JP3283003B2 - Composite centrifugal casting method - Google Patents
Composite centrifugal casting methodInfo
- Publication number
- JP3283003B2 JP3283003B2 JP28606398A JP28606398A JP3283003B2 JP 3283003 B2 JP3283003 B2 JP 3283003B2 JP 28606398 A JP28606398 A JP 28606398A JP 28606398 A JP28606398 A JP 28606398A JP 3283003 B2 JP3283003 B2 JP 3283003B2
- Authority
- JP
- Japan
- Prior art keywords
- metal
- powder
- layer
- melting point
- mold
- 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
- 238000000034 method Methods 0.000 title claims description 18
- 239000002131 composite material Substances 0.000 title claims description 14
- 238000009750 centrifugal casting Methods 0.000 title claims description 12
- 229910052751 metal Inorganic materials 0.000 claims description 76
- 239000002184 metal Substances 0.000 claims description 76
- 239000000843 powder Substances 0.000 claims description 53
- 230000008018 melting Effects 0.000 claims description 35
- 238000002844 melting Methods 0.000 claims description 35
- 238000005245 sintering Methods 0.000 claims description 16
- 230000002093 peripheral effect Effects 0.000 claims description 13
- 239000007791 liquid phase Substances 0.000 claims description 11
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 claims description 10
- 229910045601 alloy Inorganic materials 0.000 claims description 9
- 239000000956 alloy Substances 0.000 claims description 9
- 229910017888 Cu—P Inorganic materials 0.000 claims description 7
- 239000011812 mixed powder Substances 0.000 claims description 7
- 229910052742 iron Inorganic materials 0.000 claims description 6
- 238000005507 spraying Methods 0.000 claims description 6
- 230000000704 physical effect Effects 0.000 claims description 5
- 239000011230 binding agent Substances 0.000 claims description 4
- 230000005484 gravity Effects 0.000 claims description 4
- 238000002156 mixing Methods 0.000 claims description 4
- 239000011248 coating agent Substances 0.000 claims description 3
- 238000000576 coating method Methods 0.000 claims description 3
- 239000007788 liquid Substances 0.000 claims description 3
- 239000012071 phase Substances 0.000 claims description 3
- 239000010935 stainless steel Substances 0.000 claims description 2
- 229910001220 stainless steel Inorganic materials 0.000 claims description 2
- 239000010410 layer Substances 0.000 description 34
- 238000005260 corrosion Methods 0.000 description 31
- 230000007797 corrosion Effects 0.000 description 30
- PXHVJJICTQNCMI-UHFFFAOYSA-N nickel Substances [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 13
- 239000000463 material Substances 0.000 description 11
- 229910001018 Cast iron Inorganic materials 0.000 description 9
- 239000010949 copper Substances 0.000 description 9
- 238000005266 casting Methods 0.000 description 8
- 229910052802 copper Inorganic materials 0.000 description 7
- 230000000694 effects Effects 0.000 description 6
- 229910052759 nickel Inorganic materials 0.000 description 5
- 229910001141 Ductile iron Inorganic materials 0.000 description 4
- 239000011651 chromium Substances 0.000 description 4
- 230000005496 eutectics Effects 0.000 description 4
- 238000007654 immersion Methods 0.000 description 4
- 150000003839 salts Chemical class 0.000 description 4
- 238000007711 solidification Methods 0.000 description 4
- 230000008023 solidification Effects 0.000 description 4
- 230000004580 weight loss Effects 0.000 description 4
- 238000003466 welding Methods 0.000 description 4
- 239000010953 base metal Substances 0.000 description 3
- 238000009792 diffusion process Methods 0.000 description 3
- 239000000203 mixture Substances 0.000 description 3
- 239000002245 particle Substances 0.000 description 3
- 238000010587 phase diagram Methods 0.000 description 3
- 229920002689 polyvinyl acetate Polymers 0.000 description 3
- 239000011118 polyvinyl acetate Substances 0.000 description 3
- 239000011241 protective layer Substances 0.000 description 3
- 229910052710 silicon Inorganic materials 0.000 description 3
- 239000007921 spray Substances 0.000 description 3
- 239000000126 substance Substances 0.000 description 3
- FAPWRFPIFSIZLT-UHFFFAOYSA-M Sodium chloride Chemical compound [Na+].[Cl-] FAPWRFPIFSIZLT-UHFFFAOYSA-M 0.000 description 2
- 229910052796 boron Inorganic materials 0.000 description 2
- 229910052804 chromium Inorganic materials 0.000 description 2
- 239000011247 coating layer Substances 0.000 description 2
- 230000000052 comparative effect Effects 0.000 description 2
- 230000007547 defect Effects 0.000 description 2
- 238000004453 electron probe microanalysis Methods 0.000 description 2
- 239000000945 filler Substances 0.000 description 2
- 230000001737 promoting effect Effects 0.000 description 2
- 238000004445 quantitative analysis Methods 0.000 description 2
- 230000003014 reinforcing effect Effects 0.000 description 2
- 239000011780 sodium chloride Substances 0.000 description 2
- 239000007787 solid Substances 0.000 description 2
- 238000005728 strengthening Methods 0.000 description 2
- 239000012085 test solution Substances 0.000 description 2
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 2
- ZOXJGFHDIHLPTG-UHFFFAOYSA-N Boron Chemical compound [B] ZOXJGFHDIHLPTG-UHFFFAOYSA-N 0.000 description 1
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 description 1
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 1
- 229910000990 Ni alloy Inorganic materials 0.000 description 1
- 229910018100 Ni-Sn Inorganic materials 0.000 description 1
- 229910018532 Ni—Sn Inorganic materials 0.000 description 1
- 229910018619 Si-Fe Inorganic materials 0.000 description 1
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 description 1
- 229910008289 Si—Fe Inorganic materials 0.000 description 1
- 229910000831 Steel Inorganic materials 0.000 description 1
- 238000005299 abrasion Methods 0.000 description 1
- 239000000654 additive Substances 0.000 description 1
- 230000000996 additive effect Effects 0.000 description 1
- 229910001566 austenite Inorganic materials 0.000 description 1
- 238000005219 brazing Methods 0.000 description 1
- 238000005256 carbonitriding Methods 0.000 description 1
- 238000013329 compounding Methods 0.000 description 1
- 239000012141 concentrate Substances 0.000 description 1
- 238000012790 confirmation Methods 0.000 description 1
- 239000013078 crystal Substances 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000004512 die casting Methods 0.000 description 1
- 230000001747 exhibiting effect Effects 0.000 description 1
- 230000002349 favourable effect Effects 0.000 description 1
- 230000004927 fusion Effects 0.000 description 1
- 238000005470 impregnation Methods 0.000 description 1
- 238000002347 injection Methods 0.000 description 1
- 239000007924 injection Substances 0.000 description 1
- 238000011081 inoculation Methods 0.000 description 1
- 238000009413 insulation Methods 0.000 description 1
- 230000010354 integration Effects 0.000 description 1
- 239000000155 melt Substances 0.000 description 1
- 238000005058 metal casting Methods 0.000 description 1
- 150000002739 metals Chemical class 0.000 description 1
- 230000010287 polarization Effects 0.000 description 1
- 239000012255 powdered metal Substances 0.000 description 1
- 238000010791 quenching Methods 0.000 description 1
- 230000000171 quenching effect Effects 0.000 description 1
- 230000002787 reinforcement Effects 0.000 description 1
- 230000000717 retained effect Effects 0.000 description 1
- 239000010703 silicon Substances 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
- 239000002344 surface layer Substances 0.000 description 1
- 238000004381 surface treatment Methods 0.000 description 1
- 238000007751 thermal spraying Methods 0.000 description 1
- 239000011800 void material Substances 0.000 description 1
Landscapes
- Other Surface Treatments For Metallic Materials (AREA)
- Coating By Spraying Or Casting (AREA)
Description
【0001】[0001]
【発明の属する技術分野】金属の鋳造法において、特定
の性質を発揮するような金属又は合金を全面又は部分的
に付加して機能性を高める、金属の鋳造法に関するもの
である。BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a metal casting method in which a metal or an alloy exhibiting a specific property is added to the whole or part of the metal to enhance the functionality.
【0002】[0002]
【従来の技術】鋳造品の一部特定の箇所に、耐食性を付
与する方法として鋳造品自体に溶射や、部分焼入れ浸炭
窒化など、鋳造後に表面処理を加える方法もあるが、作
業工数が確実に増加する問題が有る。そのため、鋳造前
の金型の空隙表面の所望の部位に特定の物質を含む硬化
材層を設け、溶融金属を注湯し、その熱で該硬化材層を
溶着させ、凝固後に所望の部署に硬化層を形成しようと
する、鋳造方法が種々提案されてきた。2. Description of the Related Art As a method of imparting corrosion resistance to a specific part of a cast product, there is a method of applying a surface treatment after casting, such as thermal spraying or partial quenching and carbonitriding, to the cast product itself. There is an increasing problem. Therefore, a hardening material layer containing a specific substance is provided at a desired portion of the cavity surface of the mold before casting, molten metal is poured, the hardening material layer is welded by the heat, and after solidification, it is transferred to a desired department. Various casting methods have been proposed to form a hardened layer.
【0003】例えば特公平5−20184号公報による
従来技術では、Ni含有量80重量%またはそれ以上の
Ni合金から成る充填剤を、粉末のままで金型内へ鋳込
直前に装入し、注湯して外周面に防食性層を形成するこ
とを要旨とし、合金元素としてホウ素、硅素、クロム、
銅より選び出し、融点1300℃以下の充填剤とした。
あるいは溶融鋳鉄の溶融点1150℃以下となるように
選択する実施態様をも示している。In the prior art disclosed in Japanese Patent Publication No. 5-20184, for example, a filler made of a Ni alloy having a Ni content of 80% by weight or more is charged as a powder into a mold immediately before casting. The main point is to form a corrosion-resistant layer on the outer peripheral surface by pouring, and boron, silicon, chromium,
A filler having a melting point of 1300 ° C. or less was selected from copper.
Alternatively, an embodiment in which the melting point of the molten cast iron is selected to be 1150 ° C. or lower is also shown.
【0004】特開平5−77019号公報に係る従来技
術ではほぼ同じ目的で金型内へ凝固促進用の粉末層をN
i、Cr、又はその合金とCa、Siとの混合粉末によ
って形成することを呈示した。この粉末層による注湯時
の断熱作用によって、欠陥の防止と金型の保護と鋳込ま
れた溶湯の急速凝固によって、ピンホールの発生を防止
すると謳っている。すなわちこの場合のCa、Siは一
種の脱酸接種効果と、混合粉末層の溶融点の低下作用を
意としたものである。In the prior art disclosed in Japanese Patent Application Laid-Open No. 5-77019, a powder layer for accelerating solidification is placed in a mold for almost the same purpose.
It has been shown that it is formed by a mixed powder of i, Cr, or an alloy thereof and Ca, Si. It is stated that the heat insulation effect at the time of pouring by the powder layer prevents the occurrence of pinholes by preventing defects, protecting the mold, and rapidly solidifying the cast molten metal. That is, Ca and Si in this case are intended to have a kind of deoxidizing inoculation effect and an effect of lowering the melting point of the mixed powder layer.
【0005】[0005]
【発明が解決しようとする課題】金型遠心力鋳造におい
て、製品の外周面に耐食性に優れる層を形成するため、
金型内へ耐食性金属の粉末を塗布又は散布すること自体
は既に公知であり、先に引用した二件の従来技術もその
範畴に属する。しかし、その主旨はあくまで耐食性を付
与する金属の溶融点を低温側へ移すように、成分コント
ロールする点に焦点が絞られ、被覆する外周面保護層自
体の強化レベルについては、なお万全とは云えないので
はないか。SUMMARY OF THE INVENTION In centrifugal die casting, a layer having excellent corrosion resistance is formed on the outer peripheral surface of a product.
The application or spraying of the corrosion resistant metal powder into the mold is already known, and the two prior arts cited above also belong to that category. However, the main point is to focus on controlling the components so that the melting point of the metal imparting corrosion resistance is shifted to the lower temperature side, and the reinforcement level of the outer peripheral surface protective layer itself to be coated is still perfect. Isn't it?
【0006】粉末層の溶融点を低温化することを第一義
的に求めれば、一種の金属鑞の態様を踏襲することに外
ならず、もし溶融点が低すぎれば、注湯された溶融金属
内へ拡散して、表面の成分濃度が大巾に失われることを
意味し、又、溶融点が高すぎれば母剤金属との一体溶着
に疑問が残る。[0006] If it is primarily desired to lower the melting point of the powder layer, it must follow the form of a kind of metal brazing. It means that it diffuses into the metal and the concentration of components on the surface is greatly lost, and if the melting point is too high, there remains a question about the integral welding with the base metal.
【0007】先に本願発明の出願人は特公平5−201
87号公報において、主として耐摩耗鋼の局部的強化を
目指した、まったく新しい液相焼結による複合一体化を
開示した。即ち、金型空隙部に溶融金属を注入して、凝
固後所望の形状をなす鋳造法で、Aに特定の物性を付与
する特定の金属又は合金、Bに前記Aを構成する金属よ
り明確に低融点を有する金属の粉末を使用し、Cは適当
量の有機系結合材とし、3者を練りあわせて所望の位置
に取り付け、該空隙部にBを構成する金属よりは融解点
が高い溶融金属を注入する鋳造法。この様な構成による
ことによりまず注入した溶融金属の保有熱により低融点
のBの金属を融解しA、B及び注入金属の3者を液相焼
結により一体化し、続いて注入した金属と層表面を通じ
て拡散溶着する。[0007] The applicant of the present invention previously filed Japanese Patent Publication No. Hei 5-201.
No. 87 discloses a completely new composite integration by liquid phase sintering mainly aimed at locally strengthening wear-resistant steel. That is, by injecting a molten metal into the mold cavity and casting it into a desired shape after solidification, a specific metal or alloy imparting specific physical properties to A, and B is more clearly defined than the metal constituting A. Using a metal powder having a low melting point, C is an appropriate amount of an organic binder, and the three are kneaded together and attached at a desired position, and the melting point of the void is higher than the metal constituting B. Casting method to inject metal. With this configuration, first, the low melting point metal B is melted by the retained heat of the injected molten metal, and the three components A, B and the injected metal are integrated by liquid phase sintering, and then the injected metal and the layer are integrated. Diffusion welds through the surface.
【0008】耐摩耗材は強固であると共に時間の経過に
伴って外面から消耗していくからある程度の強化層の厚
さを必要とし又具体的にはAとしてFe−Cr粉末、B
としてNi−Cr−Si−Fe粉末、Cとしてポリビニ
ルアセテート等で形成して、母材となる鋳鉄溶湯を注湯
して、耐摩耗鋳鉄部品のうち、特に摩耗面を局部的に強
化した実績を示した。[0008] Since the wear-resistant material is strong and is consumed from the outer surface with the passage of time, a certain thickness of the reinforcing layer is required.
Of Ni-Cr-Si-Fe powder as C and polyvinyl acetate as C, and pouring molten cast iron as a base material, especially in abrasion-resistant cast iron parts, the results of locally strengthening the wear surface Indicated.
【0009】これに反し耐食性材に関しては外表面の強
化層の厚み自体が主題ではなく、母材と一体的に溶着し
た保護層が、如何に緻密で堅牢な複合層を形成出来るか
の一点に尽きる。たとえば母材金属の表面上へ溶着した
別種の金属皮膜の結晶粒度にバラツキがあったり、組織
的に異なる部分や粗密の差があるとき、粒界と粒内、格
子欠陥と正常な格子構造など、腐食電池を形成して電位
差を生じる場合には、保護層の厚さに拘らず分極、点
食、孔食、粒界腐食など金属独自の腐食の進行が甚だし
く、局部的な腐食が集中して母材の一部が早々に機能を
喪失することは周知の事実である。本発明は以上の耐食
性部材、特に遠心力鋳造法による鋳鉄管の外周面を、最
も効果的に耐食性を向上させる方法を、目的とする。On the other hand, regarding the corrosion-resistant material, the thickness itself of the reinforcing layer on the outer surface is not the main subject, and one point is how the protective layer integrally welded with the base material can form a dense and robust composite layer. run out. For example, when there is variation in the crystal grain size of different kinds of metal films deposited on the surface of the base metal, or when there are structurally different parts or differences in density, grain boundaries and intragranules, lattice defects and normal lattice structure, etc. When a corrosion battery is formed and a potential difference is generated, regardless of the thickness of the protective layer, the unique corrosion of the metal such as polarization, pitting, pitting, and intergranular corrosion progresses extremely, and local corrosion concentrates. It is a well-known fact that some of the base materials lose their functions quickly. An object of the present invention is to provide a method for most effectively improving the corrosion resistance of the above-described corrosion-resistant member, particularly the outer peripheral surface of a cast iron pipe formed by centrifugal casting.
【0010】[0010]
【課題を解決するための手段】本発明にかかる複合遠心
鋳造法は特定の物性を向上するために、金型内へ特定の
金属類などを添加し、高速回転しつつ溶融金属を注湯し
て、外周面を複合強化する複合遠心鋳造法において、N
iまたはNi系合金、Ni及び/又はCrを含むステン
レス鋼もしくはCrを少くとも10重量%以上含む鉄系
合金の中から選ばれた1又は複数の金属粉末Aと、Pを
5〜12重量%を含むことにより該金属粉末Aより明確
に低温の溶融点に調整したCu−Pよりなる金属粉末B
とを混合割合がA/B=40/60〜90/10の範囲
内で均一に混合した粉末を作成し、金型を高速に回転し
つつ、金属粉末Bの溶融点よりは高い溶融点よりなる溶
融金属を注湯する直前、又は同時に前記粉末を金型内に
散布することにより、溶融金属より比重の高いA、Bが
遠心力の差によって金型内面に分離添着した粉末層を形
成し、溶融金属から受熱して前記3溶融点の相互関係に
よって発現する液相焼結と遠心作用を受けて、製品の外
周面に強固で緻密な焼結層を一体的に形成することによ
って前記の課題を解決した。According to the composite centrifugal casting method of the present invention, in order to improve specific physical properties, specific metals and the like are added into a mold, and molten metal is poured while rotating at a high speed. In the composite centrifugal casting method in which the outer peripheral surface is
i or a Ni-based alloy, one or more metal powders A selected from stainless steel containing Ni and / or Cr or an iron-based alloy containing at least 10% by weight of Cr , and 5 to 12% by weight of P , A metal powder B of Cu-P adjusted to a melting point at a lower temperature than that of the metal powder A more clearly.
And the mixing ratio is in the range of A / B = 40/60 to 90/10
Create a powder uniformly mixed within, while rotating the mold at high speed, immediately before pouring the molten metal having a melting point higher than the melting point of the metal powder B, or at the same time the powder in the mold By spraying, liquids A and B having a higher specific gravity than the molten metal form a powder layer which is separated and attached to the inner surface of the mold due to a difference in centrifugal force, heat is received from the molten metal, and a liquid developed by the interrelation of the three melting points The above-mentioned problem has been solved by forming a strong and dense sintered layer integrally on the outer peripheral surface of the product by phase sintering and centrifugal action.
【0011】前記の構成において金型内面への混合粉末
の散布に替えて、前記金属粉末A,金属粉末Bと有機系
結合材Cの三者を混合して、金型の内面上に塗布し、高
速に回転しつつ、金属粉末Bの溶融点よりは高い溶融点
よりなる溶融金属を注湯して、前記3溶融点の相互関係
によって発現する液相焼結と遠心作用を受けて、該粉末
層または添着層を製品の外周面に強固で緻密に形成する
焼結層に変換する方法であってもよい。In the above configuration, instead of spraying the mixed powder on the inner surface of the mold, the metal powder A, the metal powder B and the organic binder C are mixed and applied onto the inner surface of the mold. While rotating at a high speed, a molten metal having a melting point higher than the melting point of the metal powder B is poured and subjected to liquid phase sintering and centrifugal action developed by the interrelation of the three melting points. A method of converting the powder layer or the adhering layer into a sintered layer that is firmly and densely formed on the outer peripheral surface of the product may be used.
【0012】高速回転する金型内に目的の溶着金属を注
入する直前、または同時に金属粉末A,Bの混合粉末を
散布すると、この溶湯の熱の為に混合粉末を構成するB
粉末がその溶融点に達して溶けはじめる。この時粉末金
属Aは、配合された材質により溶解する場合と、一部表
面近くのみ溶解する場合と、全く溶解しない場合と三態
様が生じる。これは、粉末金属Aの成分と注入する溶解
金属の湯温とのかね合いで幾通りにも条件が異なるが、
これらは事前に計算し策定することの出来る要素であ
る。最も重要な作用の特徴は、散布または塗布された金
属粉末が比重差に基づく遠心力の差によって溶湯と分離
し、金型の内周面へ移行して添着して形成した環状の粉
末層の全てがそのまま溶湯に溶解拡散して反応層をスト
レートに形成するのではなく、低融点の粉末金属Bがま
ず溶湯の熱を受けて溶解し、粉末金属Aを強固に抱込ん
で、溶解金属と協力して溶着する、いわゆる液相焼結を
起こす点である。したがって後の実施例で示されるよう
に、反応層は物性を支配する粉末金属Aを抱込んで粉末
金属Bと溶解金属母材と結合し、粉末金属A成分はあら
かじめ計画した鋳造方案通り、所定の深度にわたり母材
に拡散接合している。When a mixed powder of the metal powders A and B is sprayed immediately before or simultaneously with injection of a target welding metal into a mold rotating at a high speed, heat is applied to the molten metal to form the mixed powder B.
The powder reaches its melting point and begins to melt. At this time, the powder metal A has three modes: a case where it is dissolved by the compounded material, a case where it is dissolved only near a part of the surface, and a case where it is not dissolved at all. This depends on the balance between the components of the powdered metal A and the temperature of the molten metal to be injected.
These are elements that can be calculated and formulated in advance. The most important feature of the operation is that the dispersed or applied metal powder is separated from the molten metal by the difference in centrifugal force based on the difference in specific gravity, transferred to the inner peripheral surface of the mold, and adhered to the annular powder layer. Rather than dissolving and dispersing all in the molten metal as it is to form a reaction layer straight, the powder metal B having a low melting point is first melted by receiving the heat of the molten metal, and the powder metal A is firmly embraced, and the molten metal A This is the point where so-called liquid phase sintering occurs in which welding is performed in cooperation. Therefore, as will be shown in a later embodiment, the reaction layer embraces the powder metal A, which controls the physical properties, and combines with the powder metal B and the molten metal base material. Diffusion bonding to the base material over a depth of
【0013】したがって金属粉末A,Bの溶融点の差、
および配合する比率が良好な液相焼結を進行させる上で
大事なポイントとなる。図6はCu−Pの二元状態図で
あり、横軸上欄の重量%と縦軸の温度℃との相関から読
み取れるように、Pは約8重量%付近に共晶点があり共
晶温度は約720℃付近にある。Cu−P合金はこの共
晶点で最低の溶融温度を形成し、この前後へ離れると共
に急カーブで高温側へ移行する。したがって実用的にP
がCuにどの範囲まで溶け込むことができるかというこ
とが重要な要件を定めるが、状態図の読み取りと実地テ
ストの結果を衝き合せると、Pを5〜12重量%に限定
し、溶融温度を900℃以下に設定することによって実
用上、最も優れた液相焼結を得るという臨界的意義を確
定することができた。また、単なる耐食性だけでなくア
グレッシーブな摩耗作用にも直面する場合には、脆性を
避けるために比較的低いP側、たとえばP:5〜10重
量%に制限することが望ましい結果に繋がることがあ
る。配合については、溶融点の高いAだけでは溶解金属
の溶融熱による焼結は困難であり、さらにAが40%以
下では耐食性が不十分であるので、A/Bが40/60
より大きいことが焼結進行の下限の配合条件となる。一
方、低溶融点のBだけでは溶解金属の注湯と共にその溶
解熱のために完全に溶融して溶解金属中に拡散してしま
い表面に耐食性の優れた層を形成するという目的が達成
できないし、Bの配合比率が10%より少ないとAの焼
結作用を補完する働きが不十分であって堅牢緻密な液相
焼結層の形成という本来の目的を果たせないので、A/
Bが90/10より小さいことが焼結進行の上限の配合
条件となる。Accordingly, the difference between the melting points of the metal powders A and B,
In addition, the mixing ratio is an important point in promoting favorable liquid phase sintering. FIG. 6 is a binary phase diagram of Cu-P. As can be read from the correlation between the weight% in the upper column of the horizontal axis and the temperature ° C. in the vertical axis, P has a eutectic point at about 8% by weight and has a eutectic point. The temperature is around 720 ° C. The Cu-P alloy forms the lowest melting temperature at this eutectic point, moves away from this eutectic point, and moves to a high temperature side in a sharp curve. Therefore, P
It is important to determine the extent to which P can dissolve in Cu. However, when the phase diagram reading and the results of the field test are performed, P is limited to 5 to 12% by weight, and the melting temperature is set to 900%. The critical significance of obtaining the best liquid phase sintering for practical use could be determined by setting the temperature below ℃. Also, when facing not only mere corrosion resistance but also aggressive wear action, it may lead to a desirable result to limit to a relatively low P side, for example, P: 5 to 10% by weight in order to avoid brittleness. . Regarding the composition, sintering of the molten metal by the heat of fusion is difficult with only A having a high melting point, and further, when A is 40% or less, the corrosion resistance is insufficient, so that A / B is 40/60.
A larger value is the lower limit of the sintering process. On the other hand, B alone having a low melting point alone completely melts and diffuses into the molten metal due to the heat of melting together with the pouring of the molten metal, so that the purpose of forming a layer having excellent corrosion resistance on the surface cannot be achieved. If the compounding ratio of B is less than 10%, the function of complementing the sintering action of A is insufficient and the original purpose of forming a robust and dense liquid phase sintered layer cannot be fulfilled.
B is smaller than 90/10, which is the upper limit of the sintering process.
【0014】C成分に関しては、金型内面に塗布するこ
とによって塗膜を形成する形態の場合にのみ使用し、金
型面との結合を保持し、注湯時には、その流勢に押され
て層が剥離しないで、凝固が表面から始まるまで把持す
る役割を果たす。The component C is used only in the case where the coating film is formed by applying it to the inner surface of the mold, and keeps the bond with the mold surface. It does not peel off, but serves to grip until solidification starts at the surface.
【0015】本発明の対象は後述の実施形態でも明示す
るように、ダクタイル鋳鉄管の外面の耐食性向上を主た
る目的とする。具体的にこの場合の作用を説明すると、
金型内へダクタイル鋳鉄の溶湯(溶融点約1150℃)
を注湯すると、比重の差による遠心力の差によって散布
された混合金属粉末は金型内周面へ移行して層状に分離
添着し、さらに溶湯の保有熱を受けて、まず粉末B(C
u−P、溶融点は約900〜約720℃の範囲に限定)
が溶解すると共に、遠心力によって鋳鉄溶湯が粉末層内
へ押し込まれて含浸をはじめ、粉末金属Bより溶融点の
高い粉末金属A(例えばニッケル、溶融点約1450
℃)を包み込む状態でミクロ的な液相焼結がはじまる。
遠心力によって、この状態で相互に包持しあったまま強
力に金型内面に押し付けられ、急速冷却されて一体的に
堅牢な複合層を形成する。凝固後の組織は例えば鋳鉄溶
湯の熱容量が大きい場合、鋳鉄溶湯からのFe,C等の
浸入が多く、共にオーステナイト化促進成分であるNi
とCuの合計濃度の高い基地がオ−ステナイト化したニ
−レジストに類似する組織が得られ、また鋳鉄溶湯の溶
け込みが少ない場合表層部ではFe、C等の拡散が少な
く、Ni、Cu濃度のさらに高い(具体的にはNi+C
uが20重量%以上)オ−ステナイト組織が得られ耐食
性外層部を形成する。あらかじめ金属粉末A,Bを混合
調整して金型内に塗布する形態の場合も、基本的な液相
焼結の進行の経過は同様であり、凝固後の製品外周面に
はA成分がリッチで堅牢緻密な耐食性の複合層が得られ
る。The main object of the present invention is to improve the corrosion resistance of the outer surface of a ductile cast iron pipe, as will be clearly shown in the embodiments described later. Specifically, the operation in this case will be described.
Melt of ductile cast iron into mold (melting point about 1150 ℃)
When the molten metal is poured, the mixed metal powder sprayed due to the difference in centrifugal force due to the difference in specific gravity moves to the inner peripheral surface of the mold and separates and adheres in a layer form.
u-P, melting point limited to the range of about 900 to about 720 ° C)
Is melted, and the molten cast iron is pushed into the powder layer by centrifugal force to start impregnation, and powder metal A having a melting point higher than powder metal B (for example, nickel, melting point of about 1450).
℃), microscopic liquid phase sintering starts.
In this state, they are strongly pressed against the inner surface of the mold while being held together by the centrifugal force, and are rapidly cooled to form a solid composite layer integrally. In the solidified structure, for example, when the heat capacity of the cast iron melt is large, Fe, C, and the like infiltrate much from the cast iron melt, and Ni, which is an austenitization promoting component, is both used.
In the case where the base having a high total concentration of Cu and Cu is similar to an austenitized niresist, and the molten cast iron is less molten, the diffusion of Fe, C, etc. in the surface layer is small, and the Ni and Cu concentrations are low. Higher (specifically, Ni + C
u is 20% by weight or more) An austenite structure is obtained and a corrosion-resistant outer layer is formed. In the case of the form in which the metal powders A and B are mixed and adjusted in advance and applied in the mold, the progress of the liquid phase sintering is basically the same, and the A component is rich on the outer peripheral surface of the solidified product. To obtain a rigid and dense corrosion-resistant composite layer.
【0016】[0016]
【発明の実施の形態】本発明の耐食性を立証する為に次
の要領で確認テストを行った。図3は遠心鋳造用金型の
一部断面図であり、遠心鋳造金型1を回転支承2で水平
に支持し低速で回転しつつ供給管4より混合粉末を散布
して全長にわたり均等な厚さの粉末層3を形成した。図
3に示す金型を使用して、遠心力鋳鉄管(外径169m
m、長さ1080mm、厚さ7.5mm)を鋳造した。
溶湯は1350℃のダクタイル鋳鉄を使用した。鋳造
後、焼純を施し(980℃×1hr+730℃×1h
r)、その後テストピースを切出した。金属粉末A、B
として粒径150ミクロン以下のものを使用し、混合し
て溶湯の注湯直前、または同時に平均厚さが約500ミ
クロンになるように金型内面へ散布した。表1は実施例
(1)〜(5)におけるそれぞれの金属粉末A、および
Bの成分と配合比を示す。DESCRIPTION OF THE PREFERRED EMBODIMENTS In order to prove the corrosion resistance of the present invention, a confirmation test was performed in the following manner. FIG. 3 is a partial cross-sectional view of a centrifugal casting mold. The centrifugal casting mold 1 is horizontally supported by a rotary bearing 2, and while being rotated at a low speed, the mixed powder is sprayed from a supply pipe 4 to have a uniform thickness over the entire length. Thus, a powder layer 3 was formed. Using the mold shown in FIG. 3, a centrifugal cast iron tube (outer diameter 169 m) was used.
m, length 1080 mm, thickness 7.5 mm).
The molten metal used was 1350 ° C. ductile cast iron. After casting, it is refined (980 ° C x 1hr + 730 ° C x 1h)
r) Then, the test piece was cut out. Metal powder A, B
The particles having a particle diameter of 150 μm or less were used and mixed and sprayed on the inner surface of the mold immediately before pouring of the molten metal or simultaneously with an average thickness of about 500 μm. Table 1 shows the components and mixing ratios of the metal powders A and B in Examples (1) to (5).
【0017】[0017]
【表1】 注)散布の場合はバインダーCは使用しないが、塗布す
る場合は、A+B=100に対して約5の割合で使用
し、ポリビニールアセテート(PVAc)が好適であ
る。なお表2は前記表1の粉末層を形成する為に使用し
た、各種材料の化学組成の一覧表である。粉末の粒径は
200ミクロン以下、好ましくは150ミクロン以下、
さらには50ミクロン以下が最も好ましい。[Table 1] Note) In the case of spraying, the binder C is not used, but in the case of application, it is used in a ratio of about 5 with respect to A + B = 100, and polyvinyl acetate (PVAc) is preferable. Table 2 is a list of chemical compositions of various materials used for forming the powder layer of Table 1. The particle size of the powder is less than 200 microns, preferably less than 150 microns,
Most preferably, it is 50 microns or less.
【0018】[0018]
【表2】 [Table 2]
【0019】鋳造したテストピースは適当な大きさに加
工し、次に述べる試験を行なった。 A、EPMAによる定量分析、表面近傍に含まれる元素
の化学組成比を測定。すなわち、Ni,Cuを主体とし
た添加成分の濃度の変動を知って表面からの耐食性の有
効深度を見極める点に意義がある。 B、耐食性試験 JIS K 5400に記載された方法により、JIS
Z 2371に規定された装置を使用し、35℃の雰
囲気で5.0%NaClaqの塩水噴霧試験と3.0%
NaClaqの塩水浸漬試験を行なった。浸漬試験の場
合、試験溶液は2週間毎に新しく交換し、所定時間毎に
重量測定を行なって減量分を記録すると共に図表化し、
時間経過との関係をプロットした。テストピースは45
mm×45mm×厚さ7.5mmの大きさで、被覆層が
形成された面を暴露し、その他の面はシールを施した。The cast test piece was processed into an appropriate size, and the following test was performed. A, Quantitative analysis by EPMA, measuring the chemical composition ratio of elements contained near the surface. That is, it is significant to know the fluctuation of the concentration of the additive component mainly composed of Ni and Cu to determine the effective depth of corrosion resistance from the surface. B, Corrosion resistance test According to the method described in JIS K 5400, JIS
Using a device specified in Z2371 and a salt spray test of 5.0% NaClaq in an atmosphere of 35 ° C. and 3.0%
A salt water immersion test of NaClaq was performed. In the case of the immersion test, the test solution is newly changed every two weeks, and the weight is measured every predetermined time to record the weight loss and charted.
The relationship with time was plotted. The test piece is 45
The surface having the coating layer formed thereon was exposed in a size of mm × 45 mm × thickness 7.5 mm, and the other surfaces were sealed.
【0020】試験の結果について図表とともに簡単な説
明を加えると、図4、図5は鋳造品の表面からの距離
(μm)を横軸にとり、縦軸にEPMA(X線マイクロ
アラナイザー)によって得られたFe、Ni、Cu各成
分の定量分析値をプロットし相互の関係を示したもので
ある。両図ではそれぞれNiおよびCuが表面から50
0〜600μmの深さまで認められ、Niと同様に鉄の
オーステナイト化促進成分であるCuが共存することに
よって高耐食性の緻密な複合相を形成していることを示
唆している。4 and 5, the horizontal axis represents the distance (μm) from the surface of the casting, and the vertical axis represents the results obtained by EPMA (X-ray micro-analyzer). The quantitative analysis values of the obtained Fe, Ni and Cu components are plotted to show the mutual relationship. In both figures, Ni and Cu are 50
It was observed to a depth of 0 to 600 μm, suggesting that a dense composite phase with high corrosion resistance was formed by the coexistence of Cu, which is an austenitizing component of iron, like Ni.
【0021】表3は前記各試料を塩水(5.0%NaC
laq)噴霧試験によって、その腐食減量(mg/cm
2 )と浸漬期間(day)との関係を示したものであ
り、この表に基づいて時間の経過と腐食の進行をプロッ
トしたものが図1である。また、表4は3.0%NaC
laqの塩水試験液内へテストピースを浸漬した場合の
減量と時間の関係を示し、図2はこのデータを図に表現
し直したものである。Table 3 shows that each of the samples was treated with saline (5.0% NaC).
laq) By spray test, its corrosion weight loss (mg / cm
FIG. 1 shows the relationship between 2) and the immersion period (day), and FIG. 1 plots the passage of time and the progress of corrosion based on this table. Table 4 shows that 3.0% NaC
The relationship between weight loss and time when a test piece is immersed in a saline test solution of laq is shown, and FIG. 2 is a representation of this data in the figure.
【0022】[0022]
【表3】 [Table 3]
【表4】 [Table 4]
【0023】この表、図からうかがえることは、従来技
術として比較例のダクタイル鋳鉄(FCD)に対し、時
間の経過と共に何れのテストピースについても腐食減量
の差が比例的に広がり、試験条件が苛酷な噴霧継続の場
合には、特にNi/Cu−Pの実施例(1)は約8倍以
上、Ni−Sn/Cu−Pの実施例(4)でも6倍以上
の耐食性が認められ、最も経済的なSUS304Lの粉
末を適用した実施例(5)ですら4倍を超える耐食性を
記録している。この差は期間の経過と共にほぼ比例的に
拡大し、実地の使用に当っては格段の耐用期間の差とし
て顕われることは、この図からも容易に推定できること
である。It can be seen from this table and figure that the difference in corrosion weight loss spreads proportionally over time for all test pieces with respect to the ductile cast iron (FCD) of the comparative example as the prior art, and the test conditions are severe. In the case of continuous spraying, the corrosion resistance of the Ni / Cu-P example (1) was about 8 times or more, and the Ni-Sn / Cu-P example (4) was 6 times or more. Even Example (5), which applied the economical SUS304L powder, recorded more than 4 times the corrosion resistance. It can be easily estimated from this figure that the difference increases almost proportionally with the passage of time, and appears as a marked difference in the service life in actual use.
【0024】[0024]
【発明の効果】本発明にかかる複合遠心鋳造法は、ほぼ
同じ目的で計画され実施された従来技術の耐食被覆層
が、単一な被膜を主体とし背後の母材金属の溶着性や、
層自体の物性に対する配慮に若干の懸念を否定せざるを
得なかったのに対し、本発明の複合層は、液相焼結とい
う独創的な発想を原点として抜群の耐食性を具えた、緻
密で堅牢な複合層を一体的に溶着させ形成したものであ
るから、使用後の耐久性でははるかに優越する効果があ
る。According to the composite centrifugal casting method of the present invention, the conventional anti-corrosion coating layer, which is planned and implemented for almost the same purpose, comprises a single coating as a main component and the weldability of the base metal behind,
While some concerns had to be denied in consideration of the physical properties of the layer itself, the composite layer of the present invention is a dense, dense, highly corrosion-resistant alloy based on the original idea of liquid phase sintering. Since the solid composite layer is formed by integrally welding, there is an effect that the durability after use is far superior.
【図1】本発明の実施の効果のうち、塩水噴霧試験によ
る耐食性を比較表示した図である。FIG. 1 is a view comparatively showing the corrosion resistance by a salt spray test among the effects of the present invention.
【図2】本発明の実施の効果のうち、塩水浸漬試験によ
る耐食性を比較表示した図である。FIG. 2 is a diagram showing a comparative display of corrosion resistance by a salt water immersion test among the effects of the present invention.
【図3】本発明の実施に使用した、遠心鋳造金型の一部
断面正面図である。FIG. 3 is a partially sectional front view of a centrifugal casting mold used for carrying out the present invention.
【図4】実施例(1)の表面からの深度と成分の関係を
示す図表である。FIG. 4 is a table showing a relationship between a depth from a surface and a component in the embodiment (1).
【図5】実施例(3)の表面からの深度と成分の関係を
示す図表である。FIG. 5 is a table showing a relationship between a depth and a component from the surface in Example (3).
【図6】Cu−P二元状態図である。FIG. 6 is a Cu-P binary phase diagram.
1 遠心鋳造金型 2 回転支承 3 粉末層 4 供給管 DESCRIPTION OF SYMBOLS 1 Centrifugal casting die 2 Rotation bearing 3 Powder layer 4 Supply pipe
───────────────────────────────────────────────────── フロントページの続き (72)発明者 田辺 重則 大阪府大阪狭山市西山台2丁目15番3号 (56)参考文献 特開 平10−272547(JP,A) (58)調査した分野(Int.Cl.7,DB名) B22D 13/02 ──────────────────────────────────────────────────続 き Continued on the front page (72) Inventor Shigenori Tanabe 2- 15-3 Nishiyamadai, Osaka Sayama City, Osaka Prefecture (56) References JP-A-10-272547 (JP, A) (58) Fields investigated (Int) .Cl. 7 , DB name) B22D 13/02
Claims (2)
特定の金属類などを添加し、高速回転しつつ溶融金属を
注湯して、外周面を複合強化する複合遠心鋳造法におい
て、NiまたはNi系合金、Ni及び/又はCrを含む
ステンレス鋼もしくはCrを少くとも10重量%以上含
む鉄系合金の中から選ばれた1又は複数の金属粉末A
と、Pを5〜12重量%を含むことにより該金属粉末A
より明確に低温の溶融点に調整したCu−Pよりなる金
属粉末Bとを混合割合がA/B=40/60〜90/1
0の範囲内で均一に混合した粉末を作成し、金型を高速
に回転しつつ、金属粉末Bの溶融点よりは高い溶融点よ
りなる溶融金属を注湯する直前、又は同時に前記粉末を
金型内に散布することにより、溶融金属より比重の高い
A、Bが遠心力の差によって金型内面に分離添着した粉
末層を形成し、溶融金属から受熱して前記3溶融点の相
互関係によって発現する液相焼結と遠心作用を受けて、
製品の外周面に強固で緻密な焼結層を一体的に形成する
ことを特徴とする複合遠心鋳造法。1. A composite centrifugal casting method in which a specific metal or the like is added into a metal mold and molten metal is poured while rotating at a high speed, and the outer peripheral surface is compositely strengthened in order to improve specific physical properties. , Ni or a Ni-based alloy, stainless steel containing Ni and / or Cr, or one or more metal powders A selected from iron-based alloys containing at least 10% by weight or more of Cr
And 5 to 12% by weight of P to make the metal powder A
A / B = 40/60 to 90/1 when the mixing ratio with the metal powder B made of Cu-P, which is more clearly adjusted to a low melting point, is used.
0, and a powder mixed uniformly within a range of 0 is prepared. While the mold is being rotated at a high speed, immediately before or simultaneously with pouring a molten metal having a melting point higher than the melting point of the metal powder B, the powder is mixed with a metal. By dispersing in the mold, A and B having a higher specific gravity than the molten metal form a powder layer separated and attached to the inner surface of the mold due to a difference in centrifugal force. Due to the liquid phase sintering and centrifugal action that appears,
A composite centrifugal casting method characterized by integrally forming a strong and dense sintered layer on the outer peripheral surface of a product.
末の散布に替えて、前記金属粉末A,金属粉末Bと有機
系結合材Cの三者を混合して金型の内面上に塗布して粉
末層または添着層を形成し、高速に回転しつつ、金属粉
末Bの溶融点よりは高い溶融点よりなる溶融金属を注湯
して、前記3溶融点の相互関係によって発現する液相焼
結と遠心作用を受けて、該粉末層または添着層を製品の
外周面に強固で緻密に形成する焼結層に変換することを
特徴とする複合遠心鋳造法。2. The method according to claim 1, wherein the metal powder A, the metal powder B, and the organic binder C are mixed and dispersed on the inner surface of the mold instead of spraying the mixed powder on the inner surface of the mold. A liquid layer having a melting point higher than the melting point of the metal powder B is poured by pouring a molten metal having a melting point higher than the melting point of the metal powder B while forming a powder layer or an adhering layer by coating. A composite centrifugal casting method characterized by converting the powder layer or the adhering layer into a sintered layer which is firmly and densely formed on the outer peripheral surface of the product by phase sintering and centrifugal action.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP28606398A JP3283003B2 (en) | 1998-09-21 | 1998-09-21 | Composite centrifugal casting method |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP28606398A JP3283003B2 (en) | 1998-09-21 | 1998-09-21 | Composite centrifugal casting method |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JP2000094106A JP2000094106A (en) | 2000-04-04 |
| JP3283003B2 true JP3283003B2 (en) | 2002-05-20 |
Family
ID=17699480
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP28606398A Expired - Lifetime JP3283003B2 (en) | 1998-09-21 | 1998-09-21 | Composite centrifugal casting method |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JP3283003B2 (en) |
Families Citing this family (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106363151B (en) * | 2016-09-18 | 2018-08-21 | 江西省科学院应用物理研究所 | A method of preparing copper and iron double metallic composite material |
| CN109554627B (en) * | 2018-11-23 | 2020-02-11 | 中国航发北京航空材料研究院 | Graphene composite high-speed tool steel |
-
1998
- 1998-09-21 JP JP28606398A patent/JP3283003B2/en not_active Expired - Lifetime
Also Published As
| Publication number | Publication date |
|---|---|
| JP2000094106A (en) | 2000-04-04 |
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