JPH0230800B2 - PURAZUMAFUNTAIYOSETSUNIKUMORYOFUKUGOYOSETSUZAI - Google Patents
PURAZUMAFUNTAIYOSETSUNIKUMORYOFUKUGOYOSETSUZAIInfo
- Publication number
- JPH0230800B2 JPH0230800B2 JP16608987A JP16608987A JPH0230800B2 JP H0230800 B2 JPH0230800 B2 JP H0230800B2 JP 16608987 A JP16608987 A JP 16608987A JP 16608987 A JP16608987 A JP 16608987A JP H0230800 B2 JPH0230800 B2 JP H0230800B2
- Authority
- JP
- Japan
- Prior art keywords
- ceramic particles
- metal
- matrix
- layer
- 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.)
- Expired - Lifetime
Links
- 239000002245 particle Substances 0.000 claims description 29
- 239000000843 powder Substances 0.000 claims description 27
- 239000000919 ceramic Substances 0.000 claims description 25
- 229910052751 metal Inorganic materials 0.000 claims description 23
- 239000002184 metal Substances 0.000 claims description 23
- 238000003466 welding Methods 0.000 claims description 22
- 239000000463 material Substances 0.000 claims description 19
- 239000011159 matrix material Substances 0.000 claims description 19
- 239000002131 composite material Substances 0.000 claims description 18
- 239000000203 mixture Substances 0.000 claims description 12
- 238000002156 mixing Methods 0.000 claims description 7
- 229910052804 chromium Inorganic materials 0.000 claims description 4
- 229910052759 nickel Inorganic materials 0.000 claims description 4
- 229910052710 silicon Inorganic materials 0.000 claims description 3
- 239000010410 layer Substances 0.000 description 22
- 230000000694 effects Effects 0.000 description 17
- 238000000034 method Methods 0.000 description 8
- 230000003647 oxidation Effects 0.000 description 7
- 238000007254 oxidation reaction Methods 0.000 description 7
- 239000011651 chromium Substances 0.000 description 5
- 238000005728 strengthening Methods 0.000 description 5
- 238000007751 thermal spraying Methods 0.000 description 5
- MCMNRKCIXSYSNV-UHFFFAOYSA-N Zirconium dioxide Chemical compound O=[Zr]=O MCMNRKCIXSYSNV-UHFFFAOYSA-N 0.000 description 4
- 239000011324 bead Substances 0.000 description 4
- 239000011247 coating layer Substances 0.000 description 4
- 230000007423 decrease Effects 0.000 description 4
- OKKJLVBELUTLKV-UHFFFAOYSA-N Methanol Chemical compound OC OKKJLVBELUTLKV-UHFFFAOYSA-N 0.000 description 3
- 239000006185 dispersion Substances 0.000 description 3
- 239000002923 metal particle Substances 0.000 description 3
- UNASZPQZIFZUSI-UHFFFAOYSA-N methylidyneniobium Chemical compound [Nb]#C UNASZPQZIFZUSI-UHFFFAOYSA-N 0.000 description 3
- HBMJWWWQQXIZIP-UHFFFAOYSA-N silicon carbide Chemical compound [Si+]#[C-] HBMJWWWQQXIZIP-UHFFFAOYSA-N 0.000 description 3
- 239000007921 spray Substances 0.000 description 3
- 229910003470 tongbaite Inorganic materials 0.000 description 3
- 230000000052 comparative effect Effects 0.000 description 2
- 239000002612 dispersion medium Substances 0.000 description 2
- 238000005469 granulation Methods 0.000 description 2
- 230000003179 granulation Effects 0.000 description 2
- 230000005484 gravity Effects 0.000 description 2
- 239000012535 impurity Substances 0.000 description 2
- 238000003475 lamination Methods 0.000 description 2
- 229910052748 manganese Inorganic materials 0.000 description 2
- 238000002844 melting Methods 0.000 description 2
- 230000008018 melting Effects 0.000 description 2
- 239000012188 paraffin wax Substances 0.000 description 2
- 238000002360 preparation method Methods 0.000 description 2
- 238000005204 segregation Methods 0.000 description 2
- 238000000926 separation method Methods 0.000 description 2
- 239000002002 slurry Substances 0.000 description 2
- UONOETXJSWQNOL-UHFFFAOYSA-N tungsten carbide Chemical compound [W+]#[C-] UONOETXJSWQNOL-UHFFFAOYSA-N 0.000 description 2
- 229910018072 Al 2 O 3 Inorganic materials 0.000 description 1
- 229910020598 Co Fe Inorganic materials 0.000 description 1
- 229910002519 Co-Fe Inorganic materials 0.000 description 1
- LFQSCWFLJHTTHZ-UHFFFAOYSA-N Ethanol Chemical compound CCO LFQSCWFLJHTTHZ-UHFFFAOYSA-N 0.000 description 1
- 229910018487 Ni—Cr Inorganic materials 0.000 description 1
- 229910000831 Steel Inorganic materials 0.000 description 1
- 239000000956 alloy Substances 0.000 description 1
- 229910045601 alloy Inorganic materials 0.000 description 1
- PNEYBMLMFCGWSK-UHFFFAOYSA-N aluminium oxide Inorganic materials [O-2].[O-2].[O-2].[Al+3].[Al+3] PNEYBMLMFCGWSK-UHFFFAOYSA-N 0.000 description 1
- 238000001354 calcination Methods 0.000 description 1
- 239000012159 carrier gas Substances 0.000 description 1
- 239000003795 chemical substances by application Substances 0.000 description 1
- UFGZSIPAQKLCGR-UHFFFAOYSA-N chromium carbide Chemical compound [Cr]#C[Cr]C#[Cr] UFGZSIPAQKLCGR-UHFFFAOYSA-N 0.000 description 1
- 230000003749 cleanliness Effects 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 230000002950 deficient Effects 0.000 description 1
- 230000004927 fusion Effects 0.000 description 1
- 239000007789 gas Substances 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 239000008240 homogeneous mixture Substances 0.000 description 1
- 230000001771 impaired effect Effects 0.000 description 1
- 230000002401 inhibitory effect Effects 0.000 description 1
- 230000003993 interaction Effects 0.000 description 1
- 239000011229 interlayer Substances 0.000 description 1
- 229910052574 oxide ceramic Inorganic materials 0.000 description 1
- 239000011224 oxide ceramic Substances 0.000 description 1
- 238000005096 rolling process Methods 0.000 description 1
- 229920006395 saturated elastomer Polymers 0.000 description 1
- 229910010271 silicon carbide Inorganic materials 0.000 description 1
- 238000004513 sizing Methods 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 230000000087 stabilizing effect Effects 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
- MTPVUVINMAGMJL-UHFFFAOYSA-N trimethyl(1,1,2,2,2-pentafluoroethyl)silane Chemical compound C[Si](C)(C)C(F)(F)C(F)(F)F MTPVUVINMAGMJL-UHFFFAOYSA-N 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
- 239000001993 wax Substances 0.000 description 1
Landscapes
- Coating By Spraying Or Casting (AREA)
- Nonmetallic Welding Materials (AREA)
Description
〔産業上の利用分野〕
本発明は、プラズマ粉体溶接肉盛法により、金
属マトリツクスと分散相である炭化物系セラミツ
ク粒子からなる複合組織を有する肉盛層を形成す
るための溶接材に関する。
〔従来の技術〕
圧延用ロール、熱処理炉用ロール、搬送ロール
等のロール類、その他の構造部材の表面に、金属
マトリツクスと分散相であるセラミツク粒子から
なる複合組織を有する被覆層を形成することは、
これらの部材の耐熱性や耐摩耗性等を改善するた
めの極めて有効な方法である。この被覆層の形成
方法としては専ら溶射法が使用されている。その
溶射材としては、炭化珪素(SiC)、炭化タング
ステン(WC)等の炭化物系セラミツク、アルミ
ナ(Al2O3)、ジルコニア(ZrO)等の酸化物系セ
ラミツクを主体とする複合粉末が工業的に供給さ
れている。
〔発明が解決しようとする問題点〕
しかるに、溶射法により形成される被覆層(溶
射層)は、密着強度に乏しく、機械衝撃により剥
離し易いため、実機使用における安定性や耐久性
に問題がある。また、その被覆層は、複合組織の
均質性や緻密性に乏しいため、金属−セラミツク
の複合効果、特にセラミツク粒子の分散強化作用
が十分ではなく、高温域における強度、耐摩耗
性、耐熱性等の諸特性についてそれほどの改善効
果を期待することはできない。
本発明は上記問題点を解決するためのプラズマ
粉体溶接肉盛用複合溶接材を提供するものであ
る。
〔問題点を解決するための手段および作用〕
本発明は、マトリツクスとなる金属分と分散相
となる炭化物系セラミツク粒子とからなるプラズ
マ粉体溶接肉盛用溶接材において、
分散相となる炭化物系セラミツク粒子の配合割
合が20〜80重量%であり、
マトリツクスとなる金属分が、C:0.08%以
下、Si:0.5〜3%、Mn:2%以下、Ni:2〜10
%、Cr:15〜30%、Co:20〜40%、残部実質的
にFeからなる成分組成を有するものであること
を特徴としている。
本発明の複合溶接材において、分散相となるセ
ラミツク粒子は炭化物系セラミツク粒子である。
炭化物系セラミツク粒子は、硬質で強度が高く、
また金属マトリツクスとの濡れもよく、分散強化
成分としてすぐれている。その好ましい例とし
て、クロム炭化物(Cr3C2、Cr7C2等)、タングス
テン炭化物(WC)、チタン炭化物(TiC)、ニオ
ブ炭化物(NbC)、炭化珪素(SiC)等が挙げら
れる。
分散相となる上記炭化物系セラミツク粒子の配
合割合(マトリツクスとなる金属分との混合物中
に占める重量比)を20%以上とするのは、それよ
り少いと分散強化作用が十分でなく、例えば硬度
不足等が生じるからである。その配合割合を高め
るに従つて、分散強化作用による硬度、耐摩耗
性、耐熱性、高温強度等の向上をみるが、80%を
こえると、溶接ビードの多層盛りにおいて、ビー
ド積層間の密着不良が生じる等、溶接施工性が悪
くなり、また形成される肉盛層が靭性の乏しいも
のとなる等の不都合をきたすので、80%を上限と
した。なお、炭化物系セラミツク粒子の粒度は特
に限定しないけれども、その分散強化作用を十分
なものとするために、約50μm以下であることが
好ましく、特に2〜15μmの微細粒子である場合
は、肉盛層内の転位移動の阻止効果が高く、低温
および高温域におけるより高いレベルの強度を確
保することが可能となる。
他方、マトリツクスとなる金属分は、Ni−Cr
−Co−Fe合金であり、その成分組成の限定理由
は次のとおりである。
C:0.08%以下
Cは不純物元素である。マトリツクス金属を高
融点に保つために、上限を0.08%とする。
Si:0.5〜3%以下
Siは溶接肉盛時に形成される溶融金属の流動性
の確保および脱酸効果の点から、少なくとも0.5
%を必要とする。しかし、3%をこえると、マト
リツクスの靭性が低くなるので、3%を上限とす
る。
Mn:2%以下
MnはSiと同様に、溶融金属の脱酸作用を有す
るほか、溶融金属中の不純物であるSをMnSと
して固定化することにより、有害なFeSの生成を
防止する。しかし、含有量が多くなると、溶融金
属中におけるMnSの残存量が増加し、マトリツ
クス金属の清浄度が損なわれるので、2%を上限
とする。
Cr:15〜30%
Crはマトリツクス金属の耐酸化性を高める。
この効果を十分なものとするには、少なくとも15
%を必要とする。含有量の増加に伴つてその効果
は増すが、30%を越えると、靭性が低下するの
で、30%を上限とする。
Ni:2〜10%
Niは金属マトリツクスの靭性を高めると共に、
Crとの相互作用により耐酸化性を強化する。ま
た分散相である炭化物系セラミツク粒子との濡れ
性を良くし、複合組織の緻密性および均質性を高
める効果を有する。含有量が2%に満たないと、
上記効果が不足し、他方10%をこえると、マトリ
ツクスの融点の低下を免れない。よつて2〜10%
とする。
Co:20〜40%
Coはマトリツクスの高温強度の確保、および
炭化物系セラミツク粒子に対する濡れ性の確保の
ために少くとも20%を必要とする。その効果は含
有量の増加に伴つて強化されるが、40%をこえる
と、その効果はほぼ飽和するので、それ以上の増
量は経済的でない。よつて、40%を上限とする。
マトリツクスとなる金属分の粉末粒度は特に限
定されないが、前記セラミツク粒子との混合物の
均質性を高めるためには40〜100μm程度の粒径で
あるのが好ましい。その粉末混合物は、そのまま
溶接肉盛材として使用してよいけれども、金属粒
子とセラミツク粒子とは比重差が大きいため、溶
接肉盛施工時に、Arガス等をキヤリヤガスとし
て粉体送給配管を介して溶接トーチまで送給する
過程で、また溶接トーチからその直下の溶接母材
表面の溶融プールに散布する際に、金属粒子とセ
ラミツク粒子の分離・偏析が生じることがある。
特に、粉末粒径が微細であるほどその傾向が著し
くなる。この粉末混合物の比重差による分離・偏
析の防止策としては、粉末混合物を、適当な粒径
好ましくは50〜300μm程度の造粒粉として使用す
ることが極めて効果的である。その造粒粉は公知
の造粒法により、例えば粉末混合物に、適当な糊
剤、例えばパラフイン等のワツクスを適量(例え
ば、粉末混合物100重量部に対して、2〜3重量
部)添加し、これをアルコール、水等の分散媒に
懸濁してスラリーとしたうえ、湿式噴霧乾燥機
(スプレードライヤ)に供して、造粒粉となし、
脱ろう後、焼成し、ついで粉砕機で300〜60メツ
シユに解砕処理することにより製造される。
本発明の溶接材を用いるプラズマ粉体溶接肉盛
法によりロール等の部材表面に形成される複合肉
盛層は、部材表面に対する強固な融着結合関係を
有し、1200℃以上の高温度においても良好な密着
強度を失うことがなく、またその複合組織は均
質・緻密であり、耐熱性、耐酸化性にすぐれてい
ると同時に、高温での硬度が高く、従つて高温域
においても高い摩耗抵抗性を示す。また、溶接施
工性が良いので、用途に応じた厚薄任意の層厚を
有する肉盛層を形成することができる。
〔実施例〕
〔〕 溶接肉盛材の調製
(1) マトリツクス金属粉末粒径:50μm
(2) 炭化物系セラミツク粉末および粒径:
Cr3C2、NbC、SiC、15μm。
金属粉末とセラミツク粉末との均一な混合物
100重量部に3重量部のパラフインを添加し、
スラリー調製(分散媒:メチルアルコール、固
形分濃度:60重量%)、スプレードライヤによ
る造粒(造粒粉粒径:1〜3.5μm)、脱ろう
(Ar雰囲気中、600℃)、焼成(Ar雰囲気中、
1350〜1450℃)、および解砕処理を経て、50〜
300μmの造粒粉を得る。
〔〕 溶接肉盛の施行
上記造粒粉を溶接材とし、プラズマ粉体肉盛
溶接機により、耐熱鋼板(C:0.08%、Cr:27
%、Co:40%、Ni:17%、残部Fe)の表面に
ビードを5層盛りして層厚15mmの肉盛層を形成
する。
〔〕 肉盛層の品質
上記肉盛溶接施工後、試験片を調製し、各種
試験を行つて第1表に示す結果を得た。表中、
試番(No.)1〜8%発明例、No.101〜110は比較
例である。比較例No.101〜110のうち、No.101〜
103は炭化物系セラミツク粒子の配合量が不足
しまたは過剰である例、No.104〜108はマトリツ
クス金属の成分組成が本発明の規定からはずれ
ている例である。また、No.109は溶射法による
肉盛層の例であり、No.110は肉盛層を有しない
母材についての試験結果を示している。また、
表中、「耐酸化性」欄は、1200℃における酸化
損耗量(mm/年)で評価し、その値が0.30mm/
年以下を、「〇」(良好)とし、0.3mm/年をこ
えるものを「×」(不良)とした。また、「溶接
施行性」は、3層以上のビード積層(層厚10mm
以上)が可能なものを「〇」(良好)とし、3
層盛りが不可能(層間接合不良)なものを
「×」(不良)と判定した。
第1表に示したように、本発明の溶接材を用い
て形成される複合肉盛層(No.1〜8)は、溶射法
により形成される複合肉盛層(No.109)に比し、
基材との密着強度が高く、また高温域での硬さ、
強度、耐酸化性等にすぐれている。しかも、溶接
施工性が良好で、多層盛りが容易であり、部材の
用途や使用条件に応じた厚薄任意の厚さを有する
複合肉盛層を形成することができる。他方、セラ
ミツク粒子配合割合が不足する場合(No.101)は
高温強度や圧縮強度が低く、逆にその配合割合が
過剰の場合(No.102、103)は、溶接施工性が劣
る。また、マトリツクス金属の成分組成が本発明
の規定からはずれると、耐酸化性の不足をきたし
たり、またセラミツク粒子の配合割合が十分であ
つても、高温硬度がそれほど高くないため、耐摩
耗性や高温圧縮強度等の材質低下をさけることが
できず、いずれの場合も、本発明例の複合肉盛層
の材料特性に及ばない。
[Industrial Application Field] The present invention relates to a welding material for forming a build-up layer having a composite structure consisting of a metal matrix and carbide ceramic particles as a dispersed phase by a plasma powder weld build-up method. [Prior Art] Forming a coating layer having a composite structure consisting of a metal matrix and ceramic particles as a dispersed phase on the surface of rolls such as rolling rolls, heat treatment furnace rolls, conveyor rolls, and other structural members. teeth,
This is an extremely effective method for improving the heat resistance, wear resistance, etc. of these members. Thermal spraying is exclusively used as a method for forming this coating layer. Industrially available thermal spraying materials include composite powders mainly made of carbide ceramics such as silicon carbide (SiC) and tungsten carbide (WC), and oxide ceramics such as alumina (Al 2 O 3 ) and zirconia (ZrO). is supplied to. [Problems to be solved by the invention] However, the coating layer (sprayed layer) formed by the thermal spraying method has poor adhesion strength and is easily peeled off by mechanical impact, so there are problems with stability and durability in actual use. be. In addition, the coating layer lacks homogeneity and density of the composite structure, so the metal-ceramic composite effect, especially the dispersion strengthening effect of ceramic particles, is insufficient, resulting in poor strength, wear resistance, and heat resistance in high temperature ranges. It is not possible to expect such an improvement effect on the various characteristics of . The present invention provides a composite welding material for plasma powder weld build-up in order to solve the above problems. [Means and effects for solving the problems] The present invention provides a welding material for plasma powder welding that consists of a metal component as a matrix and carbide-based ceramic particles as a dispersed phase. The blending ratio of ceramic particles is 20 to 80% by weight, and the metal content of the matrix is C: 0.08% or less, Si: 0.5 to 3%, Mn: 2% or less, Ni: 2 to 10.
%, Cr: 15-30%, Co: 20-40%, and the remainder substantially consists of Fe. In the composite welding material of the present invention, the ceramic particles serving as the dispersed phase are carbide ceramic particles.
Carbide ceramic particles are hard and have high strength.
It also has good wettability with metal matrices, making it an excellent dispersion-strengthening component. Preferred examples thereof include chromium carbide ( Cr3C2 , Cr7C2 , etc.), tungsten carbide (WC), titanium carbide ( TiC), niobium carbide (NbC), silicon carbide (SiC), and the like. The reason for setting the blending ratio of the carbide ceramic particles as the dispersed phase (weight ratio in the mixture with the metal component as the matrix) to 20% or more is because if it is less than 20%, the dispersion strengthening effect will not be sufficient, and for example, the hardness This is because shortages etc. will occur. As the blending ratio increases, hardness, wear resistance, heat resistance, high-temperature strength, etc. improve due to dispersion strengthening effect, but when it exceeds 80%, adhesion between bead laminations becomes poor in multi-layer weld bead buildup. 80% is set as the upper limit because this causes problems such as poor welding workability and poor toughness of the built-up layer formed. Although the particle size of the carbide ceramic particles is not particularly limited, it is preferably about 50 μm or less in order to ensure sufficient dispersion-strengthening effect. It has a high effect of inhibiting dislocation movement within the layer, and it is possible to secure a higher level of strength in low temperature and high temperature ranges. On the other hand, the metal component that forms the matrix is Ni-Cr.
-Co-Fe alloy, and the reasons for limiting its composition are as follows. C: 0.08% or less C is an impurity element. In order to keep the matrix metal at a high melting point, the upper limit is set at 0.08%. Si: 0.5 to 3% or less Si is at least 0.5% from the viewpoint of ensuring the fluidity of the molten metal formed during weld overlay and deoxidizing effect.
% is required. However, if it exceeds 3%, the toughness of the matrix decreases, so the upper limit is set at 3%. Mn: 2% or less Like Si, Mn has a deoxidizing effect on molten metal, and also prevents the generation of harmful FeS by fixing S, an impurity in molten metal, as MnS. However, if the content increases, the amount of MnS remaining in the molten metal increases and the cleanliness of the matrix metal is impaired, so the upper limit is set at 2%. Cr: 15-30% Cr increases the oxidation resistance of the matrix metal.
For this effect to be sufficient, at least 15
% is required. The effect increases as the content increases, but if it exceeds 30%, the toughness decreases, so 30% is the upper limit. Ni: 2-10% Ni increases the toughness of the metal matrix and
Enhances oxidation resistance through interaction with Cr. It also has the effect of improving wettability with carbide ceramic particles, which are the dispersed phase, and increasing the density and homogeneity of the composite structure. If the content is less than 2%,
If the above effects are insufficient, and if the amount exceeds 10%, the melting point of the matrix will inevitably decrease. 2-10%
shall be. Co: 20-40% Co is required to be at least 20% in order to ensure high temperature strength of the matrix and wettability to carbide ceramic particles. The effect becomes stronger as the content increases, but when it exceeds 40%, the effect is almost saturated, so it is not economical to increase the content any further. Therefore, the upper limit is 40%. The particle size of the metal powder forming the matrix is not particularly limited, but in order to improve the homogeneity of the mixture with the ceramic particles, the particle size is preferably about 40 to 100 μm. The powder mixture may be used as a weld overlay material as it is, but since there is a large difference in specific gravity between metal particles and ceramic particles, it is necessary to use Ar gas as a carrier gas through powder feed piping during weld overlay construction. Separation and segregation of metal particles and ceramic particles may occur during the process of feeding the metal particles to the welding torch, or when dispersing them from the welding torch to the molten pool on the surface of the welding base material directly below.
In particular, this tendency becomes more pronounced as the powder particle size becomes finer. As a measure to prevent separation and segregation due to the difference in specific gravity of the powder mixture, it is extremely effective to use the powder mixture as granulated powder with a suitable particle size, preferably about 50 to 300 μm. The granulated powder is produced by a known granulation method, for example, by adding an appropriate sizing agent, such as wax such as paraffin, to a powder mixture in an appropriate amount (for example, 2 to 3 parts by weight per 100 parts by weight of the powder mixture). This is suspended in a dispersion medium such as alcohol or water to form a slurry, and then subjected to a wet spray dryer (spray dryer) to form a granulated powder.
After dewaxing, it is fired and then crushed into 300 to 60 mesh pieces using a crusher. The composite build-up layer formed on the surface of a member such as a roll by the plasma powder weld build-up method using the welding material of the present invention has a strong fusion bond relationship with the member surface, and can be used at high temperatures of 1200°C or higher. Also, its composite structure is homogeneous and dense, and has excellent heat resistance and oxidation resistance, as well as high hardness at high temperatures, and therefore high wear resistance even in high temperature ranges. Shows resistance. In addition, since the welding workability is good, it is possible to form a built-up layer having an arbitrary thickness depending on the application. [Example] [] Preparation of weld overlay material (1) Matrix metal powder particle size: 50 μm (2) Carbide ceramic powder and particle size:
Cr3C2 , NbC, SiC , 15μm. Homogeneous mixture of metal powder and ceramic powder
Add 3 parts by weight of paraffin to 100 parts by weight,
Slurry preparation (dispersion medium: methyl alcohol, solid content concentration: 60% by weight), granulation using a spray dryer (granulated powder particle size: 1 to 3.5 μm), dewaxing (Ar atmosphere, 600℃), calcination (Ar In the atmosphere,
1350~1450℃), and after crushing treatment, 50~
Obtain 300μm granulated powder. [] Execution of weld build-up Using the above granulated powder as welding material, heat-resistant steel plate (C: 0.08%, Cr: 27
%, Co: 40%, Ni: 17%, balance Fe), five layers of beads are piled up on the surface to form a built-up layer with a layer thickness of 15 mm. [] Quality of Overlay Layer After the above-mentioned overlay welding, test pieces were prepared and various tests were conducted to obtain the results shown in Table 1. In the table,
Trial numbers (No.) 1 to 8% are invention examples, and Nos. 101 to 110 are comparative examples. Among comparative examples No. 101 to 110, No. 101 to
No. 103 is an example in which the blended amount of carbide ceramic particles is insufficient or excessive, and Nos. 104 to 108 are examples in which the component composition of the matrix metal deviates from the specifications of the present invention. Further, No. 109 is an example of a build-up layer formed by thermal spraying, and No. 110 shows test results for a base material without a build-up layer. Also,
In the table, the "oxidation resistance" column is evaluated based on the amount of oxidation loss (mm/year) at 1200℃, and the value is 0.30mm/year.
If it is less than 0.3 mm/year, it is marked as "〇" (good), and if it exceeds 0.3 mm/year, it is marked as "x" (poor). In addition, "welding performance" is based on three or more layers of bead lamination (layer thickness 10 mm).
If the above) is possible, mark it as “〇” (good), and mark it as “3”.
Those in which layering was impossible (poor interlayer bonding) were determined to be "x" (defective). As shown in Table 1, the composite build-up layers (No. 1 to 8) formed using the welding material of the present invention are compared to the composite build-up layer (No. 109) formed by thermal spraying. death,
High adhesion strength to the base material, hardness in high temperature range,
It has excellent strength and oxidation resistance. Moreover, it has good weldability, is easy to build up in multiple layers, and can form a composite built-up layer having an arbitrary thickness depending on the application and usage conditions of the member. On the other hand, when the blending ratio of ceramic particles is insufficient (No. 101), the high temperature strength and compressive strength are low, and conversely, when the blending ratio is excessive (Nos. 102 and 103), weldability is poor. Furthermore, if the component composition of the matrix metal deviates from the specifications of the present invention, oxidation resistance may be insufficient, and even if the blending ratio of ceramic particles is sufficient, high temperature hardness is not so high, resulting in poor wear resistance. Decrease in material properties such as high-temperature compressive strength cannot be avoided, and in either case, the material properties are inferior to those of the composite overlay layer of the example of the present invention.
本発明の溶接材を用いてプラズマ粉体溶接肉盛
法により形成される複合肉盛層は、基材表面との
密着強度が高く、高温域での強度、耐熱性、耐摩
耗性等にすぐれている。また、溶接施工性が良好
であり、多層盛りによる厚い層厚の肉盛層を形成
することも容易である。従つて、ロール類、その
他の高温域における耐摩耗性、強度、耐熱性等を
必要とする各種部材の耐久性の向上安定化に大き
く貢献する。
The composite overlay layer formed by the plasma powder welding overlay method using the welding material of the present invention has high adhesion strength to the base material surface, and has excellent strength in high temperature ranges, heat resistance, wear resistance, etc. ing. In addition, welding workability is good, and it is easy to form a thick build-up layer by multi-layer build-up. Therefore, it greatly contributes to improving and stabilizing the durability of rolls and other various members that require wear resistance, strength, heat resistance, etc. in high temperature ranges.
Claims (1)
粒子とからなる複合組織を有する溶接肉盛層を形
成するための、マトリツクスとなる金属分と分散
相となる炭化物系セラミツク粒子との均一な粉末
混合物であるプラズマ粉体溶接肉盛用複合溶接材
において、 炭化物系セラミツク粒子の配合割合が20〜80重
量%であり、 金属分は、C:0.08%以下、Si:0.5〜3%、
Mn:2%以下、Ni:2〜10%、Cr:15〜30%、
Co:20〜40%、残部実質的にFeからなる成分組
成を有するものであることを特徴とするプラズマ
粉体溶接肉盛用複合溶接材。[Scope of Claims] 1. Uniformity of the metal component serving as the matrix and the carbide ceramic particles serving as the dispersed phase in order to form a weld build-up layer having a composite structure consisting of a metal matrix and ceramic particles serving as the dispersed phase. In the composite welding material for plasma powder welding, which is a powder mixture, the blending ratio of carbide ceramic particles is 20 to 80% by weight, and the metal content is C: 0.08% or less, Si: 0.5 to 3%,
Mn: 2% or less, Ni: 2-10%, Cr: 15-30%,
A composite welding material for plasma powder welding, characterized in that it has a composition consisting of Co: 20 to 40% and the remainder substantially Fe.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP16608987A JPH0230800B2 (en) | 1987-07-02 | 1987-07-02 | PURAZUMAFUNTAIYOSETSUNIKUMORYOFUKUGOYOSETSUZAI |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP16608987A JPH0230800B2 (en) | 1987-07-02 | 1987-07-02 | PURAZUMAFUNTAIYOSETSUNIKUMORYOFUKUGOYOSETSUZAI |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS6411093A JPS6411093A (en) | 1989-01-13 |
| JPH0230800B2 true JPH0230800B2 (en) | 1990-07-09 |
Family
ID=15824787
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP16608987A Expired - Lifetime JPH0230800B2 (en) | 1987-07-02 | 1987-07-02 | PURAZUMAFUNTAIYOSETSUNIKUMORYOFUKUGOYOSETSUZAI |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPH0230800B2 (en) |
Families Citing this family (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE102006045481B3 (en) * | 2006-09-22 | 2008-03-06 | H.C. Starck Gmbh | metal powder |
| JP4412563B2 (en) * | 2008-07-02 | 2010-02-10 | 住友金属工業株式会社 | High temperature material conveying member |
| JP4517008B1 (en) | 2009-12-16 | 2010-08-04 | 住友金属工業株式会社 | High temperature material conveying member |
-
1987
- 1987-07-02 JP JP16608987A patent/JPH0230800B2/en not_active Expired - Lifetime
Also Published As
| Publication number | Publication date |
|---|---|
| JPS6411093A (en) | 1989-01-13 |
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