CN103409745A - Nickel and nickel alloy alumina reinforced composite surface strengthening layer making method - Google Patents

Nickel and nickel alloy alumina reinforced composite surface strengthening layer making method Download PDF

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Publication number
CN103409745A
CN103409745A CN2013103026297A CN201310302629A CN103409745A CN 103409745 A CN103409745 A CN 103409745A CN 2013103026297 A CN2013103026297 A CN 2013103026297A CN 201310302629 A CN201310302629 A CN 201310302629A CN 103409745 A CN103409745 A CN 103409745A
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surfacing
nickel
powder
reinforced composite
spray
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王文权
卢宝胜
徐国成
宫文彪
商延赓
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Jilin University
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Jilin University
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Abstract

The invention discloses a nickel and nickel alloy alumina reinforced composite surface strengthening layer making method, and belongs to the technical fields of the surface material preparation and surface processing. The method concretely comprises the following steps: 1, cleaning the surface of a die steel substrate, and putting component-distributed surfacing powder in a powder feeder; 2, carrying out plasma surfacing: carrying out automatic powder feeding surfacing under a current of 25A by adopting a mixed gas formed by 25% of hydrogen and 75% of argon after the arc stabilization, and controlling the moving speed and the powder feeding rate of a spray gun to obtain a surfaced layer having a thickness according with a requirement; and 3, controlling the overlapping portion of the loci of the spray gun being 20% of the width of a single spraying locus to make the surface of the surfaced layer smooth and flat. The use of a small current in the invention realizes the substantial reduction of the heat input, decreases the heat influence zone range, and reserves alumina as possible as a hard sport reinforcement; and compared with surface layers made through using flame surfacing or laser cladding methods, the surface layer obtained in the invention has the characteristics of thickness control convenience, good surface quality and high hardness.

Description

A kind of nickel and nickelalloy aluminum oxide reinforced composite surface strengthen layer preparation method
Technical field
The present invention relates to a kind of die steel matrix alumina reinforced composite surface strengthen layer, belong to surfacing preparation and Surface-micromachining process field, particularly a kind of nickel and nickelalloy aluminum oxide reinforced composite surface strengthen layer preparation method.
Background technology
Die steel 4Cr5MoSiV1 (being commonly referred to as H13) is because containing higher carbon and vanadium, and this steel has high hardening capacity, thermal crack resistant ability, good thermotolerance and heat resistance and higher anti-temper resistance.Based on the good over-all properties of this steel, all be widely applied aspect hammer forging die, hot extruding die and transfer mold.But because the working conditions of die steel is severe, not only to repeatedly experience high temperature-low temperature thermal cycling effect, and to bear larger repeated stress, make die surface usually because of wearing and tearing or thermal fatigue generation defect, one of key technical problem that so die surface strengthening (life-prolonging technique) and defect repair are relevant enterprises always will be solved (Song Qiang etc.: plasma spray wear-resistant coating preparation and property is analyzed. Nanjing University of Technology's journal, 2009,31 (5), 102-105).
The die surface strengthening life-prolonging technique is the wear-resisting modified layer of die cavity damageable zone deposition one deck at mould, after modification, the mould working-surface has high hardness, and inside still has good toughness, thereby can improve the use properties of mould, give full play to the performance potential of moulding stock.The mould repair technology is that the position that mould has damaged is repaired, and makes its reinstatement (shape and performance), the mould after processing treatment can continue to use, thereby has extended the work-ing life of mould.At present, die surface reparation commonly used or the major project means of strengthening have carburizing or the methods such as nitriding, arc surfacing, electric spark deposition, Brush Plating and laser melting coating.In the processing method for preparing the die surface repair layer, arc surfacing is often very large due to heat input, and the heat affected zone of causing on mould is very large being repaired, and easily causes die deformation even to ftracture; The electric spark deposition method, because the bond quality of settled layer and matrix is uncertain, particularly porosity and compactness are discontinuous, and some intends the repair materials of use, as the alloy system complicated component, or, for high rigidity, high-strength material, be difficult to be processed into silk material or the bar of electrode requirement, and when the reparation amount is larger, production efficiency is extremely low, rehabilitation cost very high (Xu Dong etc.: the application of electric discharge surface treatment technology on mould. the equipment manufacturing technology, 2010,4:150-153); For the Brush Plating method, coating is generally very thin, mostly be less than 0.3mm, and because the combination of coating and matrix is a kind of mechanical bond, so lower with substrate combinating strength, the practical application of above the whole bag of tricks is very limited (Zhao Weilin etc.: Brush Plating and the surfacing of vehicle mould are repaired fast. mould industry, 2007,33(2), 64-66); Laser cladding is because equipment is once invested greatly, promotion and application also have certain difficulty (Jiang Shengbo etc.: forge die coating structure and performance study are scrapped in the laser melting coating reparation. the material heat treatment technology, 2009(38), 86-88).
Summary of the invention
Technical problem to be solved by this invention is to have overcome problems of the prior art, a kind of nickel and nickelalloy aluminum oxide reinforced composite surface strengthen layer preparation method are provided, adopt the plasma spray welding technology on the die steel surface, to prepare the composite surface layer of nickel and the enhancing of nickel alloy base aluminum oxide, reach the effect of rectification of defects or strengthening matrix, recover and extend the work-ing life of mould.
For solving the problems of the technologies described above, the present invention adopts following technical scheme to realize, accompanying drawings is as follows:
The present invention is the powder alloy material (C:0.6 that adopts specific chemical composition, Si:3.0, Cr:12.8, B:2.6, Fe:7.5, WC:22, Co:3, Ni:46.5) with aluminium sesquioxide mechanically mixing carry out ball-milling processing, making its size range is 40 μ m-100 μ m, utilizes plasma spray welding technology to prepare the composite repair layer on the die steel surface.
A kind of nickel and nickelalloy aluminum oxide reinforced composite surface strengthen layer preparation method, concrete steps are as follows:
1) the die steel matrix surface is cleared up, the surfacing powder that one-tenth distributes is put into to powder feeder;
2) plasma spray: the mixed gas that the hydrogen of employing 25% and 75% argon form, current setting is 25A, after arc stability, starts the automatic powder feeding surfacing, controls spray gun translational speed and powder feeding rate to obtain the satisfactory spray-welding coating of thickness;
3) lap of controlling between the spray gun spraying track is 20% of single spraying profile width, makes spray-welding coating smooth surface, smooth.
Described surfacing powder is 85% Co-based alloy powder and 15% aluminium sesquioxide miscellany.
Described spray gun translational speed is 2.5mm/s, and described powder feeding rate is 75g/min.
The thickness of described spray-welding coating is 3mm-5mm.
Compared with prior art the invention has the beneficial effects as follows:
The present invention adopts plasma spray to be welded in the matrix material strengthening layer that the die steel matrix surface prepares nickel and the enhancing of nickel alloy base aluminum oxide, the method can be controlled the less electric current of use, heat input is reduced greatly, the heat affected zone scope is reduced, and aluminum oxide is remained as much as possible as hard point wild phase, with upper layer prepared by the methods such as flame spray welding or laser melting coating, compare, it is convenient that this upper layer has gauge control, surface quality is good, the characteristics that hardness is high are a kind of desirable die surface defect-restoration method therefor or strengthening means; Adopt " thermospray+remelting " technique or electrical arc powder bead-welding technology, also can prepare similar upper layer, but, because reflow process can cause larger heat input, make the heat affected zone range extension, seriously undermine its strengthening effect.
The accompanying drawing explanation
The present invention is further illustrated below in conjunction with accompanying drawing:
Fig. 1 prepares the mixed powder that repair layer is used;
Fig. 2 a is the Interface Microstructure of spray-welding coating and matrix;
Fig. 2 b is the tissue of spray-welding coating.
Embodiment
Below in conjunction with accompanying drawing, the present invention is explained in detail:
A) prepare the die steel body material, the acetone wiping is dipped in to absorbent cotton in surface and deoil, and the surfacing powder that one-tenth distributes is put into to powder feeder;
B) plasma arc that ignites, the adjusting flame current is 25A, and voltage is 38V, and surfacing speed is 2.5mm/s, and keeping the surfacing distance is 200mm;
C) amount of lap of controlling between per pass is 20%, makes surface spraying weld layer tissue performance even, and surface is more smooth; Per pass refers to the track of spray gun single spraying; Amount of lap refers to the spraying profile lap.
D) the mensuration microhardness distribution is as can be known, and the hardness of die steel matrix is that HV630(is about as much as HRC56), the average hardness of spray-welding coating is that HV720(is about as much as HRC61).
E) adopt pin disc type wear testing machine to carry out simultaneous test to die steel matrix and surface spraying weld layer sample, die steel matrix abrasion loss is 20.8mg, and the upper layer abrasion loss is 6.3mg, and the surface spraying weld layer improves more than 3 times than the wear resistance of die steel matrix.
Consult Fig. 2 a, metallurgical analysis shows, there are metallurgical reaction in spray-welding coating and basal body interface place, and the column crystal that epitaxial solidification forms, perpendicular to interface growth, belongs to typical metallurgical binding, has guaranteed the bonding strength between spray-welding coating and matrix.Consult Fig. 2 b, the XRD diffraction analysis shows, the main strengthening phase in the surface spraying weld layer has Al 2O 3, Cr 7C 3And Ni 4B 3Deng, be embedded on matrix.

Claims (4)

1. a nickel and nickelalloy aluminum oxide reinforced composite surface strengthen layer preparation method, is characterized in that, concrete steps are as follows:
1) the die steel matrix surface is cleared up, the surfacing powder that one-tenth distributes is put into to powder feeder;
2) plasma spray: the mixed gas that the hydrogen of employing 25% and 75% argon form, current setting is 25A, automatic powder feeding surfacing after arc stability is controlled spray gun translational speed and powder feeding rate to obtain the satisfactory spray-welding coating of thickness;
3) lap of controlling between the spray gun spraying track is 20% of single spraying profile width, makes spray-welding coating smooth surface, smooth.
2. a kind of nickel according to claim 1 and nickelalloy aluminum oxide reinforced composite surface strengthen layer preparation method, it is characterized in that: described surfacing powder is 85% Co-based alloy powder and 15% aluminium sesquioxide miscellany.
3. a kind of nickel according to claim 1 and nickelalloy aluminum oxide reinforced composite surface strengthen layer preparation method, it is characterized in that: described spray gun translational speed is 2.5mm/s, described powder feeding rate is 75g/min.
4. a kind of nickel according to claim 1 and nickelalloy aluminum oxide reinforced composite surface strengthen layer preparation method, it is characterized in that: the thickness of described spray-welding coating is 3mm-5mm.
CN2013103026297A 2013-07-18 2013-07-18 Nickel and nickel alloy alumina reinforced composite surface strengthening layer making method Pending CN103409745A (en)

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Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104611663A (en) * 2015-01-07 2015-05-13 马鞍山蓝科再制造技术有限公司 Manufacturing process of nanomaterial surface layer for mould
CN104831226A (en) * 2015-04-21 2015-08-12 吉林大学 Plasma spray welding gas-solid reaction in-situ generated nitride enhanced wear-resisting layer and process
CN109735831A (en) * 2019-03-12 2019-05-10 姜水英 A method of in aluminum alloy surface chemical plating stannum-intercalation corrosion inhibiter ion-laser melting coating
CN110238482A (en) * 2019-07-08 2019-09-17 福尼斯(南京)表面工程技术有限公司 The welding method of robot automation's two-step method flame spray welding tungsten carbide of nickel-base
CN110238483A (en) * 2019-07-08 2019-09-17 福尼斯(南京)表面工程技术有限公司 The welding method of robot automation's one-step method flame spray welding tungsten carbide of nickel-base
CN111876717A (en) * 2020-07-14 2020-11-03 江苏科环新材料有限公司 High-temperature-resistant abrasion-resistant remelting nickel-based composite material coating for grate segment of garbage incinerator and preparation thereof

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH0432579A (en) * 1990-05-30 1992-02-04 Nippon Steel Corp Surface hardening treatment of titanium-based material
CN1766151A (en) * 2005-11-17 2006-05-03 广州有色金属研究院 Method for supersonic flame spraying crystallizer brass plate
CN102212771A (en) * 2011-05-13 2011-10-12 吉林大学 Tungsten carbide reinforced composite material strengthened layer of mould steel basal body and preparation process thereof
CN102650029A (en) * 2012-04-25 2012-08-29 常州大学 Preparation method for nanometer ceramic composite coating material on surface of hot work die steel
CN101580938B (en) * 2009-06-19 2012-10-03 吉林大学 Method for preparing metallic matrix composite coating reinforced by alumina ceramics particles

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH0432579A (en) * 1990-05-30 1992-02-04 Nippon Steel Corp Surface hardening treatment of titanium-based material
CN1766151A (en) * 2005-11-17 2006-05-03 广州有色金属研究院 Method for supersonic flame spraying crystallizer brass plate
CN101580938B (en) * 2009-06-19 2012-10-03 吉林大学 Method for preparing metallic matrix composite coating reinforced by alumina ceramics particles
CN102212771A (en) * 2011-05-13 2011-10-12 吉林大学 Tungsten carbide reinforced composite material strengthened layer of mould steel basal body and preparation process thereof
CN102650029A (en) * 2012-04-25 2012-08-29 常州大学 Preparation method for nanometer ceramic composite coating material on surface of hot work die steel

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
宫文彪等: "氧化铝增强镍基合金涂层的组织与耐冲蚀磨损性能研究", 《材料热处理学报》, vol. 27, no. 1, 28 February 2006 (2006-02-28) *

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104611663A (en) * 2015-01-07 2015-05-13 马鞍山蓝科再制造技术有限公司 Manufacturing process of nanomaterial surface layer for mould
CN104831226A (en) * 2015-04-21 2015-08-12 吉林大学 Plasma spray welding gas-solid reaction in-situ generated nitride enhanced wear-resisting layer and process
CN109735831A (en) * 2019-03-12 2019-05-10 姜水英 A method of in aluminum alloy surface chemical plating stannum-intercalation corrosion inhibiter ion-laser melting coating
CN110238482A (en) * 2019-07-08 2019-09-17 福尼斯(南京)表面工程技术有限公司 The welding method of robot automation's two-step method flame spray welding tungsten carbide of nickel-base
CN110238483A (en) * 2019-07-08 2019-09-17 福尼斯(南京)表面工程技术有限公司 The welding method of robot automation's one-step method flame spray welding tungsten carbide of nickel-base
CN110238483B (en) * 2019-07-08 2021-06-08 福尼斯(南京)表面工程技术有限公司 Welding method for welding nickel-based tungsten carbide through automatic one-step flame spray welding by robot
CN110238482B (en) * 2019-07-08 2021-06-08 福尼斯(南京)表面工程技术有限公司 Welding method for welding nickel-based tungsten carbide through automatic two-step flame spray welding by robot
CN111876717A (en) * 2020-07-14 2020-11-03 江苏科环新材料有限公司 High-temperature-resistant abrasion-resistant remelting nickel-based composite material coating for grate segment of garbage incinerator and preparation thereof
CN111876717B (en) * 2020-07-14 2022-07-08 江苏科环新材料有限公司 High-temperature-resistant, abrasion-resistant and remelting nickel-based composite material coating for fire grate segment of garbage incinerator and preparation method thereof

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Application publication date: 20131127