JPS63313649A - Production of cast-in liner member - Google Patents
Production of cast-in liner memberInfo
- Publication number
- JPS63313649A JPS63313649A JP62149499A JP14949987A JPS63313649A JP S63313649 A JPS63313649 A JP S63313649A JP 62149499 A JP62149499 A JP 62149499A JP 14949987 A JP14949987 A JP 14949987A JP S63313649 A JPS63313649 A JP S63313649A
- Authority
- JP
- Japan
- Prior art keywords
- liner member
- circumferential surface
- cast
- irradiation
- hardened layer
- 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
- 238000004519 manufacturing process Methods 0.000 title claims description 8
- 230000002093 peripheral effect Effects 0.000 claims abstract description 17
- 238000000034 method Methods 0.000 claims abstract description 13
- 238000005266 casting Methods 0.000 claims abstract description 5
- 239000010953 base metal Substances 0.000 claims description 3
- 230000001678 irradiating effect Effects 0.000 abstract description 7
- 238000010791 quenching Methods 0.000 abstract description 3
- 230000000171 quenching effect Effects 0.000 abstract description 3
- 239000000463 material Substances 0.000 description 6
- 229910052782 aluminium Inorganic materials 0.000 description 5
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 5
- 230000015572 biosynthetic process Effects 0.000 description 5
- 229910001018 Cast iron Inorganic materials 0.000 description 4
- 229910045601 alloy Inorganic materials 0.000 description 3
- 239000000956 alloy Substances 0.000 description 3
- 229910000838 Al alloy Inorganic materials 0.000 description 2
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 229910052751 metal Inorganic materials 0.000 description 2
- 239000002184 metal Substances 0.000 description 2
- 238000007796 conventional method Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000010894 electron beam technology Methods 0.000 description 1
- 229910052742 iron Inorganic materials 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
- B23K26/00—Working by laser beam, e.g. welding, cutting or boring
- B23K26/08—Devices involving relative movement between laser beam and workpiece
- B23K26/0823—Devices involving rotation of the workpiece
Landscapes
- Physics & Mathematics (AREA)
- Optics & Photonics (AREA)
- Engineering & Computer Science (AREA)
- Plasma & Fusion (AREA)
- Mechanical Engineering (AREA)
- Laser Beam Processing (AREA)
Abstract
Description
【発明の詳細な説明】
(産業上の利用分野)
本発明は、例えばエンジンのシリンダブロック等に鋳ぐ
るまれるライナー部材の製造方法に関する9
(従来の技術)
近年、エンジンの軽量化を図るべくシリンダブロックを
アルミニウムもしくはその合金で形成することか試みら
れている。この場合、シリンダ内周面を鋳鉄製等のライ
ナー部材で形成し、これを鋳造時に母材(アルミニウム
もしくはその合金)溶湯で鋳ぐるむことになるが、一般
にアルミニウムと鉄とは冶金的に良好な接合性が得られ
ず、そのためシリンダブロック本体とライナー部材とが
強固に結合しないといっな問題が生じる。Detailed Description of the Invention (Industrial Field of Application) The present invention relates to a method of manufacturing a liner member that is cast into, for example, the cylinder block of an engine. Attempts have been made to form the cylinder block from aluminum or its alloys. In this case, the inner circumferential surface of the cylinder is formed of a liner member made of cast iron, etc., and this is then filled with molten base metal (aluminum or its alloy) during casting, but generally aluminum and iron have good metallurgical properties. Therefore, a problem arises in that the cylinder block body and the liner member are not firmly connected.
これに対しては、例えば特開昭55−8370号公報に
示されているように、鋳鉄製スリーブの外周面に凹凸を
設け、これをアルミニウム合金で鋳ぐるむことにより、
ボディとスリーブとを機械的に結合するようにした発明
が示されており、これによれば、ブロック本体(ボディ
)とライナー部材(スリーブ)とが強固に結合されたシ
リンダブロックが得られることになる。To solve this problem, for example, as shown in Japanese Patent Application Laid-Open No. 55-8370, by providing unevenness on the outer peripheral surface of a cast iron sleeve and surrounding it with aluminum alloy,
An invention is disclosed in which the body and the sleeve are mechanically coupled, and according to this invention, a cylinder block in which the block main body (body) and the liner member (sleeve) are firmly coupled can be obtained. Become.
一方、この種のシリンダブロックに鋳ぐるまれるライナ
ー部材は、ピストンリングとの摺動面となる内周面の耐
窄耗性を向上させるため、該面を焼入れ処理するのが通
例であり、この焼入れ処理にレーザビームを用いること
がある。その場合、第5図に示すように、ライナー部材
Aの内側に反射鏡Bを傾斜状に配備し、これを回動及び
軸方向に移動させながらライナー部材Aの一方の開口部
から照射したレーザビームCを該反射鏡Bで反射させる
ことにより、ライナー部材内周面A′の全面にレーザビ
ームCを照射して、核部A′を焼入れ硬化させる、とい
った方法が用いられる。On the other hand, the liner member cast into this type of cylinder block is usually hardened to improve the wear resistance of the inner circumferential surface, which is the sliding surface with the piston ring. A laser beam may be used for this hardening process. In that case, as shown in FIG. 5, a reflecting mirror B is arranged in an inclined manner inside the liner member A, and the laser beam is irradiated from one opening of the liner member A while rotating and moving it in the axial direction. A method is used in which the laser beam C is reflected by the reflecting mirror B to irradiate the entire inner circumferential surface A' of the liner member with the laser beam C, thereby hardening the core portion A' by quenching.
(発明が解決しようとする問題点)
ところで、上記のようにライナー部材を母材内に鋳ぐる
む場合において、これらを機械的に結合すべくライナー
部材の外周面に凹凸を設け、且つ内周面の耐摩耗性向上
のため焼入れ処理を施す場合、これら2つの加工ないし
処理を外周面及び内周面の夫々について行わなければな
らないことになる。そのため、この種のライナー部材の
製造が著しく面倒となり、また第5図に示すようなレー
ザビームを用いる焼入れ方法にあっては、反射鏡Bを駆
動するための複雑な装置が必要となると共に、該反射鏡
BがレーザビームCのエネルギーで早期に損傷するため
頻繁に交換しなければならず、そのためコストが高く付
くという問題が発生する。(Problems to be Solved by the Invention) By the way, when the liner member is cast into the base material as described above, in order to mechanically connect them, the outer peripheral surface of the liner member is provided with irregularities, and the inner peripheral surface is When performing hardening treatment to improve the wear resistance of the surface, these two processes must be performed on the outer circumferential surface and the inner circumferential surface, respectively. Therefore, manufacturing this type of liner member becomes extremely troublesome, and the hardening method using a laser beam as shown in FIG. 5 requires a complicated device for driving the reflecting mirror B. Since the reflecting mirror B is damaged early by the energy of the laser beam C, it must be replaced frequently, resulting in a problem of high costs.
また、レーザビームを用いる場合に限らず、一般に焼入
れ処理においては、被処理面における焼入れ状態の確認
が困難なため、核部の硬度等を最適値に仕上げることが
むずかしく、品質のばらつきが生じ易いという問題があ
る。In addition, not only when a laser beam is used, but in hardening treatment in general, it is difficult to confirm the hardened state of the surface to be treated, so it is difficult to finish the hardness of the core part to the optimum value, and quality variations are likely to occur. There is a problem.
本発明は、例えばアルミニウム合金製シリンダブロック
のように、ライナー部材を母材溶湯で鋳ぐるむ場合にお
ける上記のような問題に対処するもので、外周面に母材
との結合を強固とするための凹凸が形成され、且つ内周
面に耐摩耗性向上等のための焼入れ硬化層が形成された
鋳ぐるみライナー部材を容易に製造することができ、し
かも上記硬化層が所望の硬度に精度良く且つ安定的に形
成される方法を実現することを目的とする。The present invention addresses the above-mentioned problems when a liner member is cast with molten base metal, such as an aluminum alloy cylinder block. It is possible to easily manufacture a cast liner member in which irregularities are formed, and a quenched hardened layer is formed on the inner circumferential surface for improving wear resistance, etc., and the hardened layer is precisely controlled to the desired hardness. The object of the present invention is to realize a method that allows stable formation.
(問題点を解決するための手段)
即ち、本発明に係る鋳ぐるみライナー部材の製造方法は
、該ライナー部材の外周面にレーザビームや電子ビーム
等の高エネルギービームを照射して凹部を形成する一方
、この照射による熱影響を該ライナー部材の内周面に及
ぼして核部に焼入れ硬化層を形成することを特徴とする
。その場合に、該硬化層が略均一となるように、外周面
に対する高エネルギービームの照射エネルギー、具体的
には照射出力やビームの走査速度等と、照射位置の間隔
とをコントロールする。(Means for Solving the Problems) That is, the method for manufacturing a cast liner member according to the present invention includes forming a recess by irradiating the outer peripheral surface of the liner member with a high-energy beam such as a laser beam or an electron beam. On the other hand, the method is characterized in that a thermal effect caused by this irradiation is exerted on the inner circumferential surface of the liner member to form a quenched hardened layer in the core portion. In this case, the irradiation energy of the high-energy beam to the outer peripheral surface, specifically, the irradiation output, beam scanning speed, etc., and the interval between irradiation positions are controlled so that the cured layer is substantially uniform.
(作 用)
上記の構成によれば、高エネルギービームが直接照射さ
れるライナー部材の外周面においては、金属組織が部分
的に溶出して凹部が形成され、従って、該ライナー部材
を母材溶湯で鋳ぐるんでシリンダブロック等の製品を鋳
造する場合に、該ライナー部材と母材とが機械的に強固
に結合されることになる。また、上記高エネルギービー
ムの照射時に、その熱影響−がライナー部材の内周面に
及んで核部に焼入れ硬化層が形成されると共に、その照
射エネルギーや照射位置の間隔等が適切にコントロール
されるので、内周面に上記硬化層が略均一に形成される
ことになる。従って、該ライナー部材の内周面がピスト
ンリング等との摺動面である場合に、良好な耐摩耗性が
得られることになる。(Function) According to the above configuration, on the outer circumferential surface of the liner member that is directly irradiated with the high-energy beam, the metal structure is partially eluted to form a concave portion, so that the liner member is exposed to the molten base material. When a product such as a cylinder block is cast by casting, the liner member and the base material are mechanically and firmly connected. In addition, during irradiation with the high-energy beam, the thermal influence extends to the inner circumferential surface of the liner member, forming a hardened layer in the core, and the irradiation energy and spacing of irradiation positions are appropriately controlled. Therefore, the hardened layer is formed substantially uniformly on the inner circumferential surface. Therefore, when the inner circumferential surface of the liner member is a sliding surface with a piston ring or the like, good wear resistance can be obtained.
尚、外周面に形成される凹部の大きさ等と、内周面に及
ぶ熱影響、即ち内周面の焼入れ硬化状態とは略対応する
ので、上記凹部の形成状態を観察もしくは検出すること
によって内周面の硬化状態が間接的に把握されることに
なる。従って、高エネルギービームの照射出力等を、内
周面に最適な硬化層が形成されるようにフィードバック
しながらコントロールすることが可能となる。It should be noted that the size of the recess formed on the outer peripheral surface approximately corresponds to the thermal influence on the inner peripheral surface, that is, the quenching and hardening state of the inner peripheral surface, so by observing or detecting the formation state of the recess mentioned above, The hardening state of the inner circumferential surface can be indirectly understood. Therefore, it is possible to control the irradiation output of the high-energy beam and the like while giving feedback so that an optimal hardened layer is formed on the inner circumferential surface.
(実 施 例)
以下、本発明に係る鋳ぐるみライナー部材の製造方法の
実施例について説明する。(Example) Hereinafter, an example of the method for manufacturing a cast liner member according to the present invention will be described.
先ず、第1図に示すように、この方法では回転治具1と
レーザビーム照射装置2とが用いられる。そして、上記
回転治具1に予め形成された鋳鉄製のライナー部材10
を取付け、これをその軸心回りに回転駆動するね共に、
該ライナー部材10の外周面11に上記照射装置2によ
りレーザビーム3を照射しながら、該照射装置2をライ
ナー部材10の軸方向に移動させる。これにより、レー
ザビーム3がライナー部材10の外周面11に螺旋状に
連続して照射されることになり、第2図に示すように、
その照射軌跡に沿ってライナー部材10の外周面11か
ら一部の金属組織が溶出されて、該面11に螺旋状に連
続する凹1!412が形成されることになる。First, as shown in FIG. 1, a rotating jig 1 and a laser beam irradiation device 2 are used in this method. A liner member 10 made of cast iron is formed in advance on the rotating jig 1.
and drive it to rotate around its axis.
The irradiation device 2 is moved in the axial direction of the liner member 10 while irradiating the outer circumferential surface 11 of the liner member 10 with the laser beam 3 by the irradiation device 2 . As a result, the laser beam 3 is continuously irradiated onto the outer circumferential surface 11 of the liner member 10 in a spiral manner, as shown in FIG.
A part of the metal structure is eluted from the outer circumferential surface 11 of the liner member 10 along the irradiation trajectory, and a spirally continuous recess 1!412 is formed on the surface 11.
この時、ライナー部材10の金属組織内においては、レ
ーザビーム3のエネルギーにより凹溝12を中心として
焼入れ硬化層が形成されるが、第3図に示すように、該
部材10の断面において隣り合う各凹溝12a・・・1
2aを中心とする硬化層が互いに重合し合う結果、該ラ
イナー部材10の内周面13には該面13の全体に連続
する硬化層14が形成されることになる。その場合に、
レーザビーム3の照射出力や、ライナー部材10の回転
速度と照射装置2の送り速度とによるレーザビーム3の
走査速度等に対応するレーザビーム3の照射エネルギー
と、螺旋状凹11112のピッチ、即ち第3図の断面に
おける各凹溝12a・・・12aの間隔ηを適切に設定
することにより、ライナー部材内周面13には略均一な
硬化層14がその全面にわたって形成されることになる
。At this time, in the metallographic structure of the liner member 10, a hardened layer is formed centering on the groove 12 due to the energy of the laser beam 3, but as shown in FIG. Each groove 12a...1
As a result of the cured layers 2a being centered on each other, a cured layer 14 is formed on the inner circumferential surface 13 of the liner member 10, which is continuous over the entire surface 13. In that case,
The irradiation energy of the laser beam 3 corresponding to the irradiation output of the laser beam 3, the scanning speed of the laser beam 3 depending on the rotation speed of the liner member 10 and the feed speed of the irradiation device 2, and the pitch of the spiral recess 11112, that is, the By appropriately setting the interval η between the grooves 12a .
このようにして、ライナー部材10の外周面11に対し
て、レーザビーム3をその照射エネルギーや照射位置の
間隔等を適切にコントロールしながら照射することによ
り、外周面11に凹溝12を形成すると同時に、内周面
13には略均一な焼入れ硬化層14を形成することがで
き、これを例えばエンジンのアルミニウム製シリンダブ
ロックの鋳造時における鋳ぐるみ部材として用いれば、
該ライナー部材10が母材と強固に結合され、且つ内周
面13がピストンリング等の摺動5に対して良好な耐摩
耗性を示すことになる。In this way, by irradiating the outer circumferential surface 11 of the liner member 10 with the laser beam 3 while appropriately controlling the irradiation energy, the interval between the irradiation positions, etc., the grooves 12 are formed on the outer circumferential surface 11. At the same time, a substantially uniform quenched hardened layer 14 can be formed on the inner circumferential surface 13, and if this is used, for example, as a cast member when casting an aluminum cylinder block for an engine,
The liner member 10 is firmly connected to the base material, and the inner circumferential surface 13 exhibits good wear resistance against sliding parts 5 such as piston rings.
尚、レーザビーム3の照射開始時からの経過時間に従っ
てライナー部材10の全体の温度が次第に上昇するので
、該部材10の全体にわたって均一な深さの凹溝12を
形成し且つ均一な焼入れ硬化層14を形成するためには
、レーザビーム3の照射出力を照射開始時から次第に低
下させ、或は走査速度を次第に早くするのが望ましい。Incidentally, since the overall temperature of the liner member 10 gradually increases as time elapses from the start of irradiation with the laser beam 3, it is possible to form grooves 12 of uniform depth throughout the member 10 and to form a uniform hardened layer. 14, it is desirable to gradually reduce the irradiation output of the laser beam 3 from the start of irradiation, or to gradually increase the scanning speed.
また、該ライナー部材外周面11に形成する凹部は、上
記実施例の如き螺旋状凹溝12に限らず、第4図に示す
ような円環状凹溝12′でもよく、更にスポット状の凹
部等でもよい。そして、いずれの場合にも、レーザビー
ムの照射エネルギーと照射位置の間隔を適切に設定する
ことによ゛り内周面に略均一な焼入れ硬化層を形成する
ことができる。Further, the recess formed in the outer circumferential surface 11 of the liner member is not limited to the spiral groove 12 as in the above embodiment, but may be an annular groove 12' as shown in FIG. But that's fine. In either case, by appropriately setting the irradiation energy of the laser beam and the interval between the irradiation positions, a substantially uniform hardened layer can be formed on the inner circumferential surface.
(発明の効果)
以上のように本発明方法によれば、例えばアルミニウム
もしくはその合金等でなる母材に鋳ぐるまれる鋳鉄製等
のライナー部材の製造に関し、その外周面に照射エネル
ギーと照射位置の間隔を適切にコントロールして高エネ
ルギービームを照射するようにしたから、外周面に凹部
が形成されると同時に、内周面に略均一な焼入れ硬化層
が形成されることになる。(Effects of the Invention) As described above, according to the method of the present invention, irradiation energy and irradiation position are applied to the outer peripheral surface of a liner member made of cast iron or the like that is cast into a base material made of aluminum or its alloy. Since the high-energy beam is irradiated by appropriately controlling the interval between the two, a concave portion is formed on the outer circumferential surface, and at the same time, a substantially uniform hardened layer is formed on the inner circumferential surface.
従って、例えばエンジンのシリンダブロック用のライナ
ー部材等として用いる場合に、母材との結合を強固にす
るための外周面の加工と、ピストンリング等の摺動に対
する内周面の耐摩耗性の向上処理とが、同時に且つ極め
て容易に行われることになり、その結果、この種のライ
ナー部材のコストが低減されることになる。また、外周
面に形成される凹部の状態を観察することによって、内
周面における焼入れ硬化層の形成状態を把握することが
できるので、該硬化層を所望の硬度に精度良く且つ安定
的に形成することが可能となる。Therefore, when used as a liner member for an engine cylinder block, for example, the outer peripheral surface must be processed to strengthen the bond with the base material, and the inner peripheral surface must be improved in wear resistance against sliding of piston rings, etc. processing will be carried out simultaneously and very easily, resulting in a reduction in the cost of this type of liner element. In addition, by observing the state of the recesses formed on the outer circumferential surface, it is possible to grasp the formation state of the quenched hardened layer on the inner circumferential surface, so the hardened layer can be accurately and stably formed to the desired hardness. It becomes possible to do so.
第1〜4図は本発明方法の実施例を示すもので、第1図
は高エネルギービームの照射状態を示す断面図、第2図
は外周面に凹部が形成されたライナー部材の外観図、第
3図は焼入れ硬化層の形成状態を示すライナー部材の部
分拡大断面図、第4図は他の実施例における凹部の形成
状態を示すライナー部材の外観図である。また、第5図
はライナー部材内周面に焼入れ硬化層を形成する従来方
法の概略説明図である。
10・・・ライナー部材、11・・・外周面、12゜1
2′・・・凹部、13・・・内周面、14・・・焼入れ
硬化層。Figures 1 to 4 show examples of the method of the present invention, in which Figure 1 is a cross-sectional view showing the state of high-energy beam irradiation, Figure 2 is an external view of a liner member with a recess formed on its outer peripheral surface, FIG. 3 is a partially enlarged cross-sectional view of the liner member showing the state of formation of the quench-hardened layer, and FIG. 4 is an external view of the liner member showing the state of formation of the recess in another embodiment. Furthermore, FIG. 5 is a schematic explanatory diagram of a conventional method for forming a hardened layer on the inner circumferential surface of a liner member. 10...Liner member, 11...Outer peripheral surface, 12°1
2'... Recessed portion, 13... Inner peripheral surface, 14... Quenched hardened layer.
Claims (1)
ー部材の製造方法であつて、該ライナー部材の外周面に
高エネルギービームを照射して凹部を形成する一方、そ
の照射エネルギー及び照射位置の間隔を、該ライナー部
材の内周面に略均一な焼入れ硬化層が形成されるように
コントロールすることを特徴とする鋳ぐるみライナー部
材の製造方法。(1) A method for manufacturing a cast liner member that is cast with molten base metal during casting, in which the outer peripheral surface of the liner member is irradiated with a high-energy beam to form a recess, and the irradiation energy and irradiation position are A method for producing a cast liner member, comprising controlling the interval between the liner member and the liner member so that a substantially uniform hardened layer is formed on the inner circumferential surface of the liner member.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP62149499A JPS63313649A (en) | 1987-06-16 | 1987-06-16 | Production of cast-in liner member |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP62149499A JPS63313649A (en) | 1987-06-16 | 1987-06-16 | Production of cast-in liner member |
Publications (1)
Publication Number | Publication Date |
---|---|
JPS63313649A true JPS63313649A (en) | 1988-12-21 |
Family
ID=15476491
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP62149499A Pending JPS63313649A (en) | 1987-06-16 | 1987-06-16 | Production of cast-in liner member |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPS63313649A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2003529021A (en) * | 2000-03-24 | 2003-09-30 | マーレ ゲゼルシヤフト ミツト ベシユレンクテル ハフツング | Pistons for internal combustion engines |
JP2015213960A (en) * | 2013-07-18 | 2015-12-03 | ダイセルポリマー株式会社 | Method for producing composite molding |
-
1987
- 1987-06-16 JP JP62149499A patent/JPS63313649A/en active Pending
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2003529021A (en) * | 2000-03-24 | 2003-09-30 | マーレ ゲゼルシヤフト ミツト ベシユレンクテル ハフツング | Pistons for internal combustion engines |
JP2015213960A (en) * | 2013-07-18 | 2015-12-03 | ダイセルポリマー株式会社 | Method for producing composite molding |
JP2015213961A (en) * | 2013-07-18 | 2015-12-03 | ダイセルポリマー株式会社 | Method for producing composite molding |
US10434741B2 (en) | 2013-07-18 | 2019-10-08 | Daicel Polymer Ltd. | Composite molded article |
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