively heating of instrument.The intensity of instrument reduces and can not bear mechanical load after heated.Instrument is deformed and damaged in itself.
In order to improve service life, perforating head uses natural oxidizing layer.The oxide layer reduces workpiece and conducted to instrument
Heat simultaneously prevents being rapidly heated for instrument to be lost in quick intensity.The oxide layer is but quickly in the forming process of high alloy material
Come off and lose heat insulating function.
Plug is according to the different using instrument that is autoxidation or possessing layers of chrome of forming method.Corresponding top example can
With referring to the A1 of German patent DE 10 2,008 056988 (SMS MEER).The shortcoming of the technology is to be conducted for workpiece to instrument
Heat effect of heat insulation it is too small.So particularly at a slow speed with the interior shaping jig under the conditions of small contact length, can generate heat and become
Shape is damaged.
If the thickness of oxide layer is improved, the life-span of these instruments can also be lifted.Because effect of heat insulation is more preferable
And protective layer preserves the longer time in abrasion.
The iron oxide protective layer formed by matrix material autoxidation does not have high stability.It was not only crisp but also porous
It can thus be damaged easily under machinery and thermic load.Therefore the thickness of such protective layer is limited under 0.8 millimeter, protects
Effect is similarly limited.Heat can be penetrated into the matrix of instrument and reduce its intensity and be allowed to damage ahead of time.High alloy Workpiece shaping
When abrasion, protective layer can be made comparatively fast to be come off after by a bit of rolling stock.
Indicate that a kind of perforated for seamless pipe is pushed up in the A1 of international patent application WO 2,011 107214 (SMS MEER)
Head or plug or warm and hot forging tubular metal thing drift, it possesses oxide layer surface specific profile attached thereto.So can be real
Now more preferable adhesive force and longer service life.Surface forms groove during processing, i.e., resulting " frame " will not surmount
Top or the surface of plug.
Similar instrument, its coating is made up of molybdenum oxide, known by the A1 of patent EP 0385439 (NKK CORP.).
The A1 of european patent application EP 2404680 (SUMITOMO) theme is given birth to using the seamless steel pipe of Mannesmann's method
Production.It requires a perforating head, and its feature is that the top has a passage, can be by the passage by lubricant during perforation
Import perforation lanes.[0053] section of the patent points out that the top can add iron coating.A piece iron wire is imported into a spray
Painting instrument simultaneously is allowed to melt.The iron being melted is sprayed onto on top again, so as to form a continuous coating.
But cost is too high for the production of the instrument of this kind of surface specific profile in actual production, because each perforating head
Need finished surface specific profile, and can also cause the waste of material respectively.Production cost is with the increasing of Surface Machining depth
Plus superproportional increase.Economy and the feasibility upper limit are several millimeters.Another defect of processing matrix surface specific profile exists
Oxidizable steel is limited in material.Such steel chrome content is low therefore hardness is also low.
The present invention target therefore that, production possess improve service life hot forming tool, its do not possess it is above-mentioned lack
Fall into.Particularly compared with prior art, the hot forming tool possesses the oxide layer of higher intensity, and it is easy to apply and not had
Spillage of material.
The content of the invention
The first topic of the present invention is related to a kind of by possessing the heat that at least tool base of face coat is constituted in proportion
Shaping jig, thus it can be obtained, and a metal bump thing is added on matrix, and it then completely or partially aoxidizes and be converted into
Protective layer.
" projection " is meant, protrusion (" peak structure ") higher than tool surfaces and groove (" the paddy knot with being carved into surface
Structure ") the processing of surface specific profile it is opposite.
In addition present invention additionally comprises it is a kind of manufacture by possess at least in proportion the tool base of face coat constitute heat into
The method of type instrument, wherein
(a) a metal bump thing is added on matrix, and
(b) then the metal bump thing completely or partially aoxidizes and is converted into protective layer.
Additional projection thing processes contrast with tool surfaces.Add in the present invention without removing material.Unexpectedly
Ground finds that additional metal protrusion is not only more obvious than Surface Machining and is easier to realize, and all or part for passing through raised material
Conversion obtains the considerably higher and durable oxide layer of hardness, therefore the life-span of instrument can also significantly improve.In addition the present invention is gone back
Can be by selecting protrusion material to change the attribute and adjusting process condition of sealer.
Economic well-being of workers and staff that the present invention is brought is carried it is clear that particularly reduce tool expense during production product made from steel
High run time, it is related generally to the waste of material of bigger length of rolled piece and reduction.
Instrument
Hot forming tool in the present invention preferably refers to perforating head or forging drift, is typically made of steel.This
Invention also includes other matrixes under the upperseat concept needs the metallic article of heat resistanceheat resistant.Here metal be not limited to iron and
Steel, but including any other metal material during thermoforming and the composite containing metal.
The perforating head of shaping jig in oblique milling is may be advantageously used with according to the face coat of the present invention, additionally it is possible to be used for
Other interior shaping jigs in seamless steel tube production process.For the several frames continuously arranged of possessing of the second formative stage
The interior shaping jig plug of milling train is, it is necessary to which it is specifically intended that the friction between instrument and rolled piece is small.Therefore according to the present invention's
Face coat must carry out grinding and buffing when applying herein.Another layer can also be added again on the protective layer of the present invention in addition
Coating, such as layers of chrome.
The protrusion being attached on matrix can have a variety of implementations, and every kind of scheme in principle can be complete
The full requirement for reaching invention.
Protrusion is the wound wire on matrix, preferably steel wire in the first embodiment.
Metal braid or wire netting on matrix are attached in second embodiment protrusions thing.
The metal object for being attached to tool surfaces is preferentially made up of steel braid, and it is about 1 to about 5 for example to possess steel wire thickness
Millimeter, preferentially about 1.5 millimeters, mesh width is about 1 to 5 millimeter, particularly from about 2.5 millimeters.Mesh width refers to two neighboring volume
The distance between unit axis processed.
Protrusion is irregular coating in the third embodiment, passes through the physically or chemically deposited metal from gas phase.
The composition of protrusion
Protrusion attachment can according to can it is numerous can letter distinct methods carry out, but can be fully achieved invention will
Ask.
Matrix is simply by a material winds, preferably metal wire rod in the first embodiment.
Wire rod is replaced using metal braid or wire netting in second embodiment.It can be allowed to coordinate by shaping
The external form of instrument is attached on matrix again.Wire rod or metal braid are welded on matrix in order to improve intensity suggestion.
In the third embodiment can be using (the Chemical/Physical Vapour that are chemically or physically vapor-deposited
Phase Deposition, CVD/PVD) protrusion is produced on matrix surface.
Chemical vapor deposition refers to the coating process for producing microelectronics original paper and light wave guide.Due to chemical reaction
Solid constituent in gas phase is deposited on the heated surface of matrix.And on condition that there is volatile chemical combination in coating composition
Thing, can deposit the coating of solid-state under certain reaction temperature.Chemical gaseous phase depositing process is characterized in need coating
Primary first-order equation at least occurs for workpiece surface.At least one gaseous feed compound (reactive material) and at least two products --- its
In at least one be solid-state --- participate in the reaction.Promote the reaction on workpiece surface in order to suppress gas phase reaction and thereby keep away
Exempt to form solid particle, this method is preferably carried out under low pressure.
It is different from CVD, it is converted into gas phase by preferred PVD raw materials.Afterwards the gaseous material be directed to need by
The matrix of coating, gaseous material cooled and solidified simultaneously forms coating.Example is traditional evaporation, such as thermal evaporation, electron beam evaporation
(Electron Beam Evaporation) and pulsed laser deposition (Pulsed Laser Deposition).In the present invention
It is preferred that sputtering method, makes raw material atomization using Ions Bombardment and is converted into gas phase, coating is therefrom deposited on matrix again.On
It is that coating material is placed in the painting interlayer of usual vacuum with solid-state to state the methodical common ground of institute.Pass through laser bombardment, magnetic deflection
Ion or the electric discharge of electronics and arc of lighting evaporate object.The ratio of atom, electronics or big congeries is according to method in steam
It is different and variant.The material of evaporation needs coating along ballistic movement or by electron field guiding by applying interlayer and being attached to
Coating is formed on workpiece.
In order that steam particle is reached at workpiece and will not be lost in due to gas particles scattering, it is necessary to using low pressure.
Typical operating pressure is generally in 10-4 handkerchiefs between about 10 handkerchiefs.Because steam particle straight line extend, using vapor source as origin not
Visible surface is coated with low coating rate.In order to form protrusion rather than uniform coating, do not use what is generally used specially
Matrix rotary process.
The 4th embodiment for forming protrusion uses so-called plasma spray technology.The technology makes additional materials, i.e.,
So-called spray application of additive accelerates to be injected in for gaseous sprayed particle and need coating in spray gun internal and external parts or all fusings
On workpiece surface.Workpiece surface will not melt in itself (from welding it is different) and only by the thermic load of very little.Due to spraying
Grain is when touching workpiece surface according to technique and the difference of material, and more or less flattening is protected especially by mechanical grip
Hold and adhere to and successively form sprayed coating, so as to form coating.The mass property of sprayed coating is low-porosity, the high attachment with workpiece
Power, free from flaw and uniform microstructure.The coating properties realized largely are touched to be coated by sprayed particle
The influence of temperature and speed during surface.Surface state (cleaning, activation, temperature) also has notable shadow to qualitative character such as adhesive force
Ring.
The energy source of spray application of additive melt material is usually electric arc (electric arc spraying), beam-plasma (plasma spray
Apply), oxygen fuel flame or high velocity oxygen fuel flame (common or HVOF), rapidly pre-warming gas (cold gas spray) and
Laser (laser spraying).Spraying method is classified by above-mentioned standard according to DIN standards EN 657.
Metal can not only be used using this method, moreover it is possible to (or logical using oxide ceramic material and carbide material
Referred to as composite) coated substrates.It is preferred that the mixture coating of iron and ceramics carries out embodiment.
Matrix is preferably made up of steel, and the condition that the material of protrusion needs are met is：It at least can partly form oxide layer.
Therefore preferably iron or steel, so as to form iron oxide layer, preferred oxide layer (Zunder).It can also be mixed using steel/iron with ceramic
Compound, such as from 20:80 to 80:Weight between 20 scopes is than mixing.
Protrusion is it is of course possible to be of a variety of shapes, from rule (circle, side etc.) to any irregular shape.Also may be used
To use composite, such as it is attached to steel matrix with molybdenum braid.Braid can also be by hard chrome steel (inside) and easy oxygen
The composite for changing steel (outside) composition is constituted.Combustible material can be also used for the material kept at a distance.Equally may be used in addition
With embedded ceramics so as to realize more preferable thermal insulation.
Oxidation
Metal bump thing is partially or completely converted into the method progress that protective oxide film is referred to prior art, for example
Carried out using flame-spraying, plasma spraying or heat chemistry mode.
Surface attachment has a metal object, such as instrument of steel braid in oxidation, the part on tool base surface and
A part for the metal bump thing of surface attachment is converted into oxide.Extra oxidation can be formed on all surface simultaneously
Layer, its thickness is typically about 500 to about 3000 microns, and particularly from about 1500 to about 2500 microns.Thus matrix it
Between intermediate region, such as the space between the steel braid of tool base and attachment and between steel braid mesh also can shape
Into oxide.Final result is to obtain one layer of thick protective layer of spy strengthened by internal structure.Especially, with the recessed processing in surface not
Several millimeters are not limited to coating layer thickness.10 millimeters or bigger of thickness degree can be simply realized with a low cost.
Industrial applicability
Another theme of the present invention is related to the purposes of above-mentioned New type tool, particularly for producing seamless pipe or hot forging gold
Belong to the purposes of the perforating head, forging drift and plug of tube.
Embodiment
Embodiment 1
Perforating head surface attachment and weld by forming technique preprocessing be matrix external form steel braid, steel wire
Thickness is 1.5 millimeters, and mesh width is 2.5 millimeters.Then heat chemistry oxidation is carried out to the compound.Obtain 2500 micron thickness
Imporosity oxide layer.
Fig. 1 is the side view of the hot forming tool of perforating head form.Instrument 1 has a tool base 2, and it has work
Make region 3, its certain length that extends on a direction of principal axis.Instrument has coating 4 in working region 3, and it protects instrument 1 to heat
Load or mechanical load.
Fig. 2 and Fig. 3 illustrates the Local map of " Z " on the tool level tangent plane according to Fig. 1, respectively protective oxide film
The material matrix for being attached to protrusion before and after (oxide layer) formation.
The visible zigzag protrusions of Fig. 2 a, it is produced by embodiment 1 using wire rod net.Matrix uses 7 with 6, network structure
Mark.Fig. 2 b show that the part surface of protrusion has been converted into matrix surface between oxide, but mesh and also generates oxidation instead
Should be (with the dash area of 8 marks).
Similarly, simply the cross section of protrusion is not square but circular here by Fig. 3 a and Fig. 3 b.It will again be seen that
The protrusion surface and lower section of iron content form oxide layer (dash area) with same ratio.
Claims (15)
1. a kind of by possessing the hot forming tool that at least tool base of face coat is constituted in proportion, thus it obtain, in base
Body additional metal protrusion, then completely or partially oxidation forms protective layer for it.
2. instrument according to claim 1, it is characterised in that instrument is perforating head, forging drift or plug.
3. the instrument according to claim 1 and/or 2, it is characterised in that matrix is made up of metal, preferably steel.
4. the instrument according at least one in claims 1 to 3, it is characterised in that the protrusion on matrix is winding line
Material.
5. the instrument according at least one in claims 1 to 3, it is characterised in that the metal bump thing on matrix is gold
Belong to braid.
6. a kind of production is by possessing at least method for the hot forming tool that the tool base of face coat is constituted in proportion, wherein
(a) a metal bump thing is added on matrix, and
(b) then metal bump thing completely or partially aoxidizes and is converted into protective layer.
7. method according to claim 6, it is characterised in that protrusion is attached on matrix by wound wire.
8. method according to claim 6, it is characterised in that be attached to matrix by coating metal braid by protrusion
On.
9. method according to claim 8, it is characterised in that by moulding process by metal braid preprocessing be instrument
Profile and be then arranged on matrix.
10. the method according at least one in claim 7 to 9, it is characterised in that make wire rod or metal braid and base
Body is welded.
11. method according to claim 6, it is characterised in that be attached to protrusion by chemical/physical vapor deposition
On matrix.
12. method according to claim 6, it is characterised in that protrusion is attached on matrix by thermal spraying.
13. the method according at least one in claim 6 to 12, it is characterised in that matrix is by metal, preferably steel structure
Into, and the material of composition protrusion at least partly can form oxide layer.
14. the method according at least one in claim 6 to 13, it is characterised in that pass through flame-spraying, plasma spray
Apply or thermochemical method metal bump thing is completely or partially converted into oxide protective layer.
15. a kind of instrument according at least one in claim 1 to 5 is hot for producing seamless pipe or tubular metal thing
The purposes of forging.
Applications Claiming Priority (5)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE102014016502.7 | 2014-11-07 | ||
| DE102014016502.7A DE102014016502A1 (en) | 2014-11-07 | 2014-11-07 | Hot forming tool with reinforced oxide protective layer |
| EP14197507.8 | 2014-12-11 | ||
| EP14197507.8A EP3017888B1 (en) | 2014-11-07 | 2014-12-11 | Thermoforming tool |
| PCT/EP2015/075758 WO2016071423A1 (en) | 2014-11-07 | 2015-11-04 | Hot forming tool |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN107206442A true CN107206442A (en) | 2017-09-26 |
| CN107206442B CN107206442B (en) | 2020-04-07 |
Family
ID=52278347
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201580060124.1A Active CN107206442B (en) | 2014-11-07 | 2015-11-04 | Thermoforming tool |
Country Status (9)
| Country | Link |
|---|---|
| US (1) | US20170333964A1 (en) |
| EP (1) | EP3017888B1 (en) |
| JP (1) | JP2017536237A (en) |
| KR (1) | KR20170086519A (en) |
| CN (1) | CN107206442B (en) |
| BR (1) | BR112017007858A2 (en) |
| DE (1) | DE102014016502A1 (en) |
| RU (1) | RU2687321C2 (en) |
| WO (1) | WO2016071423A1 (en) |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE102018116238A1 (en) * | 2018-07-04 | 2020-01-09 | Kme Germany Gmbh & Co. Kg | Hot forming tool and method for producing a hot forming tool |
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| CN1069915A (en) * | 1992-08-06 | 1993-03-17 | 周春林 | Mandrel for metal tube rolling mill and preparation method |
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| JP2002224713A (en) * | 2001-01-31 | 2002-08-13 | Kawasaki Steel Corp | Surface protecting material and its manufacturing method of plug for plug mill |
| CN102002710A (en) * | 2010-12-30 | 2011-04-06 | 两仪激光技术（天津）有限公司 | Cladding layer crack control method of laser surface cladding process |
| CN102341193A (en) * | 2009-03-03 | 2012-02-01 | 住友金属工业株式会社 | Plug, piercing rolling apparatus and method of manufacturing seamless tube using the same |
| CN102781600A (en) * | 2010-03-02 | 2012-11-14 | Sms米尔股份有限公司 | Hot work tool and method for producing same |
| JP2014054637A (en) * | 2012-09-11 | 2014-03-27 | Jfe Steel Corp | Seamless steel pipe rolling plug and method for manufacturing the same |
Family Cites Families (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
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2015
- 2015-11-04 KR KR1020177013758A patent/KR20170086519A/en unknown
- 2015-11-04 US US15/519,988 patent/US20170333964A1/en not_active Abandoned
- 2015-11-04 CN CN201580060124.1A patent/CN107206442B/en active Active
- 2015-11-04 JP JP2017522549A patent/JP2017536237A/en active Pending
- 2015-11-04 WO PCT/EP2015/075758 patent/WO2016071423A1/en active Application Filing
- 2015-11-04 RU RU2017118964A patent/RU2687321C2/en active
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Also Published As
| Publication number | Publication date |
|---|---|
| WO2016071423A1 (en) | 2016-05-12 |
| KR20170086519A (en) | 2017-07-26 |
| RU2687321C2 (en) | 2019-05-13 |
| CN107206442B (en) | 2020-04-07 |
| JP2017536237A (en) | 2017-12-07 |
| DE102014016502A1 (en) | 2016-05-12 |
| EP3017888B1 (en) | 2019-04-24 |
| RU2017118964A (en) | 2018-12-07 |
| US20170333964A1 (en) | 2017-11-23 |
| BR112017007858A2 (en) | 2018-01-16 |
| EP3017888A1 (en) | 2016-05-11 |
| RU2017118964A3 (en) | 2018-12-07 |
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