CN106480363B - 30CrMnSiNi2A steel laser cladding powder and preparation method - Google Patents

30CrMnSiNi2A steel laser cladding powder and preparation method Download PDF

Info

Publication number
CN106480363B
CN106480363B CN201611026294.0A CN201611026294A CN106480363B CN 106480363 B CN106480363 B CN 106480363B CN 201611026294 A CN201611026294 A CN 201611026294A CN 106480363 B CN106480363 B CN 106480363B
Authority
CN
China
Prior art keywords
laser cladding
cladding powder
steel
steel laser
powder
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.)
Active
Application number
CN201611026294.0A
Other languages
Chinese (zh)
Other versions
CN106480363A (en
Inventor
陈海牛
张保森
许宜军
阚艳
孙涛
程宗辉
曹强
张志强
张小辉
曾晓利
黄卫华
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
State Run Wuhu Machinery Factory
Original Assignee
State Run Wuhu Machinery Factory
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by State Run Wuhu Machinery Factory filed Critical State Run Wuhu Machinery Factory
Priority to CN201611026294.0A priority Critical patent/CN106480363B/en
Publication of CN106480363A publication Critical patent/CN106480363A/en
Application granted granted Critical
Publication of CN106480363B publication Critical patent/CN106480363B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/04Ferrous alloys, e.g. steel alloys containing manganese
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F1/00Metallic powder; Treatment of metallic powder, e.g. to facilitate working or to improve properties
    • B22F1/05Metallic powder characterised by the size or surface area of the particles
    • B22F1/052Metallic powder characterised by the size or surface area of the particles characterised by a mixture of particles of different sizes or by the particle size distribution
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F9/00Making metallic powder or suspensions thereof
    • B22F9/02Making metallic powder or suspensions thereof using physical processes
    • B22F9/06Making metallic powder or suspensions thereof using physical processes starting from liquid material
    • B22F9/08Making metallic powder or suspensions thereof using physical processes starting from liquid material by casting, e.g. through sieves or in water, by atomising or spraying
    • B22F9/082Making metallic powder or suspensions thereof using physical processes starting from liquid material by casting, e.g. through sieves or in water, by atomising or spraying atomising using a fluid
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/005Ferrous alloys, e.g. steel alloys containing rare earths, i.e. Sc, Y, Lanthanides
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/02Ferrous alloys, e.g. steel alloys containing silicon
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/18Ferrous alloys, e.g. steel alloys containing chromium
    • C22C38/40Ferrous alloys, e.g. steel alloys containing chromium with nickel
    • C22C38/42Ferrous alloys, e.g. steel alloys containing chromium with nickel with copper
    • 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
    • C23C24/00Coating starting from inorganic powder
    • C23C24/08Coating starting from inorganic powder by application of heat or pressure and heat
    • C23C24/10Coating starting from inorganic powder by application of heat or pressure and heat with intermediate formation of a liquid phase in the layer
    • C23C24/103Coating with metallic material, i.e. metals or metal alloys, optionally comprising hard particles, e.g. oxides, carbides or nitrides
    • C23C24/106Coating with metal alloys or metal elements only

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Manufacture Of Metal Powder And Suspensions Thereof (AREA)
  • Powder Metallurgy (AREA)

Abstract

The present invention relates to 30CrMnSiNi2A steel laser cladding powder and preparation methods, the amount of each component is Cr0.8% 1.0% by weight percentage in the laser cladding powder, Mn0.75% 1.10%, Si0.65% 1.10%, Ni2.0% 3.2%, C0.16% 0.22%, Cu0.15% 0.20%, P0.015% 0.020%, S0.01% 0.015%, rare earth 0.001% 0.015%, surplus is iron.Present invention further propose that the preparation method of cladding powder, laser cladding powder is exclusively used in the laser melting and coating technique of 30CrMnSiNi2A steel, ensure the excellent bond strength in cladding interface, the dilution rate of lower metallurgical imperfection and reduction, and improve the toughness of cladding layer, the wetability of cladding powder is changed, cladding layer is inhibited to crack and delay crack growth rate.

Description

30CrMnSiNi2A steel laser cladding powder and preparation method
Technical field
The present invention relates to laser melting and coating techniques, and in particular to 30CrMnSiNi2A steel laser cladding powder and preparation side Method.
Background technology
30CrMnSiNi2A ultrafort steels are because it is with higher intensity, good plasticity, toughness and quenching degree and good Antifatigue and abrasion resistance etc., is widely used in the important forging of aviation, sheet metal component and weldment, such as wing crossbeam, connection spiral shell The primary structure members such as bolt, undercarriage.30CrMnSiNi2Tensile strength (the σ of A ultrafort steelsb) up to 1600~1800MPa, fracture toughness (KIc) up to 105MPa/m, it cools down in the oil, quenching degree diameter of section can reach 50mm or more.However aircraft is under service condition High-frequency vibration be easy to make parts to generate fatigue failure, most of crackles originate from workpiece surface, and harmfulness is suitable Big;In addition, 30CrMnSiNi2A is more sensitive to notch, it is breakneck that corrosion, which occurs, in key position, using traditional Renovation technique is susceptible to crackle, it is most important that workpiece can be made to generate the deformation beyond tolerance.In recent years, laser melting coating Technology is quickly grown, and is widely used in the reparation of aviation part etc..
Laser melting and coating technique is a kind of use laser beam heats cladding material and matrix surface, makes required special material melting welding In the new surface modifications technology of piece surface.The principle of laser melting coating refers to being added cladding material with different adding material modes To on by the surface of cladding matrix, using the laser emission of high-energy-density to matrix surface, make matrix surface thin layer and cladding material Material rapid melting simultaneously solidifies generation metallurgical binding, significantly improves the wear resistance and corrosion resistance of matrix surface.Laser melting coating and conventional surface Engineering is compared, and heat input is relatively low, and the thermal deformation of material is small, and energy consumption is small, theoretically can be on a variety of materials surface layer using flexible Using laser melting and coating technique, and following process very little or need not process.In addition, the chilling in laser cladding process can make The tissue of cladding layer is finer and close, and crystal grain more refines, to make mechanical property be significantly improved.
Laser cladding of material refers mainly to form the material used in consolidation layer, to obtain the ideal laser cladding layer of performance, The selection of cladding material is most important, it is necessary to should meet part operating mode and the requirement of laser melting coating common processes.Cladding material is not But there is good laser melting coating performance, and the metallurgical compatibility that cladding material should have with base material, can be formed uniformly Combination interface.Under normal conditions, first, cladding material and parent metal coefficient of thermal expansion are as close as possible, if the two Coefficient of thermal expansion difference is too big, then cladding layer is also easy to produce crackle and even peels off;Second is that the fusing point of cladding material and parent metal is wanted It is close;Third, should have good wetability between cladding material and parent metal.
Currently, dedicated laser cladding powder powder material shortage is the key that restrict laser melting and coating technique engineer application and popularization One of factor.Mostly using hot spray powder as raw material, existing main problem is because swashing for the implementation of existing many melting and coating process Optical energy density bigger causes ingredient scaling loss in cladding process serious, and powder flowbility is insufficient.It is super for 30CrMnSiNi2A The laser cladding powder correlative study report of strong steel matrix is less, because its tensile strength is up to 1600~1800MPa, elongation of having no progeny Rate is maintained at 10% or so, larger using laser melting coating difficulty, and difficulty is to be difficult to ensure that laser cladding layer reaches and parent Consistent or close intensity and toughness matching.It is a variety of that Co50, Ni60, GH4169, AF1410, Fe90 etc. are used in the prior art The superpower steel matrix of existing hot spraying powder foot couple 30CrMnSiNi2A has carried out cladding reparation, is extremely difficult to preferable effect.It is main The mass defect wanted is that cladding layer dilution rate is high, cladding layer porosity is high, cladding bed boundary melts bad, oxidation folder there are more Miscellaneous and micro-crack, cladding layer aoxidize serious etc..
Invention content
It is an object of the invention to provide 30CrMnSiNi2A steel laser melting coatings for overcome the deficiencies in the prior art Powder and preparation method.The main component of the laser cladding powder of the present invention is close with the composition of 30CrMnSiNi2A steel, and this Invention further provides the preparation method of laser cladding powder, and the laser cladding powder in the present invention is exclusively used in In the laser melting and coating technique of 30CrMnSiNi2A ultrafort steels, ensure the excellent bond strength in cladding interface, lower metallurgical imperfection With the dilution rate of reduction, and the toughness of cladding layer is improved, improve the wetability of cladding powder, cladding layer is inhibited to crack and delay Crack growth rate.
In order to achieve the above technical purposes, the technical solution adopted by the present invention is:
30CrMnSiNi2A steel laser cladding powders, each component in the 30CrMnSiNi2A steel laser cladding powder It measures and is by weight percentage:Cr 0.8%-1.0%, Mn 0.75%-1.10%, Si 0.65%-1.10%, Ni 2.0%- 3.2%, C 0.16%-0.22%, Cu 0.15%-0.20%, P 0.015%-0.020%, S 0.01%-0.015% is dilute Native 0.001%-0.015%, surplus are iron.
The further preferred scheme of 30CrMnSiNi2A steel laser cladding powder proposed by the present invention is:
Wherein, the amount of each component is by weight percentage in the 30CrMnSiNi2A steel laser cladding powder:Cr 0.85%-0.95%, Mn 0.85%-1.0%, Si 0.80%-1.0%, Ni 2.3%-3.0%, C 0.18%-0.20%, Cu 0.15%-0.18%, P 0.015%-0.018%, S 0.01%-0.013%, rare earth 0.005%-0.013%, surplus For iron.
Further preferably, the amount of each component is by weight percentage in the 30CrMnSiNi2A steel laser cladding powder For:Cr 0.90%-0.95%, Mn 0.90%-1.0%, Si 0.85%-0.90%, Ni 2.5%-2.7%, C 0.18%- 0.19%, Cu 0.15%-0.17%, P 0.015%-0.016%, S 0.01%-0.013%, rare earth 0.008%- 0.010%, surplus is iron.
Most preferably, the amount of each component in the 30CrMnSiNi2A steel laser cladding powder is by weight percentage: Cr 0.9%, Mn 1.0%, Si 0.85%, Ni 2.6%, C 0.19%, Cu 0.15%, P 0.015%, S 0.012%, Rare earth 0.009%, surplus are iron.
Wherein, at least one of rare earth La, Ce, Y, preferably La.
Wherein, the size of 30CrMnSiNi2A steel laser cladding powder proposed by the present invention includes micron order and nanometer Grade, the wherein weight ratio of micron order and nano level laser cladding powder are 10-20:1.Wherein, micron-sized laser cladding powder The average grain diameter at end is 40-200 μm;The average grain diameter of nano level laser cladding powder is 80-350nm.Wherein, described The microscopic appearance of 30CrMnSiNi2A steel laser cladding powder is spherical.
The preparation method of the special laser cladding powder of 30CrMnSiNi2A ultrafort steels proposed by the present invention, the present invention directly with 30CrMnSiNi2A base materials are the body material of laser cladding powder, by adding Fe/Ni/ on the basis of the body material Rare earth alloy is prepared;Preparation method includes mixing raw material 30CrMnSiNi2A bars and Fe/Ni/ rare earth alloy powders to melt Melt, then is prepared by being atomized to be granulated.Wherein, the Fe/Ni/ rare earth alloy powders are by melting, tundish refining, Gao Zhen Empty deoxygenation refining is made.
Wherein, the preparation method of the 30CrMnSiNi2A steel laser cladding powder includes the following steps:
Step 1:Dispensing:Each component weight percent content prepares in laser cladding powder described in accordance with the claim 1 Raw material 30CrMnSiNi2A bars and Fe/Ni/ rare earth alloy powders;
Step 2:Melting:The raw material of step steady is subjected to melting, obtains alloy molten solution;
Step 3:Atomization:The alloy solution that step 2 obtains further is atomized, atomizing medium is -15 DEG C -- 5 DEG C of argon The pressure of gas atmosphere, atomization is 3-6MPa;After atomization, obtained after room temperature, drying in the inert atmosphere of room temperature.
Wherein, the atomizing medium described in step 3 is preferably -11 DEG C -- and 9 DEG C of argon gas atmosphere, atomizing pressure are preferably 4- 5MPa。
Wherein, the smelting temperature described in step 2 is 1400-1500 DEG C, and soaking time is 12-18 hours.
Wherein, inert atmosphere is preferably argon gas atmosphere.
In the preparation method of 30CrMnSiNi2A steel laser cladding powder proposed by the present invention, preferably in the mist of step 3 Hydrogen is passed through during changing simultaneously, the wherein volume ratio of argon gas and hydrogen is 20-30:1;So that further being dropped in atomization process Impurity in eutectic whiting end.Wherein, the detailed process of step 3 is:The alloy solution that step 2 obtains further is atomized, Atomizing medium is -15 DEG C -- the pressure of 5 DEG C of argon gas atmosphere, atomization is 3-6MPa;It is passed through hydrogen simultaneously during atomization, The volume ratio of middle argon gas and hydrogen is 20-30:1;After atomization, room temperature inert atmosphere down toward room temperature, it is dry after to obtain the final product It arrives.
Wherein, in the atomization steps described in step 3, the volume ratio of argon gas and hydrogen is preferably 25-30:1.Wherein, hydrogen The gas of room temperature may be used.
A kind of 30CrMnSiNi2A steel laser cladding powder proposed by the present invention and preparation method have the beneficial effect that:
(1) laser cladding powder that the present invention obtains is in 30CrMnSiNi2A ultrafort steels so that main group of cladding layer It point is consistent, makes it have good wetability, physics and chemistry compatibility and similar melts with the superpower steel matrix of 30CrMnSiNi2A Point so that cladding interface has excellent bond strength, lower metallurgical imperfection and lower dilution rate.
(2) present invention regulates and controls the carbon equivalent in laser cladding powder, and regulates and controls out suitable carbon equivalent value, carries The high toughness of cladding layer, reaches the matched well of intensity and toughness.
(3) content that Ni elements are suitably increased in laser cladding powder of the invention exists the content regulation and control of Ni elements In appropriate range, be conducive to further increase the wetability of cladding powder and the toughness of cladding layer and crack arrest ability, inhibit molten Coating cracks and delays crack growth rate;Contain trace rare-earth in laser cladding powder simultaneously, can crystal grain thinning, purification is molten Body strengthens crystal boundary, improves the obdurability of cladding layer.
(4) size for the laser cladding powder that the present invention obtains includes micron order and nanometer grade powder, wherein further adjusting The weight ratio of micron powder and nanometer grade powder has been controlled, while micron powder size and nanometer grade powder size have been carried out Regulation and control so that the compactness for the cladding layer that laser cladding powder is used to be formed in laser melting and coating technique greatly improves, and improves molten The quality of coating.
(5) in the preparation method of laser cladding powder proposed by the present invention, -15 DEG C are used in atomization steps for the first time -- 5 DEG C argon gas, further regulated and controled the size of cladding powder, regulated and controled micron powder and nanometer grade powder in cladding powder Content;And the impurity content that a small amount of hydrogen further decreases cladding powder is passed through while atomization.
(6) impact flexibility for the cladding layer that laser cladding powder proposed by the present invention is formed is 428-475kJ/m2, tension Intensity is 1570-1820MPa, elongation percentage 9%-13%.
Specific implementation mode
Technical scheme of the present invention is described in detail with reference to specific embodiment.
Embodiment 1
30CrMnSiNi2A steel laser cladding powders, wherein in the 30CrMnSiNi2A steel laser cladding powder The amount of each component is by weight percentage:Cr 0.8%, Mn 0.75%, Si 0.65%, Ni 2.0%, C 0.16%, Cu 0.15%, P 0.015%, S 0.01%, La 0.001%, surplus are iron.
Specifically preparation method is:
Step 1:Dispensing:Prepare raw material according to each component weight percent content in above-mentioned laser cladding powder 30CrMnSiNi2A bars and Fe/Ni/La alloy powders.
Step 2:Melting:The raw material of step steady is placed in high vacuum protection electric furnace under the protection of argon gas and is carried out Melting, smelting temperature are 1400 DEG C, and soaking time 12 hours obtains alloy molten solution;
Step 3:Atomization:The alloy solution that step 2 obtains further is atomized, the argon gas gas that atomizing medium is -15 DEG C The pressure of atmosphere, atomization is 3MPa;Hydrogen is passed through during atomization simultaneously, the wherein volume ratio of argon gas and hydrogen is 25:1;Mist After change, obtained after room temperature, drying in the inert atmosphere of room temperature.
Size in obtained laser cladding powder includes micron order and nanoscale, wherein micron-sized cladding powder and receiving The weight ratio of the cladding powder of meter level is 10:1.
Embodiment 2
A kind of 30CrMnSiNi2A steel laser cladding powder, wherein the 30CrMnSiNi2A steel laser cladding powder The amount of each component is by weight percentage in end:Cr 0.85%, Mn 0.85%, Si 0.80%, Ni 2.3%, C 0.18%, Cu 0.15%, P 0.015%, S 0.01%, La 0.005%, surplus are iron.
Specifically preparation method is:
Step 1:Dispensing:Prepare raw material according to each component weight percent content in above-mentioned laser cladding powder 30CrMnSiNi2A bars and Fe/Ni/La alloy powders.
Step 2:Melting:The raw material of step steady is placed in high vacuum protection electric furnace under the protection of argon gas and is carried out Melting, smelting temperature are 1400 DEG C, and soaking time is 15 hours, obtains alloy molten solution;
Step 3:Atomization:The alloy solution that step 2 obtains further is atomized, the argon gas gas that atomizing medium is -14 DEG C The pressure of atmosphere, atomization is 3.5MPa;Hydrogen is passed through during atomization simultaneously, the wherein volume ratio of argon gas and hydrogen is 25:1; After atomization, obtained after room temperature, drying in the inert atmosphere of room temperature.
Size in obtained laser cladding powder includes micron order and nanoscale, wherein micron-sized cladding powder and receiving The weight ratio of the cladding powder of meter level is 12:1.
Embodiment 3
A kind of 30CrMnSiNi2A steel laser cladding powder, wherein the 30CrMnSiNi2A steel laser cladding powder The amount of each component is by weight percentage in end:Cr 0.90%, Mn 0.90%, Si 0.85%, Ni 2.50%, C 0.18%, Cu 0.15%, P 0.015%, S 0.01%, La 0.005%, Ce 0.003%, surplus are iron.
Specifically preparation method is:
Step 1:Dispensing:Prepare raw material according to each component weight percent content in above-mentioned laser cladding powder 30CrMnSiNi2A bars and Fe/Ni/La/Ce alloy powders.
Step 2:Melting:The raw material of step steady is placed in high vacuum protection electric furnace under the protection of argon gas and is carried out Melting, smelting temperature are 1400 DEG C, and soaking time is 15 hours, obtains alloy molten solution;
Step 3:Atomization:The alloy solution that step 2 obtains further is atomized, the argon gas gas that atomizing medium is -13 DEG C The pressure of atmosphere, atomization is 3.5MPa;Hydrogen is passed through during atomization simultaneously, the wherein volume ratio of argon gas and hydrogen is 25:1; After atomization, obtained after room temperature, drying in the inert atmosphere of room temperature.
Size in obtained laser cladding powder includes micron order and nanoscale, wherein micron-sized cladding powder and receiving The weight ratio of the cladding powder of meter level is 13:1.
Embodiment 4
A kind of 30CrMnSiNi2A steel laser cladding powder, wherein the 30CrMnSiNi2A steel laser cladding powder The amount of each component is by weight percentage in end:Cr 0.95%, Mn 1.0%, Si 0.90%, Ni 2.70%, C 0.19%, Cu 0.17%, P 0.016%, S 0.013%, La 0.010%, surplus are iron.
Specifically preparation method is:
Step 1:Dispensing:Prepare raw material according to each component weight percent content in above-mentioned laser cladding powder 30CrMnSiNi2A bars and Fe/Ni/La alloy powders.
Step 2:Melting:The raw material of step steady is placed in high vacuum protection electric furnace under the protection of argon gas and is carried out Melting, smelting temperature are 1500 DEG C, and soaking time is 12 hours, obtains alloy molten solution;
Step 3:Atomization:The alloy solution that step 2 obtains further is atomized, the argon gas gas that atomizing medium is -11 DEG C The pressure of atmosphere, atomization is 3.5MPa;Hydrogen is passed through during atomization simultaneously, the wherein volume ratio of argon gas and hydrogen is 23:1; After atomization, obtained after room temperature, drying in the inert atmosphere of room temperature.
Size in obtained laser cladding powder includes micron order and nanoscale, wherein micron-sized cladding powder and receiving The weight ratio of the cladding powder of meter level is 14:1.
Embodiment 5
A kind of 30CrMnSiNi2A steel laser cladding powder, wherein the 30CrMnSiNi2A steel laser cladding powder The amount of each component is by weight percentage in end:Cr 0.90%, Mn 1.0%, Si 0.85%, Ni 2.60%, C 0.19%, Cu 0.15%, P 0.015%, S 0.012%, La 0.009%, surplus are iron.
Specifically preparation method is:
Step 1:Dispensing:Prepare raw material according to each component weight percent content in above-mentioned laser cladding powder 30CrMnSiNi2A bars and Fe/Ni/La/Ce alloy powders.
Step 2:Melting:The raw material of step steady is placed in high vacuum protection electric furnace under the protection of argon gas and is carried out Melting, smelting temperature are 1450 DEG C, and soaking time is 15 hours, obtains alloy molten solution;
Step 3:The alloy solution that step 2 obtains further is atomized by atomization, the argon gas gas that atomizing medium is -10 DEG C The pressure of atmosphere, atomization is 4.5MPa;Hydrogen is passed through during atomization simultaneously, the wherein volume ratio of argon gas and hydrogen is 23:1; After atomization, obtained after room temperature, drying in the inert atmosphere of room temperature.
Size in obtained laser cladding powder includes micron order and nanoscale, wherein micron-sized cladding powder and receiving The weight ratio of the cladding powder of meter level is 16:1.
Embodiment 6
A kind of 30CrMnSiNi2A steel laser cladding powder, wherein the 30CrMnSiNi2A steel laser cladding powder The amount of each component is by weight percentage in end:Cr 0.95%, Mn 1.0%, Si 1.0%, Ni 3.0%, C 0.20%, Cu 0.18%, P 0.018%, S 0.013%, La 0.009%, 0.004% surpluses of Ce are iron.
Specifically preparation method is:
Step 1:Dispensing:Prepare raw material according to each component weight percent content in above-mentioned laser cladding powder 30CrMnSiNi2A bars and Fe/Ni/La alloy powders.
Step 2:Melting:The raw material of step steady is placed in high vacuum protection electric furnace under the protection of argon gas and is carried out Melting, smelting temperature are 1400 DEG C, and soaking time is 15 hours, obtains alloy molten solution;
Step 3:Atomization:The alloy solution that step 2 obtains further is atomized, the argon gas gas that atomizing medium is -8 DEG C The pressure of atmosphere, atomization is 4MPa;Hydrogen is passed through during atomization simultaneously, the wherein volume ratio of argon gas and hydrogen is 20:1;Mist After change, obtained after room temperature, drying in the inert atmosphere of room temperature.
Size in obtained laser cladding powder includes micron order and nanoscale, wherein micron-sized cladding powder and receiving The weight ratio of the cladding powder of meter level is 18:1.
Embodiment 7
A kind of 30CrMnSiNi2A steel laser cladding powder, wherein the 30CrMnSiNi2A steel laser cladding powder The amount of each component is by weight percentage in end:Cr 1.0%, Mn 1.10%, Si 1.10%, Ni 3.2%, C 0.22%, Cu 0.20%, P 0.020%, S 0.015%, La 0.015%, surplus are iron.
Specifically preparation method is:
Step 1:Dispensing:Prepare raw material according to each component weight percent content in above-mentioned laser cladding powder 30CrMnSiNi2A bars and Fe/Ni/La alloy powders.
Step 2:Melting:The raw material of step steady is placed in high vacuum protection electric furnace under the protection of argon gas and is carried out Melting, smelting temperature are 1400 DEG C, and soaking time is 15 hours, obtains alloy molten solution;
Step 3:Atomization:The alloy solution that step 2 obtains further is atomized, the argon gas gas that atomizing medium is -5 DEG C The pressure of atmosphere, atomization is 5MPa;Hydrogen is passed through during atomization simultaneously, the wherein volume ratio of argon gas and hydrogen is 20:1;Mist After change, obtained after room temperature, drying in the inert atmosphere of room temperature.
Size in obtained laser cladding powder includes micron order and nanoscale, wherein micron-sized cladding powder and receiving The weight ratio of the cladding powder of meter level is 20:1.
Performance test:
The cladding powder of cladding embodiment 1- embodiments 7 is distinguished on 30CrMnSiNi2A ultrafort steels using high power laser End forms cladding layer on 30CrMnSiNi2A ultrafort steels.
Specially:Drying and processing is carried out to the cladding powder of embodiment 1- embodiments 7 respectively before cladding, it is right 30CrMnSiNi2A extra-strong steel belts cladding area is cleared up, it is ensured that substrate material surface is bright and is cleaned with acetone, to reduce table Planar defect impacts laser technology.Powder is sent out by powder feeder, and laser molten pool, cladding are sent by coaxial powder-feeding nozzle Cheng Zhong, using argon gas protective gas, good gas shield can reduce the formation of defects in cladding layer.Finally in matrix surface shape At one layer of fine and close cladding layer.Laser melting coating parameter uses basis material laser melting coating Optimal Parameters of the same race.Design parameter is as follows Shown in table.Using multi-track overlapping melting and coating technique, overlapping rate is 40~50%, and single track cladding layer height is not more than 0.5mm.Its In, laser melting coating parameter is:Laser power 1200W, sweep speed 0.01m/s, powder feeding rate keep off for Low, shielding gas velocity 400L/h。
One layer of cladding layer is prepared on 30CrMnSiNi2A ultrafort steels using the laser melting coating parameter of optimization.Macroscopically cladding Layer surface no significant defect.Cladding layer is formed uniformly, and bright in color is consistent.To cladding layer capability test result referring to following table:
All explanations being not directed to belong to techniques known in the specific implementation mode of the present invention, can be public for reference Know that technology is implemented.
Above-mentioned specific implementation mode is to 30CrMnSiNi2A steel laser cladding powder proposed by the present invention and preparation side The specific support of law technology thought cannot limit protection scope of the present invention with this, everything thinks according to technology proposed by the present invention Think, any same variation made on the basis of the technical program or equivalent change, belongs to technical solution of the present invention guarantor Protect range.

Claims (9)

1.30CrMnSiNi2A steel laser cladding powders, which is characterized in that the 30CrMnSiNi2A steel laser cladding powder The amount of each component is by weight percentage in end:Cr 0.8%-1.0%, Mn 0.75%-1.10%, Si 0.65%- 1.10%, Ni 2.0%-3.2%, C 0.16%-0.22%, Cu 0.15%-0.20%, P 0.015%-0.020%, S 0.01%-0.015%, rare earth 0.001%-0.015%, surplus are iron;The 30CrMnSiNi2A steel laser cladding powder Size include micron order and nanoscale, wherein the weight ratio of micron order and nano level laser cladding powder is 10-20:1.
2. 30CrMnSiNi2A steel laser cladding powder according to claim 1, which is characterized in that described The amount of each component is by weight percentage in 30CrMnSiNi2A steel laser cladding powders:Cr 0.85%-0.95%, Mn 0.85%-1.0%, Si 0.80%-1.0%, Ni 2.3%-3.0%, C 0.18%-0.20%, Cu 0.15%-0.18%, P 0.015%-0.018%, S 0.01%-0.013%, rare earth 0.005%-0.013%, surplus is iron.
3. 30CrMnSiNi2A steel laser cladding powder according to claim 1, which is characterized in that described The amount of each component is by weight percentage in 30CrMnSiNi2A steel laser cladding powders:Cr 0.9%, Mn 1.0%, Si 0.85%, Ni 2.6%, C 0.19%, Cu 0.15%, P 0.015%, S 0.012%, rare earth 0.009%, surplus are iron.
4. according to any 30CrMnSiNi2A steel laser cladding powders of claim 1-3, which is characterized in that described dilute Soil is at least one of La, Ce, Y.
5. 30CrMnSiNi2A steel laser cladding powder according to claim 1, which is characterized in that described micron-sized The grain size of laser cladding powder is 40-200 μm;The grain size of the nano level laser cladding powder is 80-350nm.
The preparation method of 6.30CrMnSiNi2A steel laser cladding powders, which is characterized in that include the following steps:
Step 1:Dispensing:Each component weight percent content prepares raw material in laser cladding powder described in accordance with the claim 1 30CrMnSiNi2A bars and Fe/Ni/ rare earth alloy powders;
Step 2:Melting:The raw material of step steady is subjected to melting, obtains alloy molten solution;
Step 3:Atomization:The alloy molten solution that step 2 obtains further is atomized, atomizing medium is -15 DEG C -- 5 DEG C of argon gas The pressure of atmosphere, atomization is 3-6MPa;After atomization, obtained after room temperature, drying in the inert atmosphere of room temperature.
7. the preparation method of 30CrMnSiNi2A steel laser cladding powder according to claim 6, which is characterized in that step Atomizing medium described in rapid three is -11 DEG C -- 9 DEG C of argon gas atmosphere, atomizing pressure 4-5MPa.
8. the preparation method of 30CrMnSiNi2A steel laser cladding powder according to claim 6, which is characterized in that step Hydrogen is passed through in atomization process described in rapid three simultaneously, the wherein volume ratio of argon gas and hydrogen is 20-30:1.
9. the preparation method of 30CrMnSiNi2A steel laser cladding powder according to claim 6, which is characterized in that step Smelting temperature described in rapid two is 1400-1500 DEG C, and soaking time is 12-18 hours.
CN201611026294.0A 2016-11-22 2016-11-22 30CrMnSiNi2A steel laser cladding powder and preparation method Active CN106480363B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201611026294.0A CN106480363B (en) 2016-11-22 2016-11-22 30CrMnSiNi2A steel laser cladding powder and preparation method

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201611026294.0A CN106480363B (en) 2016-11-22 2016-11-22 30CrMnSiNi2A steel laser cladding powder and preparation method

Publications (2)

Publication Number Publication Date
CN106480363A CN106480363A (en) 2017-03-08
CN106480363B true CN106480363B (en) 2018-08-17

Family

ID=58272633

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201611026294.0A Active CN106480363B (en) 2016-11-22 2016-11-22 30CrMnSiNi2A steel laser cladding powder and preparation method

Country Status (1)

Country Link
CN (1) CN106480363B (en)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111593343B (en) * 2020-06-10 2022-03-15 中国航发北京航空材料研究院 Process method for repairing flap slide rail chromium plating surface chipping defect by laser cladding
CN112296328B (en) * 2020-09-24 2022-12-30 山东鲁银新材料科技有限公司 Preparation method of railway pantograph slide plate
CN114351136A (en) * 2021-12-15 2022-04-15 国营芜湖机械厂 Gradient repairing and enhancing method for wear surface of airplane super-strong steel part
CN114505486A (en) * 2022-02-11 2022-05-17 三明辰亿五金制品有限公司 Stainless steel powder for powder metallurgy high-density balance block and manufacturing method thereof
CN115386871A (en) * 2022-08-29 2022-11-25 黄河水利委员会黄河水利科学研究院 High-impact-cavitation-corrosion-resistant coating
CN116179945B (en) * 2023-01-29 2023-10-27 济南大学 Laser cladding powder for high temperature 45# steel

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101758219A (en) * 2009-12-28 2010-06-30 天津大族烨峤激光技术有限公司 Iron-based alloy material for laser repair of rotor main shaft and manufacturing method thereof
CN102652181A (en) * 2010-01-18 2012-08-29 住友金属工业株式会社 Steel sheet with small welding deformation and excellent corrosion resistance
CN103966599A (en) * 2014-05-26 2014-08-06 山东能源机械集团大族再制造有限公司 Alloy powder used for laser cladding and preparation method thereof
CN105108294A (en) * 2015-08-31 2015-12-02 中国船舶重工集团公司第七二五研究所 Vacuum electron beam welding method for 30CrMnSiNi2A steel

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101758219A (en) * 2009-12-28 2010-06-30 天津大族烨峤激光技术有限公司 Iron-based alloy material for laser repair of rotor main shaft and manufacturing method thereof
CN102652181A (en) * 2010-01-18 2012-08-29 住友金属工业株式会社 Steel sheet with small welding deformation and excellent corrosion resistance
CN103966599A (en) * 2014-05-26 2014-08-06 山东能源机械集团大族再制造有限公司 Alloy powder used for laser cladding and preparation method thereof
CN105108294A (en) * 2015-08-31 2015-12-02 中国船舶重工集团公司第七二五研究所 Vacuum electron beam welding method for 30CrMnSiNi2A steel

Also Published As

Publication number Publication date
CN106480363A (en) 2017-03-08

Similar Documents

Publication Publication Date Title
CN106480363B (en) 30CrMnSiNi2A steel laser cladding powder and preparation method
WO2022174766A1 (en) Titanium alloy powder for selective laser melting 3d printing, and selective laser melting titanium alloy and preparation thereof
CN110344053B (en) Alloy powder for high-strength bainitic steel laser repair and preparation method thereof
CN111593238A (en) Laser coaxial powder feeding additive manufacturing aluminum alloy powder and application thereof in repairing 5-series aluminum alloy
CN113445041B (en) Preparation method of low-cost light high-entropy alloy/aluminum oxide composite coating on surface of magnesium alloy
CN101994113A (en) Laser cladding process of wear-resistant and corrosion-resistant coating of top cover of hydraulic turbine set
CN111647884A (en) Gradient nanocrystalline and ultrafine-grained coating and preparation method thereof
CN113042748B (en) Method for preparing high-strength high-elongation Al-Cu-Mg alloy by SLM
CN100547114C (en) A kind of on the metallic surface method of fusing and coating high-hardness tungsten carbide coat
CN106756994A (en) A kind of nickel-based composite pow-der of laser cladding coating and the method for prepares coating
CN101284334B (en) Application of laser weld in ultra-high tensile steel welding and welding method
CN113817935A (en) High-purity nickel-based high-temperature alloy and preparation method of spherical powder thereof
CN113416952A (en) TiC reinforced metal matrix composite alloy powder for laser cladding of nodular iron castings and preparation method thereof
CN109440049B (en) Method for preparing amorphous aluminum coating by compounding electric arc spraying and laser remelting
CN104498774A (en) Alloy powder for gray pig iron laser cladding repair and preparation method thereof
CN114054775B (en) Aging strengthening type nickel-based high-temperature alloy 3D printing process and manufactured 3D printing piece
CN114411056A (en) Iron-based alloy powder, laser cladding coating and preparation method thereof
CN106480449A (en) A kind of method that laser manufactures heavy section universal mill horizontal roller
CN114892043A (en) High-toughness high-temperature nickel-based alloy powder special for laser additive manufacturing and preparation method thereof
CN113136532B (en) Iron-based alloy powder for laser cladding and preparation method thereof
CN105312752B (en) A kind of iron-based amorphous coating and preparation method thereof
CN110760841B (en) Preparation method of amorphous nanocrystalline coating on aluminum alloy surface
CN102127729A (en) Soldering strengthening method for thermal sprayed coating on surface of metal material
CN105220084B (en) Iron-based amorphous nanocrystalline composite coating and preparation method thereof
CN112157269A (en) Preparation method of cold spray coating based on heat treatment of aluminum alloy powder

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
CB03 Change of inventor or designer information

Inventor after: Chen Hainiu

Inventor after: Zeng Xiaoli

Inventor after: Huang Weihua

Inventor after: Zhang Baosen

Inventor after: Xu Yijun

Inventor after: Han Yan

Inventor after: Sun Tao

Inventor after: Cheng Zonghui

Inventor after: Cao Qiang

Inventor after: Zhang Zhiqiang

Inventor after: Zhang Xiaohui

Inventor before: Chen Hainiu

Inventor before: Huang Weihua

Inventor before: Xu Yijun

Inventor before: Han Yan

Inventor before: Sun Tao

Inventor before: Cheng Zonghui

Inventor before: Cao Qiang

Inventor before: Zhang Zhiqiang

Inventor before: Zhang Xiaohui

Inventor before: Zeng Xiaoli

COR Change of bibliographic data
SE01 Entry into force of request for substantive examination
SE01 Entry into force of request for substantive examination
GR01 Patent grant
GR01 Patent grant