[go: up one dir, main page]

JP2001341015A - Twist drill for cutting stainless steel - Google Patents

Twist drill for cutting stainless steel

Info

Publication number
JP2001341015A
JP2001341015A JP2001069801A JP2001069801A JP2001341015A JP 2001341015 A JP2001341015 A JP 2001341015A JP 2001069801 A JP2001069801 A JP 2001069801A JP 2001069801 A JP2001069801 A JP 2001069801A JP 2001341015 A JP2001341015 A JP 2001341015A
Authority
JP
Japan
Prior art keywords
stainless steel
drill
cutting
twist drill
chips
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
JP2001069801A
Other languages
Japanese (ja)
Inventor
Tokuhide Onizuka
徳英 鬼塚
Takenori Shimizu
武則 清水
Isao Yokota
勲 横田
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.)
Moldino Tool Engineering Ltd
Original Assignee
Hitachi Tool Engineering 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 Hitachi Tool Engineering Ltd filed Critical Hitachi Tool Engineering Ltd
Priority to JP2001069801A priority Critical patent/JP2001341015A/en
Publication of JP2001341015A publication Critical patent/JP2001341015A/en
Pending legal-status Critical Current

Links

Landscapes

  • Drilling Tools (AREA)

Abstract

PROBLEM TO BE SOLVED: To provide a twist drill for cutting stainless steel with excellent durability by applying a tool profile of a sharper edge when drilling a comparatively ductile material to be cut such as stainless steel and adopting a shape without applying load to a drill main body in a high speed cutting of 25 m or more. SOLUTION: This coated cemented carbide stainless steel twist drill is constituted of a helix angle: 30 to 45 deg. and a curvature of an edge groove bottom part continuous to a cutting face: 0.2 to 0.4 of a drill diameter and a groove width ratio: 45 to 70% in a cross section diagram perpendicular to the axis.

Description

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

【0001】[0001]

【産業上の利用分野】本願発明は、延性のある被削材、
例えば、軟鋼、ステンレス鋼等の難削材の穴明け工具に
関し、特に高速度工具鋼を用いたステンレス鋼の穴明け
工具にする。
BACKGROUND OF THE INVENTION The present invention relates to a ductile work material,
For example, the present invention relates to a drilling tool made of difficult-to-cut materials such as mild steel and stainless steel, and particularly to a stainless steel drilling tool using high-speed tool steel.

【0002】[0002]

【従来の技術】従来、延性のある被削材、特にステンレ
ス鋼の穴あけ工具には多種多様なドリルが提案されてい
る。ステンレス鋼の穴加工においては、図1に示すよう
な、30度前後のねじれ角を有する一般的なツイストド
リルでも切削できるが、加工硬化するために削りにく
く、切屑が分断されにくいという特性があり、切屑排出
性(切削動力)や穴精度(拡大代、特に被削材の入口で
の拡大代)が悪くなるという欠点がある。しかも、切削
点の温度を下げ、工具寿命の延長を図り、切削抵抗を下
げるため、切屑排出溝のねじれ角は30度前後と大きく
設定されている。これを改良したものに特開平9−11
015号公報に記載の穴あけ工具が有る。特開平9−1
1015号公報には、先端刃のみ、ねじれ角を大きく
し、切れ味は良くした例である。
2. Description of the Related Art Conventionally, various kinds of drills have been proposed for a drilling tool made of a ductile work material, particularly a stainless steel. In the drilling of stainless steel, as shown in Fig. 1, a general twist drill having a twist angle of about 30 degrees can be cut, but it has the property that it is hard to cut due to work hardening, and it is difficult to cut chips. In addition, there is a disadvantage that the chip discharging property (cutting power) and the hole accuracy (enlargement allowance, particularly enlargement allowance at the entrance of the work material) are deteriorated. In addition, the torsion angle of the chip discharge groove is set to be as large as about 30 degrees in order to lower the temperature of the cutting point, prolong the tool life, and lower the cutting resistance. An improved version of this is disclosed in JP-A-9-11.
No. 015 discloses a drilling tool. JP-A-9-1
Japanese Patent Publication No. 1015 is an example in which only the tip blade has a large torsion angle and good sharpness.

【0003】更に、ステンレス鋼を切削する際のチゼル
部の形状は、該と同じ理由により、シャープな形状であ
るX型シンニングが用いられるが、切削抵抗の軽減や求
心性の向上を目的にX型シンニングを改良してその段差
を無くし、スムーズな切屑排出が行えるようにした特開
平11−267912号の例が有る。また、先端刃も凹
状として、切り屑処理性を高めている。また、ステンレ
ス鋼の穴あけ加工では、切り屑形態も重要な課題であ
る。切り屑形態は遷移折段型と称される切り屑が最も扱
いやすく排出性も良いが、特に、ステンレス切削で切り
屑の形態に着目した例はほとんどない。
[0003] Further, for the same reason as above, a sharp shape of X-type thinning is used for the shape of the chisel portion when cutting stainless steel, but X-type thinning is used for the purpose of reducing cutting resistance and improving centripetality. Japanese Patent Application Laid-Open No. H11-267912 discloses an example in which the mold thinning is improved to eliminate the step, thereby enabling smooth chip discharge. In addition, the tip blade is also concave so as to enhance chip disposal. In drilling stainless steel, the form of chips is also an important issue. Regarding the chip form, a chip called a transition folding step type is the easiest to handle and has good dischargeability, but there is hardly any example focusing on the chip form in stainless steel cutting.

【0004】[0004]

【発明が解決しようとする課題】ステンレス切削におけ
る切り屑としては、一般の鋼と同様遷移折段型の切り屑
が得られるが、先端切れ刃の損傷により切り屑の形態が
崩れるため、損傷を防止する検討が多く、適切な形状と
なっているか検討されていないのが現状である。そのた
め、ステンレス鋼の穴あけ加工を進めると、切削初期は
切り屑も分断されるが、穴数が増えるに従い、切り屑が
連続するようになり、しばらく継続すると寿命となる。
この過程で、工具側の損傷は先端切れ刃の外周端部に集
中して発生する。この切り屑が連続するまえの形態を長
持ちさせるため、特に、すくい面から刃溝形状に着目し
た。
As cutting chips in stainless steel cutting, transition step-shaped chips can be obtained as in the case of ordinary steel, but since the shape of the chips is broken by damage to the tip cutting edge, damage is caused. There are many studies to prevent this, and it has not been studied whether the shape is appropriate. Therefore, when the drilling of stainless steel is advanced, the chips are also separated in the initial stage of cutting, but as the number of holes increases, the chips become continuous, and if they continue for a while, the life is extended.
In this process, damage on the tool side is concentrated on the outer peripheral end of the leading edge. In order to extend the form before the chips continue, attention was paid particularly to the shape of the blade groove from the rake face.

【0005】上記課題を解決するために、本願発明で
は、ステンレス鋼の様に比較的延性のある被削材の穴明
け加工に際して、より一層のシャープエツジな刃型を適
用し、25m以上の高速切削において、ドリル本体に負
荷のかからない形状を採用することにより、耐久性に優
れたステンレス切削用ツイストドリルを提供することを
目的とする。
[0005] In order to solve the above-mentioned problems, the present invention employs a sharper edge cutter for drilling a relatively ductile work material such as stainless steel, and has a high speed of 25 m or more. An object of the present invention is to provide a stainless steel twist drill having excellent durability by adopting a shape in which a load is not applied to a drill body in cutting.

【0006】[0006]

【課題を解決するための手段】本発明によるツイストド
リルは、被覆した超硬質合金製からなるステンレス製ツ
イストドリルにおいて、ねじれ角を30〜45度とし、
軸直角断面図で、すくい面に連なる刃溝底部の曲率をド
リル刃径の0.2〜0.4、溝幅比を45〜70%、と
したことを特徴とするステンレス切削用ツイストドリル
である。
The twist drill according to the present invention is a stainless steel twist drill made of a coated super-hard alloy and having a twist angle of 30 to 45 degrees.
A twist drill for stainless steel cutting, characterized in that the curvature of the bottom of the blade groove connected to the rake face is 0.2 to 0.4 of the drill blade diameter and the groove width ratio is 45 to 70% in a cross section perpendicular to the axis. is there.

【0007】先ず、刃溝底部の曲率半径は一般的にドリ
ル外径の0.15〜0.35程度が用いられている。こ
の曲率半径は小さいほど切り屑がカールし、大きいほど
カール径が大きく、切り屑としては分断されにくくな
る。そのため、強ねじれとの相乗効果により曲率半径を
0.2〜0.4として、切り屑を分断させるようにする
と、0.2〜0.40においても遷移折段型の切り屑が
得られ、且つ、大きな曲率でカールさせるため、ドリル
にかかる負荷が軽減され、分断された切り屑が長く継続
するようになる。従って、ツイストドリルの軸方向すく
い角であるねじれ角は、大きく採れば切れ味をよくでき
るが、その反面、強度が低下する。ねじれ角が30度未
満だと切削抵抗が大きく拡大代が大きくなり、穴精度が
低下し、ねじれ角が45度を超えると、切り屑排出の妨
げになるため30度〜45度の範囲とした。
First, the radius of curvature at the bottom of the blade groove is generally about 0.15 to 0.35 of the outer diameter of the drill. The smaller the radius of curvature is, the more the chips are curled, and the larger the radius of curvature is, the larger the curl diameter is, and it is difficult to separate the chips as chips. For this reason, if the radius of curvature is set to 0.2 to 0.4 by a synergistic effect with strong torsion and the chips are separated, transition step type chips are obtained even at 0.2 to 0.40. In addition, since the curl is performed with a large curvature, the load applied to the drill is reduced, and the cut chips continue for a long time. Therefore, if the twist angle, which is the rake angle in the axial direction of the twist drill, is large, the sharpness can be improved, but the strength is reduced. If the torsion angle is less than 30 degrees, the cutting resistance is large and the margin for enlargement is large, the hole accuracy is reduced, and if the torsion angle exceeds 45 degrees, the chip discharge is hindered, so the range was 30 to 45 degrees. .

【0008】次に、曲率半径の大きさをドリル刃径の
0.2〜0.4の範囲としたのは、ドリルの内壁を用い
てカールさせるのではなく、被切削面である被削材を内
壁と同様に用いて切り屑処理を行うこととしたもので、
そのため大きな刃溝を設けることができる。0.2未満
では、切り屑処理にかかる負荷が大きく、ドリル本体に
負荷がかかるため寿命が短くなるためである。
Next, the reason why the radius of curvature is set in the range of 0.2 to 0.4 of the drill blade diameter is not to use the inner wall of the drill to curl, but to use Is to be used in the same way as the inner wall for chip processing.
Therefore, a large blade groove can be provided. If it is less than 0.2, the load applied to chip processing is large, and a load is applied to the drill body, so that the life is shortened.

【0009】溝幅比は(断面図における、切屑排出溝の
溝幅を工具外周長さで除し、百分率で表す。)45〜7
0%とした。ここで、溝幅比45%未満では、強ねじれ
と相まって溝幅が狭くなり切屑詰まりを引き起こすこと
になり、70%を超えると、溝幅が広い分、ランド部が
薄くなりすぎ不安定となるため、溝幅比は45〜70%
の範囲とした。更に、大きな溝幅比は、溝のヒール部の
形状により調整することもできる。ヒール部の先端を円
弧状に形成することにより、溝幅比を大きくとり、前述
のような切り屑の内壁との接触を少なめることができ
る。ドリルの芯厚は、0.10D〜0.30Dの範囲と
した。0.10D未満では工具剛性が不足して、穴加工
時の被削材入口の拡大代の精度が悪くなり、0.30D
を越えると溝自体のスペースを狭くなりすぎるため、壁
との接触が増え、切削抵抗が大きくなると共に切屑排出
性が悪くなり、切屑詰まりを起し易くなるめである。
The groove width ratio is 45 to 7 (in the sectional view, the groove width of the chip discharge groove is divided by the outer peripheral length of the tool and expressed as a percentage).
0%. Here, if the groove width ratio is less than 45%, the groove width becomes narrow in combination with strong torsion, causing chip clogging. Therefore, the groove width ratio is 45 to 70%
Range. Furthermore, a large groove width ratio can be adjusted by the shape of the heel portion of the groove. By forming the tip of the heel portion in an arc shape, the groove width ratio can be increased and the contact of the chip with the inner wall as described above can be reduced. The core thickness of the drill was in the range of 0.10D to 0.30D. If it is less than 0.10D, the rigidity of the tool is insufficient, and the precision of the enlargement allowance of the work material entrance at the time of drilling becomes poor.
Exceeding the limit causes the space of the groove itself to be too narrow, increasing the contact with the wall, increasing the cutting resistance, deteriorating the chip discharge property, and easily causing chip clogging.

【0010】本発明のツイストドリルは、高速度鋼を用
いて説明してきたが、より好ましくは粉末ハイスのほう
が良い。通常の溶製ハイスに比して炭化物の粒度が細か
いため、ねじれ角が強い本発明のドリルには好都合であ
る。また、溶製ハイスでもねじれを生かし、ホーニング
の大小により適用することができる。更に、ステンレス
鋼等の延性に富む材料には被覆が必須なものであり、本
発明においても公知な被膜、例えばTiNやTiAlN
等の物理蒸着法を用いて行われる膜が適している。特
に、切り屑の溶着や圧着を生じやすい先端刃のチゼル近
傍には、潤滑性にとむ2硫化モリブデンや固体潤滑剤等
の被膜も有効である。
Although the twist drill of the present invention has been described using high-speed steel, powdered high-speed steel is more preferred. Since the carbide has a finer grain size as compared with the ordinary ingot high-speed steel, it is advantageous for the drill of the present invention having a large torsion angle. In addition, it can be applied to the size of the honing by making use of the torsion even in the melted high speed steel. Further, a coating is essential for a highly ductile material such as stainless steel, and a coating known in the present invention, for example, TiN or TiAlN
A film formed using a physical vapor deposition method such as described above is suitable. In particular, a film of molybdenum disulfide, a solid lubricant, or the like, which improves lubricity, is effective in the vicinity of the chisel of the tip blade where chip welding and pressure bonding are likely to occur.

【0011】30〜45度のねじれ角を採用することに
より、切れ味がよく高い穴精度が得られる。更に、穴精
度をより高めるため、シンニング形状をより求心性の高
い形状とする事が好ましい。例えば、図5の様に、シン
ニング角度を大きく採り、図4に示すように、軸方向の
すくい角を−5度以上の負角とし、刃溝まで十分な距離
を、滑らかに結ぶように設けることにより、切り屑のつ
まりを防止することができる。以下、実施例に基づき、
本発明を具体的に説明する。
By using a twist angle of 30 to 45 degrees, sharpness and high hole accuracy can be obtained. Further, in order to further improve the hole accuracy, it is preferable to make the thinning shape a shape with higher centripetality. For example, as shown in FIG. 5, a large thinning angle is used, and as shown in FIG. 4, the rake angle in the axial direction is set to a negative angle of -5 degrees or more, and a sufficient distance to the blade groove is provided so as to be smoothly connected. This can prevent chips from being clogged. Hereinafter, based on the examples,
The present invention will be specifically described.

【0012】[0012]

【実施例】図3は、本発明の実施例によるドリルの正面
図、図4は、図3に示すドリルの90度回転させた上面
図、図5は、図3の先端視である。本実施例によるツイ
ストドリル1は、高速度鋼(粉末ハイス)製、刃径6m
m、2枚刃、ねじれ角2は40度で、TiAlNを被覆
した。図5に示すように、軸線Oの周りの先端切れ刃3
が設けられている。また、図6に示す軸直角断面図にお
ける曲率半径Rはドリル外径の30%の曲率で結んでい
る。先端切れ刃3のシンニングはX型とした。
FIG. 3 is a front view of a drill according to an embodiment of the present invention, FIG. 4 is a top view of the drill shown in FIG. 3 rotated by 90 degrees, and FIG. 5 is a front view of FIG. The twist drill 1 according to the present embodiment is made of high-speed steel (powder high-speed steel) and has a blade diameter of 6 m.
m, two blades, helix angle 2 was 40 degrees, and TiAlN was coated. As shown in FIG. 5, the tip cutting edge 3 around the axis O
Is provided. Further, the radius of curvature R in the cross-section perpendicular to the axis shown in FIG. 6 is connected at a curvature of 30% of the outer diameter of the drill. The thinning of the tip cutting edge 3 was X-shaped.

【0013】次に、本発明によるドリル、図1に示すね
じれ角30度の従来ドリル1、図2に示す従来ドリル2
とについて、各種被削材の切削性能に関する試験を行っ
た。尚、従来ドリルは、同一径でTiAlN被覆を行っ
た。切削試験にあたっては、被削材として、SUS30
4を用い、穴加工深さ3Dとし、切削油剤は水溶性のエ
マルジョンタイプを用い、切削速度30m/min、送
り量0.15mm/revで行い、切れ刃のチッピング
状態、摩耗量・摩耗状態を一定数ごとに確認し、穴あけ
を継続した。また、1穴目の加工で拡大代を測定し、更
に、定常摩耗域で測定した。先ず、100穴加工したと
き、本発明例のドリルは、切り屑形態としては図7に示
すように、処理性の良いカールされた切り屑が得られ、
拡大代は、入り口、中央とも0.02mmと良好であ
り、チッピングもなく正常な摩耗を示したが、従来例1
では切削速度が速すぎるため、1穴も加工できずに寿命
となった。従来例2のドリルも、外周側部にチッピング
を生じた。そのため拡大代は、0.09mmと大きくな
った。
Next, a drill according to the present invention, a conventional drill 1 having a twist angle of 30 degrees shown in FIG. 1, and a conventional drill 2 shown in FIG.
With respect to and, tests regarding the cutting performance of various work materials were performed. The conventional drill was coated with TiAlN at the same diameter. In the cutting test, SUS30
4, the drilling depth is 3D, the cutting fluid is a water-soluble emulsion type, the cutting speed is 30 m / min, the feed rate is 0.15 mm / rev, and the chipping state, wear amount and wear state of the cutting edge are determined. Checking was performed at a fixed number of times, and drilling was continued. In addition, the allowance for enlargement was measured in the processing of the first hole, and further, it was measured in the steady wear region. First, when 100 holes are drilled, the drill of the present invention can obtain curled chips with good processing properties as shown in FIG.
The enlargement allowance was as good as 0.02 mm at the entrance and at the center, showing normal wear without chipping.
In this case, the cutting speed was too high, so that one hole could not be machined, and the life was shortened. The drill of Conventional Example 2 also had chipping on the outer peripheral side. Therefore, the enlargement allowance was as large as 0.09 mm.

【0014】更に、試験を継続し、200穴、400
穴、600穴と続けたが、切れ刃に徐々に溶着がみられ
るようになり、その脱落等により逃げ面最大摩耗量が
0.2mm程度となったため、切削試験を止めた。60
0穴加工での拡大代も0.03mmと良好であった。ま
た、切り屑の形態もほとんど変化が無く、600穴加工
時の切り屑を図8に示すが、図7の切り屑と大差なく、
切り屑がドリル本体に巻き付いてトラブルようなことも
なく、分断された切り屑が得られた。
Further, the test was continued, and 200 holes, 400 holes
Although the number of holes and the number of holes continued to be 600, the cutting test was stopped because welding gradually began to be observed on the cutting edge, and the maximum wear amount of the flank became about 0.2 mm due to falling off. 60
The enlargement allowance in the 0-hole processing was as good as 0.03 mm. In addition, the form of the chip has almost no change, and the chip at the time of machining 600 holes is shown in FIG. 8, but not much different from the chip in FIG. 7.
There was no problem with the chips wrapping around the drill body, and the divided chips were obtained.

【0015】次に、曲率半径のRの大きさをドリル外径
の15%、20%、30%、40%の試料を製作し、同
様に切削試験を行った。その結果、50穴目までで、切
り屑が連なるようになったのは15%の曲率半径のみで
他は良好で、正常な摩耗を示した。更に試験を継続し、
200穴まで試験を継続すると、20%で切り屑形態が
変化し、連続する切り屑が排出されようになった。他の
試料は正常な摩耗を示した。
Next, samples having a radius of curvature R of 15%, 20%, 30%, and 40% of the outer diameter of the drill were manufactured, and a cutting test was performed in the same manner. As a result, up to the 50th hole, only 15% of the radius of curvature led to continuous cutting chips, and the others were good and showed normal wear. Further testing,
When the test was continued up to 200 holes, the chip morphology changed at 20% and continuous chips began to be discharged. Other samples showed normal wear.

【0016】尚、上述の実施例においては高速度鋼を用
いて説明したが、これに限定されることなく、超硬ソリ
ッドタイプやスローアウェイタイプのドリル等であって
も、同様に本発明を適用できる。
Although the above embodiment has been described using high-speed steel, the present invention is not limited to this, and the present invention is similarly applicable to a solid carbide type or a throw-away type drill. Applicable.

【0017】[0017]

【発明の効果】上記のように、本発明に係る穴明け工具
を用いることにより、切削抵抗が小さく、穴精度(拡大
代)の良い加工が行え、また、切り屑がからみつき能率
を落とすようなトラブルが無く、優れた工具寿命を発揮
する。
As described above, by using the drilling tool according to the present invention, it is possible to perform machining with small cutting resistance and high hole accuracy (enlargement allowance), and also to reduce the efficiency with which chips are entangled and reduce efficiency. Demonstrate excellent tool life without any trouble.

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

【図1】図1は、従来例のツイストドリルの正面図を示
す。
FIG. 1 is a front view of a conventional twist drill.

【図2】図2は、他の従来例のツイストドリルの正面図
を示す。
FIG. 2 is a front view of another conventional twist drill.

【図3】図3は、本発明例の実施例のドリルの正面図を
示す。
FIG. 3 shows a front view of a drill according to an embodiment of the present invention.

【図4】図4は、図3の要部拡大図を示す。FIG. 4 is an enlarged view of a main part of FIG. 3;

【図5】図5は、図3の先端視を示す。FIG. 5 shows a front view of FIG. 3;

【図6】図6は、図3のA−A線の軸直角断面図を示
す。
FIG. 6 is a sectional view taken along the line AA of FIG. 3 at right angles to the axis;

【図7】図7は、本発明例の50穴加工時の切り屑を示
す。
FIG. 7 shows chips when machining 50 holes according to the example of the present invention.

【図8】図8は、本発明例の600穴加工時の切り屑を
示す。
FIG. 8 shows cuttings at the time of machining 600 holes according to the present invention.

【符号の説明】 1 ツイストドリル 2 ねじれ角 3 先端切れ刃 R 曲率半径[Description of Signs] 1 Twist drill 2 Helix angle 3 Tip cutting edge R Curvature radius

Claims (3)

【特許請求の範囲】[Claims] 【請求項1】被覆した超硬質合金製からなるステンレス
製ツイストドリルにおいて、ねじれ角を30〜45度と
し、軸直角断面図で、すくい面に連なる刃溝底部の曲率
をドリル刃径の0.2〜0.4、溝幅比を45〜70
%、としたことを特徴とするステンレス切削用ツイスト
ドリル。
In a coated stainless steel twist drill made of a super-hard alloy, the torsion angle is set to 30 to 45 degrees, and the curvature of the bottom of the blade groove connected to the rake face is defined as 0. 2 to 0.4, groove width ratio 45 to 70
%, A twist drill for stainless steel cutting.
【請求項2】請求項1記載のステンレス切削用ツイスト
ドリルにおいて、該被覆がTiN、TiAlN等の硬質
皮膜からなることを特徴とするステンレス切削用ツイス
トドリル。
2. The twist drill for stainless steel cutting according to claim 1, wherein said coating is made of a hard film such as TiN or TiAlN.
【請求項3】請求項1記載のステンレス切削用ツイスト
ドリルにおいて、該超硬質合金が高速度鋼からなること
を特徴とするステンレス切削用ツイストドリル。
3. The twist drill for stainless steel cutting according to claim 1, wherein said super-hard alloy is made of high-speed steel.
JP2001069801A 2000-03-31 2001-03-13 Twist drill for cutting stainless steel Pending JP2001341015A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP2001069801A JP2001341015A (en) 2000-03-31 2001-03-13 Twist drill for cutting stainless steel

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
JP2000096827 2000-03-31
JP2000-96827 2000-03-31
JP2001069801A JP2001341015A (en) 2000-03-31 2001-03-13 Twist drill for cutting stainless steel

Publications (1)

Publication Number Publication Date
JP2001341015A true JP2001341015A (en) 2001-12-11

Family

ID=26589061

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2001069801A Pending JP2001341015A (en) 2000-03-31 2001-03-13 Twist drill for cutting stainless steel

Country Status (1)

Country Link
JP (1) JP2001341015A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2006187860A (en) * 2005-01-05 2006-07-20 Sandvik Intellectual Property Ab Drill
JP2007229899A (en) * 2006-03-03 2007-09-13 Mitsubishi Materials Corp Drill

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS634211U (en) * 1986-06-23 1988-01-12
JPH02124210A (en) * 1987-12-22 1990-05-11 Mitsubishi Metal Corp twist drill
JPH0460606U (en) * 1990-09-28 1992-05-25
JPH0671015U (en) * 1993-03-11 1994-10-04 株式会社東洋製作所 Twist drill
JPH0911015A (en) * 1995-06-30 1997-01-14 Mitsubishi Materials Corp Hole drilling tool
JPH09501109A (en) * 1993-08-06 1997-02-04 ケンナメタル ヘルテル アクチェンゲゼルシャフト ウェルクツォイゲ ウント ハルトシュトッフェ Twist drill

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS634211U (en) * 1986-06-23 1988-01-12
JPH02124210A (en) * 1987-12-22 1990-05-11 Mitsubishi Metal Corp twist drill
JPH0460606U (en) * 1990-09-28 1992-05-25
JPH0671015U (en) * 1993-03-11 1994-10-04 株式会社東洋製作所 Twist drill
JPH09501109A (en) * 1993-08-06 1997-02-04 ケンナメタル ヘルテル アクチェンゲゼルシャフト ウェルクツォイゲ ウント ハルトシュトッフェ Twist drill
JPH0911015A (en) * 1995-06-30 1997-01-14 Mitsubishi Materials Corp Hole drilling tool

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2006187860A (en) * 2005-01-05 2006-07-20 Sandvik Intellectual Property Ab Drill
JP2007229899A (en) * 2006-03-03 2007-09-13 Mitsubishi Materials Corp Drill

Similar Documents

Publication Publication Date Title
JP5762547B2 (en) drill
EP2698219B1 (en) Drill
JP6892503B2 (en) Rotating tool
JP2008137125A (en) Drill
JP2002144125A (en) Boring tool
JPS62188616A (en) Rotary cutting tool
JP2010099778A (en) Drill, cutting insert, and cutting method
WO2021230176A1 (en) Drill and method for manufacturing cut workpiece
JP2006239829A (en) Drill
JPS6389211A (en) Twist drill
JP3337804B2 (en) End mill
JP2019115939A (en) Rotary tool and manufacturing method of cutting workpiece
JP2006281407A (en) Machining drill for nonferrous metal
JP2001341015A (en) Twist drill for cutting stainless steel
WO2012053090A1 (en) Three-bladed drill
JP2001341016A (en) Twist drill for cutting stainless steel
JP2623304B2 (en) Cermet twist drill
JP4954044B2 (en) drill
JP2001341020A (en) Drilling tool
JP2002254234A (en) Ball end mill
JP7714763B2 (en) Reamer
JP2001341019A (en) Twist drill
JP2005186247A (en) Twist drill
JP2003039218A (en) Drill for deep hole
JP2005205526A (en) Deep hole boring tool

Legal Events

Date Code Title Description
A621 Written request for application examination

Free format text: JAPANESE INTERMEDIATE CODE: A621

Effective date: 20080212

A131 Notification of reasons for refusal

Free format text: JAPANESE INTERMEDIATE CODE: A131

Effective date: 20100812

A977 Report on retrieval

Free format text: JAPANESE INTERMEDIATE CODE: A971007

Effective date: 20100819

A521 Written amendment

Free format text: JAPANESE INTERMEDIATE CODE: A523

Effective date: 20101008

A131 Notification of reasons for refusal

Free format text: JAPANESE INTERMEDIATE CODE: A131

Effective date: 20101125

A521 Written amendment

Free format text: JAPANESE INTERMEDIATE CODE: A523

Effective date: 20110124

A131 Notification of reasons for refusal

Free format text: JAPANESE INTERMEDIATE CODE: A131

Effective date: 20110318

A02 Decision of refusal

Free format text: JAPANESE INTERMEDIATE CODE: A02

Effective date: 20110809