JPH0151538B2 - - Google Patents
Info
- Publication number
- JPH0151538B2 JPH0151538B2 JP18627684A JP18627684A JPH0151538B2 JP H0151538 B2 JPH0151538 B2 JP H0151538B2 JP 18627684 A JP18627684 A JP 18627684A JP 18627684 A JP18627684 A JP 18627684A JP H0151538 B2 JPH0151538 B2 JP H0151538B2
- Authority
- JP
- Japan
- Prior art keywords
- pores
- wear
- sintered
- present
- comparative example
- 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 59
- 239000011148 porous material Substances 0.000 claims description 34
- 239000000956 alloy Substances 0.000 claims description 18
- 229910045601 alloy Inorganic materials 0.000 claims description 16
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 claims description 12
- 229910052698 phosphorus Inorganic materials 0.000 claims description 10
- 229910052717 sulfur Inorganic materials 0.000 claims description 10
- NINIDFKCEFEMDL-UHFFFAOYSA-N Sulfur Chemical compound [S] NINIDFKCEFEMDL-UHFFFAOYSA-N 0.000 claims description 9
- OAICVXFJPJFONN-UHFFFAOYSA-N Phosphorus Chemical compound [P] OAICVXFJPJFONN-UHFFFAOYSA-N 0.000 claims description 8
- 239000011574 phosphorus Substances 0.000 claims description 8
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims description 7
- 239000011593 sulfur Substances 0.000 claims description 6
- 229910052799 carbon Inorganic materials 0.000 claims description 5
- 229910052742 iron Inorganic materials 0.000 claims description 3
- 230000000052 comparative effect Effects 0.000 description 23
- 238000012360 testing method Methods 0.000 description 16
- 230000000694 effects Effects 0.000 description 9
- 238000005245 sintering Methods 0.000 description 8
- 229910001018 Cast iron Inorganic materials 0.000 description 7
- 239000000843 powder Substances 0.000 description 7
- 238000007789 sealing Methods 0.000 description 6
- 238000005299 abrasion Methods 0.000 description 4
- 239000007791 liquid phase Substances 0.000 description 4
- 238000000034 method Methods 0.000 description 4
- XOOUIPVCVHRTMJ-UHFFFAOYSA-L zinc stearate Chemical compound [Zn+2].CCCCCCCCCCCCCCCCCC([O-])=O.CCCCCCCCCCCCCCCCCC([O-])=O XOOUIPVCVHRTMJ-UHFFFAOYSA-L 0.000 description 4
- 238000005275 alloying Methods 0.000 description 3
- 230000005496 eutectics Effects 0.000 description 3
- 230000014759 maintenance of location Effects 0.000 description 3
- 239000011159 matrix material Substances 0.000 description 3
- 238000001000 micrograph Methods 0.000 description 3
- 239000000203 mixture Substances 0.000 description 3
- 229910052750 molybdenum Inorganic materials 0.000 description 3
- 238000000465 moulding Methods 0.000 description 3
- 238000007747 plating Methods 0.000 description 3
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 description 2
- 229910001021 Ferroalloy Inorganic materials 0.000 description 2
- 229910000831 Steel Inorganic materials 0.000 description 2
- 230000015572 biosynthetic process Effects 0.000 description 2
- 238000005266 casting Methods 0.000 description 2
- 229910052804 chromium Inorganic materials 0.000 description 2
- 238000005461 lubrication Methods 0.000 description 2
- 238000003754 machining Methods 0.000 description 2
- 230000013011 mating Effects 0.000 description 2
- 238000002156 mixing Methods 0.000 description 2
- 229910052759 nickel Inorganic materials 0.000 description 2
- 239000002245 particle Substances 0.000 description 2
- 230000000704 physical effect Effects 0.000 description 2
- 231100000241 scar Toxicity 0.000 description 2
- 238000005204 segregation Methods 0.000 description 2
- 239000010959 steel Substances 0.000 description 2
- 229910001141 Ductile iron Inorganic materials 0.000 description 1
- 230000002159 abnormal effect Effects 0.000 description 1
- 239000000654 additive Substances 0.000 description 1
- 229910001567 cementite Inorganic materials 0.000 description 1
- 238000002485 combustion reaction Methods 0.000 description 1
- 230000008602 contraction Effects 0.000 description 1
- 230000003247 decreasing effect Effects 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 239000002283 diesel fuel Substances 0.000 description 1
- 238000003912 environmental pollution Methods 0.000 description 1
- 238000004880 explosion Methods 0.000 description 1
- 230000002349 favourable effect Effects 0.000 description 1
- 238000005242 forging Methods 0.000 description 1
- 229910002804 graphite Inorganic materials 0.000 description 1
- 239000010439 graphite Substances 0.000 description 1
- 230000008595 infiltration Effects 0.000 description 1
- 238000001764 infiltration Methods 0.000 description 1
- KSOKAHYVTMZFBJ-UHFFFAOYSA-N iron;methane Chemical compound C.[Fe].[Fe].[Fe] KSOKAHYVTMZFBJ-UHFFFAOYSA-N 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000005259 measurement Methods 0.000 description 1
- 230000008018 melting Effects 0.000 description 1
- 238000002844 melting Methods 0.000 description 1
- 229910001562 pearlite Inorganic materials 0.000 description 1
- 238000011176 pooling Methods 0.000 description 1
- 239000002244 precipitate Substances 0.000 description 1
- 238000012545 processing Methods 0.000 description 1
- 238000007711 solidification Methods 0.000 description 1
- 230000008023 solidification Effects 0.000 description 1
- 230000002195 synergetic effect Effects 0.000 description 1
- 238000009827 uniform distribution Methods 0.000 description 1
- 229910000859 α-Fe Inorganic materials 0.000 description 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05C—INDEXING SCHEME RELATING TO MATERIALS, MATERIAL PROPERTIES OR MATERIAL CHARACTERISTICS FOR MACHINES, ENGINES OR PUMPS OTHER THAN NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES
- F05C2203/00—Non-metallic inorganic materials
- F05C2203/04—Phosphor
Landscapes
- Cylinder Crankcases Of Internal Combustion Engines (AREA)
- Powder Metallurgy (AREA)
Description
(産業上の利用分野)
本発明は内燃機関や圧縮機に用いられる高い気
密性を有し、耐摩耗性にすぐれた焼結合金製シリ
ンダ・スリーブ(シリンダ・ライナを含む)に係
るものである。本発明に係るシリンダ・スリーブ
はインサート・タイプのシリンダ・スリーブとし
て用いられる。
(従来の技術)
従来使用されているインサート・タイプのスリ
ーブ材はそのほとんどが溶解鋳造法で製造された
鋳鉄材である。シリンダ・スリーブの溶解鋳造法
による製造では必然的に加工代が多くなり、省資
源の要求に反する上に環境汚染の問題も内在し、
偏析、鋳巣の発生などの問題も生じやすい。さら
に昨今の傾向としてエンジンの軽量化、コンパク
ト化等からシリンダのボア間隔を狭くしていく傾
向にあり、必然的にスリーブ材肉厚の薄肉化が求
められるに到り、鋳鉄材以上の高剛性を有するシ
リンダ・スリーブが要求される様になつた。この
要求に応する為に高い剛性を有する鋼材に高価な
クロムメツキ等を施して対処しているのが現状で
ある。
このような従来技術の現状を改善すべく、本出
願人は特開昭54−20911号公報において、0.5〜
2.0%C、0.1〜5.0%のMoおよび/またはCr、0.1
〜3.0%のNiおよび/またはCu、0.01〜0.5%S、
残部Feからなり、内部に多数の独立空孔を有す
る焼結合金製シリンダーライナ材を提供した。一
般に焼結材には多数の空孔が存在し、これら空孔
が材料表面に開孔していて、この空孔が油だまり
となるため、焼結合金材は耐摩耗摺動部材として
好ましい効果を発揮する。
しかしながら、シリンダライナやスリーブの如
く、高い爆発圧力を受けなおかつ高度のガスシー
ル特性を必要とする材料においては焼結材に内在
する連続空孔がガスの通路になり、ブローバイガ
スの増加等の好ましくない結果を生ずる。これら
の空孔を例えば焼結後の鍛造やCu溶浸処理など
で埋め、ガスをシールすることは可能であるがこ
の方法は非経済的な上に量産性に乏しく、しかも
かゝる処理を施すと表面に開孔した空孔も消滅す
るので前述の油だまり効果が期待出来なるなると
いう欠点がある。
上記本出願人の提案に係る焼結合金製シリンダ
ーライナ材は、この欠点を解消するために、特に
Sの作用によつて連続空孔を独立にしたことに特
色がある。
(発明が解決しようとする問題点)
シリンダ・スリーブとして現状で使用されてい
る鋳鉄材には、加工代が多い、同様に鋼材には高
価なクロムメツキが必要であるという問題があ
り、また一般の焼結材には連続空孔があるためか
かる焼結材は薄肉のシリンダ・スリーブには適し
ていないという問題がある。さらに、上記特開昭
54−20911号公報に記載された焼結合金製シリン
ダーライナ材については、本発明者等がその特性
を研究したところ、剛性が十分ではないために薄
肉材として十分な機械的特性を有していないとい
う問題があることが分かつた。
(問題点を解決するための手段および作用)
本発明は上記の従来の一般的焼結材の欠陥を是
正する目的で焼結材中に存在する互に連続した多
数の空孔を各々独立した空孔となるようにし、こ
れによつてガスの通路を遮断し、表面には開孔し
た空孔を残して油だまりとして作用させるととも
に、高剛性を得るために、空孔形状を適正にする
ことにより上記問題点を解決したものであつて、
本発明の特徴とするところは、重量比で0.5〜1.5
%C、0.1〜0.6%P、0.1〜0.5%Sを含有し残部
が実質的に鉄からなり、内部に多数の球状化した
独立空孔を有する焼結合金であつて、6.7〜7.3
g/cm3の密度および5−15%の空孔率を有する焼
結合金よりシリンダ・スリーブ材を構成したとこ
ろにある。
先ず、焼結合金の組成および物性限定理由を説
明す。C(炭素)Feと結合して耐摩耗性および剛
性上望ましいパーライト・マトリツクスを形成す
るに必要な元素であるが、Cの含有率が0.5%未
満では、得られる合金中にフエライトの残留が多
くなり、上記性質上好ましくない。又、Cの含有
率が1.5%を超えると、セメンタイトが粗大に析
出して、材料が脆弱になるためその範囲を0.5〜
1.5%とする。S(硫黄)は焼結材料内部で互に連
結している空孔を互に独立したものにする作用を
有し、かつ機械加工時にチツプ・ブレーカーとし
て、被削性を向上せしめるものである。しかしそ
の含有率が0.1%未満では、上記効果に乏しく、
又含有率が0.5%を超えると、材料の脆弱化をも
たらすとともに、焼結炉の損傷も助長するのでS
の含有率は0.1〜0.5%の範囲内になければならな
い。
一般に焼結鉄中のP(リン)は、Fe−C−Pの
共晶を生成して耐摩耗性の改良に用いられること
が多い。しかし本発明におけるPは上記と異なり
少量の添加で焼結中に微少な液相を多くの箇所で
発生させて焼結材中の空孔を局部的に消失させ、
Sにより独立化された空孔の形状の球状化をもた
らす。すなわち、Pは連続空孔を独立した空孔に
する作用を有するSとの相互作用により、本発明
の目的とする空孔形状適正化に重要な役割をはた
すものである。このように空孔形状が球状化され
ることによつて、焼結合金の剛性が高められる。
これは、ダクタイル鋳鉄における黒鉛球状化のよ
うに、材料中脆弱な部分が球状化せしめられるこ
とによつて高強度が得られるためと考えられる。
さらに、Pは、液相の凝固によつて焼結時の寸
法変化を収縮方向に導くため高密度材を得る事が
出来る。しかもリンはマトリツクスに固溶して、
マトリツクスの強化に役立つ。Pの含有率が0.1
%未満では上記空孔の球状化・高高密度化等の効
果及び強度増大効果に乏しく一方Pが0.6%を超
過した場合は、焼結中にFe−P−Cの共晶の液
相量が過大となつて脆弱化するので好ましくな
い。
リンはフエロアロイ粉として所定の割合で配合
し、混合することによつて得られるが、共晶生成
をもたらすような偏析をできるだけ少なくして均
一な分布を果たす目的から、10μ以下のフエロア
ロイ微粉の使用が望ましい。
次に上述の成分組成を有する本発明に係るシリ
ンダ・ライナやスリーブ材の密度と空孔率との関
係については、これらの関係は一義的なものであ
るが、密度は6.7〜7.3g/cm3の範囲内にあること
が必要である。密度が6.7g/cm3未満の場合、材
料の強度が不足し、空孔を独立したものにしても
主として空孔の祖大化によつてガスシールが不十
分となる傾向があり、密度が7.3g/cm3を超える
と、摺動面における空孔率が少なくなり、油の保
油性が不十分となり、材料の摩耗を促進する傾向
がある。一方空孔率は5〜15%であることが必要
である。空孔率が5%未満のときは摺動面での油
だまり効果による保油性が乏しくなる傾向があり
又空孔率が15%を超えると、空孔の粗大化による
材料の脆弱化及びガスシールが不十分となる傾向
がある。
本発明に係る焼結合金は、少量の合金元素も含
有しうるものである。すなわち、上記空孔の球状
化は、Cr、Mo等の耐摩耗性向上元素を添加した
場合でも可能であり、球状化による効果はCr、
Mo等により損われない。但し、本発明において
は、上述のC、PおよびSのみによつてシリン
ダ・スリーブ材に要求される性質を具備する点に
もその大きな特色がある。この点は、焼結合金に
おけるCr、Mo、Ni等の合金元素が合金を強化し
て上記要求特性を満足するように作用するが、空
孔の形状および量ならびに密度も合金元素と同等
以上に上記要求特性に影響するためであろうと考
えられる。
本発明の焼結合金材料は、従来慣用の方法によ
つて加圧成形し、焼結することにより製造可能で
ある。
本発明の材料の内部構造および諸物性について
下記実施例および比較例により詳しく説明する。
実施例 1
−150メツシユのアトマイズ鉄粉に−325メツシ
ユの黒鉛粉を1%、10μ以下のFeP(フエロフオス
フオル)粉(P25%)を1.8%、−250メツシユの硫
黄粉を0.25%添加し、これにステアリン酸亜鉛
0.8%を添加して混合し、6ton/cm2の成形圧で抗
張力試験片(JSPM2−65)、摩耗試験片(寸法70
mm×17mm×7mm)およびシリンダスリーブ素材
(80mmφ×74mmφ×100mm)を各々成形し、還元性
ガス雰囲気中1160℃で30分間焼結した。
比較例 1
−150メツシユのアトマイズ鉄粉に、−325メツ
シユの黒鉛粉を1%、10μ以下のFeP(フエロフオ
スフオル)粉(P25%)を1.8%添加し、これにス
テアリン酸亜鉛を0.8%添加して混合し、6ton/
cm2の成形圧で実施例1と同じ抗張力試験片および
摩耗試験片を各々成形し、還元性ガス雰囲気中
1160℃で30分間焼結し比較材1を得た。
比較例 2
比較例1の添加剤のうちFep粉の添加をしなか
つた他は比較例1と同じ条件で試験片を製造し
た。
比較例 3
現在、シリンダ・スリーブ材として一般に使用
されている鋳鉄材で、実施例1と同一寸法の抗張
力試験片、摩耗試験片およびシリンダ・スリーブ
を製造した。
比較例 4
−100メツシユのアトマイズ鉄粉に−325メツシ
ユの黒鉛粉を1%、10μ以下の粒径のFeP(フエロ
フオスフオル)粉(P25%)を1.8%、−250メツシ
ユ硫黄粉0.23%を添加し、これにステアリン酸亜
鉛を0.8%添加して混合し4ton/cm2の低い成形圧
で抗張力試験片摩耗試験片、シリンダ・スリーブ
を各々成形し、還元性ガス雰囲気中1130℃で30分
間焼結した。
比較例 5
−250メツシユのアトマイズ鉄粉に−325メツシ
ユの黒鉛粉を1%、粒径10μ以下のFeP(フエロフ
オスフオル)粉(P25%)を1.8%、−250メツシユ
の硫黄粉0.23%を添加し、これにステアリン酸亜
鉛を0.8%添加して混合し、7ton/cm2の成形圧で
抗張力試験片、摩耗試験片、およびシリンダ・ス
リーブ素材を各々成形し、還元性ガス雰囲気中
1200℃で30分焼結した。
上記実施例1および比較例1〜5で得られた材
料の諸特性を第1表に示す。
(Field of Industrial Application) The present invention relates to a cylinder sleeve (including cylinder liner) made of a sintered alloy that has high airtightness and excellent wear resistance and is used in internal combustion engines and compressors. . The cylinder sleeve according to the present invention is used as an insert type cylinder sleeve. (Prior Art) Most insert-type sleeve materials conventionally used are cast iron materials manufactured by melting and casting. Manufacturing cylinders and sleeves using the melt-casting method inevitably requires a large amount of processing costs, which goes against the need for resource conservation and also has the inherent problem of environmental pollution.
Problems such as segregation and formation of cavities are also likely to occur. Furthermore, the recent trend has been to narrow the bore spacing between cylinders due to lighter and more compact engines, and this has inevitably led to a need for thinner sleeve materials, resulting in higher rigidity than cast iron materials. There is a growing demand for cylinder sleeves with In order to meet this demand, the current practice is to apply expensive chrome plating to high-rigidity steel materials. In order to improve the current state of the prior art, the present applicant has published a patent application in Japanese Patent Application Laid-Open No. 54-20911,
2.0% C, 0.1-5.0% Mo and/or Cr, 0.1
~3.0% Ni and/or Cu, 0.01-0.5% S,
We provided a cylinder liner material made of sintered alloy, the remainder of which is Fe, and which has a large number of independent pores inside. Generally, sintered materials have many pores, and these pores open on the material surface, and these pores become oil pools, so sintered alloy materials have favorable effects as wear-resistant sliding members. demonstrate. However, in materials such as cylinder liners and sleeves that are subject to high explosion pressure and require advanced gas sealing properties, the continuous pores inherent in the sintered material become gas passages, resulting in undesirable problems such as an increase in blow-by gas. produces no results. Although it is possible to seal gas by filling these pores by forging after sintering or Cu infiltration treatment, this method is uneconomical and has poor mass productivity, and furthermore, such treatment is difficult. When applied, the pores formed on the surface also disappear, so the above-mentioned oil pool effect cannot be expected. The sintered alloy cylinder liner material proposed by the present applicant is characterized in that, in order to eliminate this drawback, the continuous pores are made independent through the action of S, in particular. (Problems to be solved by the invention) The cast iron materials currently used for cylinders and sleeves have the problem that there is a large machining allowance, and similarly, steel materials require expensive chrome plating. Since sintered materials have continuous pores, such sintered materials are not suitable for thin-walled cylinder sleeves. In addition, the above-mentioned JP-A-Sho
Regarding the cylinder liner material made of sintered alloy described in Publication No. 54-20911, the present inventors researched its properties and found that it did not have sufficient rigidity and had sufficient mechanical properties as a thin material. I found out that there is a problem. (Means and effects for solving the problem) The present invention aims to correct the above-mentioned defects of the conventional general sintered material by separating a large number of interconnected pores existing in the sintered material into individual pores. This blocks the gas passage, leaving open pores on the surface to act as oil pools, and the shape of the pores is appropriate in order to obtain high rigidity. This solves the above problems, and
The feature of the present invention is that the weight ratio is 0.5 to 1.5.
%C, 0.1 to 0.6% P, and 0.1 to 0.5% S, the remainder being substantially iron, and having a large number of spheroidal independent pores inside, the alloy having 6.7 to 7.3%
The cylinder sleeve material is constructed from a sintered alloy having a density of g/cm 3 and a porosity of 5-15%. First, the reason for limiting the composition and physical properties of the sintered alloy will be explained. C (carbon) is an element necessary to combine with Fe to form a pearlite matrix that is desirable for wear resistance and rigidity, but if the C content is less than 0.5%, a large amount of ferrite remains in the resulting alloy. This is not preferable due to the above properties. In addition, if the C content exceeds 1.5%, cementite will precipitate coarsely and the material will become brittle, so the range should be limited to 0.5% to 1.5%.
The rate shall be 1.5%. S (sulfur) has the effect of making the interconnected pores in the sintered material independent from each other, and acts as a chip breaker during machining to improve machinability. However, if its content is less than 0.1%, the above effects will be poor,
Also, if the content exceeds 0.5%, it will cause the material to become brittle and also promote damage to the sintering furnace.
The content must be within the range of 0.1-0.5%. Generally, P (phosphorus) in sintered iron is often used to improve wear resistance by forming a Fe-C-P eutectic. However, unlike the above, P in the present invention is added in a small amount to generate minute liquid phases in many places during sintering, and locally eliminates pores in the sintered material.
S causes the shape of the isolated pores to become spheroidal. That is, P plays an important role in optimizing the shape of the pores, which is the object of the present invention, by interacting with S, which has the effect of turning continuous pores into independent pores. By making the pore shape spherical in this manner, the rigidity of the sintered alloy is increased.
This is thought to be because high strength is obtained by spheroidizing weak parts of the material, like the spheroidization of graphite in ductile cast iron. Furthermore, since P directs dimensional changes during sintering in the direction of contraction due to solidification of the liquid phase, a high-density material can be obtained. Moreover, phosphorus is dissolved in the matrix,
Helps strengthen the matrix. P content is 0.1
If P is less than 0.6%, the effect of making the pores spheroidized and denser and increasing the strength will be poor. On the other hand, if P exceeds 0.6%, the amount of Fe-P-C eutectic liquid phase will decrease during sintering. This is not preferable because it becomes too large and becomes brittle. Phosphorus can be obtained by blending and mixing ferroalloy powder in a predetermined ratio, but in order to achieve uniform distribution by minimizing segregation that would lead to eutectic formation, ferroalloy fine powder of 10μ or less is used. is desirable. Next, regarding the relationship between the density and porosity of the cylinder liner or sleeve material according to the present invention having the above-mentioned component composition, these relationships are unique, but the density is 6.7 to 7.3 g/cm It is necessary to be within the range of 3 . If the density is less than 6.7 g/ cm3 , the strength of the material will be insufficient, and even if the pores are made independent, gas sealing will tend to be insufficient mainly due to enlargement of the pores. If it exceeds 7.3 g/cm 3 , the porosity on the sliding surface will decrease, the oil retention will be insufficient, and there will be a tendency to accelerate wear of the material. On the other hand, the porosity needs to be 5 to 15%. When the porosity is less than 5%, oil retention tends to be poor due to the oil pooling effect on the sliding surface, and when the porosity exceeds 15%, the pores become coarse and the material weakens and gas There is a tendency for poor sealing. The sintered alloy according to the present invention may also contain small amounts of alloying elements. In other words, the spheroidization of the pores is possible even when wear resistance improving elements such as Cr and Mo are added, and the effect of spheroidization is
Not damaged by Mo etc. However, a major feature of the present invention is that only the above-mentioned C, P, and S provide the properties required for a cylinder sleeve material. In this respect, alloying elements such as Cr, Mo, and Ni in the sintered alloy work to strengthen the alloy and satisfy the above required properties, but the shape, amount, and density of pores are also equal to or higher than those of the alloying elements. It is thought that this is because it affects the above-mentioned required characteristics. The sintered alloy material of the present invention can be produced by pressure forming and sintering by a conventionally used method. The internal structure and physical properties of the material of the present invention will be explained in detail with reference to the following Examples and Comparative Examples. Example 1 -150 mesh atomized iron powder, 1% -325 mesh graphite powder, 1.8% FeP powder (P25%) of 10μ or less, and 0.25% -250 mesh sulfur powder. Add zinc stearate to this
0.8% was added and mixed, and a tensile strength test piece ( JSPM2-65 ) and an abrasion test piece (size 70
mm x 17 mm x 7 mm) and cylinder sleeve material (80 mmφ x 74 mmφ x 100 mm) were each molded and sintered at 1160°C for 30 minutes in a reducing gas atmosphere. Comparative Example 1 To -150 mesh atomized iron powder, 1% -325 mesh graphite powder and 1.8% FeP powder (P25%) of 10μ or less were added, and zinc stearate was added to this. Add 0.8% and mix, 6ton/
The same tensile strength test piece and abrasion test piece as in Example 1 were molded at a molding pressure of cm2, and then molded in a reducing gas atmosphere.
Comparative material 1 was obtained by sintering at 1160°C for 30 minutes. Comparative Example 2 A test piece was manufactured under the same conditions as Comparative Example 1 except that Fep powder among the additives in Comparative Example 1 was not added. Comparative Example 3 A tensile strength test piece, an abrasion test piece, and a cylinder sleeve having the same dimensions as in Example 1 were manufactured using cast iron, which is currently commonly used as a cylinder sleeve material. Comparative Example 4 -100 mesh atomized iron powder, 1% -325 mesh graphite powder, 1.8% FeP powder (P25%) with a particle size of 10μ or less, -250 mesh sulfur powder 0.23 % and 0.8% zinc stearate were added and mixed, and molded into tensile strength test pieces, wear test pieces, and cylinder sleeves at a low molding pressure of 4 ton/cm 2 , and then molded at 1130°C in a reducing gas atmosphere. Sintered for 30 minutes. Comparative Example 5 -250 mesh atomized iron powder, -325 mesh graphite powder 1%, FeP powder (P25%) with a particle size of 10μ or less 1.8%, -250 mesh sulfur powder 0.23 % and 0.8% zinc stearate were added and mixed, and a tensile strength test piece, an abrasion test piece, and a cylinder/sleeve material were each molded at a molding pressure of 7 ton/cm 2 in a reducing gas atmosphere.
It was sintered at 1200℃ for 30 minutes. Table 1 shows various properties of the materials obtained in Example 1 and Comparative Examples 1 to 5 above.
【表】【table】
【表】
第1表に示したごとく、本発明に係る実施例1
で高強度と高ヤング率が得られている。比較例1
は実施例1より硫黄を除いた場合であるが強度、
剛性率とも大巾な低下が見られる比較例2は、硫
黄とともにリンも除いた場合であるが、強度、剛
性率ともさらに低下が見られる。これらのデータ
から本発明材(実施例1)の高い強度と高いヤン
グ率とは硫黄とリン添加の相乗効果である事が分
かる。
比較例4は密度が低くかつ空孔率が高いために
強度が低くなつており、また比較例5は密度が高
くかつ空孔率が低いために強度は十分であるが後
述の如く耐摩耗性にすぐれない。
次に本発明に係る実施例1および比較例1にお
いて製造したシリンダ・スリーブの顕微鏡写真を
それぞれ第1図A,Bおよび第2図A,Bに示
す。これより第2図A,Bのリンのみ添加材では
空孔は連続しているが本発明に係る実施例1で
は、空孔が独立しており、かつ球状化している。
この球状化した空孔が高ヤング率を示す原因であ
り本発明材の特色である。
次に本発明に係る実施例1および現在一般に使
用されている鋳鉄材スリーブである比較例3で得
られた摩耗試験片を用いて往復動摩耗試験機を用
いて下記条件で湿式摩耗試験を行い摩耗係数と摩
耗量を求めた。
(i) 潤滑:湿式デイーゼルOil(SAE10#)
(ii) ストローク:50mm×2(往復)
(iii) 荷重、速度、時間:10Kgf−600C.P.m−60
分
(iv) 摩耗量の測定法
棒状のクロムメツキ材を相手材として供試材
(スリーブ材)に対してによつて摺動せしめた後
供試材の摩耗痕深さ(ミクロン)を求めまた相手
材の摩耗痕径(mm)を求めた。
測定結果を次表にしめす。[Table] As shown in Table 1, Example 1 according to the present invention
High strength and high Young's modulus have been obtained. Comparative example 1
is the case in which sulfur is removed from Example 1, but the strength is
Comparative Example 2, in which both the rigidity and the rigidity are significantly reduced, is a case in which phosphorus is removed along with sulfur, but the strength and the rigidity are further decreased. These data show that the high strength and high Young's modulus of the material of the present invention (Example 1) are due to the synergistic effect of the addition of sulfur and phosphorus. Comparative Example 4 has a low density and high porosity, so its strength is low, and Comparative Example 5 has a high density and a low porosity, so it has sufficient strength, but as described below, its wear resistance is poor. Not very good. Next, micrographs of cylinder sleeves manufactured in Example 1 according to the present invention and Comparative Example 1 are shown in FIGS. 1A and B and FIGS. 2A and B, respectively. From this, the pores are continuous in the materials with only phosphorus added in FIGS. 2A and 2B, but in Example 1 according to the present invention, the pores are independent and spherical.
These spherical pores are the cause of the high Young's modulus and are a feature of the material of the present invention. Next, using the wear test pieces obtained in Example 1 according to the present invention and Comparative Example 3, which is a currently commonly used cast iron sleeve, a wet wear test was conducted using a reciprocating wear tester under the following conditions. The wear coefficient and amount of wear were determined. (i) Lubrication: Wet diesel oil (SAE10#) (ii) Stroke: 50mm x 2 (reciprocating) (iii) Load, speed, time: 10Kgf−600C.Pm−60
(iv) Measuring method of wear A rod-shaped chrome-plated material is used as a mating material and is slid against the specimen material (sleeve material), and then the wear scar depth (microns) of the specimen material is determined. The wear scar diameter (mm) of the material was determined. The measurement results are shown in the table below.
【表】
第2表から明らかな如く本発明に係る実施例1
の材料は比較例3の材料に対して摩耗係数も小さ
く又摩耗量も少ないことがわかる。さらに相手
Crメツキの摩耗量も少なくすぐれた摺動部材で
あることが認められた。
更に実施例1及び比較例3〜5において得られ
たシリンダ・スリーブを用いて4ストロークガソ
リンエンジン(4気筒、1500c.c.、ボアー74×スト
ローク80)を用いてエンジンテストを実施した。
実験条件は5500rpm、全負荷で500hrの耐久テス
トであつた。第3表に実験結果を示す。[Table] As is clear from Table 2, Example 1 according to the present invention
It can be seen that the material of Comparative Example 3 has a smaller wear coefficient and a smaller amount of wear than the material of Comparative Example 3. Furthermore, the opponent
It was confirmed that the Cr plating has less wear and is an excellent sliding member. Further, an engine test was conducted using the cylinder sleeves obtained in Example 1 and Comparative Examples 3 to 5 in a 4-stroke gasoline engine (4 cylinders, 1500 c.c., bore 74 x stroke 80).
The experimental conditions were a 500 hr durability test at 5500 rpm and full load. Table 3 shows the experimental results.
【表】
このエンジンテストの結果より、本発明に係る
実施例1の材料は、実エンジンにおけるブローバ
イが比較例3の鋳鉄製スリーブの結果と同一水準
となつていることが明らかである。これはリンと
硫黄の添加によつて焼結材内部で連結する空孔を
独立したものにしてガスシール性を改善した結果
である。
さらに、実施例1の材料ではスリーブ、リング
摩耗共鋳鉄スリーブ材に比べ大巾に減少した結果
となつている。これは空孔がスリーブ表面に開孔
しているために摩耗面の潤滑状態が改善されてい
るためである。また比較例4は密度6.4、空孔率
19%と意図的に低密度化した場合であるが、空孔
の粗大化により、ガスシール性が悪くなり、ブロ
ーバイ量が異常に多くなつている。さらに比較例
5は、意図的に焼結時の液相量を多くして、空孔
をつぶした場合であるが、油の保油性がないため
にスリーブ、リング共スカツフ気味の異常摩耗を
起こしていた。
(効果)
以上のように本発明に係るシリンダ・ライナ及
びスリーブは、溶製材と同等のガスシール性を有
し、かつ耐摩耗性にすぐれている上に相手材の摩
耗を軽減せしめて機関寿命の延長を可能にするも
のであり、さらに加うるに高強度、高ヤング率を
有する材料であるため、エンジンの軽量化、コン
パクト化で要求されるスリーブの薄肉化に十分耐
えうるものである。かような理由により本発明材
は新しいエンジン設計に要求されるスリーブ材の
特性を十分そなえもつた材料である。さらに、上
述の特性を発揮する用途として、ロータリーコン
プレツサのベーン等が考えられ、これらの用途に
も本発明の焼結合金を用いることができる。[Table] From the results of this engine test, it is clear that the blow-by of the material of Example 1 according to the present invention in an actual engine is at the same level as the result of the cast iron sleeve of Comparative Example 3. This is the result of the addition of phosphorus and sulfur, which makes the pores connected inside the sintered material independent and improves gas sealing properties. Furthermore, the material of Example 1 resulted in a significant reduction in sleeve and ring wear compared to the co-cast iron sleeve material. This is because the lubrication state of the worn surface is improved because the holes are formed on the sleeve surface. Comparative example 4 has a density of 6.4 and a porosity of
In this case, the density was intentionally lowered to 19%, but due to the coarsening of the pores, the gas sealing performance deteriorated and the amount of blow-by increased abnormally. Furthermore, in Comparative Example 5, the amount of liquid phase was intentionally increased during sintering to collapse the pores, but due to the lack of oil retention, both the sleeve and ring suffered abnormal wear with a slight stubble. was. (Effects) As described above, the cylinder liner and sleeve according to the present invention have gas sealing properties equivalent to those of melt-molded materials, have excellent wear resistance, and reduce wear of the mating material, thereby extending the life of the engine. Furthermore, since it is a material with high strength and a high Young's modulus, it can sufficiently withstand the thinning of the sleeve required for lighter and more compact engines. For these reasons, the material of the present invention has sufficient characteristics of a sleeve material required for new engine designs. Furthermore, rotary compressor vanes and the like can be considered as applications that exhibit the above-mentioned characteristics, and the sintered alloy of the present invention can also be used in these applications.
第1A図および第1B図は実施例1の焼結合金
の金属組織顕微鏡写真(倍率それぞれ100倍およ
び500倍)、第2A図および第2B図は比較例1の
焼結合金の金属組織顕微鏡写真(倍率それぞれ
100倍および500倍)である。
Figures 1A and 1B are micrographs of the metallographic structure of the sintered alloy of Example 1 (100x and 500x magnification, respectively), and Figures 2A and 2B are micrographs of the metallographic structure of the sintered alloy of Comparative Example 1. (Each magnification
100x and 500x).
Claims (1)
のリン及び0.1〜0.5%の硫黄を含有し、残部が実
質的に鉄からなり内部に多数の球状化した独立空
孔を有する焼結合金からなるシリンダ・スリーブ
材であつて、前記焼結合金が6.7〜7.3g/cm3の密
度および5−15%の空孔率を有し、剛性率が高い
ことを特徴とするシリンダ・スリーブ材。1 0.5-1.5% carbon and 0.1-0.6% by weight
of phosphorus and 0.1 to 0.5% sulfur, the remainder being substantially iron, and having a large number of spheroidal independent pores inside, the cylinder sleeve material comprising the sintered alloy. A cylinder sleeve material having a density of 6.7 to 7.3 g/cm 3 and a porosity of 5 to 15%, and having a high rigidity.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP18627684A JPS6164851A (en) | 1984-09-07 | 1984-09-07 | Cylinder sleeve material made of sintered alloy having high rigidity |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP18627684A JPS6164851A (en) | 1984-09-07 | 1984-09-07 | Cylinder sleeve material made of sintered alloy having high rigidity |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS6164851A JPS6164851A (en) | 1986-04-03 |
| JPH0151538B2 true JPH0151538B2 (en) | 1989-11-06 |
Family
ID=16185459
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP18627684A Granted JPS6164851A (en) | 1984-09-07 | 1984-09-07 | Cylinder sleeve material made of sintered alloy having high rigidity |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS6164851A (en) |
Families Citing this family (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2942839B2 (en) * | 1989-01-30 | 1999-08-30 | 株式会社小松製作所 | Two-layer sintered seal ring and method of manufacturing the same |
| US6149736A (en) * | 1995-12-05 | 2000-11-21 | Honda Giken Kogyo Kabushiki Kaisha | Magnetostructure material, and process for producing the same |
| JP2006046540A (en) * | 2004-08-05 | 2006-02-16 | Matsushita Electric Ind Co Ltd | Hydrodynamic bearing device |
| US8257462B2 (en) | 2009-10-15 | 2012-09-04 | Federal-Mogul Corporation | Iron-based sintered powder metal for wear resistant applications |
| CN103361538B (en) * | 2013-07-18 | 2014-12-24 | 江苏爱吉斯海珠机械有限公司 | Cylinder sleeve alloy cast iron medium-frequency induction furnace melting method and centrifugal casting method |
-
1984
- 1984-09-07 JP JP18627684A patent/JPS6164851A/en active Granted
Also Published As
| Publication number | Publication date |
|---|---|
| JPS6164851A (en) | 1986-04-03 |
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