JPS6089307A - Manufacture of abrasion-resistant composite layer - Google Patents
Manufacture of abrasion-resistant composite layerInfo
- Publication number
- JPS6089307A JPS6089307A JP58196167A JP19616783A JPS6089307A JP S6089307 A JPS6089307 A JP S6089307A JP 58196167 A JP58196167 A JP 58196167A JP 19616783 A JP19616783 A JP 19616783A JP S6089307 A JPS6089307 A JP S6089307A
- Authority
- JP
- Japan
- Prior art keywords
- composite layer
- layer
- powder
- slurry
- wear
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
- 239000002131 composite material Substances 0.000 title claims description 33
- 238000004519 manufacturing process Methods 0.000 title claims description 11
- 238000005299 abrasion Methods 0.000 title 1
- 239000000843 powder Substances 0.000 claims description 41
- 239000000956 alloy Substances 0.000 claims description 35
- 229910045601 alloy Inorganic materials 0.000 claims description 35
- 239000000919 ceramic Substances 0.000 claims description 27
- 239000002002 slurry Substances 0.000 claims description 27
- 239000011230 binding agent Substances 0.000 claims description 17
- 238000000034 method Methods 0.000 claims description 15
- 239000002184 metal Substances 0.000 claims description 13
- 238000009423 ventilation Methods 0.000 claims description 6
- 239000012298 atmosphere Substances 0.000 claims description 5
- 239000000203 mixture Substances 0.000 claims description 4
- 230000001590 oxidative effect Effects 0.000 claims description 4
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims description 4
- 238000009792 diffusion process Methods 0.000 claims description 3
- ATJFFYVFTNAWJD-UHFFFAOYSA-N Tin Chemical compound [Sn] ATJFFYVFTNAWJD-UHFFFAOYSA-N 0.000 claims description 2
- -1 ZrN Chemical class 0.000 claims 1
- 238000002485 combustion reaction Methods 0.000 claims 1
- 238000000354 decomposition reaction Methods 0.000 claims 1
- 150000004767 nitrides Chemical class 0.000 claims 1
- 239000003960 organic solvent Substances 0.000 claims 1
- 239000000126 substance Substances 0.000 claims 1
- 239000010410 layer Substances 0.000 description 42
- 239000002245 particle Substances 0.000 description 9
- 239000000463 material Substances 0.000 description 8
- 150000001875 compounds Chemical class 0.000 description 6
- 238000002844 melting Methods 0.000 description 5
- 230000008018 melting Effects 0.000 description 5
- 229920000642 polymer Polymers 0.000 description 5
- 239000011247 coating layer Substances 0.000 description 4
- 238000010586 diagram Methods 0.000 description 4
- 230000005484 gravity Effects 0.000 description 4
- 238000001000 micrograph Methods 0.000 description 4
- 238000002156 mixing Methods 0.000 description 4
- 238000005245 sintering Methods 0.000 description 4
- ZWEHNKRNPOVVGH-UHFFFAOYSA-N 2-Butanone Chemical compound CCC(C)=O ZWEHNKRNPOVVGH-UHFFFAOYSA-N 0.000 description 3
- YXFVVABEGXRONW-UHFFFAOYSA-N Toluene Chemical compound CC1=CC=CC=C1 YXFVVABEGXRONW-UHFFFAOYSA-N 0.000 description 3
- 238000010438 heat treatment Methods 0.000 description 3
- 239000002904 solvent Substances 0.000 description 3
- 239000004372 Polyvinyl alcohol Substances 0.000 description 2
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N Silicium dioxide Chemical compound O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 description 2
- 229910000831 Steel Inorganic materials 0.000 description 2
- 238000009750 centrifugal casting Methods 0.000 description 2
- 238000000576 coating method Methods 0.000 description 2
- 239000013078 crystal Substances 0.000 description 2
- 238000001035 drying Methods 0.000 description 2
- 239000011159 matrix material Substances 0.000 description 2
- 238000010137 moulding (plastic) Methods 0.000 description 2
- 229920002451 polyvinyl alcohol Polymers 0.000 description 2
- 238000005204 segregation Methods 0.000 description 2
- 239000010959 steel Substances 0.000 description 2
- JOYRKODLDBILNP-UHFFFAOYSA-N Ethyl urethane Chemical compound CCOC(N)=O JOYRKODLDBILNP-UHFFFAOYSA-N 0.000 description 1
- 229920002319 Poly(methyl acrylate) Polymers 0.000 description 1
- 239000000853 adhesive Substances 0.000 description 1
- 230000001070 adhesive effect Effects 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 239000003795 chemical substances by application Substances 0.000 description 1
- 239000011248 coating agent Substances 0.000 description 1
- 238000009826 distribution Methods 0.000 description 1
- 238000002309 gasification Methods 0.000 description 1
- 239000007791 liquid phase Substances 0.000 description 1
- 239000000155 melt Substances 0.000 description 1
- 229920005615 natural polymer Polymers 0.000 description 1
- 229920000728 polyester Polymers 0.000 description 1
- 239000011148 porous material Substances 0.000 description 1
- 239000000377 silicon dioxide Substances 0.000 description 1
- 229920001059 synthetic polymer Polymers 0.000 description 1
- 239000002699 waste material Substances 0.000 description 1
Landscapes
- Compositions Of Oxide Ceramics (AREA)
- Manufacturing Of Tubular Articles Or Embedded Moulded Articles (AREA)
- Powder Metallurgy (AREA)
- Laminated Bodies (AREA)
- Ceramic Products (AREA)
Abstract
(57)【要約】本公報は電子出願前の出願データであるた
め要約のデータは記録されません。(57) [Summary] This bulletin contains application data before electronic filing, so abstract data is not recorded.
Description
【発明の詳細な説明】
〔発明の属する技術分野〕
本発明は、耐摩耗複合層の製造方法、詳しくはプラスチ
ック成形機のシリンダなど耐摩耗性を要求される円筒形
状部品の内径部に適する耐摩耗複合材の被覆層の製造方
法に関するものである。DETAILED DESCRIPTION OF THE INVENTION [Technical field to which the invention pertains] The present invention relates to a method for manufacturing a wear-resistant composite layer, and more particularly, to a method for manufacturing a wear-resistant composite layer, which is suitable for the inner diameter portion of a cylindrical part that requires wear resistance, such as a cylinder of a plastic molding machine. The present invention relates to a method for manufacturing a coating layer of a wear composite material.
従来、プラスチック成形機のシリンダなどの円筒形状部
品の内径部忙耐摩耗性の被覆層の製造方法として遠心鋳
造法が知られている。この遠心鋳造法は、シリンダの一
方の開口部に鋼板の蓋をし、他の開口部よりセラミック
ス粉末と自溶性合金粉末を添加して鋼板の蓋をした後、
炉中で950〜1250℃に加熱して自溶性合金を溶融
し、次いで炉外へ出してシリンダを回転下に自溶性合金
の融点下に冷却後、炉内で徐冷することによシ複合被覆
層を形成するものである。しかし、この方法は、シリン
ダ内面に均一な厚さの複合被覆層を形成させるためには
、自溶性合金の溶融体とセラミックス粉末の混合物に流
動性を持たせなければならず、そのためセラミックス粉
末に対し、相浩量多くの自溶性合金を加えなければなら
ない。そのためセラミックス粒子と自溶性合金との間の
比重差があると耐摩耗粉末が偏析して均一な複合層が得
られない。すなわち、セラミックス粉末の比重が自溶性
合金の比重より大なる場合はセラミックス粉末がシリン
ダ内壁側に偏析し、複合層を得るためには加工代が多く
要し、加工費がかか)材料も無駄になる欠点があり、一
方、セラミックス粉末の比重が自溶性合金の比重より小
さい場合はセラミックス粉末がシリンダ中心側に偏析し
、このため自溶性合金だけの部分は耐摩耗複合層として
の性質を示さないので材料の無駄となる。Conventionally, centrifugal casting is known as a method for manufacturing a wear-resistant coating layer on the inner diameter of a cylindrical part such as a cylinder of a plastic molding machine. In this centrifugal casting method, one opening of the cylinder is covered with a steel plate, ceramic powder and self-fusing alloy powder are added to the other opening, and then the steel plate is covered.
The self-fusing alloy is heated to 950-1250°C in a furnace to melt it, then taken out of the furnace and cooled to below the melting point of the self-fusing alloy while rotating the cylinder, and then slowly cooled in the furnace. It forms a covering layer. However, in this method, in order to form a composite coating layer with a uniform thickness on the inner surface of the cylinder, the mixture of the molten self-fusing alloy and the ceramic powder must have fluidity. On the other hand, a large amount of self-fusing alloy must be added. Therefore, if there is a difference in specific gravity between the ceramic particles and the self-fusing alloy, the wear-resistant powder will segregate, making it impossible to obtain a uniform composite layer. In other words, if the specific gravity of the ceramic powder is greater than the specific gravity of the self-fusing alloy, the ceramic powder will segregate on the inner wall of the cylinder, requiring a large amount of processing to obtain a composite layer, resulting in high processing costs and wasted material. On the other hand, if the specific gravity of the ceramic powder is lower than that of the self-fusing alloy, the ceramic powder will segregate toward the center of the cylinder, and as a result, the area made only of the self-fusing alloy will exhibit properties as a wear-resistant composite layer. Because there is no material, it is a waste of material.
ま大、この方法は、薄肉の被覆ができず、しかも高温の
赤熱部品を回転させるため作業性が悪い等の欠点があっ
た。However, this method had drawbacks such as not being able to provide a thin coating and having poor workability because it rotated hot red-hot parts.
それ故、本発明の一般的な目的は、先に述べた多くの欠
点を除去し、偏析のない耐摩耗複合層を所望の厚さに成
形できる被覆方法を提供するにある。It is therefore a general object of the present invention to provide a coating method which obviates many of the drawbacks mentioned above and which makes it possible to form a segregation-free wear-resistant composite layer to the desired thickness.
この目的を達成するため、本発明に係る耐摩耗複合層の
製造方法においては、セラミックス粉末と有機バインダ
ーとを混合してスラリー状とし、このスラリーを回転シ
リンダ内面に注入して回転下に通風乾燥後、金属粉末と
有機バインダーとの混合によシ得られるスラリーを前記
回転シリンダ内に注入し回転下に通風乾燥して所定厚の
2重層を形成した後、加熱して有機バインダー成分を分
解燃焼により完全に除去し、次いで真空中または無酸化
雰囲気中にて加熱してセラミックス層と金属粉末層とが
焼結した耐摩耗性に優れた均一な複合層とすると同時に
、この複合層とシリンダ内面とが拡散層を介して一体的
に結合した均一な複合層を形成せしめることを特徴とす
る6
本発明における金属粉末には次のものを用いる。In order to achieve this objective, in the method for manufacturing a wear-resistant composite layer according to the present invention, ceramic powder and an organic binder are mixed to form a slurry, the slurry is injected into the inner surface of a rotating cylinder, and the slurry is dried with ventilation while rotating. After that, the slurry obtained by mixing the metal powder and the organic binder is injected into the rotating cylinder and dried with ventilation while rotating to form a double layer of a predetermined thickness, and then heated to decompose and burn the organic binder component. The ceramic layer and the metal powder layer are completely removed by heating in a vacuum or in a non-oxidizing atmosphere to sinter the ceramic layer and the metal powder layer to form a uniform composite layer with excellent wear resistance. The following metal powders are used as the metal powder in the present invention.
(1) N1基自溶性合金(CrO〜20%、B1,0
〜5.0%、S11.5〜5.0%、CI、1%以下P
e 5%以下、残部Ni )
(2) Cog自溶性合金(Cr 0〜24%、B1,
0〜5.0%、S11.5〜5.0%、CI、5%以下
、 k’e 5%以下、 Nf O〜33 % 、残部
Co)以上の自溶性合金の粒度150メツシユ以下のも
のを用いる。自溶性合金を用いる理由は、融点が900
〜1100℃と比較的融点が低く、焼結にあたって高温
炉を必要としないこと、溶融中の粘度が高く、焼結中の
流れ、ダレによる変形が小さいこと、耐摩耗性、耐兼性
が優れていることである。(1) N1-based self-fusing alloy (CrO ~ 20%, B1,0
~5.0%, S11.5~5.0%, CI, 1% or less P
e 5% or less, balance Ni) (2) Cog self-fusing alloy (Cr 0-24%, B1,
0 to 5.0%, S11.5 to 5.0%, CI, 5% or less, k'e 5% or less, NfO to 33%, balance Co) or more, with a grain size of 150 mesh or less Use. The reason for using a self-fusing alloy is that its melting point is 900.
It has a relatively low melting point of ~1100°C, does not require a high-temperature furnace for sintering, has high viscosity during melting, has little deformation due to flow and sag during sintering, and has excellent wear resistance and durability. That is what we are doing.
セラミックス粉末としては、wc 、 vc 。Ceramic powders include WC and VC.
T、iB2. MoB 、 TiN 、 ZrNなどで
金属粉末の溶融体と携れ性の良いものを用いる。粒度は
約1〜100μ、これらセラミックスの硬度はHv15
00〜3400であシ、優れた耐摩耗性を有する。T, iB2. Use materials such as MoB, TiN, ZrN, etc. that have good compatibility with the molten metal powder. The particle size is approximately 1-100μ, and the hardness of these ceramics is Hv15.
00-3400 and has excellent wear resistance.
有機バインダーとしては、天然または合成の高分子化合
物を水または揮発性溶剤に溶解した粘性溶液で、シリン
ダ内壁にセラミックス層または自溶性合金層を形成させ
る際に、粉末粒子に流動性を付与するために用いる。ま
た1層の乾燥後は、粉末粒子間および粉末粒子とシリン
ダ内壁の間の接着剤の役目を果す。高分子化合物はでき
るだけ低い温度で完全に分解燃焼するものが好ましい。The organic binder is a viscous solution made by dissolving a natural or synthetic polymer compound in water or a volatile solvent, and is used to impart fluidity to powder particles when forming a ceramic layer or self-fusing alloy layer on the inner wall of a cylinder. used for Moreover, after drying of one layer, it acts as an adhesive between the powder particles and between the powder particles and the inner wall of the cylinder. The polymer compound is preferably one that completely decomposes and burns at as low a temperature as possible.
有機バインダー中の水または揮発性溶剤に対する高分子
化合物の混合割合は約1〜20ffi量%であシ、高分
子化合物および溶剤の混合割合の好適な例は、ポリエス
テルウレタン(8%)/メチルエチルケトン(92%)
。The mixing ratio of the polymer compound to water or volatile solvent in the organic binder is about 1 to 20% by weight. A preferable example of the mixing ratio of the polymer compound and the solvent is polyester urethane (8%)/methyl ethyl ketone ( 92%)
.
ポリアクリル酸メチル(13,5%)/トルエン(86
,5%)、ポリビニルアルコール(3%)/水(97%
) が挙げられる。耐摩耗剤の粉末に対する有機バイン
ダーの混合比は約0.1〜5重量%が好ましい。Polymethyl acrylate (13.5%)/Toluene (86%)
, 5%), polyvinyl alcohol (3%)/water (97%)
). The mixing ratio of the organic binder to the anti-wear powder is preferably about 0.1 to 5% by weight.
シリンダ内壁にスラリーを付着させるには、シリンダの
両端に中心部の開口した蓋をし、シリンダを回転させな
がらセラミックススラリーを所定l゛一方の開口より漏
斗を介して流し込み、スラリーがシリンダ内壁に充分均
一に分布した時、回転通風下に乾燥し、次いで自溶性合
金スラリーヲ流し込み同様にして先のセラミックス層の
上に自溶性合金スラリーが充分均一に分布した時、回転
下に通風乾燥する。To attach the slurry to the inner wall of the cylinder, cover both ends of the cylinder with lids that have an opening in the center, and while rotating the cylinder, pour the ceramic slurry into a predetermined amount through a funnel through one opening, so that the slurry is sufficiently coated on the inner wall of the cylinder. When the self-fusing alloy slurry is evenly distributed, it is dried under rotating ventilation, and then the self-fusing alloy slurry is poured in. When the self-fusing alloy slurry is sufficiently evenly distributed on the ceramic layer, it is dried under rotating ventilation.
乾燥スラリー層の加熱は、セラミックス粉末および自溶
性合金粉末の結合剤として用いた有機バインダーの高分
子化合物成分を分解燃焼しガス化させるため行う。約3
00〜750℃で、完全にガス化する迄行う。高分子化
合物が分解せずに残ると次の工程で焼結炉内を汚染し、
また耐摩耗複合層中に空孔形成の原因ともなる。The dry slurry layer is heated in order to decompose, burn, and gasify the polymer compound component of the organic binder used as a binder for the ceramic powder and the self-fusing alloy powder. Approximately 3
The process is carried out at 00 to 750°C until complete gasification. If the polymer compound remains undecomposed, it will contaminate the inside of the sintering furnace in the next process.
It also causes the formation of pores in the wear-resistant composite layer.
その後の真空中、無酸化雰囲気中での加熱は、セラミッ
クス粉末と自溶性合金粉末との焼結が目的であって、自
溶性合金の融点より50〜200℃高い温度、約100
0〜1600℃にて行う。自溶性合金およびセラミック
ス粉末が酸化、脱炭素されないようにするため、真空中
または無酸化雰囲気中にて行う。この温度で自溶性合金
が溶融し、WC層に浸透し1両者の間に液相焼結が行な
われ、その結果、自溶性合金をマトリックスとしその中
に耐摩耗性の優れたセラミックス粉末が均一に分布した
複合層が形成される。かつ同時にこの複合層とシリンダ
内壁(母材)との間には拡散層が生じ密着強度のすぐれ
た被覆層が得られる。The purpose of the subsequent heating in a vacuum and non-oxidizing atmosphere is to sinter the ceramic powder and the self-fusing alloy powder, and the temperature is 50 to 200°C higher than the melting point of the self-fusing alloy, about 100°C.
It is carried out at 0 to 1600°C. In order to prevent the self-fusing alloy and ceramic powder from being oxidized and decarbonized, the process is carried out in a vacuum or in a non-oxidizing atmosphere. At this temperature, the self-fusing alloy melts and penetrates into the WC layer, and liquid phase sintering occurs between the two. As a result, ceramic powder with excellent wear resistance is uniformly distributed in the self-fusing alloy as a matrix. A composite layer is formed with a distribution of At the same time, a diffusion layer is formed between this composite layer and the cylinder inner wall (base material), resulting in a coating layer with excellent adhesion strength.
次に実施例によ勺本発明を具体的に説明する。 Next, the present invention will be specifically explained with reference to Examples.
実施例において使用される自溶性合金及び有機バインダ
ーの組成を下記に一括して表示する。The compositions of the self-fusing alloy and organic binder used in the examples are shown below.
実施例1
平均粒径10μのWC粉末2警を有機ノ(インダー(1
3−5)2[10m/と混合してセラミックススラリー
とし、第1図に示すように、シリンダ100両端にそれ
ぞれ中心部に開口12を設けた蓋体14.i4を取付け
、一方の蓋体14の開口12より漏斗16を挿通配置し
、前記シリンダ10を約50 Orpmで回転させなが
らその内部に漏斗16を介してスラリー18を流し込ん
だ。その後1回転を続けながらシリンダ10内へ送風を
行い30分間スラリー18を乾燥させ、セラミックス層
20を形成した。次に、粒度250メツシユ以下の自溶
性合金粉末(Ni−2)21&を有機バインダー(B−
3)250dと混合して自溶性合金スラリー22を得、
これを前記と同様にシリンダ100回転作用下に漏斗1
6を介してシリンダ10の内面のセラミックス層200
表面に流し込み、その後送風を行って30分間スラリー
を乾燥させ、均一な自溶性合金層24を形成した(第2
図参照)。その後、完全に乾燥させるため14時間自然
乾燥を行った。Example 1 WC powder with an average particle size of 10 μm was mixed with an organic powder (ind.
3-5) A lid body 14.2 is mixed with 10m/ml to form a ceramic slurry, and as shown in FIG. i4 was attached, a funnel 16 was inserted through the opening 12 of one lid 14, and the slurry 18 was poured into the cylinder 10 through the funnel 16 while rotating the cylinder 10 at about 50 rpm. Thereafter, air was blown into the cylinder 10 while continuing one revolution to dry the slurry 18 for 30 minutes, thereby forming a ceramic layer 20. Next, a self-fusing alloy powder (Ni-2) 21& with a particle size of 250 mesh or less is mixed with an organic binder (B-
3) mixed with 250d to obtain self-fusing alloy slurry 22,
The funnel 1 was rotated 100 times in the same manner as above.
Ceramic layer 200 on the inner surface of the cylinder 10 via 6
The slurry was poured onto the surface and then blown with air to dry the slurry for 30 minutes to form a uniform self-fusing alloy layer 24 (second
(see figure). Thereafter, natural drying was performed for 14 hours to completely dry the film.
しかる後、シリンダ10を大気中で400℃に60分間
保持してポリビニルアルコールヲ完全に分解燃焼した。Thereafter, the cylinder 10 was held at 400° C. for 60 minutes in the atmosphere to completely decompose and burn the polyvinyl alcohol.
次いで、真空炉中で1100℃にて60分間静止下に加
熱した後炉冷し。Next, the mixture was heated in a vacuum furnace at 1100° C. for 60 minutes while being kept still, and then cooled in the furnace.
200℃以下で炉出して室温まで空冷した。It was taken out of the furnace at a temperature below 200°C and air cooled to room temperature.
得られた複合層は、その断面を顕微鏡写真で観察したと
ころ、第3図および第4図に示すように、N1基自溶性
合金28のマトリックス中にWCの粒子26が均一に分
散分布し、偏析等は全く見られなかった。また、複合層
の厚さは1.0目であり、硬さはHv 830〜132
0であり、しかも母材30 (80M435 )との間
に形成された拡散層62は約25μであシ、母材と強固
に結合されていることが確認された。さらに、この時の
複合層のWCの含有量は約62重量%であった。When the cross section of the obtained composite layer was observed using a micrograph, it was found that the WC particles 26 were uniformly dispersed in the matrix of the N1-based self-fusing alloy 28, as shown in FIGS. 3 and 4. No segregation was observed. In addition, the thickness of the composite layer is 1.0 mm, and the hardness is Hv 830-132.
0, and the diffusion layer 62 formed between it and the base material 30 (80M435) had a thickness of about 25μ, confirming that it was firmly bonded to the base material. Furthermore, the WC content of the composite layer at this time was about 62% by weight.
実施例2
WCスラリーの有機バインダーは(B−2)であり、自
溶性合金(Ni−13を使用し、有機)(インダー(B
−2)にてスラリーとした以外は実施例1と全く同様に
処理して、複合層の硬さHv700〜1250以外は全
く同じ性質の複合層を得た。Example 2 The organic binder of the WC slurry was (B-2), and a self-fusing alloy (Ni-13 was used, organic) (inder (B-2) was used).
-2) Except that it was made into a slurry, the process was carried out in exactly the same manner as in Example 1 to obtain a composite layer having exactly the same properties except for the hardness of the composite layer of Hv 700 to 1250.
実施例3
WCスラリーの有機バインダーが(B−1)であり、自
溶性合金(Co−1)を使用し、有機バインダー(41
3−1)にてスラリーとした以外は実施例1と同様に処
理して、複合層の硬さHv700〜1200以外は実施
例1のものと全く同じ性質の複合層を得た。Example 3 The organic binder of the WC slurry was (B-1), a self-fusing alloy (Co-1) was used, and the organic binder (41
The process was carried out in the same manner as in Example 1 except that it was made into a slurry in step 3-1) to obtain a composite layer having exactly the same properties as in Example 1 except for the hardness of the composite layer of Hv 700 to 1200.
本発明によると、シリンダ内壁に耐摩耗粉末の偏析の寿
い所望厚の、特に薄肉の複合層をシリンダを赤熱して回
転することなく容易に得ることができる。According to the present invention, it is possible to easily obtain a particularly thin composite layer of a desired thickness, which prevents segregation of wear-resistant powder, on the inner wall of the cylinder without rotating the cylinder by heating it to red.
以上、本発明の好適な実施例について説明したが、この
発明の精神を逸脱しない範囲内において種々の変化をな
し得ることは勿論である。Although the preferred embodiments of the present invention have been described above, it goes without saying that various changes can be made without departing from the spirit of the invention.
第1図は本発明の実施例1においてシリンダを回転下に
WCスラリーを添加する説明図、第2図は同じく自溶性
合金粉末スラリーを添加する説明図、第3図は本発明の
実施例1で得られた複合層の断面の顕微鏡写真(X20
0)とその説明図、第4図は同じく写X(X100)で
ある。
10・・・シリンダ 12・・・開 口14・・・蓋
体 16・・・漏 斗
18・・、WCC粉末シラ11− 20・・・セラミッ
クス層22・・・自溶性合金スラリー
24・・・自溶性合金層
26・・・WCの粒子
28・・・Ni基自溶性合金
特許川柳(東芝機械株式会社
出動入代et仄 弁理士 浜 1)治βitFl(3,
1
FIG、 3
200
FIO,4
(3z)
手続補正置型
昭和59年2月8日
特許庁長官 若杉和夫 殿
I。
1、事件の表示
昭和58年特許願 第196167号
2、発明の名称
耐摩耗複合層の製造方法
3、補正をする者
事件との関係 特許出願人
住所 東京都中央区銀座4丁目2番11号名称(345
)東芝機械株式会社
代表者版材 和雄
4、代理人
6、補正の対象
(1)明細書の図面の簡単な説明の閣。
7、補正の内容
+11 yi+駈記載の通り。
特願昭58−196167号
補正書
明細書第14頁第5〜8行
「第3図は・・・・・・である。」を
「第3図は本発明の実施例1で得られた複合層の結晶構
造の断面の顕微鏡写真(x200)とその説明図、第4
図は第3図と同じ複合層の結晶構造の断面の顕微鏡写真
(X100)である。」と補正します。
特許出願人 東芝機械株式会社Figure 1 is an explanatory diagram of adding WC slurry while rotating the cylinder in Example 1 of the present invention, Figure 2 is an explanatory diagram of adding self-fusing alloy powder slurry, and Figure 3 is Example 1 of the present invention. Micrograph of the cross section of the composite layer obtained in (X20
0) and its explanatory diagram, FIG. 4, are also copies X (X100). 10... Cylinder 12... Opening 14... Lid
Body 16...Funnel 18..., WCC powder silica 11-20...Ceramic layer 22...Self-fusing alloy slurry 24...Self-fusing alloy layer 26...WC particles 28...Ni Base self-fusing alloy patent senryu (Toshiba Machine Co., Ltd. dispatcher et al. Patent attorney Hama 1) JiβitFl (3,
1 FIG, 3 200 FIO, 4 (3z) Procedural Amendment Form February 8, 1980 Commissioner of the Patent Office Kazuo Wakasugi I. 1. Indication of the case 1982 Patent Application No. 196167 2. Name of the invention Method for manufacturing a wear-resistant composite layer 3. Person making the amendment Relationship to the case Patent applicant address 4-2-11 Ginza, Chuo-ku, Tokyo Name (345
) Toshiba Machine Co., Ltd. representative plate material Kazuo 4, agent 6, subject of amendment (1) Brief explanation of drawings in the specification. 7. Contents of amendment +11 yi+as stated. Japanese Patent Application No. 58-196167, amended specification, page 14, lines 5 to 8, “Figure 3 is...” was changed to “Figure 3 is obtained in Example 1 of the present invention.” Micrograph (x200) of the cross section of the crystal structure of the composite layer and its explanatory diagram, No. 4
The figure is a micrograph (X100) of a cross section of the crystal structure of the same composite layer as in Figure 3. ” and correct it. Patent applicant: Toshiba Machine Co., Ltd.
Claims (1)
てスラリー状とし、このスラリーを回転シリンダー内面
に注入して回転下に通風乾燥後、金属粉末と有機バイン
ダーとの混合により得られるスラリーを前記回転シリン
ダ内に注入し回転下に通風乾燥して所定厚の2重層を形
成した後、加熱して有機バインダー成分を分解燃焼によ
り完全に除去し、次いで真空中または無酸化雰囲気中に
て加熱してセラミックス層と金属粉末層とが焼結した均
一な複合層とすると同時に、この複合層とシリンダ内面
とが拡散層を介して一体的に結合した均一な複合層全形
成せ[7めることを特徴とする耐摩耗複合層の製造方法
。 (2) セラミックス粉末がwc、vc等の金属炭化物
、Tit32. Mo8等の金属硼化物、TiN 。 ZrN等の金属窒化物、またはこれらの混合物より成る
群から選択される粉末であることを特徴とする特許請求
の範囲第1項記載の耐摩耗複合層の製造方法。 (6)金属粉末がNi基自溶性合金粉末またはCO基自
溶性合金粉末であることを特徴とする特許請求の範囲第
1項記載の耐摩耗複合層の製造方法。 (4)有機バインダーが天然または合成の高分子物質の
水または揮発性有機溶剤の溶液から成ることを特徴とす
る特許請求の範囲第1項記載の耐摩耗複合層の製造方法
。[Claims] (1) Ceramic powder and organic binder are mixed to form a slurry, this slurry is injected into the inner surface of a rotating cylinder and dried with ventilation while rotating, and then the metal powder and organic binder are mixed. The slurry is injected into the rotating cylinder and dried under rotation with ventilation to form a double layer of a predetermined thickness, and then heated to completely remove the organic binder component by decomposition and combustion, and then heated in a vacuum or in a non-oxidizing atmosphere. At the same time, the ceramic layer and the metal powder layer are heated to form a uniform composite layer in which the ceramic layer and the metal powder layer are sintered, and at the same time, the entire uniform composite layer is formed in which this composite layer and the inner surface of the cylinder are integrally bonded via a diffusion layer. 7. A method for producing a wear-resistant composite layer, characterized by: (2) Ceramic powder is metal carbide such as WC, VC, Tit32. Metal borides such as Mo8, TiN. The method for producing a wear-resistant composite layer according to claim 1, characterized in that the powder is selected from the group consisting of metal nitrides such as ZrN, or mixtures thereof. (6) The method for manufacturing a wear-resistant composite layer according to claim 1, wherein the metal powder is a Ni-based self-fusing alloy powder or a CO-based self-fusing alloy powder. (4) The method for producing a wear-resistant composite layer according to claim 1, wherein the organic binder comprises a solution of a natural or synthetic polymeric substance in water or a volatile organic solvent.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP58196167A JPS6089307A (en) | 1983-10-21 | 1983-10-21 | Manufacture of abrasion-resistant composite layer |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP58196167A JPS6089307A (en) | 1983-10-21 | 1983-10-21 | Manufacture of abrasion-resistant composite layer |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS6089307A true JPS6089307A (en) | 1985-05-20 |
| JPH0221361B2 JPH0221361B2 (en) | 1990-05-14 |
Family
ID=16353318
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP58196167A Granted JPS6089307A (en) | 1983-10-21 | 1983-10-21 | Manufacture of abrasion-resistant composite layer |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS6089307A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2015157971A (en) * | 2014-02-21 | 2015-09-03 | 第一高周波工業株式会社 | Method for forming self-fluxing alloy coating layer |
-
1983
- 1983-10-21 JP JP58196167A patent/JPS6089307A/en active Granted
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2015157971A (en) * | 2014-02-21 | 2015-09-03 | 第一高周波工業株式会社 | Method for forming self-fluxing alloy coating layer |
Also Published As
| Publication number | Publication date |
|---|---|
| JPH0221361B2 (en) | 1990-05-14 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US2390160A (en) | Method of manufacture | |
| US3608170A (en) | Metal impregnated composite casting method | |
| US4299629A (en) | Metal powder mixtures, sintered article produced therefrom and process for producing same | |
| CN106944612B (en) | Vacuum sintering forming process for bimetallic pipe sleeve and product thereof | |
| JPS6089503A (en) | Coating method of wear resistant material | |
| US4851267A (en) | Method of forming wear-resistant material | |
| US3954479A (en) | High-temperature and wear-resistant antifriction material having low thermal expansions | |
| US4385020A (en) | Method for making shaped silicon-silicon carbide refractories | |
| JPH01234536A (en) | Production of aluminum/magnesium alloy containing refractory particles | |
| US3720537A (en) | Process of coating an alloy substrate with an alloy | |
| JPS6089504A (en) | Coating method of wear resistant composite material | |
| JPS6089307A (en) | Manufacture of abrasion-resistant composite layer | |
| JPS58157944A (en) | Compound cylinder and casted alloy therefor | |
| JPH03282187A (en) | Crucible and manufacture thereof | |
| US2558402A (en) | Mold composition | |
| US2476933A (en) | Manufacture of facing compositions for metal casting molds | |
| JPH0456702A (en) | Raw material powder for powder metallurgy and manufacture thereof | |
| JPS5858423B2 (en) | powder spray material | |
| Freitag et al. | Novel Ceramic Materials and Technologies for Titanium Investment Casting | |
| JPS586901A (en) | Novel metallic powder molded item and production thereof | |
| WO1997003776A1 (en) | Composite powders | |
| JPH01247539A (en) | Manufacture of metal-base composite material | |
| JPH0733279B2 (en) | Manufacturing method of molded products using slag | |
| JPS62187560A (en) | Metal coating casting method | |
| JPH04167957A (en) | Adhesive layer for mold |