JPH017721Y2 - - Google Patents
Info
- Publication number
- JPH017721Y2 JPH017721Y2 JP11674880U JP11674880U JPH017721Y2 JP H017721 Y2 JPH017721 Y2 JP H017721Y2 JP 11674880 U JP11674880 U JP 11674880U JP 11674880 U JP11674880 U JP 11674880U JP H017721 Y2 JPH017721 Y2 JP H017721Y2
- Authority
- JP
- Japan
- Prior art keywords
- liner body
- resistant layer
- temperature wear
- carbide
- liner
- 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
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 claims description 6
- 238000002485 combustion reaction Methods 0.000 claims description 6
- 229910001018 Cast iron Inorganic materials 0.000 claims description 3
- 229910017709 Ni Co Inorganic materials 0.000 claims description 2
- 229910003267 Ni-Co Inorganic materials 0.000 claims description 2
- 229910003262 Ni‐Co Inorganic materials 0.000 claims description 2
- 229910018487 Ni—Cr Inorganic materials 0.000 claims description 2
- 239000000203 mixture Substances 0.000 claims 1
- 238000007750 plasma spraying Methods 0.000 claims 1
- 238000001816 cooling Methods 0.000 description 5
- 239000000463 material Substances 0.000 description 5
- 238000005299 abrasion Methods 0.000 description 3
- UFGZSIPAQKLCGR-UHFFFAOYSA-N chromium carbide Chemical compound [Cr]#C[Cr]C#[Cr] UFGZSIPAQKLCGR-UHFFFAOYSA-N 0.000 description 3
- 238000010586 diagram Methods 0.000 description 3
- 238000005507 spraying Methods 0.000 description 3
- 229910003470 tongbaite Inorganic materials 0.000 description 3
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 2
- 238000010438 heat treatment Methods 0.000 description 2
- 238000005461 lubrication Methods 0.000 description 2
- 239000011148 porous material Substances 0.000 description 2
- MTPVUVINMAGMJL-UHFFFAOYSA-N trimethyl(1,1,2,2,2-pentafluoroethyl)silane Chemical compound C[Si](C)(C)C(F)(F)C(F)(F)F MTPVUVINMAGMJL-UHFFFAOYSA-N 0.000 description 2
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 2
- PNEYBMLMFCGWSK-UHFFFAOYSA-N aluminium oxide Inorganic materials [O-2].[O-2].[O-2].[Al+3].[Al+3] PNEYBMLMFCGWSK-UHFFFAOYSA-N 0.000 description 1
- 239000000498 cooling water Substances 0.000 description 1
- 229910052742 iron Inorganic materials 0.000 description 1
- 239000003921 oil Substances 0.000 description 1
- 238000007747 plating Methods 0.000 description 1
- 230000005855 radiation Effects 0.000 description 1
- HBMJWWWQQXIZIP-UHFFFAOYSA-N silicon carbide Chemical compound [Si+]#[C-] HBMJWWWQQXIZIP-UHFFFAOYSA-N 0.000 description 1
- 229910010271 silicon carbide Inorganic materials 0.000 description 1
Description
この考案はデイゼルエンジンのような内燃機関
のシリンダライナに関する。
従来のデイゼルエンジンなどの内燃機関では、
シリンダライナの外周面を冷却水などにより冷却
することにより、シリンダライナが高熱となるの
を防止している。このため燃焼エネルギの約3分
の1は上記冷却による放熱により失なわれ、出力
の低下を招ねいている。
この考案はかかる事情に鑑みてなされたもで、
ライナ本体の表面にクロームカーバイドを溶射し
て耐熱性を向上させた内燃機関のシリンダライナ
を提供して、冷却による熱損失を低減し、熱効率
を高めることにより内燃機関の出力向上を図ろう
とするものである。
以下この考案を図示の一実施例について詳述す
る。図において1は鋳鉄製のライナ本体で、高温
耐摩耗性を向上させるために内面にクロームカー
バイドが溶射されて高温耐摩耗層2が形成されて
いる。上記高温耐摩耗層2を形成するには60〜90
重量%のクロームカーバイドと残部Ni−Crまた
はNi−CoもしくはCoを適宜混合し、これをライ
ナ本体1にプラズマ溶射すると共に、その後溶射
部を3μ以下に仕上げ加工するもので、得られる
高温耐摩耗層2は硬度がHmv350〜700である。
またクロームカーバイドの量は75重量%がもつと
も好ましが60〜90%の範囲でよい結果が得られ
る。60%以下では耐摩耗性が低下し、また90%以
上では皮膜の結合度が弱いため、耐摩耗性が劣化
する。
一方クロームカーバイドを溶射することによつ
て高温耐摩耗層2に多数の微細な気孔ができ、こ
れら気孔が油溜りとなつて潤滑に寄与するので高
温下でも潤滑性能は低下することがない。
次に上記により得られたライナ本体1の耐摩耗
テスト及び耐焼付きテストの結果を説明する。
はじめに耐摩耗性テストについて第2図に示す
ように密閉構造の加熱炉3内に試験すべきライナ
本体1を回転自在に取付け、このライナ本体1に
一端側に重錘4を垂下したテコ5によりリング材
6を圧接する。リング材6は鉄系材料にチタンカ
ーバイドメツキを施したもので、上記加熱炉3内
を450℃の雰囲気に維持しながら、ライナ本体1
を毎秒1mの早さで回転させて試験を行つた。そ
の結果クロームカーバイド2の摩耗は下記の表の
通りであつた。比較のために鋳鉄、硬質クローム
メツキを施したもの及びアルミナを溶射したもの
についても同様な試験を行つたところ、結果は下
記の表の通りであつた。
This invention relates to cylinder liners for internal combustion engines such as diesel engines. In internal combustion engines such as conventional diesel engines,
By cooling the outer circumferential surface of the cylinder liner with cooling water or the like, the cylinder liner is prevented from becoming extremely hot. For this reason, about one-third of the combustion energy is lost due to heat radiation due to the cooling, resulting in a decrease in output. This idea was made in view of these circumstances,
Provides a cylinder liner for internal combustion engines that has improved heat resistance by thermally spraying chrome carbide on the surface of the liner body, thereby reducing heat loss due to cooling and increasing thermal efficiency, thereby increasing the output of internal combustion engines. It is. This invention will be described in detail below with reference to an illustrated embodiment. In the figure, reference numeral 1 denotes a liner body made of cast iron, and in order to improve high-temperature wear resistance, chrome carbide is thermally sprayed on the inner surface to form a high-temperature wear-resistant layer 2. 60 to 90 to form the above high temperature wear-resistant layer 2
% by weight of chromium carbide and the balance Ni-Cr or Ni-Co or Co are appropriately mixed, this is plasma sprayed onto the liner body 1, and the sprayed area is then finished to a thickness of 3μ or less, resulting in high-temperature wear resistance. Layer 2 has a hardness of Hmv350-700.
The amount of chromium carbide is preferably 75% by weight, but good results can be obtained when it is preferably in the range of 60 to 90%. If it is less than 60%, the abrasion resistance will decrease, and if it is more than 90%, the degree of bonding of the film will be weak, so the abrasion resistance will deteriorate. On the other hand, by spraying chromium carbide, a large number of fine pores are formed in the high-temperature wear-resistant layer 2, and these pores become oil reservoirs and contribute to lubrication, so that the lubrication performance does not deteriorate even at high temperatures. Next, the results of the wear resistance test and seizure resistance test of the liner body 1 obtained above will be explained. First, regarding the abrasion resistance test, as shown in Fig. 2, the liner body 1 to be tested is rotatably mounted in a heating furnace 3 with a closed structure, and a lever 5 with a weight 4 hanging from one end of the liner body 1 is used. The ring material 6 is pressed. The ring material 6 is made of iron-based material plated with titanium carbide, and the liner body 1 is heated while maintaining the inside of the heating furnace 3 at a temperature of 450°C.
The test was conducted by rotating at a speed of 1 m per second. As a result, the wear of chrome carbide 2 was as shown in the table below. For comparison, similar tests were conducted on cast iron, hard chrome-plated materials, and alumina-sprayed materials, and the results were as shown in the table below.
【表】
次に耐焼付きテストを説明すると、ライナ本体
1と同条件で高温耐摩耗層2を形成した円板状の
試料を第3図に示すように固定部材7に取付け、
これにピストンリングを想定してチタンカーバイ
ドを0.3mmの厚さに溶射し、かつ表面を1.5〜2μの
粗さに仕上げた摺動部材8を回転体9に取付け
て、上記試料に圧接させながら毎秒8mの早さで
回転させ、摺動部には給油した。
また回転体9の回転に伴う摺動部の摩擦トルク
を第4図に示すようにしてロードセル10で測定
した。その結果は第5図aに示す通りであつた。
同様にしてアルミナ溶射の試料b,c硬質クロー
ムメツキの試料d及びシリコンカーバイド焼付体
eについても試験をした結果、第5図bないしe
に示す通りであり、高温耐摩耗層2を設けたこの
考案のものがもつとも優れていることが明らかと
なつた。
この考案は以上許述したようにライナ本体の内
面にクロームカーバイドを溶射して高温耐摩耗層
を形成したことから、耐摩耗性、耐焼付性が飛躍
的に向上すると共に、十分高温に耐え得ることか
ら、水による冷却を必要としないシリンダライナ
が得られるようになる。これによつて水による冷
却によつて生じる熱損失を低減することができる
と同時に熱効率の向上によりエンジン出力の増大
が図れるようになる。[Table] Next, to explain the seizure resistance test, a disk-shaped sample on which a high-temperature wear-resistant layer 2 was formed under the same conditions as the liner body 1 was attached to the fixing member 7 as shown in FIG.
A sliding member 8, which is assumed to be a piston ring, is sprayed with titanium carbide to a thickness of 0.3 mm and has a surface roughened to a roughness of 1.5 to 2 μm.The sliding member 8 is attached to the rotating body 9, and is brought into pressure contact with the sample. It was rotated at a speed of 8 m/s, and the sliding parts were lubricated. Further, the friction torque of the sliding portion due to the rotation of the rotating body 9 was measured using a load cell 10 as shown in FIG. The results were as shown in Figure 5a.
Similarly, alumina sprayed samples b and c, hard chrome plating sample d, and silicon carbide baked body e were tested, and the results were shown in Figures 5 b to e.
As shown in FIG. 2, it has become clear that this invention provided with the high-temperature wear-resistant layer 2 is extremely superior. As mentioned above, this idea forms a high-temperature wear-resistant layer by thermally spraying chrome carbide on the inner surface of the liner body, which dramatically improves wear resistance and seizure resistance, as well as being able to withstand high temperatures. Therefore, a cylinder liner that does not require water cooling can be obtained. This makes it possible to reduce heat loss caused by water cooling, and at the same time, increase engine output by improving thermal efficiency.
図面はこの考案の一実施例を示し、第1図は一
部を拡大したシリンダライナの断面図、第2図は
摩耗テストの説明図、第3図及び第4図は耐焼付
テストの説明図、第5図は焼付きテストの結果を
示す線図である。
1はライナ本体、2は高温耐摩耗層。
The drawings show one embodiment of this invention; Fig. 1 is a partially enlarged sectional view of a cylinder liner, Fig. 2 is an explanatory diagram of a wear test, and Figs. 3 and 4 are explanatory diagrams of a seizure resistance test. , FIG. 5 is a diagram showing the results of the burn-in test. 1 is the liner body, 2 is the high temperature wear resistant layer.
Claims (1)
Ni−CrまたはNi−CoもしくはCoを混合して、こ
れを鋳鉄製ライナ本体1の内面にプラズマ溶射す
ることにより、ライナ本体1の内面に高温耐摩耗
層2を形成してなる内燃機関のシリンダライナ。 From 60% to 90% chrome carbide by weight%
A cylinder for an internal combustion engine in which a high-temperature wear-resistant layer 2 is formed on the inner surface of the liner body 1 by mixing Ni-Cr, Ni-Co, or Co and plasma spraying the mixture on the inner surface of the liner body 1 made of cast iron. Raina.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP11674880U JPH017721Y2 (en) | 1980-08-20 | 1980-08-20 |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP11674880U JPH017721Y2 (en) | 1980-08-20 | 1980-08-20 |
Publications (2)
Publication Number | Publication Date |
---|---|
JPS5740638U JPS5740638U (en) | 1982-03-04 |
JPH017721Y2 true JPH017721Y2 (en) | 1989-03-01 |
Family
ID=29477570
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP11674880U Expired JPH017721Y2 (en) | 1980-08-20 | 1980-08-20 |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPH017721Y2 (en) |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS62296699A (en) * | 1986-06-17 | 1987-12-23 | Matsushita Electric Ind Co Ltd | Low magnetism leak speaker |
WO2019224861A1 (en) * | 2018-05-21 | 2019-11-28 | Tpr株式会社 | Cylinder liner and method for manufacturing same |
-
1980
- 1980-08-20 JP JP11674880U patent/JPH017721Y2/ja not_active Expired
Also Published As
Publication number | Publication date |
---|---|
JPS5740638U (en) | 1982-03-04 |
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