JPH0839319A - Three-blade drill - Google Patents

Three-blade drill

Info

Publication number
JPH0839319A
JPH0839319A JP19610994A JP19610994A JPH0839319A JP H0839319 A JPH0839319 A JP H0839319A JP 19610994 A JP19610994 A JP 19610994A JP 19610994 A JP19610994 A JP 19610994A JP H0839319 A JPH0839319 A JP H0839319A
Authority
JP
Japan
Prior art keywords
angle
drill
hole
tip
cutting
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.)
Withdrawn
Application number
JP19610994A
Other languages
Japanese (ja)
Inventor
Riichi Otani
利一 大谷
Kiyoshi Hasegawa
清 長谷川
Nobuyasu Nonaka
延恭 野中
Yoshiomi Sugano
悦臣 菅野
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.)
Via Mechanics Ltd
Nissan Motor Co Ltd
Moldino Tool Engineering Ltd
Original Assignee
Nissan Motor Co Ltd
Hitachi Tool Engineering Ltd
Hitachi Seiko 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 Nissan Motor Co Ltd, Hitachi Tool Engineering Ltd, Hitachi Seiko Ltd filed Critical Nissan Motor Co Ltd
Priority to JP19610994A priority Critical patent/JPH0839319A/en
Publication of JPH0839319A publication Critical patent/JPH0839319A/en
Withdrawn legal-status Critical Current

Links

Abstract

PURPOSE:To provide a drill in which not only a deep hole machining having no prepared hole but also a high speed drilling work having a casted hole can be stably performed. CONSTITUTION:In a three-blade drill, an oil hole for blowing out cutting oil agent from the drill top end is provided within a land 3 along a helical angle, the helical angle is set to 30 deg.-45 deg., the point angle alpha is set to 140 deg.-160 deg., the sinning angle gamma is set to 25 deg.-35 deg., the core thickness omega is set to 1/3D-3/5D to the outer diameter D of the drill top end, and the groove width ratio represented by the ratio of the angle theta2 of a groove part 1 to the angle theta1 of the land part 3 is set to theta2/theta1=1.5/1-2.5/1.

Description

【発明の詳細な説明】Detailed Description of the Invention

【0001】[0001]

【産業上の利用分野】本発明は、アルミ合金等の軟質材
の穴あけ用のドリルに関する。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a drill for drilling a soft material such as an aluminum alloy.

【0002】[0002]

【従来の技術】アルミ合金等の軟質材の穴あけ加工で
は、高精度の穴あけ用として3枚刃ドリルが知られてい
る(特開平5−301108号)。
2. Description of the Related Art In drilling a soft material such as an aluminum alloy, a three-flute drill is known for highly accurate drilling (Japanese Patent Laid-Open No. 5-301108).

【0003】[0003]

【発明が解決しようとする課題】ところが、従来の3枚
刃ドリルでは、例えば穴深さLがドリル先端の外径Dの
3〜5倍以上の深穴加工を高速(切削速度300〜50
0m/min以上)で加工しようとすると、次のような
問題点がある。
However, in the conventional three-blade drill, for example, deep hole drilling with a hole depth L of 3 to 5 times or more of the outer diameter D of the drill tip is performed at high speed (cutting speed of 300 to 50).
Attempting to machine at 0 m / min or more) has the following problems.

【0004】高速ゆえ、刃先温度が上昇し過ぎる。Because of the high speed, the cutting edge temperature rises too much.

【0005】排出される切りくずにより、切削油が刃
先までかからない。
Due to the chips that are discharged, cutting oil does not reach the cutting edge.

【0006】高速ゆえ、切りくず排出速度も早いの
で、切りくず排出が一瞬でも滞ると切りくずづまりを起
こしやすく、ビビリ、ひいてはドリル折損をきたす等に
より、ドリル寿命が極端に短くなり安定性に欠け実用に
耐えない。
Since the chip discharge speed is high because of the high speed, if the chip discharge is delayed even for a moment, chip jamming is likely to occur, and the drill life is extremely shortened due to chatter, and eventually drill breakage, etc. Can not stand.

【0007】そこで、本発明の目的は、上述した従来の
技術が有する問題点を解消し、アルミ合金等の穴あけ加
工において、下穴のない深穴加工はもちろん、鋳抜き穴
を有する高速穴あけ加工でも安定した穴あけ加工のでき
るドリルを提供する。
Therefore, an object of the present invention is to solve the problems of the above-mentioned conventional techniques, and in drilling an aluminum alloy or the like, not only deep hole drilling without a pilot hole but also high speed drilling with a cast hole. However, we provide a drill that can perform stable drilling.

【0008】[0008]

【課題を解決するための手段】上記目的を達成するため
に、第1の発明は、3枚刃ドリルにおいて、切削油剤を
ドリル先端から噴出させるための油穴をねじれ角にそっ
てランド部内に有し、ねじれ角βを30°〜45°、先
端角αを140°〜160°、シンニング角度γを25
°〜35°、心厚ωをドリル先端の外径Dの1/3D〜
3/5D、及び溝部の角度θ2とランド部の角度θ1の
比によって表される溝幅比をθ2/θ1=1.5/1〜
2.5/1としたものである。
In order to achieve the above object, the first invention is a three-blade drill, and an oil hole for ejecting a cutting fluid from the drill tip is formed in the land portion along the helix angle. The twist angle β is 30 ° to 45 °, the tip angle α is 140 ° to 160 °, and the thinning angle γ is 25.
° ~ 35 °, core thickness ω 1 / 3D of the outer diameter D of the drill tip ~
The groove width ratio represented by 3 / 5D and the ratio of the groove angle θ2 and the land angle θ1 is θ2 / θ1 = 1.5 / 1 to
It is set to 2.5 / 1.

【0009】第2の発明は、溝部の少なくとも刃先先端
を含めた部分に、TiN、TiCN、ダイヤモンド等か
らなる硬質物質を1層又は複層形成したものである。
A second aspect of the present invention is one in which a hard material made of TiN, TiCN, diamond or the like is formed in a single layer or multiple layers in at least a portion including the tip of the cutting edge of the groove.

【0010】[0010]

【作用】本発明の3枚刃ドリルは、3枚刃なので鋳抜き
穴などの下穴がある加工でも、通常の2枚刃と比べてマ
ージン部によるガイド性が増し穴拡大穴曲り等に伴うビ
ビリもなく安定切削できる。又、下穴のない深穴加工で
も、確実に刃先先端に切削油を供給できるので、以下の
優れた特徴がある。
Since the three-blade drill of the present invention is a three-blade drill, even in the processing where there is a prepared hole such as a cast hole, the guideability is increased by the margin portion as compared with the ordinary two-blade, and the hole expansion hole bending is accompanied. Stable cutting is possible without chattering. Further, even in deep hole machining without a prepared hole, the cutting oil can be reliably supplied to the tip of the cutting edge, so that it has the following excellent features.

【0011】イ)刃先冷却により摩耗進行を遅らせられ
る。
B) The progress of wear can be delayed by cooling the cutting edge.

【0012】ロ)刃先に生じる溶着を少なくできる。(B) It is possible to reduce welding that occurs on the cutting edge.

【0013】ハ)給油圧により切りくず排出も円滑にな
る。
C) The supply of hydraulic pressure also facilitates chip discharge.

【0014】又、ねじれ角はバイトのすくい角に相当
し、切れ味及び切りくず排出の点で30°以上必要であ
るが、刃先強度の点で45°以下とした。
The helix angle corresponds to the rake angle of the cutting tool and is required to be 30 ° or more in terms of sharpness and chip discharge, but it is set to 45 ° or less in terms of the strength of the cutting edge.

【0015】次に、シンニング角度γは25°より小さ
い方が切りくず排出性は良いが、先端チゼル部が強度低
下をきたし欠けやすくなる。35°より大きくなると切
りくず排出性が悪くなり、切りくずづまり及び中心近傍
切れ刃の溶着の原因となる。そこで、シンニング角度γ
は25°〜35°とした。
Next, if the thinning angle γ is smaller than 25 °, the chip discharging property is good, but the tip chisel portion is liable to be chipped and chipped easily. If the angle is larger than 35 °, the chip discharging property is deteriorated, which causes chip jamming and welding of the cutting edge near the center. Therefore, the thinning angle γ
Was 25 ° to 35 °.

【0016】先端角αは、ねじり剛性向上及び3枚刃に
おける切りくず流出方向を考慮し、α=140°〜16
0°とした。
The tip angle α is α = 140 ° to 16 ° in consideration of the improvement in torsional rigidity and the chip outflow direction in the three-blade.
It was set to 0 °.

【0017】心厚ωは大きい程ねじり剛性が増すがフル
ートが浅くなるため切りくず排出性が悪くなる。高速切
削になる程、安定性、信頼性の点からも通常作業以上に
ねじり剛性及び切りくず排出性に配慮が必要である。そ
こで、心厚ωをドリル先端の外径Dの1/3D〜3/5
Dと大きめにして剛性を確保し、溝幅比θ2/θ1、ね
じれ角β、先端角α、及びシンニング角度γを組み合わ
せることにより、切りくず排出性の向上を計った。
The larger the core thickness ω, the more the torsional rigidity increases, but the flute becomes shallower, so that the chip discharging property deteriorates. Higher-speed cutting requires more consideration in torsional rigidity and chip evacuation than in normal work in terms of stability and reliability. Therefore, the core thickness ω is set to 1 / 3D to 3/5 of the outer diameter D of the drill tip.
D was set to a larger value to secure rigidity, and by combining the groove width ratio θ2 / θ1, the helix angle β, the tip angle α, and the thinning angle γ, the chip discharging property was improved.

【0018】溝部の少なくとも刃先先端を含めた部分に
TiN、TiCN、ダイヤモンド等からなるコーティン
グ層を1層又は複層形成すれば、コーティングにより耐
摩耗性が向上し、かつ切削速度の遅くなる中心軸近傍の
凝着を少なくできる。特にアルミ合金に穴あけ加工する
場合には、溶着が少なく硬さの高いダイヤモンド膜又は
アモルファス状のダイヤライクカーボン膜を設けること
が好ましい。
By forming a coating layer or layers of TiN, TiCN, diamond or the like on at least a portion of the groove portion including the tip of the cutting edge, the coating improves the wear resistance and reduces the cutting speed of the central shaft. Adhesion in the vicinity can be reduced. Particularly when drilling a hole in an aluminum alloy, it is preferable to provide a diamond film or an amorphous diamond-like carbon film that is less welded and has a higher hardness.

【0019】[0019]

【実施例】以下、本発明の一実施例を図面に基づき説明
する。
DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS An embodiment of the present invention will be described below with reference to the drawings.

【0020】図1において、100は3枚刃ドリルのド
リル先端部を示し、このドリル先端部100には言うま
でもなく3枚の刃部100aが設けられる。3枚刃ドリ
ルのランド部3には、切削油剤をドリル先端から噴出さ
せるための油穴4が設けられ、この油穴4はねじれ角β
にそって延びている。
In FIG. 1, reference numeral 100 denotes a drill tip portion of a three-blade drill, and needless to say, the drill tip portion 100 is provided with three blade portions 100a. The land portion 3 of the three-blade drill is provided with an oil hole 4 for ejecting cutting fluid from the tip of the drill, and the oil hole 4 has a helix angle β.
Extending along.

【0021】そして、この実施例によれば、後述する実
験の結果に従って、ドリル先端部100の各種寸法がつ
ぎのように定められる。
Further, according to this embodiment, various dimensions of the drill tip 100 are determined as follows according to the result of the experiment described later.

【0022】図1、及び図2を参照し、ねじれ角βは3
0°〜45°、先端角αは140°〜160°、シンニ
ング角度γは25°〜35°、心厚ωはドリル先端の外
径Dの1/3D〜3/5D、溝部1の角度θ2とランド
部3の角度θ1の比によって表される溝幅比はθ2/θ
1=1.5/1〜2.5/1と定められる。
Referring to FIGS. 1 and 2, the twist angle β is 3
0 ° to 45 °, tip angle α is 140 ° to 160 °, thinning angle γ is 25 ° to 35 °, core thickness ω is 1 / 3D to 3 / 5D of outer diameter D of the drill tip, and angle θ2 of groove 1 is And the groove width ratio represented by the ratio of the angle θ1 of the land portion 3 is θ2 / θ
1 = 1.5 / 1 to 2.5 / 1.

【0023】つぎに、実験例を示す。Next, an experimental example will be shown.

【0024】まず、ねじれ角αと溝幅比θ2/θ1につ
いて、外径D寸法8mmの超硬合金製3枚刃油穴付きド
リルを使用して、立型マシニングセンタにて切削試験を
行なった。ねじれ角及び溝幅比以外の寸法は、 外径D=8mm 先端角α=150° シンニング角度γ=30° マージン部2(t=0.8mm)の当たり幅b=0.4
mm 心厚ω=3.6mm(=0.45D) 油穴径d=1.0mm バックテーパ=0.15/100 であり、該ドリルの超硬丸棒素材は押出し成形時にドリ
ル外径Dで所定のねじれ角になるようなねじれに伴って
穴が120°等配に3カ所あいており、一般超硬同様焼
結にて製作した。
First, with respect to the twist angle α and the groove width ratio θ2 / θ1, a cutting test was carried out at a vertical machining center using a cemented carbide 3-flute drill with oil holes having an outer diameter D of 8 mm. The dimensions other than the twist angle and the groove width ratio are the outer diameter D = 8 mm, the tip angle α = 150 °, the thinning angle γ = 30 °, and the contact width b = 0.4 of the margin 2 (t = 0.8 mm).
mm Core thickness ω = 3.6 mm (= 0.45 D) Oil hole diameter d = 1.0 mm Back taper = 0.15 / 100 The carbide round bar material of the drill has a drill outer diameter D at the time of extrusion molding. Three holes were formed at equal intervals of 120 ° according to the twist so that a predetermined helix angle was obtained, and it was manufactured by sintering similarly to general cemented carbide.

【0025】切削試験条件は、 被削材 ADC12 回転数(切削速度) 1000min-1(380m/min) 1回転当たりの送り量 0.12mm/rev 穴深さ 40mm 切削油 水溶性切削油 であり、この時の結果の評価を表1に示す。The cutting test conditions are as follows: Work material ADC12 rotation speed (cutting speed) 1000 min -1 (380 m / min) Feed amount per rotation 0.12 mm / rev Hole depth 40 mm Cutting oil Water-soluble cutting oil The evaluation of the results at this time is shown in Table 1.

【0026】尚、評価基準は切りくず排出性、ビビリ振
動及び穴あけ精度(穴の面粗さ、拡大代、倒れ量)より
判断し、全般的評価の良好なものから不良なものへ順次
◎(優)、○(良)、△(可)、x(不良)の記号で表
中に示した。
The evaluation criteria are judged by chip evacuation, chatter vibration and hole drilling accuracy (hole surface roughness, expansion allowance, amount of tilt), and sequentially from good to bad overall evaluation ◎ ( It is shown in the table by symbols of excellent, good (good), fair (fair), and bad (x).

【0027】[0027]

【表1】表1において、ねじれ角55°では、ビビリが
激しく、刃先にチッピング欠損を生じているものもあ
り、正常な切削ができなかった。これは、 a)同じ溝幅比θ2/θ1でもねじれの弱いものと比べ
て、ねじれに直角にみた溝部の有効断面積が狭くなって
いるので、切りくず詰まりを起こし易くなっている、 b)ねじれ角55°ではアルミ切削とはいえくさび角が
小さくなりすぎて刃先強度の低下をきたす、等のためと
思われる。
[Table 1] In Table 1, when the helix angle was 55 °, there was severe chattering, and some chips had chipping defects, so normal cutting could not be performed. This is because a) the effective cross-sectional area of the groove is small when viewed at right angles to the twist, even if the groove width ratio is θ2 / θ1 and the twist is weak, so chip clogging is likely to occur, b) At a helix angle of 55 °, this is probably because the wedge angle becomes too small and the strength of the cutting edge deteriorates even though it is aluminum cutting.

【0028】又、溝幅比θ2/θ1に関してみると、θ
2/θ1=1.5/1〜2.5/1が良好な範囲と考え
られる。
Regarding the groove width ratio θ2 / θ1, θ
It is considered that 2 / θ1 = 1.5 / 1 to 2.5 / 1 is a good range.

【0029】つぎに、外径D寸法6.8mmのドリルに
て、鋳抜き穴加工を想定し偏心した下穴ありでのテスト
を以下の切削条件で行なった。
Next, with a drill having an outer diameter D of 6.8 mm, a test with an eccentric prepared hole was performed under the following cutting conditions, assuming casting hole processing.

【0030】使用ドリルは3枚刃油穴付きドリル(超硬
合金製、K10相当) 外径D=6.8mm 先端角α=150° ねじれ角β=35° シンニング角度γ=30° 溝幅比θ2/θ1=1.8/1 心厚ω=3.5mm(=0.51D) マージン幅t=0.4mm 油穴径d=0.8mm バックテーパ=0.15/100 切削条件 被削材 ADC12 回転数 12000、15000 min-1 切削速度 256 320 m/min 1回転当たりの送り量 0.1mm/rev 穴深さ16mm、但し下穴あり(φ4mm、深さ20mm、 芯ずれ量0.8mm) 切削油 水溶性切削油 なお、比較のため刃数を2枚にした比較品(刃数以外の
形状は、本発明品と基本的に同一)も一緒にテストし
た。
The drill used is a 3-flute oil hole drill (made of cemented carbide, equivalent to K10) outer diameter D = 6.8 mm tip angle α = 150 ° helix angle β = 35 ° thinning angle γ = 30 ° groove width ratio θ2 / θ1 = 1.8 / 1 Core thickness ω = 3.5 mm (= 0.51 D) Margin width t = 0.4 mm Oil hole diameter d = 0.8 mm Back taper = 0.15 / 100 Cutting conditions Work material ADC12 Rotational speed 12000, 15000 min -1 Cutting speed 256 320 m / min Feed per rotation 0.1 mm / rev Hole depth 16 mm, but with prepared hole (φ4 mm, depth 20 mm, misalignment 0.8 mm) Cutting oil Water-soluble cutting oil For comparison, a comparative product having two blades (the shape is basically the same as the product of the present invention except for the number of blades) was also tested.

【0031】比較品の2枚刃ドリルでは、切削初期より
ビビリが激しかったが、本発明品は偏心下穴加工でもビ
ビリが無く切削音も静かだった。この状態の差は、この
時に測定した図2に示す切削負荷(軸方向分力〈スラス
ト力〉、半径方向分力〈曲げ力〉)において、本発明品
は比較品に比べ切削速度256、320m/minのい
ずれの条件でも半径方向分力の平均値及びその変動が極
端に小さく安定していることからもうかがうことができ
る。
The two-flute drill of the comparative product exhibited a great amount of chattering from the early stage of cutting, but the product of the present invention showed no chattering even in the machining of the eccentric prepared hole, and the cutting sound was quiet. The difference between these states is that the cutting load (axial component force <thrust force>, radial component force <bending force>) shown in FIG. This can be seen from the fact that the average value of the radial component force and its fluctuation are extremely small and stable under any condition of / min.

【0032】さらに、同一条件にて、下穴なしでの穴加
工も行なった。この時の加工する穴深さは30mmであ
る。
Further, under the same conditions, drilling was performed without a pilot hole. The hole depth to be machined at this time is 30 mm.

【0033】これによれば、本発明のドリル先端外径D
=6.8mm3枚刃ドリルは切れ刃中心部近傍に溶着は
あるものの、内部給油の効果もあり切りくずづまりを起
こすことなく安定して穴あけ加工することができた。
According to this, the outer diameter D of the drill tip of the present invention
Although the 6.8 mm 3-flute drill had welding in the vicinity of the center of the cutting edge, it was possible to perform stable drilling without chipping due to the effect of internal lubrication.

【0034】なお、刃先に生じた溶着は、ダイヤライク
カーボン膜をコーティングしたドリルを使用することに
より、格段に少なくすることができ、穴あけ精度、及び
寿命の向上を計ることができた。
By using a drill coated with a diamond-like carbon film, the welding generated on the cutting edge could be significantly reduced, and the drilling accuracy and the service life could be improved.

【0035】[0035]

【発明の効果】以上の説明から明らかなように、第1の
発明によれば、3枚刃ドリルでオイルホール付きとし、
かつ、ねじれ角、溝幅比、シンニング角度、心厚、及び
溝幅比を特定することにより、下穴のない深穴加工はも
ちろん、鋳抜き穴を有する高速安定した切削が可能とな
り、加工精度の向上を計ることができる。
As is apparent from the above description, according to the first aspect of the invention, the three-blade drill is provided with the oil hole,
In addition, by specifying the helix angle, groove width ratio, thinning angle, core thickness, and groove width ratio, it is possible to perform deep hole machining without a pilot hole as well as high-speed and stable cutting with a cast hole. Can be improved.

【0036】又、第2の発明によれば、刃先先端を含む
溝部にアルミとの親和性の低いダイヤライク膜等をコー
ティングすることにより、信頼性を向上し、更に加工精
度の向上を計ることができる。
According to the second aspect of the invention, by coating the groove portion including the tip of the cutting edge with a diamond-like film having a low affinity for aluminum, the reliability is improved and the processing accuracy is further improved. You can

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

【図1】本願発明の一実施例の正面図を示す。FIG. 1 shows a front view of an embodiment of the present invention.

【図2】図1の底面図を示す。2 shows a bottom view of FIG.

【図3】切削抵抗の軸方向分力(スラスト力)と主軸動
力の測定結果を示す。
FIG. 3 shows measurement results of axial component force (thrust force) of cutting resistance and spindle power.

【符号の説明】[Explanation of symbols]

1 溝部 2 マージン部 3 ランド部 4 油穴 b マージン部の当たり幅 D 外径 γ シンニング角度 α 先端角 β ねじれ角 ω 心厚 θ1 ランド部の角度 θ2 溝幅の角度 1 Groove 2 Margin 3 Land 4 Oil hole b Margin contact width D Outer diameter γ Thinning angle α Tip angle β Twist angle ω Core thickness θ1 Land angle θ2 Groove width angle

───────────────────────────────────────────────────── フロントページの続き (72)発明者 長谷川 清 神奈川県横浜市神奈川区宝町2番地 日産 自動車株式会社内 (72)発明者 野中 延恭 神奈川県海老名市上今泉2100番地 日立精 工株式会社内 (72)発明者 菅野 悦臣 東京都江東区東陽四丁目1番13号 日立ツ ール株式会社内 ─────────────────────────────────────────────────── ─── Continuation of the front page (72) Inventor Kiyoshi Hasegawa 2 Takaracho, Kanagawa-ku, Yokohama, Kanagawa Nissan Motor Co., Ltd. (72) Inventor Nobuyasu Nonaka 2100, Kamiimaizumi, Ebina, Kanagawa Hitachi Seiko Co., Ltd. (72) Inventor Etsuomi Sugano 4-13 Toyo, Koto-ku, Tokyo Inside Hitachi Tool Co., Ltd.

Claims (2)

【特許請求の範囲】[Claims] 【請求項1】 3枚刃ドリルにおいて、切削油剤をドリ
ル先端から噴出させるための油穴をねじれ角にそってラ
ンド部内に有し、ねじれ角βを30°〜45°、先端角
αを140°〜160°、シンニング角度γを25°〜
35°、心厚ωをドリル先端の外径Dの1/3D〜3/
5D、及び溝部の角度θ2とランド部の角度θ1の比に
よって表される溝幅比をθ2/θ1=1.5/1〜2.
5/1としたことを特徴とする3枚刃ドリル。
1. A three-flute drill has an oil hole for ejecting a cutting fluid from the tip of the drill along a helix angle in a land portion, and has a helix angle β of 30 ° to 45 ° and a tip angle α of 140. ° ~ 160 °, thinning angle γ 25 ° ~
35 °, core thickness ω is 1 / 3D to 3 / of the outer diameter D of the drill tip
5D, and the groove width ratio represented by the ratio of the groove angle θ2 and the land angle θ1 is θ2 / θ1 = 1.5 / 1 to 2.
A 3-flute drill characterized by being 5/1.
【請求項2】 請求項1記載の3枚刃ドリルにおいて、
溝部の少なくとも刃先先端を含めた部分に、TiN、T
iCN、ダイヤモンド等からなる硬質物質を1層又は2
層被覆したことを特徴とする3枚刃ドリル。
2. The three-blade drill according to claim 1,
TiN, T
One or two layers of hard material such as iCN and diamond
A 3-flute drill characterized by being layered.
JP19610994A 1994-07-28 1994-07-28 Three-blade drill Withdrawn JPH0839319A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP19610994A JPH0839319A (en) 1994-07-28 1994-07-28 Three-blade drill

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP19610994A JPH0839319A (en) 1994-07-28 1994-07-28 Three-blade drill

Publications (1)

Publication Number Publication Date
JPH0839319A true JPH0839319A (en) 1996-02-13

Family

ID=16352393

Family Applications (1)

Application Number Title Priority Date Filing Date
JP19610994A Withdrawn JPH0839319A (en) 1994-07-28 1994-07-28 Three-blade drill

Country Status (1)

Country Link
JP (1) JPH0839319A (en)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2001068334A1 (en) * 2000-03-15 2001-09-20 Kabushiki Kaisha Miyanaga Drill bit
US8070398B2 (en) 2008-02-19 2011-12-06 Irwin Industrial Tool Company Multi-blade self feed bit
JP2013521899A (en) * 2010-03-19 2013-06-13 シーピーエル ホールディングス プロプライエタリー リミテッド Drill bit
JP2014054699A (en) * 2012-09-13 2014-03-27 Sumitomo Electric Hardmetal Corp Three-blade drill
WO2014155527A1 (en) 2013-03-26 2014-10-02 オーエスジー株式会社 Three-bladed drill with cutting fluid supply hole
US9604286B2 (en) 2013-01-29 2017-03-28 Osg Corporation Drill

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2001068334A1 (en) * 2000-03-15 2001-09-20 Kabushiki Kaisha Miyanaga Drill bit
US6817428B1 (en) 2000-03-15 2004-11-16 Kabushiki Kaisha Miyanaga Drill bit
US8070398B2 (en) 2008-02-19 2011-12-06 Irwin Industrial Tool Company Multi-blade self feed bit
JP2013521899A (en) * 2010-03-19 2013-06-13 シーピーエル ホールディングス プロプライエタリー リミテッド Drill bit
JP2014054699A (en) * 2012-09-13 2014-03-27 Sumitomo Electric Hardmetal Corp Three-blade drill
US9604286B2 (en) 2013-01-29 2017-03-28 Osg Corporation Drill
WO2014155527A1 (en) 2013-03-26 2014-10-02 オーエスジー株式会社 Three-bladed drill with cutting fluid supply hole
US9623490B2 (en) 2013-03-26 2017-04-18 Osg Corporation Three-bladed drill with cutting fluid supply hole

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