JPH0368257B2 - - Google Patents

Info

Publication number
JPH0368257B2
JPH0368257B2 JP59025498A JP2549884A JPH0368257B2 JP H0368257 B2 JPH0368257 B2 JP H0368257B2 JP 59025498 A JP59025498 A JP 59025498A JP 2549884 A JP2549884 A JP 2549884A JP H0368257 B2 JPH0368257 B2 JP H0368257B2
Authority
JP
Japan
Prior art keywords
shaft
recess
component
groove
protrusion
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 - Lifetime
Application number
JP59025498A
Other languages
Japanese (ja)
Other versions
JPS60172769A (en
Inventor
Genkichi Umeba
Osamu Hirakawa
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.)
Nippon Piston Ring Co Ltd
Original Assignee
Nippon Piston Ring Co 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 Nippon Piston Ring Co Ltd filed Critical Nippon Piston Ring Co Ltd
Priority to JP59025498A priority Critical patent/JPS60172769A/en
Publication of JPS60172769A publication Critical patent/JPS60172769A/en
Publication of JPH0368257B2 publication Critical patent/JPH0368257B2/ja
Granted legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16H—GEARING
    • F16H57/00—General details of gearing
    • F16H57/02—Gearboxes; Mounting gearing therein
    • F16H57/027—Gearboxes; Mounting gearing therein characterised by means for venting gearboxes, e.g. air breathers
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16D—COUPLINGS FOR TRANSMITTING ROTATION; CLUTCHES; BRAKES
    • F16D1/00—Couplings for rigidly connecting two coaxial shafts or other movable machine elements
    • F16D1/06—Couplings for rigidly connecting two coaxial shafts or other movable machine elements for attachment of a member on a shaft or on a shaft-end
    • F16D1/08—Couplings for rigidly connecting two coaxial shafts or other movable machine elements for attachment of a member on a shaft or on a shaft-end with clamping hub; with hub and longitudinal key
    • F16D1/0876—Couplings for rigidly connecting two coaxial shafts or other movable machine elements for attachment of a member on a shaft or on a shaft-end with clamping hub; with hub and longitudinal key with axial keys and no other radial clamping

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Powder Metallurgy (AREA)
  • Valve-Gear Or Valve Arrangements (AREA)
  • Gears, Cams (AREA)
  • Snaps, Bayonet Connections, Set Pins, And Snap Rings (AREA)

Description

【発明の詳細な説明】 本発明は、液相焼結により、カムロブ、ジヤー
ナル等の構成部品をシヤフトに結合して組立てカ
ムシヤフトを製造する際の仮止め構造に関する。
DETAILED DESCRIPTION OF THE INVENTION The present invention relates to a temporary fixing structure for manufacturing an assembled camshaft by bonding component parts such as a cam lobe and journal to a shaft by liquid phase sintering.

組立てカムシヤフトの製造では、液相焼結過程
で、カムロブ、ジヤーナル等の構成部品をシヤフ
トの所定位置に結合する必要があるため、シヤフ
トに対するこれらの構成部品の軸方向及び周囲方
向の正確な位置決めが重要な課題である。従来、
かかる位置決めは、液相焼結に先立つて、構成部
品、シヤフトにそれぞれ貫通孔を設け、これらの
貫通孔に油孔付き位置決めピンを通すことによつ
て行なわれてきた。しかしながら、この方法で
は、構成部品を構成する粉末焼結材の液相焼結に
よる収縮率を考慮して、ピンの径よりも大きな径
のピン孔を構成部品に設けなければならず、した
がつて、構成部品及びシヤフトに設けたピン孔に
ピンを通したとき、構成部品のピン孔と位置決め
ピンとの間に隙間が生じ、液相焼結中にこの隙間
の分、構成部品がシヤフトに対して変位し、時に
は脱落する場合さえあつた。また、ピン孔は、構
成部品とシヤフトに、互に一線を成すように設け
られなければならないので、精度の高い加工が必
要となり、したがつて加工作業に困難があつた。
In the manufacture of prefabricated camshafts, components such as cam lobes and journals must be bonded to predetermined positions on the shaft during the liquid-phase sintering process, so accurate axial and circumferential positioning of these components relative to the shaft is critical. This is an important issue. Conventionally,
Such positioning has been performed by providing through holes in each of the component parts and the shaft prior to liquid phase sintering, and passing positioning pins with oil holes through these through holes. However, in this method, a pin hole with a diameter larger than the pin diameter must be provided in the component part, taking into consideration the shrinkage rate due to liquid phase sintering of the powder sintered material that makes up the component part. Therefore, when a pin is passed through the pin hole provided in the component and the shaft, a gap is created between the pin hole of the component and the positioning pin, and during liquid phase sintering, the component is attached to the shaft by this gap. They were displaced and sometimes even fell off. Further, since the pin holes must be provided in the component parts and the shaft so as to be in line with each other, highly accurate machining is required, and therefore machining operations are difficult.

本発明の目的は、上記欠点に鑑みて、シヤフト
に対する構成部品の位置決め精度を高めうる組立
てカムシヤフトの仮止め構成を提供するにある。
SUMMARY OF THE INVENTION In view of the above-mentioned drawbacks, an object of the present invention is to provide a temporary fixing structure for an assembled camshaft that can improve the positioning accuracy of components relative to the shaft.

本発明によれば、カムロブ、ジヤーナル等の構
成部品をシヤフトに液相焼結によつて一体的に結
合される組立てカムシヤフトの仮止め構造におい
て、シヤフトの外周部にはその軸方向に所定幅の
溝を設け、さらに、シヤフト外周部の円周方向に
溝と直交する横断面半円形の凹部を設け、上記構
成部品の内周部には、その軸方向に、上記溝にぴ
つたりと嵌まる所定幅の突出部を形成し、該突出
部にその長さの中間のところでそれを横切る凹部
を設け、上記両凹部は互いに対向し、構成部品の
内周面の一部と協働して空所を構成し、該空所に
弾性部材を配置し、該弾性部材はその周面が上記
対向した2つの凹部の内面に係合してシヤフトに
対する構成部品の軸方向の変位を阻止し、さら
に、シヤフトの溝内への構成部品の突出部の嵌め
込みによつて、シヤフトに対する構成部品の周囲
方向の変位を阻止することを特徴とする。
According to the present invention, in the temporary fixing structure of an assembled camshaft in which component parts such as a cam lobe and a journal are integrally joined to the shaft by liquid phase sintering, the outer circumference of the shaft has a predetermined width in the axial direction. A groove is provided, and a recess with a semicircular cross section perpendicular to the groove is provided in the circumferential direction of the outer circumference of the shaft, and the inner circumference of the component is tightly fitted into the groove in the axial direction. A protrusion of a predetermined width is formed, and the protrusion is provided with a recess that traverses it at a midpoint of its length, the two recesses facing each other and cooperating with a portion of the inner circumferential surface of the component to form an empty space. an elastic member is disposed in the cavity, and the elastic member has a circumferential surface that engages with an inner surface of the two opposed recesses to prevent axial displacement of the component relative to the shaft; , characterized in that circumferential displacement of the component relative to the shaft is prevented by fitting the protrusion of the component into the groove of the shaft.

本発明を図面を参照して説明すれば、第1A図
及び第1B図には、本発明による組立てカムシヤ
フトが示されており、シヤフト2がカムロブ3に
設けた穴32に嵌まつている。
To illustrate the invention with reference to the drawings, FIGS. 1A and 1B show an assembled camshaft according to the invention, in which the shaft 2 fits into a hole 32 in the cam lobe 3. FIG.

第2A図、第2B図及び第2C図に示すよう
に、所定幅を有し、かつ、横断面が長方形の溝5
がシヤフト2の長さ全体に亘つてその外周部に延
びている。また、凹部21がシヤフト2の円周方
向に溝5と直交して、カムロブ、ジヤーナル等の
構成部品の取付け位置に応じて所定の間隔をへだ
てて複数個設けられている。凹部21の各々は横
断面が半円形であつてシヤフト2の円周方向に所
定長さ延びており、したがつて、各凹部21と溝
5と直交し、一方、後述する理由のために、凹部
21の深さは、凹部21内に配置する弾性部材4
の厚さよりも大きいのが望ましい。
As shown in FIGS. 2A, 2B, and 2C, a groove 5 having a predetermined width and a rectangular cross section
extends along the entire length of the shaft 2 at its outer periphery. Further, a plurality of recesses 21 are provided in the circumferential direction of the shaft 2, perpendicular to the groove 5, and spaced apart at predetermined intervals depending on the mounting positions of components such as cam lobes and journals. Each of the recesses 21 has a semicircular cross section and extends for a predetermined length in the circumferential direction of the shaft 2, so that each recess 21 and the groove 5 are perpendicular to each other. The depth of the recess 21 is determined by the elastic member 4 disposed within the recess 21.
It is preferable that the thickness be greater than the thickness of .

同様に、第3A図及び第3B図に示すように、
溝5にぴつたりと嵌るように、溝5の幅よりもわ
ずかに小さい幅を有し、横断面長方形の突出部6
が、シヤフトに嵌るカムロブ3の穴32の内周部
の所定個所に、カムロブの軸方向に形成されてい
る。また、凹部61が突出部6を横切るように設
けられている。凹部61は突出部6の長さの中間
のところに設けられるのが望ましい。というの
は、カムロブのような形状の焼結材では、かかる
中間のところは液相焼結の際に収縮の影響を最も
受けにくいからである。凹部61ほ横断面が三角
形である。
Similarly, as shown in FIGS. 3A and 3B,
A protrusion 6 having a width slightly smaller than the width of the groove 5 and having a rectangular cross section so as to fit snugly into the groove 5.
is formed in the axial direction of the cam lobe at a predetermined location on the inner circumference of the hole 32 of the cam lobe 3 that fits into the shaft. Further, a recess 61 is provided so as to cross the protrusion 6. Preferably, the recess 61 is provided in the middle of the length of the protrusion 6. This is because, in a sintered material shaped like a cam lobe, such an intermediate location is least susceptible to shrinkage during liquid phase sintering. The recess 61 has a triangular cross section.

第1B図から分かるように、シヤフト2の凹部
21とカムロブ3の凹部61が所定位置で互いに
対向し、凹部の縁21Aと61A、21Bと61
Bがそれぞれ一致し、かつ、カムロブ3の突出部
6がシヤフト2の溝5に嵌め込まれているとき、
凹部21,61及びカムロブの円周面3Aは空所
を構成する(第1A図参照)。
As can be seen from FIG. 1B, the recess 21 of the shaft 2 and the recess 61 of the cam lobe 3 face each other at predetermined positions, and the edges 21A and 61A of the recess, and 21B and 61
When B are the same and the protrusion 6 of the cam lobe 3 is fitted into the groove 5 of the shaft 2,
The recesses 21, 61 and the circumferential surface 3A of the cam lobe constitute a cavity (see FIG. 1A).

第1A図、第1B図及び第5図から分かるよう
に、組立てカムシヤフト1内の空所7の中に弾性
部材4が配置されており、該弾性部材の周面は凹
部21及び61の内面と係合し、その端縁の一部
は凹部21の内面21Cに当つている。凹部21
の内面21C及びカムロブ3の内周面3Aへの弾
性部材4の周面の係合と、シヤフトの溝5へのカ
ムロブの突出部6の嵌め込みによつてシヤフト2
に対するカムロブ3の周囲方向の変位が阻止さ
れ、一方、凹部21の内面21D及び凹部61の
対向斜面61Cへの弾性部材4の周面の係合によ
つて、シヤフト2に対するカムロブ3の軸方向の
変位が阻止される。
As can be seen from FIGS. 1A, 1B, and 5, an elastic member 4 is arranged in the cavity 7 in the assembled camshaft 1, and the circumferential surface of the elastic member meets the inner surface of the recesses 21 and 61. A portion of the edge thereof is in contact with the inner surface 21C of the recess 21. Recess 21
The shaft 2
The axial displacement of the cam lobe 3 relative to the shaft 2 is prevented by the engagement of the circumferential surface of the elastic member 4 with the inner surface 21D of the recess 21 and the opposing slope 61C of the recess 61. Displacement is prevented.

次に仮止めの手順について説明すると、まず、
シヤフト2の凹部21内に弾性部材4を配置し、
スポツト溶接又は接着剤で固定し、周知の方法に
より押案内刃(図示せず)によつて弾性部材をシ
ヤフト2の中心方向に圧縮させる。前述したよう
に、凹部21の深さは弾性部材4の厚さよりも大
きいので、圧縮された弾性部材の大部分は凹部2
1内に入り、第4図に示すようにU形に彎曲す
る。次に、カムロブ3の突出部6をシヤフト2の
溝5に嵌め込んでカムロブ3をシヤフトに嵌め、
シヤフトに対して移動させる。カムロブ3の端面
が弾性部材に達すると押案内刃を引き抜き、カム
ロブ3をシヤフトに対して、さらに移動させてシ
ヤフト2の凹部21とカムロブ3の凹部61を合
致させる。両凹部21,61が合致すると、弾性
部材4は弾力によりその形状を復元して突出部6
にある凹部61に入り、前述したように、弾性部
材の周面は両凹部の内面に係合し、シヤフト2及
びカムロブ3を所定位置に仮止めする(第1A
図、第1B図、第5図参照)。
Next, I will explain the temporary fixing procedure.
Arranging the elastic member 4 in the recess 21 of the shaft 2,
The elastic member is fixed by spot welding or adhesive, and the elastic member is compressed toward the center of the shaft 2 by a pushing guide blade (not shown) using a well-known method. As mentioned above, since the depth of the recess 21 is greater than the thickness of the elastic member 4, most of the compressed elastic member is in the recess 2.
1 and curves into a U shape as shown in Figure 4. Next, the protrusion 6 of the cam lobe 3 is fitted into the groove 5 of the shaft 2, and the cam lobe 3 is fitted onto the shaft.
Move it relative to the shaft. When the end face of the cam lobe 3 reaches the elastic member, the pushing guide blade is pulled out, and the cam lobe 3 is further moved relative to the shaft, so that the recess 21 of the shaft 2 and the recess 61 of the cam lobe 3 match. When both the recesses 21 and 61 match, the elastic member 4 restores its shape due to its elasticity and the protrusion 6
As described above, the circumferential surface of the elastic member engages with the inner surface of both recesses, temporarily fixing the shaft 2 and cam lobe 3 in a predetermined position (first A).
(See Figures 1B and 5).

次にこれらと液相焼結し、カムロブ3とシヤフ
ト2を一体化させて組立てカムシヤフトを製造す
る。
Next, these are subjected to liquid phase sintering to integrate the cam lobe 3 and the shaft 2 to produce an assembled camshaft.

本発明による組立てカムシヤフトの仮止め構造
では、弾性部材はその周囲がシヤフト及びカムロ
ブに係合状態で囲まれているので脱落する危険性
がなく、しかも、シヤフトに対するカムロブの位
置決め精度が優れており、したがつて、液相焼結
中にカムロブがシヤフトに対して変位することは
ないという利点を有している。
In the temporary fixing structure of the assembled camshaft according to the present invention, since the elastic member is surrounded by the shaft and the cam lobe in an engaged state, there is no risk of it falling off, and the positioning accuracy of the cam lobe with respect to the shaft is excellent. Therefore, it has the advantage that the cam lobe is not displaced relative to the shaft during liquid phase sintering.

本発明の実施態様では、シヤフト2の凹部を横
断面半円形とし、カムロブ3の突出部6の凹部6
1を横断面三角形としたが、変形例としてこれら
は逆であつてもよい。さらにシヤフト及びカムロ
ブに設ける凹部は任意形状のものでもよく、この
場合それらが構成する空所に応じた形状の弾性部
材を配置する。
In the embodiment of the present invention, the recess of the shaft 2 has a semicircular cross section, and the recess 6 of the protrusion 6 of the cam lobe 3
1 has a triangular cross section, but as a modification, these may be reversed. Further, the recesses provided in the shaft and the cam lobe may have any shape, and in this case, an elastic member having a shape corresponding to the space formed by the recesses is arranged.

さらに、本発明では、シヤフト、カムロブにそ
れぞれ溝、突出部を設けたが、これらは逆であつ
てもよく、また、複数の溝、突出部を設けてもよ
い。
Furthermore, in the present invention, the shaft and the cam lobe are provided with grooves and protrusions, respectively, but these may be reversed, or a plurality of grooves and protrusions may be provided.

なお、本発明では一例としてカムロブを採用し
たが、ジヤーナル等の他の構成部品にも適用しう
ることは明らかである。
Although the present invention employs a cam lobe as an example, it is clear that the present invention can also be applied to other components such as journals.

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

第1A図は本発明による組立てカムシヤフトの
仮止め構造の横断面図であり、第1B図は第1A
図の組立てカムシヤフトのA−A線における側断
面図である。第2A図、第2B図、第2C図は、
それぞれ本発明のシヤフトの横断面図、第2A図
に示したシヤフトのB−B線における側断面図、
シヤフトの平面図である。第3A図は本発明のカ
ムロブの横断面図であり、第3B図は第3A図の
カムロブのC−C線における側断面図である。第
4図は、第1A図に示した組立てカムシヤフトの
マルで囲んだ部分Dの拡大詳細図であり、カムロ
ブ及びシヤフトの凹部が互いに合致する以前の図
である。第5図は、第1A図に示した組立てカム
シヤフトのマルで囲んだ部分Dの拡大詳細図であ
り、カムロブ及びシヤフトの凹部が互いに合致し
ている図である。 1……組立てカムシヤフト、2……シヤフト、
3……カムロブ、4……弾性部材、5……溝、6
……突出部、7……空所、21,61……凹所。
FIG. 1A is a cross-sectional view of the temporary fixing structure of the assembled camshaft according to the present invention, and FIG.
FIG. 3 is a side sectional view taken along line A-A of the assembled camshaft shown in the figure. Figures 2A, 2B, and 2C are
A cross-sectional view of the shaft of the present invention, a side cross-sectional view of the shaft shown in FIG. 2A, taken along line B-B, respectively;
FIG. 3 is a plan view of the shaft. FIG. 3A is a cross-sectional view of the cam lobe of the present invention, and FIG. 3B is a side cross-sectional view of the cam lobe of FIG. 3A taken along line C--C. FIG. 4 is an enlarged detail view of the circled area D of the assembled camshaft shown in FIG. 1A, before the cam lobe and shaft recesses meet each other. FIG. 5 is an enlarged detail view of the circled area D of the assembled camshaft shown in FIG. 1A, showing the cam lobe and shaft recesses mating with each other. 1...Assembling camshaft, 2...shaft,
3...Cam lobe, 4...Elastic member, 5...Groove, 6
... protrusion, 7 ... void, 21, 61 ... recess.

Claims (1)

【特許請求の範囲】 1 カムロブ、ジヤーナル等の構成部品をシヤフ
トに液相焼結によつて一体的に結合させる組立て
カムシヤフトの仮止め構造において、シヤフトの
外周部にはその軸方向に所定幅の溝を設け、さら
に、シヤフト外周部の円周方向に溝と直交する横
断面半円形の凹部を設け、上記構成部品の内周部
には、その軸方向に、上記溝にぴつたりと嵌まる
所定幅の突出部を形成し、該突出部にその長さの
中間のところでそれを横切る凹部を設け、上記両
凹部は互いに対向し、構成部品の内周面の一部と
協働して空所を構成し、該空所に弾性部材を配置
し、該弾性部材はその周面が上記対向した2つの
凹部の内面に係合してシヤフトに対する構成部品
の軸方向の変位を阻止し、さらに、シヤフトの溝
内への構成部品の突出部の嵌め込みによつて、シ
ヤフトに対する構成部品の周囲方向の変位を阻止
することを特徴とする組立てカムシヤフトの仮止
め構造。 2 前記構成部品の前記突出部の凹部、前記シヤ
フトの前記溝の凹部は横断面がそれぞれ三角形、
半円形であることを特徴とする特許請求の範囲第
1項記載の組立てカムシヤフトの仮止め構造。
[Claims] 1. In a temporary fixing structure of an assembled camshaft in which component parts such as a cam lobe and a journal are integrally joined to a shaft by liquid phase sintering, the outer circumference of the shaft is provided with a predetermined width in the axial direction. A groove is provided, and a recess with a semicircular cross section perpendicular to the groove is provided in the circumferential direction of the outer circumference of the shaft, and the inner circumference of the component is tightly fitted into the groove in the axial direction. A protrusion of a predetermined width is formed, and the protrusion is provided with a recess that traverses it at a midpoint of its length, the two recesses facing each other and cooperating with a portion of the inner circumferential surface of the component to form an empty space. an elastic member is disposed in the cavity, and the elastic member has a circumferential surface that engages with an inner surface of the two opposed recesses to prevent axial displacement of the component relative to the shaft; A temporary fixing structure for an assembled camshaft, characterized in that circumferential displacement of a component with respect to the shaft is prevented by fitting a protrusion of the component into a groove of the shaft. 2. The recess of the protrusion of the component and the recess of the groove of the shaft each have a triangular cross section;
The temporary fixing structure for an assembled camshaft according to claim 1, characterized in that it has a semicircular shape.
JP59025498A 1984-02-14 1984-02-14 Temporarily attaching structure for shaft assebly Granted JPS60172769A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP59025498A JPS60172769A (en) 1984-02-14 1984-02-14 Temporarily attaching structure for shaft assebly

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP59025498A JPS60172769A (en) 1984-02-14 1984-02-14 Temporarily attaching structure for shaft assebly

Publications (2)

Publication Number Publication Date
JPS60172769A JPS60172769A (en) 1985-09-06
JPH0368257B2 true JPH0368257B2 (en) 1991-10-25

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Family Applications (1)

Application Number Title Priority Date Filing Date
JP59025498A Granted JPS60172769A (en) 1984-02-14 1984-02-14 Temporarily attaching structure for shaft assebly

Country Status (1)

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JP (1) JPS60172769A (en)

Also Published As

Publication number Publication date
JPS60172769A (en) 1985-09-06

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