JPS6141672B2 - - Google Patents
Info
- Publication number
- JPS6141672B2 JPS6141672B2 JP54078531A JP7853179A JPS6141672B2 JP S6141672 B2 JPS6141672 B2 JP S6141672B2 JP 54078531 A JP54078531 A JP 54078531A JP 7853179 A JP7853179 A JP 7853179A JP S6141672 B2 JPS6141672 B2 JP S6141672B2
- Authority
- JP
- Japan
- Prior art keywords
- workpiece
- hole
- holes
- drilled
- laser
- 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
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- Laser Beam Processing (AREA)
Description
【発明の詳細な説明】
本発明はレーザによる切断等の加工方法に係り
特に加工能率の向上を図つたレーザ加工方法に関
する。DETAILED DESCRIPTION OF THE INVENTION The present invention relates to a processing method such as cutting using a laser, and particularly to a laser processing method that improves processing efficiency.
近時レーザパルスを集光し、その集光スポツト
を被加工物に照射して孔をあけたり、集光スポツ
トを被加工物のくり抜き線に沿つて重ねながら移
動させ被加工物にくり抜き溝を形成して所定形状
の孔をくり抜いたりする各種の加工方法が実用化
されている。一方、最近、モータあるいは音響部
品等に焼結磁性材料が用いられ、この材料に直径
約1mm〜2mmの孔をあける必要性がしばしばあ
る。ところで、このような孔をレーザビームを利
用して孔明け加工する場合、スポツトサイズが1
mm〜2mmφのパルスレーザで照射すると、焼結体
の性質上熱衝撃等により穴の周りにクラツクが発
生し、目的の加工ができない。したがつて従来は
レーザビームを更に集光し、微小な集光スポツト
を穿設する孔の円周に沿つて順次重ねながら移動
させ、くり抜き溝を形成して孔の中心部をくり抜
くようにした加工方法が実施されている。しかし
ながらこのような方法で孔明け加工する場合、レ
ーザビームの照射によつて蒸発飛散した粒子が既
に加工されたくり抜き溝の中に再び残留物として
蓄積し、孔のくり抜きが出来なくなつたり、きれ
いな加工孔が出来ない。したがつて残留物のない
きれいな加工孔を得るためには円周に沿つて集光
スポツトを何回も走査し、くり抜き溝に蓄積する
残留物を除去しながら加工する必要があり、加工
時間が長くなるばかりでなく、一度溶融したもの
がくり抜き溝の中で再凝固するため、溝周辺を加
熱し熱影響層を形成するような弊害もあつた。 Recently, laser pulses are focused, and the focused spot is irradiated onto the workpiece to make a hole, or the focused spot is moved along the cutout line of the workpiece while overlapping to create a hollow groove in the workpiece. Various processing methods have been put into practical use, such as forming and hollowing out holes of predetermined shapes. On the other hand, recently, sintered magnetic materials have been used for motors, audio components, etc., and it is often necessary to drill holes with a diameter of about 1 mm to 2 mm in this material. By the way, when drilling such a hole using a laser beam, the spot size is 1.
When irradiated with a pulse laser of mm to 2 mmφ, cracks occur around the hole due to thermal shock due to the nature of the sintered body, making it impossible to perform the desired processing. Therefore, in the past, the laser beam was further focused and moved sequentially along the circumference of the hole in which a minute focusing spot was to be drilled, forming a hollow groove and hollowing out the center of the hole. Processing methods are implemented. However, when drilling holes using this method, particles that evaporate and scatter due to laser beam irradiation accumulate as residue in the hollowed out grooves that have already been drilled, making it impossible to drill the holes cleanly or Cannot make holes. Therefore, in order to obtain a clean machined hole with no residue, it is necessary to scan the condensing spot many times along the circumference and process while removing the residue that accumulates in the hollowed groove, which reduces the processing time. Not only did it become longer, but once it was molten, it re-solidified inside the hollowed-out groove, which caused problems such as heating the area around the groove and forming a heat-affected layer.
本発明は上記事情に鑑みなされたもので、レー
ザビームの照射によつて蒸発飛散した粒子が、既
に加工されたくり抜き溝に蓄積せず、能率的な加
工作業ができるレーザ加工方法を提供することを
目的とするものである。 The present invention was made in view of the above circumstances, and it is an object of the present invention to provide a laser machining method that allows efficient machining work without allowing particles evaporated and scattered by laser beam irradiation to accumulate in hollowed out grooves that have already been machined. The purpose is to
以下本発明の実施例を図面を参照し具体的に説
明する。図中1はベアリング2を介して回転自在
に回転する円筒状の回転体であり、この回転体1
の上端部段付開口部3に被加工物4を着脱自在に
嵌合し、この被加工物4を上記回転体1の上部開
口端に着脱自在に冠着する固定リング5で固定す
るようにしている。なお、上記被加工物4は直径
3mm、厚さ1mmの焼結磁性材料で、その中心部に
直径約1mmの孔明け加工を行なうものである。ま
た上記回転体1の下部外周にギア6を嵌入し、こ
のギア6にパルスモータ7の回転軸に固定したギ
ア8を歯合させ、上記回転体1をパルスモータ7
で駆動するようにしている。また上記パルスモー
タ7は回転制御部9が出力する駆動パルスによつ
て駆動制御される。一方、前記被加工物4の上方
部位にレーザ発振器10を配設し、このレーザ発
振器10が出力するレーザビームをレンズ11を
介して集光し、その集光スポツトを被加工物4の
中心から穿設する孔の半径尺だけ偏心した位置に
照射するようにしている。また上記レーザ発振器
10はレーザ制御部12が出力するパルス信号に
応じたレーザパルスを出力するものである。更
に、上記回転制御部9及び上記レーザ制御部12
は共に、タイミング制御部13によつて制御され
る。上記回転制御部9はタイミング制御部13が
出力するタイミングパルスに付勢され、パルスモ
ータ7に駆動パルスを出力して前記回転体1を回
転角θ分ずつ回転駆動する。一方、上記レーザ制
御部12は上記タイミング制御部13が出力する
タイミングパルスに付勢され、レーザ発振器10
に一定周期のパルス信号を出力する。ところで上
記回転体1の回転角θは第2図に示すように被加
工物4上に設定されたくり抜き線14に沿つて穿
設する孔a,b,c……………が互いに重複せ
ず、かつ隣接する各孔a,b,c……………間の
最短距離Dが上記各孔a,b,c……………の直
径dよりも小さくなるように回転体1を所定ピツ
チづつ回転させる回転角である。 Embodiments of the present invention will be specifically described below with reference to the drawings. In the figure, 1 is a cylindrical rotating body that rotates freely via a bearing 2, and this rotating body 1
A workpiece 4 is removably fitted into the stepped opening 3 at the upper end, and the workpiece 4 is fixed by a fixing ring 5 which is removably attached to the upper opening end of the rotating body 1. ing. The workpiece 4 is a sintered magnetic material with a diameter of 3 mm and a thickness of 1 mm, and a hole of about 1 mm in diameter is drilled in the center thereof. Further, a gear 6 is fitted into the outer periphery of the lower part of the rotating body 1, and a gear 8 fixed to the rotating shaft of the pulse motor 7 is meshed with this gear 6, so that the rotating body 1 is connected to the pulse motor 7.
I am trying to drive it by. Further, the pulse motor 7 is driven and controlled by drive pulses output from the rotation control section 9. On the other hand, a laser oscillator 10 is disposed above the workpiece 4, and a laser beam outputted from the laser oscillator 10 is focused through a lens 11, and the focusing spot is directed from the center of the workpiece 4. The beam is irradiated at a position that is eccentric by the radius of the hole to be drilled. Further, the laser oscillator 10 outputs a laser pulse according to a pulse signal output by the laser control section 12. Furthermore, the rotation control section 9 and the laser control section 12
Both are controlled by the timing control section 13. The rotation control section 9 is energized by the timing pulse output from the timing control section 13, outputs a drive pulse to the pulse motor 7, and rotates the rotary body 1 by a rotation angle θ. On the other hand, the laser control section 12 is energized by the timing pulse output from the timing control section 13, and the laser oscillator 10
Outputs a pulse signal with a constant period. By the way, the rotation angle θ of the rotating body 1 is such that the holes a, b, c, etc., bored along the cutout line 14 set on the workpiece 4 overlap each other, as shown in FIG. and the rotating body 1 is predetermined so that the shortest distance D between adjacent holes a, b, c........ is smaller than the diameter d of each of the holes a, b, c.... This is the rotation angle to rotate in pitch increments.
このような構成によれば、まず被加工物4を回
転体1の所定位置に固定し、タイミング制御部1
3を動作させると、タイミング制御部13は第3
図に示すタイミングチヤートに従つて、t1〜t2ま
での時間レーザ制御部12にタイミング信号T1
を出力し、レーザ発振器10は一定周期のレーザ
パルスL1,L2,L3,L4を出力する。一方、回転
制御部9にはタイミング制御部13からの入力信
号がないため、パルスモータ7は停止したままと
なり、被加工物4に第4図に示すように被加工物
4を貫通する最初の孔aが穿設される。次に、タ
イミング制御部13はt3〜t4までの時間回転制御
部9にタイミング信号S1を出力し、パルスモータ
7は回転体1を回転角θだけ回転させる。次に、
タイミング制御部13はt5〜t6までの時間レーザ
制御部12にタイミング信号T2を出力し、レー
ザ発振器10は再び一定周期のレーザパルス
L1,L2,L3,L4を出力して、被加工物4の次の
孔bを穿設する。以下同様にして、くり抜き線1
4上に被加工物4を貫通する一周分の孔a,b,
c……………を連続的に穿設する。次に、回転体
1を現在の停止位置からθ/2ずらせた状態つま
りレーザ発振器10の集光スポツトが既に穿設さ
れた各孔a,b,c……………の中間位置にくる
ようにして、第1の工程と同じ作業を再び繰返え
す。そして、くり抜き線14に沿つて被加工物4
を貫通する一周分の孔A,B,C……………を穿
設する。上記各孔A,B,C……………は前記各
孔a,b,c……………と同径であり、互いに隣
接する各孔a,b,c……………間の最短距離D
が上記各孔A,B,C……………の直径dよりも
小さいことから、被加工物4はくり抜き線14に
沿つてくり抜かれる。ところで、くり抜き線14
に沿つて穿設される孔は、まず第1の工程で所定
間隔毎に被加工物4を貫通する孔a,b,c……
………が穿設されるが、各孔a,b,c…………
…は所定距離Dを隔てて各々が独立して穿設され
るため、孔明け作業中の孔から蒸発飛散した粒子
が既に穿設した隣接する孔に残留物として蓄積す
るようなことがなく、また各孔の孔明け作業は被
加工物4の表面から加工を開始し、孔内部の溶融
物を上方に飛散させながら、内部に進行させてゆ
くためレーザの集光スポツトは順次形成される孔
の内壁で反射しながら内部に達し、孔の内壁に残
る残留物を除去しながら孔明け作業が進められ
る。またレーザビームが被加工物4の裏側に達す
ると、溶融物は孔の上下方向から外部に排出され
るため孔内部の残留物が完全に除去されきれいな
孔を穿設することができる。第1の工程が完了す
るとくり抜き線14上の被加工物4の大部分が除
去され、各孔a,b,c……………間に残る残留
物15のみとなる。したがつてこのような状態で
第2工程を実施すると、上記残存部15は各孔
a,b,c……………によつて既に円周方向に分
断された領域であるため、残存部15の温度が上
昇が容易に起り、第1の工程よりも早く孔A,
B,C……………を穿設することができる。この
場合、蒸発飛散した粒子は既に穿設されている孔
a,b,c……………にも浸入するが、第2の工
程で穿設する孔Aから飛散する粒子はその孔Aの
両側に既に穿設された孔a及びbを塞ぐ程の量で
なく、孔a及びbの一部に付着する程度のもので
ある。したがつて、被加工物4はくり抜き線14
に沿つて極めて能率良く、所望する孔をくり抜く
ことができるものである。尚、本実施例では第1
の工程をくり抜き線14に沿つて一周分完了した
時点で第2工程を実施するようにしているが、第
1の工程と第2の工程を交互に実施し、第1の工
程で隣接する2個の孔を穿設する毎に、上記孔間
の残存部に対し、第2の工程を実施するようにし
てもよい。 According to such a configuration, the workpiece 4 is first fixed at a predetermined position on the rotating body 1, and the timing control section 1
3, the timing control section 13
According to the timing chart shown in the figure, a timing signal T 1 is sent to the laser control unit 12 for a period of time from t 1 to t 2 .
The laser oscillator 10 outputs laser pulses L 1 , L 2 , L 3 , and L 4 with a constant period. On the other hand, since the rotation control section 9 does not receive the input signal from the timing control section 13, the pulse motor 7 remains stopped, and the pulse motor 7 remains stopped, and the pulse motor 7 remains stopped, and the pulse motor 7 remains stopped when the rotation control section 9 receives the input signal from the timing control section 13. A hole a is drilled. Next, the timing control unit 13 outputs a timing signal S 1 to the rotation control unit 9 from t 3 to t 4 , and the pulse motor 7 rotates the rotating body 1 by the rotation angle θ. next,
The timing control section 13 outputs the timing signal T2 to the laser control section 12 for a period of time from t5 to t6 , and the laser oscillator 10 again generates a laser pulse of a constant period.
Output L 1 , L 2 , L 3 , and L 4 to drill the next hole b in the workpiece 4. Similarly, cut out line 1
Holes a, b, and holes for one circumference passing through the workpiece 4 are formed on the
c............ are continuously drilled. Next, the rotating body 1 is shifted by θ/2 from the current stop position, that is, the convergence spot of the laser oscillator 10 is placed at an intermediate position between the holes a, b, c, etc., which have already been drilled. and repeat the same process as the first step. Then, the workpiece 4 is moved along the cutout line 14.
Holes A, B, C, etc. for one circumference are drilled through the. Each of the above holes A, B, C……………… has the same diameter as each of the above holes a, b, c………………, and between the adjacent holes a, b, c……………… Shortest distance D
is smaller than the diameter d of each of the holes A, B, C, etc., so the workpiece 4 is hollowed out along the hollow line 14. By the way, cutout line 14
In the first step, holes a, b, c, etc. are drilled along the workpiece 4 at predetermined intervals.
...... are drilled, but each hole a, b, c......
... are each drilled independently at a predetermined distance D, so that particles evaporated and scattered from the holes during drilling will not accumulate as residue in adjacent holes that have already been drilled. In addition, the drilling process for each hole starts from the surface of the workpiece 4, and the molten material inside the hole is scattered upward and progresses inside, so the laser convergence spot is focused on the holes that are formed one after another. It reaches the interior while reflecting off the inner wall of the hole, and the drilling process proceeds while removing any residue remaining on the inner wall of the hole. Furthermore, when the laser beam reaches the back side of the workpiece 4, the molten material is discharged to the outside from the top and bottom of the hole, so that the residue inside the hole is completely removed, making it possible to drill a clean hole. When the first step is completed, most of the workpiece 4 on the cutout line 14 is removed, and only the residue 15 remains between the holes a, b, c, . . . . Therefore, if the second step is carried out in such a state, the remaining portion 15 is a region that has already been divided in the circumferential direction by the holes a, b, c, and so on. The temperature of No. 15 increases easily, and the hole A,
B, C……………… can be drilled. In this case, the particles that have evaporated and scattered will also enter the holes a, b, c, etc. that have already been drilled, but the particles that will be scattered from the hole A that is drilled in the second step will be The amount is not large enough to cover the holes a and b that have already been drilled on both sides, but it is enough to adhere to a portion of the holes a and b. Therefore, the workpiece 4 has a cutout line 14
The desired hole can be bored out along the line very efficiently. In this example, the first
The second process is carried out when the process of 1 is completed for one round along the cutout line 14, but the first process and the second process are carried out alternately, and the adjacent two steps are carried out in the first process. The second step may be performed on the remaining portion between the holes each time a hole is drilled.
したがつて本発明によるものであれば、加工中
の孔から飛散した溶融粒子が既に穿設された孔に
蓄積されることなく、極めて効率良く孔明け作業
を実施できるものである。また孔明け作業ばかり
でなく、直線あるいは曲線状の溝切り作業等にも
広く応用できるものである。溝は貫通孔ばかりで
なく中途の深さのものにも同様に適用できるもの
である。 Therefore, according to the present invention, the drilling work can be carried out extremely efficiently without the molten particles scattered from the hole being processed being accumulated in the hole that has already been drilled. Moreover, it can be widely applied not only to drilling work but also to cutting straight or curved grooves. Grooves can be applied not only to through holes but also to intermediate depth grooves.
第1図は本発明の実施例を示す断面図、第2図
は同実施例の被加工物に穿設する孔の加工位置を
示す説明図、第3図は同実施例のタイミングチヤ
ート、第4図は同実施例の加工手順を示す説明図
である。
1……回転体、4……被加工物、7……パルス
モータ、10……レーザ発振器、14……くり抜
き線。
Fig. 1 is a sectional view showing an embodiment of the present invention, Fig. 2 is an explanatory diagram showing the machining position of a hole to be drilled in a workpiece in the same embodiment, and Fig. 3 is a timing chart of the same embodiment. FIG. 4 is an explanatory diagram showing the processing procedure of the same embodiment. 1... Rotating body, 4... Workpiece, 7... Pulse motor, 10... Laser oscillator, 14... Hollowed out wire.
Claims (1)
で該被加工物に設定したくり抜き線に沿うくり抜
き溝を形成して該被加工物に所定形状の孔明け加
工を施すものであつて、前記スポツトで前記被加
工物の前記くり抜き線上に孔を隣接させて、かつ
その隣接する孔間に、その孔の直径よりも小さな
間隔をあけて穿設する第1の工程と、前記第1の
工程で穿設した隣設する孔間の残存部に前記スポ
ツトで孔を穿設し、該隣接する孔間を連通させる
第2の工程からなることを特徴とするレーザ加工
方法。 2 前記第1の工程を前記くり抜き線に沿つて一
周分連続的に行ない、次いで前記第2の工程を前
記くり抜き線に沿つて一周分連続的に行うことを
特徴とする特許請求の範囲第1項記載のレーザ加
工方法。 3 前記くり抜き線に沿つて前記第1の工程と第
2の工程とを交互に繰返し行なうことを特徴とす
る特許請求の範囲第1項記載のレーザ加工方法。[Scope of Claims] 1. A method for drilling a predetermined shape in a workpiece by forming a cutout groove along a cutout line set in the workpiece using a spot focused laser beam on the workpiece. a first step of drilling adjacent holes on the cutout line of the workpiece at the spot and leaving an interval smaller than the diameter of the hole between the adjacent holes; A laser processing method comprising a second step of drilling a hole at the spot in a remaining portion between adjacent holes drilled in the first step, and communicating the adjacent holes. 2. Claim 1, characterized in that the first step is continuously carried out for one round along the cutout line, and then the second step is carried out continuously for one turn along the cutout line. Laser processing method described in section. 3. The laser processing method according to claim 1, wherein the first step and the second step are alternately repeated along the cut-out line.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP7853179A JPS564391A (en) | 1979-06-21 | 1979-06-21 | Laser working method |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP7853179A JPS564391A (en) | 1979-06-21 | 1979-06-21 | Laser working method |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS564391A JPS564391A (en) | 1981-01-17 |
| JPS6141672B2 true JPS6141672B2 (en) | 1986-09-17 |
Family
ID=13664486
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP7853179A Granted JPS564391A (en) | 1979-06-21 | 1979-06-21 | Laser working method |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS564391A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2005517839A (en) * | 2002-02-20 | 2005-06-16 | ローマ リンダ ユニヴァーシティ メディカル センター | Method for reinforcing concrete structures |
Families Citing this family (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS6047070B2 (en) * | 1981-06-30 | 1985-10-19 | 油谷鉄工株式会社 | A power tool that can detect the rotation angle after a certain torque |
| AT378306B (en) * | 1983-08-29 | 1985-07-25 | Akg Akustische Kino Geraete | USE OF A BUNDLED LASER BEAM FOR PRODUCING AN ACOUSTIC FRICTION RESISTOR FOR ELECTROACOUSTIC TRANSDUCERS |
| JPS60170590A (en) * | 1984-02-16 | 1985-09-04 | Matsutani Seisakusho:Kk | Piercing method of eyeless stitching needle |
| JPS6289590A (en) * | 1985-10-14 | 1987-04-24 | Mitsubishi Motors Corp | Manufacture of fuel jet nozzle |
| JP2583469Y2 (en) * | 1992-03-25 | 1998-10-22 | 滋賀ボルト株式会社 | Bolt tightening device |
| JP2555945Y2 (en) * | 1992-03-25 | 1997-11-26 | 滋賀ボルト株式会社 | Bolt tightening device |
| US5658474A (en) * | 1994-12-16 | 1997-08-19 | Alza Corporation | Method and apparatus for forming dispenser delivery ports |
| US6373026B1 (en) | 1996-07-31 | 2002-04-16 | Mitsubishi Denki Kabushiki Kaisha | Laser beam machining method for wiring board, laser beam machining apparatus for wiring board, and carbonic acid gas laser oscillator for machining wiring board |
| JPH1147965A (en) * | 1997-05-28 | 1999-02-23 | Komatsu Ltd | Laser processing equipment |
| US7259354B2 (en) * | 2004-08-04 | 2007-08-21 | Electro Scientific Industries, Inc. | Methods for processing holes by moving precisely timed laser pulses in circular and spiral trajectories |
-
1979
- 1979-06-21 JP JP7853179A patent/JPS564391A/en active Granted
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2005517839A (en) * | 2002-02-20 | 2005-06-16 | ローマ リンダ ユニヴァーシティ メディカル センター | Method for reinforcing concrete structures |
Also Published As
| Publication number | Publication date |
|---|---|
| JPS564391A (en) | 1981-01-17 |
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