JPS6332130Y2 - - Google Patents
Info
- Publication number
- JPS6332130Y2 JPS6332130Y2 JP1981130213U JP13021381U JPS6332130Y2 JP S6332130 Y2 JPS6332130 Y2 JP S6332130Y2 JP 1981130213 U JP1981130213 U JP 1981130213U JP 13021381 U JP13021381 U JP 13021381U JP S6332130 Y2 JPS6332130 Y2 JP S6332130Y2
- Authority
- JP
- Japan
- Prior art keywords
- base material
- silicon
- aluminum alloy
- sprayed
- hard metal
- 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
Links
- 239000000463 material Substances 0.000 claims description 32
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 claims description 31
- 229910052710 silicon Inorganic materials 0.000 claims description 31
- 239000010703 silicon Substances 0.000 claims description 31
- 229910052751 metal Inorganic materials 0.000 claims description 28
- 239000002184 metal Substances 0.000 claims description 28
- 229910000838 Al alloy Inorganic materials 0.000 claims description 20
- 238000002485 combustion reaction Methods 0.000 claims description 6
- 239000011856 silicon-based particle Substances 0.000 claims 1
- ZOKXTWBITQBERF-UHFFFAOYSA-N Molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 description 7
- 239000010410 layer Substances 0.000 description 7
- 229910052750 molybdenum Inorganic materials 0.000 description 7
- 239000011733 molybdenum Substances 0.000 description 7
- 229910001182 Mo alloy Inorganic materials 0.000 description 4
- 229910052782 aluminium Inorganic materials 0.000 description 4
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 4
- 238000000034 method Methods 0.000 description 4
- 238000005507 spraying Methods 0.000 description 4
- 238000000576 coating method Methods 0.000 description 3
- 239000013078 crystal Substances 0.000 description 3
- 238000010586 diagram Methods 0.000 description 3
- NLXLAEXVIDQMFP-UHFFFAOYSA-N Ammonia chloride Chemical compound [NH4+].[Cl-] NLXLAEXVIDQMFP-UHFFFAOYSA-N 0.000 description 2
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 2
- FAPWRFPIFSIZLT-UHFFFAOYSA-M Sodium chloride Chemical compound [Na+].[Cl-] FAPWRFPIFSIZLT-UHFFFAOYSA-M 0.000 description 2
- 239000011248 coating agent Substances 0.000 description 2
- JEIPFZHSYJVQDO-UHFFFAOYSA-N iron(III) oxide Inorganic materials O=[Fe]O[Fe]=O JEIPFZHSYJVQDO-UHFFFAOYSA-N 0.000 description 2
- 150000002739 metals Chemical class 0.000 description 2
- 239000002245 particle Substances 0.000 description 2
- 239000007921 spray Substances 0.000 description 2
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 1
- 229910000975 Carbon steel Inorganic materials 0.000 description 1
- 235000019270 ammonium chloride Nutrition 0.000 description 1
- 238000007743 anodising Methods 0.000 description 1
- 239000010953 base metal Substances 0.000 description 1
- 239000010962 carbon steel Substances 0.000 description 1
- 239000011247 coating layer Substances 0.000 description 1
- 238000005238 degreasing Methods 0.000 description 1
- 238000004070 electrodeposition Methods 0.000 description 1
- 229910002804 graphite Inorganic materials 0.000 description 1
- 239000010439 graphite Substances 0.000 description 1
- 229910052742 iron Inorganic materials 0.000 description 1
- 230000001788 irregular Effects 0.000 description 1
- -1 molybdenum Chemical class 0.000 description 1
- 238000007747 plating Methods 0.000 description 1
- 229920001296 polysiloxane Polymers 0.000 description 1
- 230000000717 retained effect Effects 0.000 description 1
- 150000003839 salts Chemical class 0.000 description 1
- 238000005480 shot peening Methods 0.000 description 1
- 239000011780 sodium chloride 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
- 238000004506 ultrasonic cleaning Methods 0.000 description 1
Landscapes
- Cylinder Crankcases Of Internal Combustion Engines (AREA)
- Coating By Spraying Or Casting (AREA)
Description
この考案は、内燃機関における、たとえばシリ
ンダライナーの摺接部分の耐摩耗性の向上を図る
ために、シリンダライナーの摺接面にモリブデン
もしくはモリブデン合金、または他の硬質金属を
溶射した場合に、密着強度を増大させてなる内燃
機関のアルミニウム合金製摺動部品に関するもの
である。
エンジンの軽量化を図るために、シリンダブロ
ツクやシリンダライナーを、高シリコンを含有し
たアルミ合金によつて製作しているが、耐摩耗性
に問題があるため、すぐれた耐摩耗性を確保する
ために、特開昭52−113415号によつて、高シリコ
ンを含有したアルミ合金製母材の摺動面に、シリ
コンを浸蝕することのないメツキの前処理を施
し、しかるのちシリコンの周囲のアルミニウム地
を浸蝕して除去するとともに、シリコンの結晶を
残溜保存し、つぎに浸蝕アルミニウム地に対して
鉛を電着もしくは溶射させて充填し、この鉛表面
を上記シリコンの表面に一致させるようにしたも
の、つまり、アルミニウム地よりも耐摩耗に対し
て安定的なシリコンの結晶体粒子を、摺動面に均
等分布させて耐摩耗性の向上を図るようにしたも
のが提案されている。
しかしながら、上記提案によつて得られる程度
の耐摩耗性では、シリンダライナーのような苛酷
な使用条件にさらされる部分にとつて満足なもの
ではない。
したがつて、たとえば第3図のように高シリコ
ン12を含有するアルミ合金母材10の摺動部
に、モリブデン11もしくはモリブデン合金、ま
たは他の硬質金属を溶射する手段が知られてい
る。
上記モリブデン11もしくはモリブデン合金、
または他の硬質金属を溶射するために、シリンダ
ライナーなどの摺接面を脱脂、除錆などの処理と
ともに清浄にし、アルミ合金母材10に対する溶
射金属の密着度を高めているけれど、実際上は、
密着強度が不充分なため、モリブデンなどの溶射
金属がアルミニウム合金母材の表面から脱落する
欠点がある。
一方、溶射金属の密着力を増大して、母材表面
からの脱落を防止するようにしたものは、すでに
実公昭43−7922号によつて黒鉛を有する鉄系金属
母材の表面の黒鉛を選択除去して、その上方に硬
質金属を溶射して表層を形成するようにした内燃
機関用摺動部品が知られている。
しかしながら、上記のものは、母材が黒鉛を含
有した鉄系のものであり、現状のように高シリコ
ンを含有したアルミニウム合金を母材とするシリ
ンダライナーなどの摺動部品には全く適用し得な
いものである。
考案者らは、高シリコンを含有したアルミニウ
ム合金母材中のシリコン結晶粒子が、モリブデン
などの硬質金属の密着力を低減させている要因で
あるとの結論を得るに至り、密着力低下の本質を
究明した。
即ち、高シリコンを含有するアルミニウム合金
母材に、モリブデンもしくはモリブデン合金、ま
たは他の硬質金属を溶射すると、シリコンの存在
する部分がポーラス状になつて、溶射金属が密着
し難くなり、溶射層が脱落する問題を生じる。
この考案は、上記の問題に鑑みなされたもの
で、高シリコンを含有するアルミニウム合金母材
に対して、硬質金属からなる溶射層の密着強度を
増大させた内燃機関のアルミニウム製摺動部品を
提供することを目的とする。
この考案の特徴とするところは、第1図に示す
ごとく、高シリコン3を含有するアルミニウム合
金製母材1の表面から、シリコン3を除去して、
硬質金属2と母材1の密着強度を増大させた点に
ある。
高シリコン3を含有するアルミニウム合金製母
材1に硬質金属を溶射する場合、その密着強度を
低下させているものは、表面に存在するシリコン
1そのものであり、脱脂、除錆などの表面処理が
不完全である場合は、密着強度が低下するけれ
ど、アルミニウム合金製母材1に本質的に存在す
るシリコン3は、溶射被覆層、つまり硬質金属2
との密着力が弱い。
この考案は、これらの本質的な欠点を有するシ
リコン3を母材1の表面から除去して、溶射金属
(硬質金属2)との結合力を向上させるとともに、
シリコン3が除去されることによつて、その表面
に不規則な凹部が形成され、表面積が増加して溶
射金属との接触面積が増大し、密着力が強大とな
る。のみならず、凹部Pへ溶射金属が進入して、
機械的結合も強化されるので、従来の溶射被覆と
比較して、きわめて強固な密着強度を有する硬質
金属2の溶射被覆が形成される。
アルミニウム合金製母材1の表面のシリコン3
を除去する手段としては、たとえば、塩化ナトリ
ウム、塩化アンモニウムを主体として、溶融塩で
陽極処理ないしはシヨツトピーニングを施し、フ
アインクリーナ210の超音波洗浄によつて容易
にシリコン3を選択除去し得る。
上記硬質金属2は、線爆溶射によつて行われ、
その材質はモリブデンと0.8%炭素鋼の交互溶射
により層厚120μに設定している。
高シリコンを含有するアルミニウム合金製母材
1の表面におけるシリコン量に対応する溶射層の
密着強さ、および引張強さのテスト結果を第2図
に示しており、図面において明らかなように、シ
リコン3の含有量が低い場合において密着強さお
よび引張り強さは著しく増大する。
また、アルミニウム合金製母材1のシリコン除
去前と除去後における密着力の比較、およびその
場合のシリコン除去方法を表1に示す。表2は、
上記表1に示したシリコン除去方法の種類を表示
した符号に対応する処理内容を示している。
In order to improve the wear resistance of the sliding contact area of a cylinder liner in an internal combustion engine, for example, when molybdenum, molybdenum alloy, or other hard metal is sprayed on the sliding contact surface of the cylinder liner, it will cause a close contact. This invention relates to aluminum alloy sliding parts for internal combustion engines with increased strength. In order to reduce the weight of the engine, the cylinder block and cylinder liner are made of aluminum alloy containing high silicone, but this has problems with wear resistance, so we have to ensure excellent wear resistance. According to Japanese Patent Application Laid-Open No. 52-113415, the sliding surface of an aluminum alloy base material containing a high silicon content is pretreated with plating that does not corrode the silicon, and then the aluminum surrounding the silicon is coated. At the same time, the base is eroded and removed, and the silicon crystals are retained and preserved. Next, the eroded aluminum base is filled with lead by electrodeposition or thermal spraying, so that the lead surface matches the silicon surface. In other words, a method has been proposed in which silicon crystal particles, which are more stable in terms of wear resistance than aluminum base, are evenly distributed on the sliding surface to improve wear resistance. However, the level of wear resistance obtained by the above proposal is not satisfactory for parts such as cylinder liners that are exposed to severe usage conditions. Therefore, it is known to spray molybdenum 11, a molybdenum alloy, or other hard metal onto the sliding portion of an aluminum alloy base material 10 containing high silicon 12, as shown in FIG. 3, for example. The above molybdenum 11 or molybdenum alloy,
In order to thermally spray other hard metals, sliding contact surfaces such as cylinder liners are degreased, rust removed and cleaned to increase the adhesion of the thermally sprayed metal to the aluminum alloy base material 10. ,
Due to insufficient adhesion strength, there is a drawback that the sprayed metal such as molybdenum falls off from the surface of the aluminum alloy base material. On the other hand, a method that increases the adhesion of thermal sprayed metal to prevent it from falling off from the surface of the base material has already been reported in Utility Model Publication No. 7922/1973, which has been developed to increase the adhesion of the sprayed metal to prevent it from falling off from the surface of the base metal. A sliding component for an internal combustion engine is known in which a surface layer is formed by selectively removing the material and then thermally spraying a hard metal onto the surface. However, the above materials are iron-based base materials containing graphite, and cannot be applied to sliding parts such as cylinder liners whose base materials are aluminum alloys containing high silicon content. It's something that doesn't exist. The inventors came to the conclusion that silicon crystal particles in the aluminum alloy base material containing high silicon content were the cause of reducing the adhesion of hard metals such as molybdenum, and discovered the essence of the reduction in adhesion. was investigated. In other words, when molybdenum, a molybdenum alloy, or other hard metal is sprayed onto an aluminum alloy base material containing high silicon content, the portion where silicon is present becomes porous, making it difficult for the sprayed metal to adhere to the base material and causing the sprayed layer to deteriorate. This creates a problem of shedding. This idea was developed in view of the above problems, and provides aluminum sliding parts for internal combustion engines in which the adhesion strength of a sprayed layer made of hard metal to an aluminum alloy base material containing high silicon content is increased. The purpose is to The feature of this invention is that, as shown in FIG. 1, silicon 3 is removed from the surface of an aluminum alloy base material 1 containing a high silicon 3 content.
The point is that the adhesion strength between the hard metal 2 and the base material 1 is increased. When a hard metal is thermally sprayed onto an aluminum alloy base material 1 containing high silicon 3, it is the silicon 1 itself present on the surface that reduces the adhesion strength, and surface treatments such as degreasing and rust removal are necessary. If it is incomplete, the adhesion strength will be reduced, but the silicon 3 that is essentially present in the aluminum alloy base material 1 can be used as a thermal spray coating layer, that is, a hard metal 2.
The adhesion is weak. This invention removes the silicon 3, which has these essential drawbacks, from the surface of the base material 1 to improve the bonding strength with the sprayed metal (hard metal 2), and
By removing the silicon 3, irregular recesses are formed on its surface, increasing the surface area, increasing the contact area with the sprayed metal, and increasing the adhesion. Not only that, the sprayed metal enters the recess P,
Since the mechanical bond is also strengthened, a thermally sprayed coating of the hard metal 2 is formed which has extremely strong adhesion strength compared to conventional thermally sprayed coatings. Silicon 3 on the surface of aluminum alloy base material 1
For example, the silicon 3 can be easily selectively removed by anodizing or shot peening with a molten salt mainly containing sodium chloride or ammonium chloride, and by ultrasonic cleaning with the fine cleaner 210. . The hard metal 2 is formed by wire bombardment spraying,
The material is alternately sprayed with molybdenum and 0.8% carbon steel, with a layer thickness of 120μ. Figure 2 shows the test results of the adhesion strength and tensile strength of the sprayed layer corresponding to the amount of silicon on the surface of the aluminum alloy base material 1 containing high silicon content. The adhesion strength and tensile strength increase significantly when the content of 3 is low. Further, Table 1 shows a comparison of the adhesion strength of the aluminum alloy base material 1 before and after silicon removal, and the silicon removal method in that case. Table 2 is
The processing contents corresponding to the symbols indicating the types of silicon removal methods shown in Table 1 above are shown.
【表】【table】
【表】【table】
【表】
上記表1からも明らかなように、シリコン量を
少なくすることで密着強度が著しく向上する。
本考案は以上述べたように、母材と溶射硬質金
属との接触面積を増大させるだけでなく、母材と
溶射硬質金属との結合力を向上させ、且つ各凹部
の形状により溶射硬質金属からなる溶射層を母材
に対して機械的に強固に保持できることから、母
材に対する溶射層の密着強度を大幅に向上させる
ことができる。[Table] As is clear from Table 1 above, adhesion strength is significantly improved by reducing the amount of silicon. As described above, the present invention not only increases the contact area between the base material and the sprayed hard metal, but also improves the bonding force between the base material and the sprayed hard metal, and the shape of each recess allows the sprayed hard metal to be removed from the sprayed hard metal. Since the sprayed layer can be mechanically firmly held against the base material, the adhesion strength of the sprayed layer to the base material can be significantly improved.
第1図はこの考案に係る溶射被覆の概念説明
図、第2図は母材表面のシリコン量に対応する溶
射層の密着強さおよび引張強さのテスト結果を示
す線図、第3図は従来の溶射被覆の概念説明図で
ある。
1……アルミニウム合金製母材、2……硬質金
属、3……シリコン。
Figure 1 is a conceptual explanatory diagram of the sprayed coating according to this invention, Figure 2 is a diagram showing the test results of the adhesion strength and tensile strength of the sprayed layer corresponding to the amount of silicon on the surface of the base material, and Figure 3 is It is a conceptual explanatory diagram of a conventional thermal spray coating. 1... Aluminum alloy base material, 2... Hard metal, 3... Silicon.
Claims (1)
製である内燃機関のアルミニウム合金製摺動部品
において、 前記母材の表面には、該母材の表面のシリコン
粒子が選択除去されて分散した多数の凹部が設け
られ、且つ該各凹部に溶射硬質金属が充填されて
いると共に該母材の表面が該溶射硬質金属で被覆
されている溶射層が設けられている、 ことを特徴とする内燃機関のアルミニウム合金製
摺動部品。[Claims for Utility Model Registration] In an aluminum alloy sliding part for an internal combustion engine in which the base material is made of an aluminum alloy containing high silicon, the surface of the base material includes selected silicon particles on the surface of the base material. A sprayed layer is provided in which a large number of removed and dispersed recesses are provided, each of the recesses is filled with a thermally sprayed hard metal, and the surface of the base material is coated with the thermally sprayed hard metal. Aluminum alloy sliding parts for internal combustion engines featuring:
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP1981130213U JPS5835644U (en) | 1981-08-31 | 1981-08-31 | Aluminum alloy sliding parts for internal combustion engines |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP1981130213U JPS5835644U (en) | 1981-08-31 | 1981-08-31 | Aluminum alloy sliding parts for internal combustion engines |
Publications (2)
Publication Number | Publication Date |
---|---|
JPS5835644U JPS5835644U (en) | 1983-03-08 |
JPS6332130Y2 true JPS6332130Y2 (en) | 1988-08-26 |
Family
ID=29923854
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP1981130213U Granted JPS5835644U (en) | 1981-08-31 | 1981-08-31 | Aluminum alloy sliding parts for internal combustion engines |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPS5835644U (en) |
Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS508693A (en) * | 1973-05-22 | 1975-01-29 | ||
JPS52123339A (en) * | 1976-04-09 | 1977-10-17 | Kawasaki Heavy Ind Ltd | Method of spraying metal to cylinder or piston |
-
1981
- 1981-08-31 JP JP1981130213U patent/JPS5835644U/en active Granted
Patent Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS508693A (en) * | 1973-05-22 | 1975-01-29 | ||
JPS52123339A (en) * | 1976-04-09 | 1977-10-17 | Kawasaki Heavy Ind Ltd | Method of spraying metal to cylinder or piston |
Also Published As
Publication number | Publication date |
---|---|
JPS5835644U (en) | 1983-03-08 |
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