JP2000087118A - Composite parts of sintered member and refined member and production thereof - Google Patents

Composite parts of sintered member and refined member and production thereof

Info

Publication number
JP2000087118A
JP2000087118A JP10262210A JP26221098A JP2000087118A JP 2000087118 A JP2000087118 A JP 2000087118A JP 10262210 A JP10262210 A JP 10262210A JP 26221098 A JP26221098 A JP 26221098A JP 2000087118 A JP2000087118 A JP 2000087118A
Authority
JP
Japan
Prior art keywords
sintered
smelted
carrier
parts
refined
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
JP10262210A
Other languages
Japanese (ja)
Inventor
Takashi Okamura
孝▲巳▼ 岡村
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.)
Sumitomo Electric Industries Ltd
Original Assignee
Sumitomo Electric Industries 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 Sumitomo Electric Industries Ltd filed Critical Sumitomo Electric Industries Ltd
Priority to JP10262210A priority Critical patent/JP2000087118A/en
Publication of JP2000087118A publication Critical patent/JP2000087118A/en
Pending legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16HGEARING
    • F16H57/00General details of gearing
    • F16H57/08General details of gearing of gearings with members having orbital motion
    • F16H57/082Planet carriers

Abstract

PROBLEM TO BE SOLVED: To provide lightweight and inexpensive composite parts of a sintered member and a refined member free from the partial shortage of rigidity. SOLUTION: A sintered member in primary parts is joined to a refined member of secondary parts by brazing, the refined member in the secondary parts is joined to a refined member of third parts and for example, a planetary carrier in which the sintered member in the primary parts is composed of a carrier bridge 8, the refined member in the secondary parts is composed of a carrier plate 9 and the refined member in the third parts is composed of a helical internal gear 10, is useful.

Description

【発明の詳細な説明】DETAILED DESCRIPTION OF THE INVENTION

【0001】[0001]

【発明の属する技術分野】本発明は焼結部材と溶製部材
との複合部品であって、自動車等の自動変速機に用いる
プラネタリキャリア及び歯車、カムのような回転部品の
構成及びその製造法に関する。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a composite part of a sintered member and a smelted member, and the construction of a planetary carrier and a rotating part such as a gear and a cam used in an automatic transmission of an automobile and a method of manufacturing the same. About.

【0002】[0002]

【従来の技術】乗用車等の自動変速機に使用されるプラ
ネタリキャリアは、従来、溶製材(少なくとも溶解、鋳
造の工程を得て製造されるものであって、鋼、軟鋼、工
具鋼、合金鋼、鋳鉄を含む。)を機械加工して製造され
ているが、機械加工の工数が多く、コスト高となるため
に、機械加工が少なく歩留まりの高い焼結部材の使用が
検討されている。
2. Description of the Related Art Planetary carriers used in automatic transmissions of passenger cars and the like are conventionally manufactured by melting and casting (at least melting and casting processes, and include steel, mild steel, tool steel, and alloy steel). , Including cast iron). However, since the number of man-hours required for machining is increased and the cost is increased, the use of a sintered member that requires less machining and has a high yield is being studied.

【0003】また、プレス成型した溶製材である鋼製の
板を用いてプラネタリキャリアのキャリヤブリッジを作
製する場合では、鋼製の板は一定の板厚(t:図1に示
す)であるために、キャリヤブリッジの柱部周辺も同じ
厚みとなる。
[0003] When a carrier bridge of a planetary carrier is manufactured by using a steel plate which is an ingot formed by press molding, the steel plate has a constant thickness (t: shown in FIG. 1). In addition, the periphery of the column portion of the carrier bridge has the same thickness.

【0004】高負荷がキャリヤブリッジの柱部にかかる
ような場合には、その柱部の厚み(T:図1に示す)を
大きくせねばならない。ところが、プレス成型した鋼製
の板を用いてプラネタリキャリアのキャリヤブリッジを
作製する場合は、t=Tとなる。
When a high load is applied to the column of the carrier bridge, the thickness of the column (T: shown in FIG. 1) must be increased. However, when a carrier bridge of a planetary carrier is manufactured using a press-formed steel plate, t = T.

【0005】しかし、焼結部材による方法では、負荷に
応じてt<<Tとすることが可能となり、形状の設計自
由度が高い焼結部材による方法が検討されている理由に
もなっている。
However, in the method using a sintered member, t << T can be set according to the load, which is the reason why a method using a sintered member having a high degree of freedom in shape design is being studied. .

【0006】なお、上記の事柄はプラネタリキャリアに
限らず一般の機械部品についても、適材適所によるコス
トダウンの設計思想により、シャフト等の長いものは溶
製部材、シャフト、カム等の複雑形状のものは焼結部材
によるものが検討されている。
The above-mentioned matter is not limited to the planetary carrier, but also for general mechanical parts, due to the design concept of cost reduction by using the right material in the right place, long ones such as shafts have complicated shapes such as melted members, shafts and cams. The use of a sintered member has been studied.

【0007】従来は、例えば図5に示すようなプラネタ
リキャリヤがある。すなわち、シャフト孔12を有する
板状体28と側板15からなる焼結部材18及び内スプ
ライン13を有する板状体14からなる焼結部材19を
製造する。
Conventionally, for example, there is a planetary carrier as shown in FIG. That is, a sintered member 18 composed of a plate 28 having the shaft hole 12 and the side plate 15 and a sintered member 19 composed of the plate 14 having the inner spline 13 are manufactured.

【0008】別々に製造した2つの焼結部材18、19
を重ねて、側板15の端面16に対応する位置に設けら
れた貫通孔17にロー材を挿入し、ロー材を加熱し、重
ねた2つの焼結部材18、19をロー付け接合するもの
である。
Two separately manufactured sintered members 18, 19
Are stacked, a brazing material is inserted into a through hole 17 provided at a position corresponding to the end face 16 of the side plate 15, the brazing material is heated, and the two sintered members 18 and 19 are brazed and joined. is there.

【0009】なお、ロー付け接合の関連技術として、本
出願人が出願した特公昭58−34524号、あるいは
特公昭57−44433号各公報において、少なくとも
一方の圧粉体に凹部を形成し、その凹部に押し固めたロ
ー材を挿入し焼結することにより、両焼結部材の接合面
にロー材が浸透して接合する技術を開示している。
As a related technique of brazing, Japanese Patent Publication No. 58-34524 or Japanese Patent Publication No. 57-44433 filed by the present applicant discloses that at least one compact is formed with a concave portion. It discloses a technique in which a brazing material compacted into a recess is inserted and sintered so that the brazing material permeates and joins the joining surfaces of the two sintered members.

【0010】さらに、特公平6−37644号公報に
は、焼結部材用圧粉体の焼結と同時に、2つの焼結部材
のロー付け接合を行って、プラネタリキャリアを製造す
る方法が開示されている。
Furthermore, Japanese Patent Publication No. 6-37644 discloses a method of manufacturing a planetary carrier by simultaneously sintering a green compact for a sintered member and brazing the two sintered members. ing.

【0011】その方法では、2つの各焼結部材によって
空間(例えば、ピニオンギヤを装着する空間)を形成す
る構造を得るために、焼結用粉末から一体に成型するこ
とを避けて、2つの別々の圧粉体を成型し、両者を焼結
して、ロー付け接合を行っている。
According to the method, in order to obtain a structure in which a space (for example, a space for mounting a pinion gear) is formed by each of the two sintered members, two separate members are avoided from being integrally molded from the sintering powder. Are compacted, sintered and sintered.

【0012】[0012]

【発明が解決しようとする課題】上記のようなプラネタ
リキャリアを2つの部分に分け、別々の圧粉体を成型
し、2つを焼結、ロー付け接合する場合、プラネタリキ
ャリアのインターナルギヤもキャリヤブリッジと同じ焼
結部材となるので、インターナルギヤを溶製部材である
鋼にしたいという要求が生じる。ところが、プラネタリ
キャリアのインターナルギヤ部が鋼であるものの製造
は、従来の焼結法では困難であった。
When the planetary carrier as described above is divided into two parts, separate green compacts are formed, and the two are sintered and brazed, the internal gear of the planetary carrier is also required. Since the sintered member is the same as the carrier bridge, there is a demand that the internal gear be made of steel which is a smelting member. However, it has been difficult to manufacture a planetary carrier whose internal gear portion is made of steel by a conventional sintering method.

【0013】また、上記のようなプラネタリキャリアを
2つの部分に分け、別々の圧粉体を成型し、2つを焼
結、ロー付け接合する場合には、ロー付け接合の熱影響
による歪みの発生により、プラネタリキャリアの部分の
寸法に狂いが生じ易いという問題がある。
Further, when the planetary carrier as described above is divided into two parts, separate green compacts are formed, and the two are sintered and brazed, the distortion caused by the heat effect of the brazed joint is reduced. Due to the occurrence, there is a problem that the dimensions of the planetary carrier are likely to be out of order.

【0014】さらに、従来の溶製材を機械加工してプラ
ネタリキャリア等の一般の機械部品が製造される工程に
は、溶接工程があって、電子ビーム装置等の溶接装置が
設置されている。この設置済みの溶接装置を有効に使用
できるため経済的である。
Further, in a process of manufacturing a general mechanical part such as a planetary carrier by machining a conventional ingot material, there is a welding process, and a welding device such as an electron beam device is installed. It is economical because the installed welding device can be used effectively.

【0015】本発明においては、2つの別々の圧粉体を
成型し、2つを焼結、ロー付け接合するかわりに、一体
に成型した圧粉体を使用し、問題の解決を行うものであ
る。
In the present invention, instead of molding two separate green compacts and sintering and brazing the two, a single green compact is used to solve the problem. is there.

【0016】[0016]

【課題を解決するための手段】第1部品の焼結部材が第
2部品の溶製部材にロー付け接合され、第2部品の溶製
部材が第3部品の溶製部材に接合されている焼結部材と
溶製部材との複合部品が有用である。
SUMMARY OF THE INVENTION A sintered member of a first part is brazed to a smelted member of a second part, and a smelted member of the second part is joined to a smelted member of a third part. A composite component of a sintered member and a smelted member is useful.

【0017】第一部品の焼結部材がキャリアブリッジ、
第2部品の溶製部材がキャリアプレート、第3部品の溶
製部材がヘリカルインターナルギヤーで構成されたプラ
ネタリキャリアが有用である。
The sintered member of the first part is a carrier bridge,
It is useful to use a planetary carrier in which the smelting member of the second part is a carrier plate and the smelting member of the third part is a helical internal gear.

【0018】第1部品の焼結部材用圧粉体と第2部品の
溶製部材を嵌合し、第1部品と第2部品の接合面に接す
る第2部品に設けた貫通孔にロー材を挿入し、焼結部材
用圧粉体の焼結と同時に、第2部品と接合面でロー付け
接合を行う。
The sintered compact of the first part and the smelting member of the second part are fitted to each other, and the brazing material is inserted into a through-hole provided in the second part in contact with the joint surface between the first and second parts. And, at the same time as sintering the green compact for a sintered member, brazing is performed on the bonding surface with the second component.

【0019】次に、第2部品を第3部品である溶製部材
に接合して焼結部材と溶製部材との複合部品を製造す
る。第2部品と第3部品の接合は、電子ビーム溶接、ア
ーク溶接、ミグ溶接、アルゴン溶接のいずれかで形成さ
れる。
Next, the second part is joined to the smelted member as the third part to produce a composite part of the sintered member and the smelted member. The joint between the second component and the third component is formed by any one of electron beam welding, arc welding, MIG welding, and argon welding.

【0020】[0020]

【発明の実施の形態】従来、図4に示すような焼結部材
1、2、3を各々ロー付け接合した焼結部品が作製され
ている。焼結部材を一体で成型することを避けて、2つ
の圧粉体による焼結部材圧粉体1、2に分けて、空間2
0(ピニオンギヤ等を装着する部分)を作っている。
DESCRIPTION OF THE PREFERRED EMBODIMENTS Conventionally, sintered parts have been produced by brazing and joining sintered members 1, 2, and 3 as shown in FIG. In order to avoid molding the sintered member integrally, the sintered member is divided into two sintered compacts 1 and 2 by two compacts, and a space 2 is formed.
0 (the part where the pinion gear etc. are mounted).

【0021】このロー付け接合された2つの焼結部材
1、2の膨張や収縮等に差がある場合、両者の焼結とロ
ー付け接合が同時でなかろうと、あるいは同時であろう
と、一体に成型焼結したものと比して、その焼結部品に
歪みが生じる。また、図4のような空間20を持たせた
場合、焼結部材3を溶製部材4にする場合は、両者の接
合は、一般に容易ではない。
If there is a difference in the expansion and contraction of the two brazed sintered members 1 and 2, whether or not the sintering and brazing of the two members are performed at the same time or at the same time, they are integrated. Distortion occurs in the sintered part as compared with the molded and sintered one. In addition, when the space 20 as shown in FIG. 4 is provided, and when the sintered member 3 is made of the smelted member 4, the joining of the two is generally not easy.

【0022】そこで、図3に示すように、多段成型等に
よって作製した圧粉体を焼結することにより、空間20
を持たせた焼結部材5と溶製部材6をロー付け接合す
る。
Therefore, as shown in FIG. 3, by sintering the compact formed by multi-stage molding or the like, the space 20
The sintering member 5 and the smelting member 6 having the above are brazed and joined.

【0023】その場合、圧粉体の焼結と前記ロー付けと
を同時に行えば、両者の歪みが同時に除去され、歪みの
ない部材5、6を得ることが出来る。また、溶製部材
6、7は共に溶製材であるため、溶接により歪みのない
強固な接合が可能である。
In this case, if the sintering of the green compact and the brazing are performed at the same time, the distortion of both of them is removed at the same time, and the members 5 and 6 having no distortion can be obtained. Further, since both of the smelting members 6 and 7 are smelting materials, strong joining without distortion is possible by welding.

【0024】なお、概略を図2に示すように、外周がギ
ヤのような複雑な形状(ギヤの図示省略)を持つ焼結部
材22で、溶製部材である円柱部材若しくは円筒部材を
芯部24としたものを、前記焼結部材22用圧粉体の焼
結と同時に、焼結部材と溶製部材をロー付け接合し、溶
製部材である円柱部材若しくは円筒部材を溶製部材27
に接合した機械部品(回転部品等)の製造も同様に可能
である。
As shown schematically in FIG. 2, the sintered member 22 has a complex shape such as a gear (not shown), and a cylindrical member or a cylindrical member, which is a smelted member, has a core portion. At the same time as the sintering of the green compact for the sintering member 22, the sintering member and the smelting member are brazed and joined, and the cylindrical member or the cylindrical member, which is the smelting member, is smelted to the
It is also possible to manufacture mechanical parts (rotary parts and the like) joined to the same.

【0025】[0025]

【実施例】以下、図示した実施例にもとづき、本発明を
さらに詳細に説明する。図1((a)横断面図、(b)
は下方からの図である。)に示すように、この実施例
は、複合部品であるプラネタキャリアを示すもので、中
央にシャフト穴を持つボス25を有し、ボス25と反対
側の周辺部に複数の柱部26により、ピニオンギヤを装
着する空間20を設けた焼結により形成されるキャリア
ブリッジ8、鋼製の板状部材をプレス仕上げしたキャリ
アプレート9、鋼製の円筒部材の内側面を機械加工によ
りギヤー(歯車)23に加工仕上げしたヘリカルインタ
ーナルギヤー10からなる。
DESCRIPTION OF THE PREFERRED EMBODIMENTS The present invention will be described below in more detail with reference to the illustrated embodiments. FIG. 1 ((a) cross-sectional view, (b)
Is a view from below. ), This embodiment shows a planetary carrier which is a composite part, which has a boss 25 having a shaft hole in the center, and a plurality of pillars 26 on a peripheral portion opposite to the boss 25. A carrier bridge 8 formed by sintering having a space 20 for mounting a pinion gear, a carrier plate 9 obtained by press-finishing a steel plate-like member, and a gear (gear) 23 by machining the inner surface of a steel cylindrical member. The helical internal gear 10 is machined and finished.

【0026】本発明品の製造方法を示す。CuとCを含
有した焼結用鉄粉を密度6.8mg/m3になるよう
に、キャリヤブリッジ8となる圧粉体を多段成型により
作製した。
A method for producing the product of the present invention will be described. A green compact to be the carrier bridge 8 was produced by multi-stage molding so that the iron powder for sintering containing Cu and C had a density of 6.8 mg / m 3 .

【0027】また、鋼製の板状部材をプレス仕上げし
て、図1(b)に示すように、5ヶ所の貫通孔11を外
周部に設けたキャリアプレート9を製造する。そのキャ
リヤプレート9と、キャリアブリッジ8となる圧粉体の
柱部26に設けた凸部(図示せず。)を嵌合する。
Further, a steel plate member is press-finished to manufacture a carrier plate 9 having five through holes 11 provided on the outer periphery as shown in FIG. 1B. The carrier plate 9 is fitted with a projection (not shown) provided on the column 26 of the green compact to be the carrier bridge 8.

【0028】ロー付け穴であるキャリヤプレート9の貫
通孔11に、Ni−Cu−Mn−Fe−Si−B系ロー
材を充填し、上記嵌合したキャリヤブリッジ8となる圧
粉体とキャリヤプレート9を、温度1130℃で時間1
5分の条件で、焼結及びロー付け接合を同時に行った。
A through hole 11 of the carrier plate 9 which is a brazing hole is filled with a Ni-Cu-Mn-Fe-Si-B-based brazing material. 9 for 1 hour at a temperature of 1130 ° C.
Sintering and brazing were performed simultaneously under the conditions of 5 minutes.

【0029】そして、通常の電子ビーム溶接にて、図1
(a)に示すように、内側面をギヤー(歯車)23に旋
盤加工仕上げされた鋼製部材であるヘリカルインターナ
ルギヤー10に、キャリヤプレート9が嵌め込まれてい
る外周面21を接合する。
Then, by ordinary electron beam welding, FIG.
As shown in (a), an outer peripheral surface 21 on which a carrier plate 9 is fitted is joined to a helical internal gear 10 which is a steel member whose inner surface is lathe-finished into a gear (gear) 23.

【0030】上記電子ビーム溶接の替わりに、通常のミ
グ溶接でも十分な接合強度がえられたのは、接合すべき
両者が鋼製であることによる。また、このプラネタキャ
リアは、歪みもなく一体化されていた。
Sufficient joining strength was obtained by ordinary MIG welding instead of the electron beam welding because the two to be joined are made of steel. Further, this planetary carrier was integrated without distortion.

【0031】[0031]

【発明の効果】本発明による焼結部材と溶製部材との複
合部品は、焼結部材で形成された部分は鋼で形成したも
のより軽量で、負荷に応じた厚さを設計できるために部
分的な剛性不足の発生がなく、しかも安価に提供でき
る。
According to the composite part of the sintered member and the smelted member according to the present invention, the portion formed by the sintered member is lighter than the one formed by steel, and the thickness can be designed according to the load. There is no partial lack of rigidity, and it can be provided at low cost.

【0032】例えば、ピニオンギヤ等を装着すべき空間
を、一体化された焼結部材で作製された複合部品である
プラネタリキャリアは、近年の自動車エンジントルクア
ップの要請にも適合した自動変速機に使用できる。
For example, a planetary carrier, which is a composite part in which a space in which a pinion gear or the like is to be mounted is made of an integrated sintered member, is used for an automatic transmission that also meets recent demands for increasing the engine torque of an automobile. it can.

【図面の簡単な説明】[Brief description of the drawings]

【図1】本発明による、焼結部材と溶製部材との複合部
品であるプラネタリキャリアを示す図で、(a)は横断
面、(b)は下方からの図である。
FIG. 1 is a view showing a planetary carrier which is a composite part of a sintered member and a smelted member according to the present invention, wherein (a) is a cross-sectional view and (b) is a view from below.

【図2】焼結部材と溶製部材との複合部品の別の図であ
る。
FIG. 2 is another view of a composite component of a sintered member and a smelted member.

【図3】本発明による、焼結部材と溶製部材との複合部
品の別の図である。
FIG. 3 is another view of a composite part of a sintered member and a smelted member according to the present invention.

【図4】2つの焼結部材1、2で空間20を作っている
部品の従来図である。
FIG. 4 is a conventional view of a part in which a space 20 is formed by two sintered members 1 and 2;

【図5】プラネタリキャリアの従来図である。FIG. 5 is a conventional view of a planetary carrier.

【符号の説明】[Explanation of symbols]

1、2、3、5、18、19、22:焼結部材 4、6、7、27:溶製部材 8:キャリヤブリッジ 9:キャリヤプレート 10:ヘリカルインターナルギヤー 11、17:貫通孔 12:シャフト孔 13:内スプライン 14、28:板状体 15:側板 16:端面 20:空間 21:外周面 23:ギヤ 24:芯部 25:ボス 26:柱部 1, 2, 3, 5, 18, 19, 22: Sintered member 4, 6, 7, 27: Smelted member 8: Carrier bridge 9: Carrier plate 10: Helical internal gear 11, 17: Through hole 12: Shaft hole 13: Internal spline 14, 28: Plate 15: Side plate 16: End surface 20: Space 21: Outer peripheral surface 23: Gear 24: Core portion 25: Boss 26: Column portion

Claims (4)

【特許請求の範囲】[Claims] 【請求項1】 第1部品の焼結部材が第2部品の溶製部
材にロー付け接合され、前記第2部品の溶製部材が第3
部品の溶製部材に接合されていることを特徴とする焼結
部材と溶製部材との複合部品。
1. A sintering member of a first part is brazed to a smelting member of a second part, and the smelting member of the second part is a third member.
A composite part comprising a sintered member and a smelted member, which is joined to the smelted member of the part.
【請求項2】 前記第1部品の焼結部材がキャリアブリ
ッジ、前記第2部品の溶製部材がキャリアプレート、前
記第3部品の溶製部材がヘリカルインターナルギヤーで
構成されたプラネタリキャリアである請求項1記載の焼
結部材と溶製部材との複合部品。
2. A sintering member of the first component is a carrier bridge, a smelting member of the second component is a carrier plate, and a smelting member of the third component is a planetary carrier including a helical internal gear. A composite part comprising the sintered member according to claim 1 and a smelted member.
【請求項3】 第1部品の焼結部材用圧粉体と第2部品
の溶製部材を嵌合し、第1部品と第2部品の接合面に接
する前記第2部品に設けた貫通孔にロー材を挿入し、焼
結部材用圧粉体の焼結と同時に、前記第2部品と前記接
合面でロー付け接合を行い、次に、前記第2部品を第3
部品である溶製部材に接合することを特徴とする焼結部
材と溶製部材との複合部品の製造方法。
3. A through-hole formed in the second part, which fits the sintered compact of the first part and the smelted member of the second part, and is in contact with the joining surface of the first part and the second part. And, at the same time as the sintering of the green compact for a sintered member, brazing is performed on the joining surface with the second component.
A method for producing a composite part of a sintered member and a smelted member, wherein the composite member is joined to a smelted member as a part.
【請求項4】 前記第2部品と前記第3部品の接合が、
電子ビーム溶接、アーク溶接、ミグ溶接、アルゴン溶接
のいずれかで形成されることを特徴とする請求項3記載
の焼結部材と溶製部材との複合部品の製造方法。
4. The bonding of the second part and the third part,
The method for producing a composite part of a sintered member and a smelted member according to claim 3, wherein the composite part is formed by any one of electron beam welding, arc welding, MIG welding, and argon welding.
JP10262210A 1998-09-17 1998-09-17 Composite parts of sintered member and refined member and production thereof Pending JP2000087118A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP10262210A JP2000087118A (en) 1998-09-17 1998-09-17 Composite parts of sintered member and refined member and production thereof

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP10262210A JP2000087118A (en) 1998-09-17 1998-09-17 Composite parts of sintered member and refined member and production thereof

Publications (1)

Publication Number Publication Date
JP2000087118A true JP2000087118A (en) 2000-03-28

Family

ID=17372617

Family Applications (1)

Application Number Title Priority Date Filing Date
JP10262210A Pending JP2000087118A (en) 1998-09-17 1998-09-17 Composite parts of sintered member and refined member and production thereof

Country Status (1)

Country Link
JP (1) JP2000087118A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2009242821A (en) * 2008-03-28 2009-10-22 Hitachi Powdered Metals Co Ltd Manufacturing method of compound sintered machine part
JP2015178111A (en) * 2014-03-18 2015-10-08 トヨタ自動車株式会社 Part joining method
CN105665711A (en) * 2016-01-29 2016-06-15 东睦新材料集团股份有限公司 Preparation method for powder metallurgy rotating hub gear

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2009242821A (en) * 2008-03-28 2009-10-22 Hitachi Powdered Metals Co Ltd Manufacturing method of compound sintered machine part
JP2015178111A (en) * 2014-03-18 2015-10-08 トヨタ自動車株式会社 Part joining method
CN105665711A (en) * 2016-01-29 2016-06-15 东睦新材料集团股份有限公司 Preparation method for powder metallurgy rotating hub gear

Similar Documents

Publication Publication Date Title
US6874231B2 (en) Method of manufacturing a rigid internal gear of a wave gear device
US6863636B2 (en) Pinion carrier for planetary gear train and method of making same
CN101218050A (en) Composite assemblies including powdered metal components
EP0862706B1 (en) Duplex sprocket/gear construction and method of making same
JPS60149703A (en) Production of cam shaft
JP4637427B2 (en) Planet carrier manufacturing method
CN100585222C (en) Torque transmitting assembly and method of producing
US5860882A (en) Process for manufacturing phased sprocket assemblies by capacitor discharge welding
JP3085627B2 (en) Synchronizer ring
JP2000087118A (en) Composite parts of sintered member and refined member and production thereof
US5197351A (en) Cam shaft and process for manufacturing the same
JP5087449B2 (en) Manufacturing method of composite sintered machine parts
CN101313160B (en) Sliding sleeve and method for producing sliding sleeve
JP4992840B2 (en) Carrier for planetary gear device for vehicle and method for manufacturing the same
JPH0637644B2 (en) Manufacturing method of planetary carrier
JPS62177357A (en) Cam piece having oil port and manufacture thereof
JPH0336454Y2 (en)
JP2517752B2 (en) Method of joining sintered parts
JPH06117519A (en) Bevel gear
JPS6132083Y2 (en)
JPH0675770B2 (en) Method for manufacturing press-formed product
JPH07286553A (en) Manufacture of cylinder block
JPS6238727A (en) Manufacture of cam shaft
JPH10314922A (en) Complex member and manufacture thereof
JP2002361397A (en) Manufacturing method for gear