JPS60230975A - Formation of reinforcing layer on base metal - Google Patents

Formation of reinforcing layer on base metal

Info

Publication number
JPS60230975A
JPS60230975A JP8669684A JP8669684A JPS60230975A JP S60230975 A JPS60230975 A JP S60230975A JP 8669684 A JP8669684 A JP 8669684A JP 8669684 A JP8669684 A JP 8669684A JP S60230975 A JPS60230975 A JP S60230975A
Authority
JP
Japan
Prior art keywords
reinforcing layer
base metal
recesses
piston
piston body
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.)
Pending
Application number
JP8669684A
Other languages
Japanese (ja)
Inventor
Masaki Okada
岡田 正貴
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Isuzu Motors Ltd
Original Assignee
Isuzu Motors Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Isuzu Motors Ltd filed Critical Isuzu Motors Ltd
Priority to JP8669684A priority Critical patent/JPS60230975A/en
Publication of JPS60230975A publication Critical patent/JPS60230975A/en
Pending legal-status Critical Current

Links

Classifications

    • CCHEMISTRY; METALLURGY
    • C23COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23CCOATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C4/00Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge
    • C23C4/02Pretreatment of the material to be coated, e.g. for coating on selected surface areas

Abstract

PURPOSE:To improve remarkably the bonding strength of a reinforcing layer to a base metal by recessing the surface of the base metal to be bonded so that the resulting recesses for engagement have the shape of an inverted unfolded fan as the cross-sectional shape and by forming the reinforcing layer while filling the recesses. CONSTITUTION:The piston head 6 of a piston body 5 as the base metal is recessed, for example, so that the resulting recesses 7 for engagement have the shape of an inverted unfolded fan as the cross-sectional shape and are distributed over the whole region of the piston head 6. Ceramics or the like is then thermally sprayed on the whole region of the piston head 6 to form the reinforcing layer 8 filling the recesses 7. The sprayed material flows in the recesses 7 and solidifies, improving the bonding strength of the reinforcing layer 8 to the piston body 5.

Description

【発明の詳細な説明】 [発明の技術分野] 本発明は、アルミ鋳物などの部品を局部的に耐熱、耐摩
耗層で補強する母材金属の強化層形成方法に係り、特に
、セラミック材などよりなる強化層の結合性を向上させ
て剥離を防止することができる母材金属の強化層形成方
法にaする。
[Detailed Description of the Invention] [Technical Field of the Invention] The present invention relates to a method for forming a reinforcing layer on a base metal for locally reinforcing parts such as aluminum castings with a heat-resistant and abrasion-resistant layer, and particularly relates to a method for forming a reinforcing layer on a base metal such as a ceramic material. The present invention is directed to a method for forming a reinforcing layer of a base metal that can improve the bonding properties of the reinforcing layer and prevent peeling.

[発明の技術的背景とその問題点1 一般に、自動車部品であるシリンダヘッドや、ピストン
などのように耐熱性、耐摩耗性を局部的に特に要求され
る部品については、その部分に例えばセラミック材より
なる強化層を溶剤等により形成し、補強することがすで
に研究乃至実施されている。
[Technical Background of the Invention and Problems Therewith 1 Generally, for automobile parts such as cylinder heads and pistons where heat resistance and wear resistance are locally required, ceramic materials are used in those parts. Research and implementation have already been carried out to form a reinforcing layer made of a solvent or the like for reinforcement.

ところで、母材金属とこの表面に形成される強化層との
熱膨張差があまり大きくない場合には問題とならないが
、例えば金属とセラミックのように熱膨張差が大きい場
合には加熱冷却の繰り返しに伴なう熱衝撃により母材金
属とセラミックとの境界面が剥離する現象が生じていた
。これは、セラミックの熱変化にともなう金属との相対
歪から生ずる応力よりも接着力の方が小さいということ
に起因するものである。
By the way, this is not a problem if the difference in thermal expansion between the base metal and the reinforcing layer formed on the surface is not very large, but if the difference in thermal expansion is large, such as between metal and ceramic, repeated heating and cooling may be necessary. Due to the thermal shock associated with this, a phenomenon occurred in which the interface between the base metal and the ceramic peeled off. This is due to the fact that the adhesive force is smaller than the stress generated from relative strain with the metal due to thermal changes in the ceramic.

これを具体的に第8図乃至第9図に基づいて説明する。This will be specifically explained based on FIGS. 8 and 9.

第8図は強化層の形成されたピストンを示す平面図、第
9図は第8図中A部を示す拡大図である。
FIG. 8 is a plan view showing the piston on which the reinforcing layer is formed, and FIG. 9 is an enlarged view showing section A in FIG. 8.

第8図に示す如く例えばAβ(アルミニウム)合金など
よりなるピストン1のヘッド部に例えばジルコニアより
なるセラミック材の強化層2を溶射して形成するもので
あるが、被着面3に直接溶射すると急冷などの熱衝撃に
より強化層2が境界面から剥離していた。
As shown in FIG. 8, a reinforcing layer 2 of a ceramic material made of, for example, zirconia is formed by thermal spraying on the head portion of a piston 1 made of, for example, an Aβ (aluminum) alloy. The reinforcing layer 2 was peeled off from the interface due to thermal shock such as rapid cooling.

そこで、第9図(a)、(b)に示す如く母材金属たる
ピストン1の被着面3を脱脂後、ショツ。
Therefore, as shown in FIGS. 9(a) and 9(b), the adhered surface 3 of the piston 1, which is the base metal, was degreased and then removed.

ドブラスト等により予め粗面加工しておき、セラミック
材を溶射する前に、母材金属とセラミック材との両方に
接着性良好な無機性の中間接着剤4を薄く溶射し、この
上に更にセラミック材を溶射して接着力を増大させる試
みもなされてはいる。
The surface is roughened in advance by doblasting etc., and before the ceramic material is thermally sprayed, a thin inorganic intermediate adhesive 4 with good adhesion is thermally sprayed on both the base metal and the ceramic material, and then the ceramic material is further applied on top of this. Attempts have also been made to increase adhesion by thermal spraying the material.

この場合、材料の特性上セラミック材と接着剤4とは強
固に接合されて一体化しているが、接着剤とピストン1
の被着面3との接着力が充分でなく、熱衝撃により強化
層2が剥離してしまい、前記問題を充分に解決するまで
に至っていない(第9図(b)参照)。
In this case, due to the characteristics of the materials, the ceramic material and the adhesive 4 are strongly bonded and integrated, but the adhesive and the piston 1
The adhesive force with the adhered surface 3 is not sufficient, and the reinforcing layer 2 peels off due to thermal shock, and the problem has not yet been fully solved (see FIG. 9(b)).

[発明の目的] 本発明は、以上のような問題点に着目し、これを有効に
解決すべく創案されたものである。
[Object of the Invention] The present invention focuses on the above-mentioned problems and has been devised to effectively solve the problems.

本発明の目的は、セラミック材よりなる強化層の結合性
を向上させて剥離を防止することができる母材金属の強
化層形成方法を提供するにある。
An object of the present invention is to provide a method for forming a reinforcing layer of a base metal that can improve the bonding properties of a reinforcing layer made of a ceramic material and prevent peeling.

[発明の概要1 本発明は、強化層形成前の母材金属の被着面に母材金属
内に拡径された係合凹部を形成することにより接着力を
向上させることができること、特に、母材金属として紡
鉄を使用する場合には燃焼ガス化しやすいへ!粉により
容易に上記係合凹部を形成することができることに着目
してなされたものであり、母材金属内へ拡径された係合
凹部を形成した被着面に、この係合凹部を埋めるように
強化層を形成することにより接着力を高めるようにした
ことを要旨とするものである。
[Summary of the Invention 1 The present invention provides that adhesive force can be improved by forming an engagement recess with an enlarged diameter in the base metal on the adhesion surface of the base metal before forming a reinforcing layer, and in particular, When using spun iron as the base metal, it is easy to burn and gasify! This method was developed based on the fact that the above-mentioned engaging recesses can be easily formed using powder, and the engaging recesses are filled in the adherend surface on which the engaging recesses have been formed, the diameter of which is expanded into the base metal. The gist of this is that the adhesive strength is increased by forming a reinforcing layer.

[発明の実施例] 以下に、本発明方法を添付図面に基づいて詳述する。[Embodiments of the invention] The method of the present invention will be explained in detail below based on the accompanying drawings.

まず、第1実施例として第1図に示す如く行なう。すな
わち母材金属としてのピストン本体5の被着面(ピスト
ンヘッド)6に、母材金属内へ拡径させて係合凹部7を
形成する。この係合凹部7の数量は接着力との関係より
決定し、被着面6の全域にわたって均等に配置する。こ
の係合凹部7を形成するには、ピストン本体5の鋳造後
、機械加工を行なってもよいし、また鋳物型に係合凹部
7に対応する部分を設けておき、鋳造と同時に係合凹部
7を形成するようにしてもよい。
First, a first embodiment will be carried out as shown in FIG. That is, an engagement recess 7 is formed in the attachment surface (piston head) 6 of the piston body 5, which is a base metal, by expanding the diameter into the base metal. The number of the engaging recesses 7 is determined based on the relationship with the adhesive force, and the engaging recesses 7 are arranged evenly over the entire area of the adherend surface 6. To form the engagement recess 7, machining may be performed after the piston body 5 is cast, or a portion corresponding to the engagement recess 7 may be provided in the casting mold, and the engagement recess 7 may be formed at the same time as casting. 7 may be formed.

このようにして、被着面6に係合凹部7を形成したら、
次に、この被着面6の全域にわたってセラミック材など
を溶射処理し、上記係合凹部7を埋めて強化層8を形成
する。これにより、セラミック材が拡径された係合凹部
7内に流れ込んで固まり、この強化層8とピストン本体
5との接着力を向上させてこれらの結合を強固にするこ
とができる。
After forming the engagement recess 7 on the adherend surface 6 in this way,
Next, a ceramic material or the like is thermally sprayed over the entire area of the attachment surface 6 to fill the engagement recess 7 and form a reinforcing layer 8. As a result, the ceramic material flows into the engagement recess 7 whose diameter has been enlarged and hardens, thereby improving the adhesive force between the reinforcing layer 8 and the piston body 5, thereby making the connection between them stronger.

尚、上記の場合、係合凹部7の形状を断面截頭円錐状と
したが、これに限定されず上端が開口された球形状など
にしてもよい。
In the above case, the engaging recess 7 has a truncated conical cross section, but is not limited to this, and may have a spherical shape with an open upper end.

次に、第2図に基づいて第2実施例について説明する。Next, a second embodiment will be described based on FIG.

この場合には、vj造された母材金属としてのピストン
本体5の被着面6に、図示する如く所定の長さだけねじ
穴加工を施して係合凹部9を形成する。尚、この係合凹
部9の数量、深さは前述と同様に接着力との関係より適
宜決定する。
In this case, an engagement recess 9 is formed by drilling a predetermined length of a screw hole in the attachment surface 6 of the piston body 5, which is a VJ-shaped base metal, as shown in the figure. Incidentally, the number and depth of the engaging recesses 9 are determined as appropriate based on the relationship with the adhesive force, as described above.

このように、係合凹部9を形成したならば、前述の如く
次に、この被着面6の全域にわたってセラミック材など
を溶射処理し、係合凹部9を埋めて′強化層10を形成
する。これにより、ネジ穴状の係合凹部9内に流れ込ん
で固まったセラミック材がネジ山と強固に接合し、この
強化層10とピストン本体5との接着力を向上させるこ
とができる。
Once the engagement recesses 9 have been formed in this manner, as described above, next, a ceramic material or the like is thermally sprayed over the entire area of the attachment surface 6 to fill the engagement recesses 9 and form the reinforcing layer 10. . As a result, the ceramic material that has flowed into the screw hole-shaped engagement recess 9 and solidified is firmly bonded to the screw thread, thereby improving the adhesive force between the reinforcing layer 10 and the piston body 5.

特に、本実施例にあっては、ピストン本体5の被着面6
にネジ穴加工を施すことにより係合凹部9を形成できる
ので、加工が非常に容易化する。
In particular, in this embodiment, the attachment surface 6 of the piston body 5
Since the engagement recess 9 can be formed by drilling a screw hole in the screw hole, the machining is greatly facilitated.

次に第3図乃至第7図に基づいて第3実施例について説
明する。
Next, a third embodiment will be described based on FIGS. 3 to 7.

この実施例は、係合凹部の形成のためにAβ粉を巧みに
使用し、その簡単化を図ったものである。
In this embodiment, Aβ powder is cleverly used to form the engaging recesses, thereby simplifying the process.

すなわち、鋳鉄にA(粉が混在するとA(の溶融点が鋳
鉄の溶融点に比べ、極端に低いことからAI!粉は急激
に燃焼してガス化し、鋳鉄の不良要因である巣の原因と
なるが、本実施例においてはこれを逆に積極的に利用し
、ピストン本体の鋳造時に被着面に相対応する鋳物型に
少量のAi!粉を塗布形成して係合凹部を形成するもの
である。まず、第3図に示す如く、ピストン型状の鋳物
型11 (#物砂型でもよい)のピストンヘッド(被着
面)に相対応する部分全体にAβ粉12を極少量均−に
塗布形成する。この際、へβ粉をアルコールまたは水な
どの液剤と予め混合させておくことにより、容易に塗布
することができる。そして、A(粉の塗布が完了したな
らば鋳鉄などの溶融金属を流し込んで第4図に示すごと
きピストン本体5を鋳造成型する。この場合、塗布され
た金属(本実施例の場合はAl1粉)が母材金属の溶融
潟変により急激に燃焼ガス化することが必要とされるの
で、このような温疫特性を有する母材金属と塗布金属と
を選定する。
In other words, if A (powder) is mixed with cast iron, the melting point of A (A) is extremely low compared to that of cast iron, so the AI! powder will rapidly burn and gasify, causing cavities that are a cause of defects in cast iron. However, in this embodiment, this is actively utilized to the contrary, and a small amount of Ai! powder is applied to the casting mold corresponding to the surface to be adhered to when casting the piston body to form an engaging recess. First, as shown in Fig. 3, a very small amount of Aβ powder 12 is uniformly applied to the entire portion of a piston-shaped casting mold 11 (a sand mold may also be used) corresponding to the piston head (adhering surface). Coating and forming. At this time, it is possible to easily coat by pre-mixing the beta powder with a liquid agent such as alcohol or water. Metal is poured and the piston body 5 as shown in Fig. 4 is cast and molded.In this case, the applied metal (Al1 powder in this example) is rapidly combusted and gasified by the melting lag of the base metal. Therefore, a base metal and a coating metal that have such thermal characteristics are selected.

この鋳造成型により、鋳物型11に塗布されたAβ粉1
2は急激に燃焼ガス化し、第5図拡大図にも示ず如くピ
ストン本体5の被着面6に発泡層13が形成される。尚
、第5図は第4図中B部の拡大図を示す。この発泡層B
の個々の孔が母材金属内へ拡径された係合四部14を構
成することになる。この係合凹部14の深さ及び数量は
塗布するへβ粉の量により決定され、接合力との関係よ
り適宜選定する。
By this casting molding, Aβ powder 1 applied to the casting mold 11
2 is rapidly combusted and gasified, and a foam layer 13 is formed on the adhered surface 6 of the piston body 5, as shown in the enlarged view of FIG. Incidentally, FIG. 5 shows an enlarged view of section B in FIG. 4. This foam layer B
The individual holes constitute an engaging quadrant 14 that expands into the base metal. The depth and number of the engaging recesses 14 are determined by the amount of β powder to be applied, and are appropriately selected in relation to the bonding force.

このように、被着面6に係合凹部14を形成したならば
、次に、前述と同様に、第6図及び第7図に示す如く、
この被着面6の全域にわたってセラミック材を溶射処理
し、上記係合凹部14を埋めて強化層15を形成する。
Once the engagement recess 14 is formed in the adherend surface 6 in this way, next, as shown in FIGS. 6 and 7, as described above,
A ceramic material is thermally sprayed over the entire area of the attachment surface 6 to fill the engagement recess 14 and form a reinforcing layer 15 .

第7図は第6図中C部の拡大図を示す。FIG. 7 shows an enlarged view of section C in FIG. 6.

これにより、セラミック材が多数の係合凹部14内に流
れ込んで固まり、この強化層15とピストン本体5との
接着力が向上してこれらの結合を強固にすることができ
る。
As a result, the ceramic material flows into the many engagement recesses 14 and solidifies, thereby improving the adhesive force between the reinforcing layer 15 and the piston body 5, thereby making the connection between them stronger.

特に、この第3実施例においては、係合凹部14を形成
するために、ピストン本体鋳造時に/1粉を鋳物型に単
に塗布するだけでよく、前記第1及び第2実施例に比較
して係合凹部形成作業を大幅に簡略化することができる
In particular, in this third embodiment, in order to form the engagement recess 14, it is sufficient to simply apply /1 powder to the casting mold during casting of the piston body, compared to the first and second embodiments. The work of forming the engagement recess can be greatly simplified.

このように、本実施例によれば、母材金属の被着面に、
母材金属内へ拡径させて係合凹部を形成し、この被着面
に上記係合四部を埋めるように強化層を形成するように
したので係合凹部とこれに流入して固化したセラミック
材とが強固に結合し、強化層と母材金属との接着力を強
くすることができる。従って、加熱冷却の繰り返しによ
る熱衝撃によって生ずる金属と強化層との相対歪力に対
して、これを吸収するだけの十分な接着力を発揮するこ
とができ、強化層が剥離することを確実に防止すること
ができる。
In this way, according to this embodiment, on the adhesion surface of the base metal,
An engaging recess is formed by expanding the diameter into the base metal, and a reinforcing layer is formed on this adhering surface to fill the four engaging parts, so that the ceramic that flows into the engaging recess and solidifies. The reinforcing layer and the base metal can be strongly bonded to each other, and the adhesive force between the reinforcing layer and the base metal can be strengthened. Therefore, it is possible to exert sufficient adhesive strength to absorb the relative strain force between the metal and the reinforcing layer caused by thermal shock caused by repeated heating and cooling, and to ensure that the reinforcing layer does not peel off. It can be prevented.

尚、上記実施例にあっては、ピストンに強化層を形成す
る場合について説明したが、これに限定されることなく
鋳物の表面に耐熱性或いは耐摩耗性に優れたセラミック
などの強化層を形成する場合につ°いて全て適用し得る
。また、強化層の材料もセラミック材に限定されないの
は勿論である。
In the above embodiments, a case where a reinforcing layer is formed on the piston is described, but the present invention is not limited to this, and a reinforcing layer made of ceramic or the like with excellent heat resistance or wear resistance can be formed on the surface of the casting. All applicable cases are applicable. Furthermore, it goes without saying that the material of the reinforcing layer is not limited to ceramic materials.

[発明の効果] 以上数するに、本発明方法によれば、母材金属の被着面
に、母材金属内へ拡径された係合凹部を形成し、この係
合凹部を埋めるように強化層を形成するようにしたので
、母材金属と強化層との接着力を可及的に向上させるこ
とができ、従って、熱衝撃にともなって相対歪が生じて
も強化層の剥離を確実に防止することができる。
[Effects of the Invention] In summary, according to the method of the present invention, an engaging recess whose diameter is expanded into the base metal is formed on the adhering surface of the base metal, and the engaging recess is filled up. By forming a reinforcing layer, it is possible to improve the adhesion between the base metal and the reinforcing layer as much as possible. Therefore, even if relative strain occurs due to thermal shock, the reinforcing layer will not peel off. can be prevented.

【図面の簡単な説明】[Brief explanation of the drawing]

第1図乃至第7図は本発明方法を説明するための説明図
であり、特に第5図は第4図中のA部拡大図、第7図は
第6図中のC部拡大図、第8図は強化層の形成されたピ
ストンを示す平面図、第9図乃至第11図は従来の強化
層形成方法を説明するだめの説明図である。 尚、図中5は鋳物型、6は結合性向上物、8は母材金属
としてのピストン本体、9は被着面、10は強化層であ
る。 手続谷Ij ilミー)(/ノエい 昭和598110月17日 特許庁長官 志 賀 学 殿 1、事件の表示 特願昭59−86696シJ2、発明
の名称 母材金属の強化層形成方法3、補正をJる者 事件どの関係 特許出願人 (017) い1ず自動中株式会社 4、代理人 郵便番号 105 東京都港区愛宕1丁目6番7号 5、補正命令の日付 昭和59年7月31日 (発送日) 6、補正の対象 明細書(図面の簡単な説明の欄)及び図面7、補正の内
容 (1) 明細書10頁11行〜19行「第1図・・・・
・・10は強化層である。」を[第1図乃至第7図は本
発明の詳細な説明するための説明図(・あり、9、′I
に第5図は第4図中のB部拡大図、第7図は第6図中の
C部1]ム人図、第8図は従来り法により強化層の形成
されたビスI〜ンを示す平面図、第9図は第8図中のA
部を示J拡人図(゛ある。。 尚、図中5)はfす材金属としてのピストン本体、6は
被着面、7.9.14は係合凹部、8,10.15は強
化層である。」と八Jiに。 【2)別紙のごとく適iF ’、に図面を提出づる。、
(但し、内容は変更けf) 8、添付書類の目録 (1)図 面 1通
1 to 7 are explanatory diagrams for explaining the method of the present invention, in particular, FIG. 5 is an enlarged view of section A in FIG. 4, FIG. 7 is an enlarged view of section C in FIG. FIG. 8 is a plan view showing a piston on which a reinforcing layer is formed, and FIGS. 9 to 11 are explanatory diagrams for explaining a conventional method for forming a reinforcing layer. In the figure, 5 is a casting mold, 6 is a bonding property improver, 8 is a piston body as a base metal, 9 is an adhering surface, and 10 is a reinforcing layer. October 17, 1981 Manabu Shiga, Commissioner of the Patent Office 1, Indication of the case Patent application 1986-86696 J2, Title of the invention Method for forming a reinforcing layer of base metal 3, Amendment Patent applicant (017) I1zu Jidochu Co., Ltd. 4, Agent postal code 105 1-6-7-5 Atago, Minato-ku, Tokyo Date of amendment order July 31, 1980 Date (shipment date) 6. Specification to be amended (column for brief description of drawings) and Drawing 7. Contents of amendment (1) Page 10 of the specification, lines 11 to 19 "Figure 1...
...10 is a reinforcement layer. ” [Figures 1 to 7 are explanatory diagrams for explaining the present invention in detail (・Yes, 9, 'I
Fig. 5 is an enlarged view of part B in Fig. 4, Fig. 7 is an enlarged view of part C in Fig. 6, and Fig. 8 is an enlarged view of part C in Fig. 6. 9 is a plan view showing A in FIG. 8.
The enlarged view (5 in the figure) shows the piston body as metal, 6 is the attachment surface, 7.9.14 is the engagement recess, and 8 and 10.15 are the piston body. It is a reinforcement layer. ” to Yaji. [2] Submit the drawings to the appropriate iF' as shown in the attached sheet. ,
(However, please change the contents.) 8. List of attached documents (1) 1 copy of drawings

Claims (1)

【特許請求の範囲】[Claims] 母材金属にセラミック材等の強化層を形成するに際して
、上記母材金属の被着面に、母材金・肩肉に拡径させて
係合凹部を形成し、次いで、上i[!m母材金属被着面
に、上記係合凹部を埋めるように上記強化層を形成づる
ようにしたことを特徴とする母材金属の強化層形成方法
When forming a reinforcing layer of ceramic material or the like on the base metal, an engaging recess is formed on the adhering surface of the base metal by expanding the diameter of the base metal shoulder, and then the upper i[! (m) A method for forming a reinforcing layer on a base metal, characterized in that the reinforcing layer is formed on a surface to which the base metal is adhered so as to fill the engagement recess.
JP8669684A 1984-04-28 1984-04-28 Formation of reinforcing layer on base metal Pending JPS60230975A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP8669684A JPS60230975A (en) 1984-04-28 1984-04-28 Formation of reinforcing layer on base metal

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP8669684A JPS60230975A (en) 1984-04-28 1984-04-28 Formation of reinforcing layer on base metal

Publications (1)

Publication Number Publication Date
JPS60230975A true JPS60230975A (en) 1985-11-16

Family

ID=13894117

Family Applications (1)

Application Number Title Priority Date Filing Date
JP8669684A Pending JPS60230975A (en) 1984-04-28 1984-04-28 Formation of reinforcing layer on base metal

Country Status (1)

Country Link
JP (1) JPS60230975A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0899053A2 (en) * 1997-08-29 1999-03-03 Sintokogio Ltd. A plated product and a method and apparatus for producing the same
CN103381539A (en) * 2012-05-01 2013-11-06 福特全球技术公司 Cylinder bore with selective surface treatment and method of making the same
US10221806B2 (en) 2012-05-01 2019-03-05 Ford Global Technologies, Llc Cylindrical engine bore
US10220453B2 (en) 2015-10-30 2019-03-05 Ford Motor Company Milling tool with insert compensation

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0899053A2 (en) * 1997-08-29 1999-03-03 Sintokogio Ltd. A plated product and a method and apparatus for producing the same
EP0899053A3 (en) * 1997-08-29 2000-04-05 Sintokogio Ltd. A plated product and a method and apparatus for producing the same
CN103381539A (en) * 2012-05-01 2013-11-06 福特全球技术公司 Cylinder bore with selective surface treatment and method of making the same
US10221806B2 (en) 2012-05-01 2019-03-05 Ford Global Technologies, Llc Cylindrical engine bore
US10220453B2 (en) 2015-10-30 2019-03-05 Ford Motor Company Milling tool with insert compensation

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