JPS62271914A - Sintered cam shaft - Google Patents
Sintered cam shaftInfo
- Publication number
- JPS62271914A JPS62271914A JP8358186A JP8358186A JPS62271914A JP S62271914 A JPS62271914 A JP S62271914A JP 8358186 A JP8358186 A JP 8358186A JP 8358186 A JP8358186 A JP 8358186A JP S62271914 A JPS62271914 A JP S62271914A
- Authority
- JP
- Japan
- Prior art keywords
- less
- sintered
- sintered alloy
- assembly pieces
- cam piece
- 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
Links
- 229910045601 alloy Inorganic materials 0.000 claims abstract description 25
- 239000000956 alloy Substances 0.000 claims abstract description 25
- 229910052804 chromium Inorganic materials 0.000 claims abstract description 4
- 229910052802 copper Inorganic materials 0.000 claims abstract description 4
- 229910052742 iron Inorganic materials 0.000 claims abstract description 4
- 229910052750 molybdenum Inorganic materials 0.000 claims 2
- 239000000463 material Substances 0.000 abstract description 12
- 238000005299 abrasion Methods 0.000 abstract description 4
- 229910052748 manganese Inorganic materials 0.000 abstract description 3
- 238000005245 sintering Methods 0.000 description 11
- 229910000831 Steel Inorganic materials 0.000 description 7
- 239000010959 steel Substances 0.000 description 7
- 230000000694 effects Effects 0.000 description 6
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 5
- 229910002804 graphite Inorganic materials 0.000 description 5
- 239000010439 graphite Substances 0.000 description 5
- 230000000052 comparative effect Effects 0.000 description 4
- 238000005520 cutting process Methods 0.000 description 4
- 230000007423 decrease Effects 0.000 description 4
- 239000000203 mixture Substances 0.000 description 4
- 229910001562 pearlite Inorganic materials 0.000 description 4
- 239000000523 sample Substances 0.000 description 3
- QGZKDVFQNNGYKY-UHFFFAOYSA-N Ammonia Chemical compound N QGZKDVFQNNGYKY-UHFFFAOYSA-N 0.000 description 2
- 238000009792 diffusion process Methods 0.000 description 2
- XEEYBQQBJWHFJM-UHFFFAOYSA-N iron Substances [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 2
- 239000007791 liquid phase Substances 0.000 description 2
- 239000010687 lubricating oil Substances 0.000 description 2
- 238000003754 machining Methods 0.000 description 2
- 238000004519 manufacturing process Methods 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 239000003921 oil Substances 0.000 description 2
- 239000000843 powder Substances 0.000 description 2
- 230000037303 wrinkles Effects 0.000 description 2
- 229910001018 Cast iron Inorganic materials 0.000 description 1
- 229910021529 ammonia Inorganic materials 0.000 description 1
- 229910052787 antimony Inorganic materials 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 229910052797 bismuth Inorganic materials 0.000 description 1
- 238000005219 brazing Methods 0.000 description 1
- 229910001567 cementite Inorganic materials 0.000 description 1
- 239000003795 chemical substances by application Substances 0.000 description 1
- 238000002485 combustion reaction Methods 0.000 description 1
- 238000012790 confirmation Methods 0.000 description 1
- 238000005260 corrosion Methods 0.000 description 1
- 230000007797 corrosion Effects 0.000 description 1
- 238000000354 decomposition reaction Methods 0.000 description 1
- 230000005496 eutectics Effects 0.000 description 1
- 239000012535 impurity Substances 0.000 description 1
- KSOKAHYVTMZFBJ-UHFFFAOYSA-N iron;methane Chemical compound C.[Fe].[Fe].[Fe] KSOKAHYVTMZFBJ-UHFFFAOYSA-N 0.000 description 1
- 238000005304 joining Methods 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 230000013011 mating Effects 0.000 description 1
- 239000011159 matrix material Substances 0.000 description 1
- 150000001247 metal acetylides Chemical class 0.000 description 1
- 229910052759 nickel Inorganic materials 0.000 description 1
- 239000002245 particle Substances 0.000 description 1
- 239000011148 porous material Substances 0.000 description 1
- 238000003860 storage Methods 0.000 description 1
- 238000005728 strengthening Methods 0.000 description 1
- 229910052718 tin Inorganic materials 0.000 description 1
Classifications
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C33/00—Making ferrous alloys
- C22C33/02—Making ferrous alloys by powder metallurgy
- C22C33/0257—Making ferrous alloys by powder metallurgy characterised by the range of the alloying elements
- C22C33/0264—Making ferrous alloys by powder metallurgy characterised by the range of the alloying elements the maximum content of each alloying element not exceeding 5%
Abstract
Description
【発明の詳細な説明】
３、発明の詳細な説明
［産業上の利用分野］
本発明は内燃機関用のカムシャフト、詳しくはカムロブ
とジャーナルピースを共に焼結合金で形成し、スチール
シャフトに接合したカムシャフトに関する。Detailed Description of the Invention 3. Detailed Description of the Invention [Field of Industrial Application] The present invention relates to a camshaft for an internal combustion engine, specifically a cam lobe and a journal piece that are both made of a sintered alloy and joined to a steel shaft. Regarding the camshaft.
［従来技術］
カムピース、ジャーナルピース等を個別に製作し、スチ
ールシャフトに接合するカムシャフトにおいて、カムピ
ース以外のジャーナル、ギア等の大部分は鋼材で製作さ
れている。しかし、鋼材は仕上げ加工が比較的容易な反
面、部品製作に要するＦＩＯ工の工程やろう付は等によ
りシャフトに接合する際の工程が多く、この種のカムシ
ャフトの製造コストを高いものにしていた。[Prior Art] In a camshaft in which cam pieces, journal pieces, etc. are individually manufactured and joined to a steel shaft, most of the journals, gears, etc. other than the cam piece are manufactured from steel. However, while steel is relatively easy to finish, it requires many steps to join it to the shaft, such as FIO machining and brazing, which makes the manufacturing cost of this type of camshaft high. Ta.
また、摺動部材、特にジャーナルとして用いた場合には
耐摩耗性が低いという問題もめった。Furthermore, when used as a sliding member, especially a journal, the problem of low wear resistance has often been encountered.
し発明の構成］
本発明は低いコストで製造できて、耐摩耗性が良好なカ
ムシャフトを提供することを目的とするものであって、
この目的は、カムピース以外の組付ピースを、重量比で
、Ｃ：１．０〜５．０％、Ｐ：０、２〜０．８％、Ｓ：
０．５％以下、Ｍｎ：１．０％以下、Ｓｉ ： ２．０
％以下、残部Ｆｅからなる焼結合金、もしくは、上記組
成に加えて、Ｈｏ：０．１〜２．０％、および／又はＮ
ｉ： ０．５〜３．０％、Ｃｒ二０．１〜２．０％、Ｂ
：０．０１〜１．０％、Ｃ０： ０．５〜３．０％のう
ちの１種または２種以上を含有する焼結合金で製造する
ことによって達成される。[Structure of the Invention] An object of the present invention is to provide a camshaft that can be manufactured at low cost and has good wear resistance,
This purpose is to assemble the assembly pieces other than the cam piece in terms of weight ratio: C: 1.0 to 5.0%, P: 0, 2 to 0.8%, S:
0.5% or less, Mn: 1.0% or less, Si: 2.0
% or less, the balance is Fe, or in addition to the above composition, Ho: 0.1 to 2.0%, and/or N
i: 0.5-3.0%, Cr2 0.1-2.0%, B
C0: 0.01 to 1.0% and C0: 0.5 to 3.0%.
またこの焼結合金はパーライト基地組織中に炭化物と黒
鉛を分布せしめれば自己潤滑性と切削性が良好となる。In addition, this sintered alloy has good self-lubricating properties and machinability when carbide and graphite are distributed in the pearlite base structure.
本発明のカムピース以外の組付ピースにおいて各成分の
数値を限定した理由は下記の通りである。The reasons for limiting the numerical values of each component in the assembly pieces other than the cam piece of the present invention are as follows.
Ｃは土０〜５．０％の範囲で一部が基地に固溶して基地
を強化し、その他が炭化物もしくは炭化物と黒鉛を形成
するが、１．０％未満ではその効果が得られず耐摩耗性
、自己潤滑性が低下する。また５、０％を超えると炭化
物が粗大化し、さらにＰと作用して過剰な液相を生じて
組付ピースとしての形状が保てない。When C is in the range of 0 to 5.0%, part of it dissolves in the base and strengthens the base, and the rest forms carbide or graphite with carbide, but if it is less than 1.0%, this effect cannot be obtained. Wear resistance and self-lubricating properties decrease. Moreover, if it exceeds 5.0%, the carbide becomes coarse and further interacts with P to generate an excessive liquid phase, making it impossible to maintain the shape of the assembly piece.
ＰはＦｅ−Ｃ−Ｐ共晶のステダイトを生じさせ耐摩耗性
に寄与するが、０．２％未満では添加効果かなく、０．
８％を超えると、析出するステダイト量が過多となって
被剛性が悪くなり、また脆化も進む。P produces Fe-C-P eutectic steadite and contributes to wear resistance, but if it is less than 0.2%, there is no addition effect;
If it exceeds 8%, the amount of precipitated steadite becomes excessive, resulting in poor rigidity and further embrittlement.
ＳはＳ単体及び）Ｉｎ３の形で基地中へ分布することに
より快削成分として動き、切削性を向上させるが、０．
５％を超えると強度が著しく低下して脆化させる。また
焼結の進行も妨げる。When S is distributed throughout the base in the form of S alone or )In3, it acts as a free-cutting component and improves machinability, but 0.
When it exceeds 5%, the strength decreases significantly and becomes brittle. It also hinders the progress of sintering.
Ｍｎを１．０％以下にする理由は、！−１ｎが１．０％
を超えると、焼結の進行が抑制される結果、粗大な空孔
が残ることと、圧粉成形性も低下することによる。The reason for keeping Mn below 1.0% is! -1n is 1.0%
If it exceeds this, the progress of sintering is suppressed, resulting in coarse pores remaining and powder formability also being reduced.
Ｓｉを２．０％以下にする理由は、Ｓｉが２．０％を超
えると、基地が脆化するほか、粉末の圧粉成形性が低下
し、焼結時の変形が大きくなることによる。The reason for setting the Si content to 2.0% or less is that if the Si content exceeds 2.0%, the matrix becomes brittle, the compactability of the powder decreases, and deformation during sintering increases.
焼結条件によっては高温による液相焼結時に粒子間の拡
散が追従できず、表面付近にシワ、割れを生ずることが
ある。そのためｌ−１ｏ８０．１〜２．０％の範囲で添
加することにより拡散を助け、シワ、割れを防ぐことが
できる。０．１％未満ではこの効果が得られず、２．０
％を超えるとＨｏ２ Ｇの形成や基地の強化により高度
が上昇し被削性が悪くなる６さらにまた、Ｎｉ ： ０
．５〜３．０． Ｃｒ ： ０．１〜２．０％、Ｂ：０
．０１〜１．０％、Ｃｕ ： ０．５〜３．０％のうち
の１種または２種以上を含んでも良く、摩耗が発生する
条件下で使用する部品に対してこれらの成分を適量添加
することにより、基地と炭化物の強化を図ることができ
る。しかし、各成分とも限定範囲を下回ると添加効果が
なく、また上限を超えると硬度が高くなり、被削性が低
下する。Depending on the sintering conditions, diffusion between particles may not follow during liquid phase sintering at high temperatures, resulting in wrinkles and cracks near the surface. Therefore, by adding l-1o in a range of 80.1 to 2.0%, diffusion can be aided and wrinkles and cracks can be prevented. This effect cannot be obtained at less than 0.1%, and 2.0%
%, the altitude increases due to the formation of Ho2G and the strengthening of the base, resulting in poor machinability.6Furthermore, Ni: 0
．． 5-3.0. Cr: 0.1-2.0%, B: 0
．． 01 to 1.0%, Cu: 0.5 to 3.0%, and may contain one or more of 0.5 to 3.0%, and these components may be added in appropriate amounts to parts used under conditions where wear occurs. By doing so, it is possible to strengthen the base and carbide. However, if each component falls below a limited range, there will be no addition effect, and if it exceeds the upper limit, hardness increases and machinability decreases.
この焼結合金はＣ：１．５〜４．０％、Ｐ：０．４〜０
．７％の範囲内で焼結温度と時間を選択することによっ
て、パーライト基地中に炭化物と黒鉛を同時に含有する
組織を得ることができる。それによって、鋳鉄材料と同
じように黒鉛による自己潤滑作用で相手材に対する攻撃
性の少ない耐摩耗材料となる。またこれに伴ない切削性
も向上する。This sintered alloy has C: 1.5-4.0%, P: 0.4-0
．． By selecting the sintering temperature and time within the range of 7%, a structure containing carbide and graphite simultaneously in the pearlite base can be obtained. As a result, like cast iron materials, the self-lubricating effect of graphite makes it a wear-resistant material that is less aggressive towards mating materials. In addition, machinability is also improved accordingly.
本発明の焼結カムシャフトは、上記焼結材料を圧粉成形
してスチールシャフトに組み付けた後、１０５０〜１２
００’Ｃの温度で焼結接合するが、製造コストを低くす
るためには、組付ピース仝体が同一条件で接合させるこ
とが必要でおる。従ってカムピース用の焼結材料として
は、例えば特願昭５８−１４０９６４号に開示されてい
る耐摩耗焼結合金（Ｃ：１．５％、ｓ； ： ０．５〜
１．２％、Ｎｎ：１．０％以下、Ｐ ： ０．２〜０．
８％、Ｃｒ：２．０〜２０％、）ｔｏ：０．５〜２．５
％、Ｎｉ：０５〜２．５％、残部Ｆｅおよび不純物）も
しくは、この焼結合金に、さらにＳｎ、 Ｂｉ、 Ｓｂ
、 Ｃｏのうち１種または２種以上を０．０１〜５．０
％含有した耐摩耗焼結合金を用いることが好ましい。The sintered camshaft of the present invention is produced by compacting the sintered material and assembling it onto a steel shaft.
Sintering and joining is carried out at a temperature of 0.000'C, but in order to reduce manufacturing costs, it is necessary to join the assembly pieces under the same conditions. Therefore, as a sintered material for the cam piece, for example, a wear-resistant sintered alloy (C: 1.5%, s: 0.5~
1.2%, Nn: 1.0% or less, P: 0.2-0.
8%, Cr: 2.0-20%, )to: 0.5-2.5
%, Ni: 05-2.5%, balance Fe and impurities) or this sintered alloy is further supplemented with Sn, Bi, Sb.
, 0.01 to 5.0 of one or two or more of Co
It is preferable to use a wear-resistant sintered alloy containing %.
［実施例］
以下、実施例および比較例に基づき本発明の性能確認試
験結果を説明する。[Example] Hereinafter, the performance confirmation test results of the present invention will be explained based on Examples and Comparative Examples.
第１表に示す通りカムピース以外の組付ピースとして、
Ｎｏ、１〜９の組成を有する本発明焼結合金、Ｎｏ、１
０．１１の比較用焼結合金、及びＮｏ。As shown in Table 1, as assembly pieces other than cam pieces,
Sintered alloy of the present invention having a composition of No. 1 to 9, No. 1
0.11 comparative sintered alloy, and no.
１２の比較用鋼材（３０Ｍ４４０）からなる試験片を得
た。焼結合金については、４〜６ｔ／ｃｍのプレス面圧
でプレス成形後、アンモニア分解ガス雰囲気の炉に入れ
、１０５０〜１２００’Ｃ（平均１１２０’Ｃの温度で
１〜２時間焼結した。鋼材は上記焼結合金と同一条件で
焼結炉を通して得たものを使用した。Twelve test specimens made of comparative steel material (30M440) were obtained. The sintered alloy was press-formed with a press surface pressure of 4 to 6 t/cm, then placed in a furnace in an ammonia decomposition gas atmosphere, and sintered at a temperature of 1050 to 1200'C (average 1120'C) for 1 to 2 hours. The steel used was one obtained through a sintering furnace under the same conditions as the sintered alloy described above.
一摩耗試験一
各供試材について表面硬さを測定するとともにアムスラ
一式摩耗試験を行なった。供試材を平面接触滑り摩耗試
験機における回転片とし、これら回転片をＡ１合金によ
って製作された平板状試料（相手材）の固定片に接触し
、その接触面に対し常時潤滑油を供給しつつ回転させた
。1. Abrasion Test 1. The surface hardness of each sample material was measured and an Amsura set abrasion test was conducted. The test material is a rotating piece in a plane contact sliding wear tester, and these rotating pieces are brought into contact with a fixed piece of a flat sample (mate material) made of A1 alloy, and lubricating oil is constantly supplied to the contact surface. I rotated it.
試験条件は以下の通りである。The test conditions are as follows.
回転片外径・・・φ４Ｑｍｍ、潤滑油・・・１０Ｗ−３
０、油温−８０’Ｃ１油！−０，５ｆ／ｍｉｎ 、荷重
・・・１００ＫＪｆ、すべり速度”−２，５ｍ／ＳｅＣ
、走行時間・・・１５０時間。Rotating piece outer diameter...φ4Qmm, lubricating oil...10W-3
0, oil temperature -80'C1 oil! -0.5f/min, load...100KJf, sliding speed "-2.5m/SeC
, driving time...150 hours.
第１表に示される通り、本発明焼結合金は相手材ととも
に、比較材に比して摩耗量の著しい減少を示した。As shown in Table 1, the sintered alloy of the present invention, together with its counterpart material, showed a significant reduction in the amount of wear compared to the comparative material.
一加エチップ寿命試験−
各供試材を直径４８＃、厚ざ２５＃の円柱状に加工し、
バイトチップを用いた旋盤によって切削してチップ寿命
を測定した。Single-chip life test - Process each sample material into a cylinder with a diameter of 48# and a thickness of 25#,
The tip life was measured by cutting with a lathe using a bite tip.
試験条件は以下の通りである。The test conditions are as follows.
ワーク回転数・・・８００ｒｐｍ、送り速度・・・０．
３２ｒｅｖ、収り代・・・１＃、水溶性切削剤使用。Work rotation speed: 800 rpm, feed speed: 0.
32rev, storage allowance...1#, water-soluble cutting agent used.
１個のチップで取り代１１ｒｕｎの切削が可能な回数を
比較したが、第１表に示される通り、本発明焼結合金を
切削した場合、バイトチップは著しく長い寿命で使用で
きることが示された。A comparison was made of the number of times that a single tip can cut with a machining allowance of 11 runs, and as shown in Table 1, it was shown that the bite tip could be used for a significantly longer life when cutting the sintered alloy of the present invention. .
第１図と第２図に本発明のカムピース以外の組付ピース
としての焼結合金の顕微鏡組織写真（ナイタール液腐蝕
、２００倍）を示す。FIGS. 1 and 2 show microscopic photographs (nital liquid corrosion, 200x magnification) of sintered alloys as assembly pieces other than the cam piece of the present invention.
第１図は、第１表のＮｏ、２の組成の焼結合金を１１０
０〜１１３０’Ｃ，１〜１．５時間で焼結して得られた
ものであり、パーライト基地（Ａ）中に耐摩耗性に寄与
する網目状の炭化物（Ｂ）（セメンタイトとステダイト
）と被削性と潤滑性を良好にする黒鉛（Ｃ）が分布して
いる。Figure 1 shows the sintered alloy with composition No. 2 in Table 1.
It is obtained by sintering at 0 to 1130'C for 1 to 1.5 hours, and contains network-like carbides (B) (cementite and steadite) that contribute to wear resistance in the pearlite base (A). Graphite (C) is distributed to improve machinability and lubricity.
第２図は、第１表のＮｏ、１の組成の焼結合金を１１３
０〜１１６０’Ｃ，１，２〜１．７時間で焼結して得ら
れたものであり、パーライト基地（Ａ）中に網目状の炭
化物（Ｂ）が分布している。Figure 2 shows the sintered alloy with the composition No. 1 in Table 1.
It was obtained by sintering at 0 to 1160'C for 1.2 to 1.7 hours, and network-like carbide (B) is distributed in the pearlite base (A).
［発明の効果］
以上述べたように、本発明の焼結カムシャフトは、−回
の焼結処理でシャフトに結合できて耐摩耗性にも優れた
焼結合金の組付ピースを用いるものであり、特にカムピ
ース以外の組付ピースには被削性の良好な焼結合金を配
したので生産性の優れたカムシャフトである。[Effects of the Invention] As described above, the sintered camshaft of the present invention uses an assembly piece of a sintered alloy that can be joined to the shaft with -1 sintering process and has excellent wear resistance. This is a camshaft with excellent productivity, especially since the assembly pieces other than the cam piece are made of sintered alloy with good machinability.
第１図と第２図は、本発明のカムピース以外の組付ピー
スとしての焼結合金の金属組織顕微鏡組織写真である。FIGS. 1 and 2 are photographs of the metallographic microstructure of a sintered alloy as an assembly piece other than the cam piece of the present invention.
Claims (4)
．０〜５．０％、Ｐ：０．２〜０．８％、Ｓ：０．５％
以下、Ｍｎ：１．０％以下、Ｓｉ：２．０％以下、を含
有し、残部Ｆｅからなる焼結合金で形成される焼結カム
シャフト。(1) Assembly pieces other than the cam piece have a weight ratio of C:1
．． 0-5.0%, P: 0.2-0.8%, S: 0.5%
Hereinafter, a sintered camshaft formed of a sintered alloy containing Mn: 1.0% or less, Si: 2.0% or less, and the balance consisting of Fe.
．０〜５．０％、Ｐ：０．２〜０．８％、Ｓ：０．５％
以下、Ｍｎ：１．０％以下、Ｓｉ：２．０％以下、Ｍｏ
：０．１〜２．０％、を含有し、残部Ｆｅからなる焼結
合金で形成される焼結カムシャフト。(2) Assembly pieces other than the cam piece have a weight ratio of C:1
．． 0-5.0%, P: 0.2-0.8%, S: 0.5%
Below, Mn: 1.0% or less, Si: 2.0% or less, Mo
:0.1 to 2.0%, and the balance is Fe.
．０〜５．０％、Ｐ：０．２〜０．８％、Ｓ：０．５％
以下、Ｍｎ：１．０％以下、Ｓｉ：２．０％以下、を含
有し、さらにＮｉ：０．５〜３．０％、Ｃｒ：０．１〜
２．０％、Ｂ：０．０１〜１．０％、Ｃｕ：０．５〜３
．０％のうちの１種または２種以上、を含有し、残部Ｆ
ｅからなる焼結合金で形成される焼結カムシャフト。(3) Assembly pieces other than the cam piece have a weight ratio of C:1
．． 0-5.0%, P: 0.2-0.8%, S: 0.5%
The following contains Mn: 1.0% or less, Si: 2.0% or less, and further includes Ni: 0.5 to 3.0%, and Cr: 0.1 to
2.0%, B: 0.01-1.0%, Cu: 0.5-3
．． Contains one or more of 0%, and the remainder F
A sintered camshaft made of a sintered alloy made of e.
．０〜５．０％、Ｐ：０．２〜０．８％、Ｓ：０．５％
以下、Ｍｎ：１．０％以下、Ｓｉ：２．０％以下、Ｍｏ
：０．１〜２．０％、を含有し、さらにＮｉ：０．５〜
３．０％、Ｃｒ：０．１〜２．０％、Ｂ：０．０１〜１
．０％、Ｃｕ：０．５〜３．０％のうちの１種または２
種以上、を含有し、残部Ｆｅからなる焼結合金で形成さ
れる焼結カムシャフト。(4) Assembly pieces other than the cam piece have a weight ratio of C:1
．． 0-5.0%, P: 0.2-0.8%, S: 0.5%
Below, Mn: 1.0% or less, Si: 2.0% or less, Mo
:0.1 to 2.0%, and further contains Ni:0.5 to 2.0%.
3.0%, Cr: 0.1-2.0%, B: 0.01-1
．． 0%, Cu: one or two of 0.5 to 3.0%
A sintered camshaft formed of a sintered alloy containing at least 100% of Fe, with the remainder being Fe.
Priority Applications (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP8358186A JPS62271914A (en) | 1986-04-11 | 1986-04-11 | Sintered cam shaft |
| GB8708020A GB2189811B (en) | 1986-04-11 | 1987-04-03 | Sintered cam shaft |
| DE19873712107 DE3712107A1 (en) | 1986-04-11 | 1987-04-10 | SINTERED CONTROL SHAFT |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP8358186A JPS62271914A (en) | 1986-04-11 | 1986-04-11 | Sintered cam shaft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPS62271914A true JPS62271914A (en) | 1987-11-26 |
Family
ID=13806458
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP8358186A Pending JPS62271914A (en) | 1986-04-11 | 1986-04-11 | Sintered cam shaft |
Country Status (3)
| Country | Link |
|---|---|
| JP (1) | JPS62271914A (en) |
| DE (1) | DE3712107A1 (en) |
| GB (1) | GB2189811B (en) |
Families Citing this family (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE3633879A1 (en) * | 1986-10-04 | 1988-04-14 | Supervis Ets | HIGH-WEAR-RESISTANT IRON-NICKEL-COPPER-MOLYBDAEN-SINTER ALLOY WITH PHOSPHORUS ADDITIVE |
| CN105618761A (en) * | 2014-11-05 | 2016-06-01 | 株式会社瑞进凸轮轴 | Sintering body suitable for sintering connection |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS5763658A (en) * | 1980-10-03 | 1982-04-17 | Kawasaki Steel Corp | Manufacture of sintered machine parts with superior specific strength |
| JPS583901A (en) * | 1981-07-01 | 1983-01-10 | Toyota Motor Corp | Manufacture of sliding member |
| JPS583950A (en) * | 1981-07-01 | 1983-01-10 | Toyota Motor Corp | Ohc type valve system |
| JPS58107470A (en) * | 1981-12-19 | 1983-06-27 | Kawasaki Steel Corp | Preparation of sintered parts |
| JPS6033343A (en) * | 1983-08-03 | 1985-02-20 | Nippon Piston Ring Co Ltd | Wear resistance sintered alloy |
Family Cites Families (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB1576143A (en) * | 1977-07-20 | 1980-10-01 | Brico Eng | Sintered metal articles |
| JPS55145151A (en) * | 1979-04-26 | 1980-11-12 | Nippon Piston Ring Co Ltd | Wear resistant sintered alloy material for internal combustion engine |
| JPS5813619B2 (en) * | 1979-05-17 | 1983-03-15 | 日本ピストンリング株式会社 | Wear-resistant iron-based sintered alloy material for internal combustion engines |
| JPS5918463B2 (en) * | 1980-03-04 | 1984-04-27 | トヨタ自動車株式会社 | Wear-resistant sintered alloy and its manufacturing method |
| JPS5837158A (en) * | 1981-08-27 | 1983-03-04 | Toyota Motor Corp | Wear resistant sintered alloy |
| JPS5925959A (en) * | 1982-07-28 | 1984-02-10 | Nippon Piston Ring Co Ltd | Valve seat made of sintered alloy |
| JPS6033344A (en) * | 1983-08-03 | 1985-02-20 | Nippon Piston Ring Co Ltd | Wear resistance sintered alloy |
| GB2153850B (en) * | 1984-02-07 | 1987-08-12 | Nippon Piston Ring Co Ltd | Method of manufacturing a camshaft |
| JPH0610321B2 (en) * | 1985-06-17 | 1994-02-09 | 日本ピストンリング株式会社 | Abrasion resistant sintered alloy |
-
1986
- 1986-04-11 JP JP8358186A patent/JPS62271914A/en active Pending
-
1987
- 1987-04-03 GB GB8708020A patent/GB2189811B/en not_active Expired
- 1987-04-10 DE DE19873712107 patent/DE3712107A1/en active Granted
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS5763658A (en) * | 1980-10-03 | 1982-04-17 | Kawasaki Steel Corp | Manufacture of sintered machine parts with superior specific strength |
| JPS583901A (en) * | 1981-07-01 | 1983-01-10 | Toyota Motor Corp | Manufacture of sliding member |
| JPS583950A (en) * | 1981-07-01 | 1983-01-10 | Toyota Motor Corp | Ohc type valve system |
| JPS58107470A (en) * | 1981-12-19 | 1983-06-27 | Kawasaki Steel Corp | Preparation of sintered parts |
| JPS6033343A (en) * | 1983-08-03 | 1985-02-20 | Nippon Piston Ring Co Ltd | Wear resistance sintered alloy |
Also Published As
| Publication number | Publication date |
|---|---|
| GB8708020D0 (en) | 1987-05-07 |
| GB2189811B (en) | 1989-12-06 |
| DE3712107A1 (en) | 1987-10-22 |
| GB2189811A (en) | 1987-11-04 |
| DE3712107C2 (en) | 1993-09-16 |
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