JPS6260202B2 - - Google Patents

Info

Publication number
JPS6260202B2
JPS6260202B2 JP59033671A JP3367184A JPS6260202B2 JP S6260202 B2 JPS6260202 B2 JP S6260202B2 JP 59033671 A JP59033671 A JP 59033671A JP 3367184 A JP3367184 A JP 3367184A JP S6260202 B2 JPS6260202 B2 JP S6260202B2
Authority
JP
Japan
Prior art keywords
drill
cutting edge
angle
cutting
range
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
Application number
JP59033671A
Other languages
Japanese (ja)
Other versions
JPS60177809A (en
Inventor
Yoshikatsu Mori
Yoshio Doi
Hideo Fukagawa
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.)
Sumitomo Electric Industries Ltd
Original Assignee
Sumitomo Electric Industries 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 Sumitomo Electric Industries Ltd filed Critical Sumitomo Electric Industries Ltd
Priority to JP59033671A priority Critical patent/JPS60177809A/en
Publication of JPS60177809A publication Critical patent/JPS60177809A/en
Publication of JPS6260202B2 publication Critical patent/JPS6260202B2/ja
Granted legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23BTURNING; BORING
    • B23B51/00Tools for drilling machines
    • B23B51/02Twist drills
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23BTURNING; BORING
    • B23B2251/00Details of tools for drilling machines
    • B23B2251/24Overall form of drilling tools
    • B23B2251/241Cross sections of the diameter of the drill
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23BTURNING; BORING
    • B23B2251/00Details of tools for drilling machines
    • B23B2251/40Flutes, i.e. chip conveying grooves
    • B23B2251/406Flutes, i.e. chip conveying grooves of special form not otherwise provided for

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Drilling Tools (AREA)

Description

【発明の詳細な説明】[Detailed description of the invention]

[発明の技術分野] 本発明は高速度鋼製ドリルに係り、特に、切削
抵抗の増大および切屑の排出機能の低下を抑制し
つつ強度を可及的に高めることができるドリルに
関するものである。 [発明の技術的背景とその問題点] 一般鋼材や鋼鉄などの穿孔作業には、従来から
高速度鋼製が使用されてきた。元来、ドリルは穿
孔によつて生成した切屑を自らの溝部を通して孔
の外部へ排出しながら進行していくものである。
この穿孔作業が効率良く行なわれるためには、切
削抵抗が小さいことと、切屑の排出が順調に行な
われることとが要求され、しかも切屑の排出の良
し要しは切削抵抗の増減にも影響を及ぼす。殊
に、穿孔深さが深くなるほど切削抵抗の増大は顕
著となる。 またドリルは、これに作用する切削抵抗に対し
て十分に耐え得る強度が要求される。ところが、
切屑の排出機能を高めるべく溝部の面積を大き
く、かつ、芯厚を小さくすると、切削抵抗、特に
スラストが必然的に小さくなるのであるが、その
反面、強度が不足するというジレンマを有し、こ
れらの関係をうまく調和させなければならない。 またドリルの強度は、その材料自体が有してい
る靭性や弾性の他に、形状に依存する剛性(曲げ
剛性やねじれ剛性)によつても与えられる。 そこで従来のドリルに関して、その強度を支配
する形状について、その切刃端面直視形状を第1
図に示して説明する。 図において破線で示されている部分1が芯厚部
であり、陸部3は溝部2が形成されていない中実
の部分である。すなわちドリルは、周知のごとく
芯厚部1の周囲に、切屑の排出通路となる溝部2
と肉厚部分である陸部3とが螺旋状に巻き付くよ
うに形成されている。したがつて、ドリル直径D
に対する芯厚部1の直径Cの比率(以後、芯厚比
と称し、%表示する。)がドリルの強度に関与
し、また陸部3の周長Aに対する溝部2の周長B
の比(以後、溝幅比と称し、B:Aで表示す
る。)も同様にドリルの強度に関与する。これら
2つの要素は、ドリルの強度を形状の上で主に支
配する因子と考えることができる。すなわち、芯
厚比が大きく溝幅比が小さいほどドリル強度は増
大するわけである。第2図は、その関係を、芯厚
比および溝幅比のそれぞれの値におけるねじれ剛
性比で示すグラフ図であり、ねじれ剛性比は溝の
ない円形断面の丸棒部材のねじれ剛性を100%と
し、その値との比率で示されている。図におい
て、サンプルイ〜ニは一般的な従来品のドリルの
形状であり、それぞれのサンプルの溝幅比はイと
ハが1:1,ロとニが1.3:1である。また、サ
ンプルホ〜チは芯厚比を大きく溝幅比を小さくし
た例であり、それぞれのサンプルの溝幅比はホと
ヘが0.4:1,トとチが0.8:1である。図示する
ように、当然のことながらサンプルホ〜チが良い
ねじれ剛性比を示し、強度的に優れていることが
明らかである。 しかし、単に芯厚比を大きく溝幅比を小さくす
るだけでは切削抵抗の増大と切屑排出機能の低下
を招くことになり、必然的にこれらの値がとり得
る範囲は限定され、従来の一般的な値は芯厚比が
15%〜23%、溝幅比が1:1〜1.3:1であつ
た。 なお、ウエブテーパについては周知の適切な勾
配がつけられている。 第3図は、上述のごとき一般的な制約を取り除
くべく工夫された、芯厚大ドリルと呼ばれる従来
品の切端端面直視形状を示している。この例にあ
つては、芯厚比が約50%と大きく設定されてい
る。すなわち、強度を高めるための芯厚比を大き
くとつているが、単に芯厚比を大きくするだけで
は溝部の面積が小さくなつてしまうので、ドリル
の先端部分にチツプポケツト4を設け、さらに剪
断応力の集中を防ぎ、ねじれ剛性を高めるべくヒ
ール部5に丸みをつけている。しかし、この場
合、チツプポケツト4の面積は大きいにもかかわ
らず、排出切屑とは異なつた断面のチツプポケツ
トであるため、決して有効な溝形状とはいえず、
むしろ、ヒール部5の丸みの部分に切屑が詰ま
り、このためにドリルの折損を招くおそれがあつ
た。したがつて、この種のドリルを使用できる条
件は、切屑形状との兼ね合いで狭い範囲に限定さ
れている。 [発明の目的] 本発明は上述のごとき事情に鑑み、ドリルの性
能を有効に改善すべく創案されたものである。 したがつて本発明の目的は、切削抵抗の増大お
よび切屑排出機能の低下を抑制しつつ強度を可及
的に高めることができるドリルを提供することに
ある。 [発明の概要] 本発明は、芯厚部の直径をドリル直径の25%〜
35%に、かつ溝幅比を0.4:1〜0.8:1の範囲内
にそれぞれ設定し、また、ドリル直径の少なくと
も2/3より外周側に位置する切刃の半径方向のす
くい角を−5゜〜正の範囲内に設定し、さらに切
刃と、これに互いに向かい合う溝壁との間の相対
的な位置関係を近接させることによつて上記目的
を達成するものである。 [発明の実施例] 以下に本発明の好適一実施例について添付図面
に従つて説明する。 第4図は本発明に係るドリルの切刃端面直視形
状を示す側面図であり、第5図はその先端部分の
概略構成を示す斜視図である。 図において、芯厚部1(破線で図示)の直径C
はドリル直径Dの25%〜35%の範囲内に設定され
ている。また、空間部分である溝部2の周長Bと
肉厚部分である陸部3の周長Aとの比は0.4:1
〜0.8:1の範囲内に設定されている。すなわ
ち、従来のドリルに比べて芯厚比が大きく溝幅比
が小さくされている。 次に、ドリル直径の少なくとも2/3よりも外周
側に位置する切刃6は、その半径方向のすくい角
θが−5゜〜正の範囲内に設定されて、切刃形
状は凹状円弧を形成している。 また、切刃6の外周端の点P1と、その切刃6上
の点であつて中心から半径の2/3の長さ外周寄り
の点P2とを直線で結ぶ仮想基準線に対する点P1
上の垂線までの、切刃6に臨んでいる溝壁7の外
周端の点P3からの距離L(以後、相対距離と称
す。)がドリル直径Dの47%以下に設定されてい
る。 また、芯厚比が大きいので、切刃6の逃げ面8
は、第5図にも示すように、ドリルの回転方向の
後側約半分がシンニングによつて研ぎ落とされて
おり、芯厚部の切刃9が形成されている。シンニ
ングはドリルの軸心Oに対して軸対称に施され、
これによつて切刃9のすくい面10とこれに隣接
する隣接研ぎ出し面11とが形成される。このよ
うなシンニングの種類をクロスシンニングと呼
び、芯厚部の切刃9は第4図に示すごとく軸心O
から180゜互いに反対側へ直線状に形成される。
切刃9が形成されないチゼル幅は0mm〜0.4mmの
範囲内に設定されており、0mmに近いほど良い。 また、切刃6の外周端の点P1および軸心Oを結
ぶ直線の方向と、芯厚部の切刃9が延びる方向と
がなす角θは35゜〜45゜の範囲内に設定されて
いる。 シンニングによつて形成されるすくい面10
は、その軸方向のすくい角θ(第7図に図示)
が−5゜〜+5゜の範囲内に設定されている。ま
た第6図にも示すように、すくい面10が軸方向
の長さは、軸心Oの部分で0mmであり、径方向外
方へいくに従つて漸増している。すくい面10と
隣接研ぎ出し面11とが交わつてなす谷線12と
ドリルの軸心Oとがなす角θは25゜〜60゜の範
囲内に設定されている。これは、切刃9によつて
切削された切屑が隣接研ぎ出し面11に当たつて
スラストを増大させることのないように、すくい
面10の軸方向の長さを十分に確保できる角度に
設定されており、かつ切屑のブレーキング作用を
十分に得られるように設定されている。また、強
度的にも十分な強度が得られるように設定されて
いる。 また、すく面10と隣接研ぎ出し面11とのな
す角θ(第7図に図示)は90゜〜110゜の範囲
内に設定されて、切屑によるスラスト増大を防止
するとともにブレーキング作用を十分に得られる
ように設定されている。 第8図はドリルの先端部分が上述のごとく構成
されたドリルにおいて、さらに切屑油の給油孔を
備えた実施例を示す斜視図である。 図示するように、ドリルの先端部から後端部ま
での中実の肉厚を有する部分である陸部3および
シヤンク13の部分の内部には、溝部2のねじれ
角に沿つて螺旋状に切削油の給油孔14が2本形
成されている。それぞれの給油孔14の吐出口1
5は切刃6の逃げ面8に開口され、吸入口16は
後端部の底面17に開口されている。給油孔14
の数は、形成されている陸部3の条数に等しく2
本が望ましいが、1本であつてもよい。また、給
油孔14の内経はドリル強度との関係からドリル
直径Dの数%〜20%が望ましい。 このドリルの給油孔14は、板状の棒部材に形
成された高速度鋼材に、その軸方向に沿つて給油
孔となるべき孔を2本形成し、この板状棒部材を
高温度下でねじることによつて塑性変形させて形
成することができる。 さらに、上述のごときそれぞれの形状に構成さ
れたドリルには、その表面にTiC,TiCN,TiN
およびAl2O3のいずれか1種または2種以上の組
合わせによる被覆層が形成されてもよい。また、
その被覆層はイオンプレーテイング法や化学蒸着
法によつて緻密に薄層が形成される。 次に、本発明の実施例の作用を従来例との比較
において実験データに基づいて説明する。 次の表1は、一般的な構成のドリル(従来品―
1)、強度を高めるべく単に芯厚比を大きくし溝
幅比を小さくしたドリル(従来品―2)、本発明
に係るドリル(発明品)の3種類のサンプルにつ
いて行なつた実験のデータを示している。 なお、シンニングによる効果を一定にするため
いずれのサンプルにおいても、発明品と同様のシ
ンニングが施されている。テストサンプルのシン
ニングの形状としては、チゼル幅=0.1mm、θ
=40゜、θ=0゜、θ=38゜、θ=100゜
である。ドリル直径は8.5mm、材質はSKH9,HRC
63である。被削材はS50C,HB250であり、切削
条件は、切削速度V=15m/分、1回転あたりの
送り量f=0.25mm/回転、穿孔深さ40mmである。
切削油はエマルジヨンタイプで、外部給油によつ
て行なつた。
[Technical Field of the Invention] The present invention relates to a high-speed steel drill, and particularly to a drill whose strength can be increased as much as possible while suppressing an increase in cutting resistance and a decrease in chip evacuation function. [Technical background of the invention and its problems] High-speed steel has traditionally been used for drilling work in general steel materials and steel. Originally, a drill advances while discharging chips generated by drilling to the outside of the hole through its own groove.
In order for this drilling work to be performed efficiently, it is required that the cutting resistance be small and that the chips be discharged smoothly, and the quality of the chip discharge also affects the increase or decrease in the cutting resistance. affect In particular, the increase in cutting resistance becomes more significant as the drilling depth increases. Further, the drill is required to have sufficient strength to withstand the cutting forces acting on it. However,
Increasing the area of the groove and decreasing the core thickness in order to improve the chip evacuation function inevitably reduces the cutting resistance, especially the thrust, but on the other hand, there is a dilemma that the strength is insufficient. The relationship between the two must be harmonized. Further, the strength of a drill is given not only by the toughness and elasticity of the material itself, but also by the rigidity (bending rigidity and torsional rigidity) that depends on the shape. Therefore, regarding the shape that governs the strength of conventional drills, the shape of the cutting edge when viewed directly from the edge is the first.
This will be explained with reference to the diagram. A portion 1 indicated by a broken line in the figure is a thick core portion, and a land portion 3 is a solid portion in which no groove portion 2 is formed. In other words, as is well known, the drill has a groove portion 2 around a thick core portion 1, which serves as a chip discharge passage.
and a land portion 3, which is a thick wall portion, are formed so as to wrap around each other in a spiral shape. Therefore, the drill diameter D
The ratio of the diameter C of the core thick portion 1 to the diameter C (hereinafter referred to as the core thickness ratio and expressed as a percentage) is involved in the strength of the drill, and the ratio of the circumference B of the groove portion 2 to the circumference A of the land portion 3 is related to the strength of the drill.
The ratio (hereinafter referred to as the groove width ratio and expressed as B:A) similarly affects the strength of the drill. These two factors can be considered to be factors that mainly control the strength of the drill in terms of shape. In other words, the drill strength increases as the core thickness ratio increases and the groove width ratio decreases. Figure 2 is a graph showing this relationship in terms of torsional rigidity ratio at each value of core thickness ratio and groove width ratio. and is expressed as a ratio to that value. In the figure, samples A to D have the shapes of general conventional drills, and the groove width ratio of each sample is 1:1 for A and C, and 1.3:1 for B and D. In addition, samples Ho to Ho are examples in which the core thickness ratio is large and the groove width ratio is small, and the groove width ratio of each sample is 0.4:1 for Ho and F, and 0.8:1 for G and Chi. As shown in the figure, it is clear that the sample hoops show a good torsional stiffness ratio and are excellent in strength. However, simply increasing the core thickness ratio and decreasing the flute width ratio will result in an increase in cutting force and a decrease in chip evacuation function, and the range in which these values can take is inevitably limited. The value is the core thickness ratio
The groove width ratio was 1:1 to 1.3:1. Note that the web taper has a well-known appropriate slope. FIG. 3 shows the shape of a conventional product called a large-core drill, when viewed directly from the incisal end surface, which has been devised to eliminate the above-mentioned general restrictions. In this example, the core thickness ratio is set to be as large as about 50%. In other words, the core thickness ratio is increased to increase strength, but simply increasing the core thickness ratio will reduce the area of the groove, so a tip pocket 4 is provided at the tip of the drill to further reduce shear stress. The heel portion 5 is rounded to prevent concentration and increase torsional rigidity. However, in this case, although the area of the chip pocket 4 is large, the chip pocket has a cross section different from that of the discharged chips, so it cannot be said to be an effective groove shape.
Rather, the rounded portion of the heel portion 5 was clogged with chips, which could cause the drill to break. Therefore, the conditions under which this type of drill can be used are limited to a narrow range due to the shape of the chips. [Object of the Invention] The present invention has been devised in view of the above-mentioned circumstances in order to effectively improve the performance of a drill. Therefore, an object of the present invention is to provide a drill that can increase the strength as much as possible while suppressing an increase in cutting resistance and a decrease in chip evacuation function. [Summary of the Invention] The present invention provides a method in which the diameter of the core thick portion is 25% or more of the drill diameter.
35%, and the flute width ratio is set within the range of 0.4:1 to 0.8:1, and the radial rake angle of the cutting edge located at least 2/3 of the drill diameter on the outer peripheral side is -5%. The above object is achieved by setting the cutting edge to be within a positive range, and by bringing the relative positional relationship between the cutting edge and the groove walls facing each other closer to each other. [Embodiments of the Invention] A preferred embodiment of the present invention will be described below with reference to the accompanying drawings. FIG. 4 is a side view showing the cutting edge end face of the drill according to the present invention when viewed directly, and FIG. 5 is a perspective view showing the schematic structure of the tip thereof. In the figure, the diameter C of the thick core portion 1 (indicated by a broken line)
is set within a range of 25% to 35% of the drill diameter D. Furthermore, the ratio of the circumference B of the groove portion 2, which is the space portion, to the circumference length A, which is the thick portion, of the land portion 3 is 0.4:1.
It is set within the range of ~0.8:1. That is, compared to conventional drills, the core thickness ratio is large and the groove width ratio is small. Next, the cutting edge 6 located on the outer peripheral side of at least 2/3 of the drill diameter has a rake angle θ 1 in the radial direction set within a range of −5° to positive, and the cutting edge shape is a concave arc. is formed. Also, a point with respect to an imaginary reference line connecting a point P 1 at the outer peripheral end of the cutting edge 6 and a point P 2 on the cutting edge 6 that is 2/3 of the radius from the center and closer to the outer periphery. P1
The distance L (hereinafter referred to as relative distance) from the point P 3 of the outer peripheral end of the groove wall 7 facing the cutting edge 6 to the upper perpendicular line is set to 47% or less of the drill diameter D. In addition, since the core thickness ratio is large, the flank surface 8 of the cutting edge 6
As shown in FIG. 5, about half of the rear side of the drill in the rotating direction is ground down by thinning to form a cutting edge 9 in the thick core portion. Thinning is performed axially symmetrically with respect to the axis O of the drill,
This forms a rake face 10 of the cutting edge 9 and an adjacent ground surface 11 adjacent thereto. This type of thinning is called cross thinning, and the cutting edge 9 in the thick core part is aligned with the axis O as shown in Fig. 4.
They are formed in straight lines 180° from the opposite sides.
The width of the chisel where the cutting edge 9 is not formed is set within the range of 0 mm to 0.4 mm, and the closer it is to 0 mm, the better. In addition, the angle θ 2 between the direction of the straight line connecting the point P 1 on the outer peripheral edge of the cutting edge 6 and the axis O and the direction in which the cutting edge 9 in the core thickness section extends is set within the range of 35° to 45°. has been done. Rake face 10 formed by thinning
is its axial rake angle θ 3 (as shown in Fig. 7)
is set within the range of -5° to +5°. Further, as shown in FIG. 6, the length of the rake face 10 in the axial direction is 0 mm at the axial center O, and gradually increases as it goes outward in the radial direction. The angle θ 4 formed between the valley line 12 formed by the intersection of the rake face 10 and the adjacent ground surface 11 and the axis O of the drill is set within the range of 25° to 60°. This angle is set at an angle that ensures a sufficient axial length of the rake face 10 so that the chips cut by the cutting edge 9 do not hit the adjacent polished surface 11 and increase the thrust. and is set so as to obtain a sufficient breaking effect on chips. In addition, it is set so that sufficient strength can be obtained. In addition, the angle θ 5 (shown in FIG. 7) between the rake face 10 and the adjacent ground surface 11 is set within the range of 90° to 110° to prevent an increase in thrust due to chips and to ensure sufficient braking action. It is set so that it can be obtained. FIG. 8 is a perspective view showing an embodiment of the drill in which the tip portion of the drill is configured as described above, and further includes an oil supply hole for chip oil. As shown in the figure, inside the land portion 3 and the shank 13, which are solid thick portions from the tip to the rear end of the drill, a spiral cut is made along the helix angle of the groove portion 2. Two oil supply holes 14 are formed. Discharge port 1 of each oil supply hole 14
5 is opened in the flank 8 of the cutting blade 6, and the suction port 16 is opened in the bottom surface 17 of the rear end. Oil supply hole 14
The number of 2 is equal to the number of stripes of the land section 3 formed.
A book is preferable, but one book is also acceptable. Further, the inner diameter of the oil supply hole 14 is preferably several percent to 20% of the drill diameter D in view of the strength of the drill. The oil supply hole 14 of this drill is made by forming two holes to serve as oil supply holes along the axial direction in a high-speed steel material formed in a plate-shaped bar member, and then holding the plate-shaped bar member under high temperature. It can be formed by being plastically deformed by twisting. Furthermore, drills configured in each of the above shapes have TiC, TiCN, and TiN on their surfaces.
A coating layer may be formed using one or a combination of two or more of Al 2 O 3 and Al 2 O 3 . Also,
The coating layer is formed into a dense thin layer by ion plating or chemical vapor deposition. Next, the operation of the embodiment of the present invention will be explained based on experimental data in comparison with the conventional example. Table 1 below shows drills with common configurations (conventional products).
1) Data from experiments conducted on three types of samples: a drill with a simply increased core thickness ratio and decreased groove width ratio to increase strength (conventional product-2), and a drill according to the present invention (invented product). It shows. In addition, in order to make the effect of thinning constant, all samples were subjected to the same thinning as the invention product. The thinning shape of the test sample is as follows: chisel width = 0.1mm, θ 2
= 40°, θ 3 = 0°, θ 4 = 38°, and θ 5 = 100°. Drill diameter is 8.5mm, material is SKH9, H RC
It is 63. The work material is S50C, H B 250, and the cutting conditions are: cutting speed V = 15 m/min, feed rate per rotation f = 0.25 mm/rotation, and drilling depth 40 mm.
The cutting oil was an emulsion type and was supplied externally.

【表】 表1から明らかなように、溝幅比を小さく芯厚
比を大きくした従来品―2と発明品とは、断面2
次モーメントおよびねじれ剛性比がともに高めら
れ、強度増大の効果が顕著である。ところで、こ
のような効果の予測は十分なされるところである
が、従来技術において従来品―2のようなドリル
が採用されなかつて理由は既に述べたとおりであ
る。表1において切削抵抗を示すトルクと推力
(スラスト)のデータ値に表わされているよう
に、本発明品によれば推力は若干増大している
が、従来品―2ほどではなく、トルクに関しては
従来品―1と同一の値に抑制されている。しかも
強度は十分に増大している。すなわち、切刃6の
半径方向のすくい角を大きくすることによつて得
られる効果である。 本発明のもう1つの特長は切屑排出機能に低下
を抑制することである。切屑排出機能の良し悪し
に関しては、生成される切屑の形状と、その溝部
2内での動きとが影響する。第9図は従来品―2
のドリルによる切屑の動きを示す模式図である。
切刃6および9から削り出される切屑18は、溝
壁7に沿つてカール形状に形成されつつドリルの
中心側から外周側へ向かつて流れる。このとき、
切刃6と溝壁7との間の距離が大きいと、切屑1
8のカール半径が大きくなり切屑18は溝部2内
に詰まりやすくなる。また、切屑18は孔の壁1
9に当たつて折れ、仕上げ面を粗くする。このよ
うに切屑18の動きを支配する重要な要素の1つ
は、切刃6の形状(曲り具合)と溝壁7の形状
(曲り具合)との互いの相対的な関係であり、し
がつて、切屑18が溝部2内を通つて順調に排出
されるためには、切刃6と溝壁6と溝壁7との間
に適切な形状関係がある。その形状を何らかの指
標によつて表わすとすれば、切刃6に対する溝壁
7の、あるいは溝壁7に対する切刃6の互いの相
対的な位置関係を、これらの間の距離(相対距
離)で表わすことが1つの表示方法として有効で
ある。そこで、相対距離Lを1つの指標として定
義し、ドリル直径Dに対する相対距離Lの比をも
つて切屑の排出機能の良し悪しを表わすことが可
能である。すなわち第9図の例では、この相対距
離Lが大きいために狭い溝部2では切屑の排出機
能を十分に発揮できない。 次に、第3図の従来ドリル、表1の従来―1の
ドリル、本発明のドリルの3種間での性能を比較
する。この場合、第3図のシンニングも他のドリ
ルと同じとした。従来―1のドリルでは、表1に
示されるごとくトルクおよびスラストがほぼ安定
している。第3図の従来ドリルでは、通常トルク
が85Kg・fcm、スラストが330Kgfであるが、穴
深さ30mm近くより急増して各々130Kgf・cm、380
Kgfとなる。これに対し、本発明のドリルでは、
表1のごとく低い値で安定している。次に、穴あ
け連続テストの結果、第3図の従来ドリルでは各
穴で穴深さが深くなると抵抗が上昇し、33穴目で
折れた。表1の従来―1ドリルは安定して切削で
きたが、350穴目で折れた。ドリルを観察すると
逃げ面最大摩耗幅が0.7mmにも達しており、抵抗
増による折れと推察された。これに対して、表1
の本発明ドリルでは、400穴加工で従来―1ドリ
ルと同程度の摩耗が生じ、従来―1ドリルと同程
度の強度を有していた。 第10図は本発明のドリルによる切屑の動きを
示す模式図である。相対距離Lがドリル直径Dの
47%以下に設定されているので、切屑18は溝壁
7に沿つてカールし、また、細かく短く折れて切
れ、溝部2内で流動しやすい、すなわち排出しや
すい形状に形成される。 また、第4図に示した角θが35゜〜45゜の範
囲内に設定されることによつて、切屑18は切刃
6によつて切削される部分と切刃9によつて切削
される部分とが互いにその方向を異にして形成さ
れ、カール切断されやすい形状に削り出される。
この角θが小さすぎると切屑18は偏平に近い
形状となつてカール切断されにくく、また、大き
すぎると切刃9によつて切削される部分の全体に
占める比率が小さくなつてカール切断されにくく
なる。角θは、中心部のすくい角に相当するも
ので、周知のごとく正に大きいほど抵抗は少なく
なるが強度も低下し、負であれば逆の効果とな
る。角θが−5゜〜+5゜の範囲であれば、切
れ味・強度が維持できる。また、角θが0゜に
近くないと、再研削のときに1回あたりの再研削
量が大きくなつてしまう。角θは、中心部の切
り屑の排出性と抵抗の大小を左右する。すなわ
ち、角θが小さいと抵抗は少なくてすむが切り
屑のブレーキング効果が劣り、逆にθが大きく
なれば逆の効果となる。実験的には、角θは25
゜〜60゜の範囲内で設定可能であるが、35゜〜41
゜が望ましい。角θは、前記角θとともに切
り屑の排出性に影響する。角θの設定範囲は90
゜〜110゜内で可能であるが、100゜が望ましい。
チゼルは周知のごとく被切削部であり、いかに狭
くして中心まで切刃とするかがポイントとなる。
チゼル幅は0〜0.4mmの範囲にあることが望まし
い。次に切削油の給油孔14を形成した場合のそ
の作用について説明する。給油孔14の吸入口1
6からドリル保持具を通して切削油を圧入する
と、切削油は給油孔14を通つて先端部の吐出口
15から切刃6の部分に供給され、刃先部分有効
に冷却することができる。また、切削油の戻りは
溝部2内を通つて孔の外部へ排出され、その際
に、切屑の排出を促し、かつ加工物の冷却をも行
なうことになる。したがつて、切削抵抗は安定
し、折損事故を防止することができる。油穴の大
きさについては、大きい方が排出油量は増えより
効果的になるが、大きすぎるとドリル断面積が小
さくなり強度の低下をきたす。ドリル直径の数%
〜20%が望ましいが、溝幅を狭く設定しかつ芯厚
を大きく設定しているため、陸部3の面積が従来
のドリルより大きくなる。したがつて、大きな給
油孔をあけても強度の低下は少なくてすむことに
なる。 さらに、これらのドリルは高速度鋼のみを素材
として形成してもよいが、ドリルの表面にTiC,
TiCN,TiNおよびAl2O3のうちの1種または2種
以上の組合わせによる被覆層を形成することによ
つてドリル自体の耐熱性を高め、その摩耗をさら
に防止することができる。また、これらの被覆材
は摩擦係数が小さいのでスラストおよびトルクを
さらに小さくすることができる。 また、ドリルは、その摩耗が進むと再研磨して
刃先部を再生するが、この再研磨に際してドリル
の逃げ面8に母材が露出してもすくい面およびマ
ージンの部分の外周面には被覆層が残り、切削抵
抗は小さいままに維持することができる。 [発明の効果] 以上の説明から明らかなように本発明によれば
次のごとき優れた効果が発揮される。 すなわち、芯厚比を大きく溝幅比を小さくした
のでドリルの強度を高めることができ、しかも切
刃の半径方向のすくい角を大きくすることによつ
て切削抵抗の増大を抑制し、かつ相対距離を小さ
くすることで切屑の排出機能の低下を抑制するこ
とができる。
[Table] As is clear from Table 1, the conventional product-2, which has a small groove width ratio and a large core thickness ratio, and the invented product have a cross section of 2.
Both the moment of order and the torsional stiffness ratio are increased, and the effect of increasing strength is significant. By the way, although such an effect is well predicted, the reason why a drill like Conventional Product-2 has not been adopted in the prior art is as already stated. As shown in the data values of torque and thrust that indicate cutting resistance in Table 1, the product of the present invention has a slight increase in thrust, but not as much as the conventional product-2, and in terms of torque. is suppressed to the same value as conventional product-1. Moreover, the strength has increased sufficiently. That is, this effect is obtained by increasing the rake angle of the cutting edge 6 in the radial direction. Another feature of the present invention is that it suppresses deterioration in chip evacuation function. The quality of the chip evacuation function is influenced by the shape of the chips generated and their movement within the groove 2. Figure 9 is conventional product-2
FIG. 3 is a schematic diagram showing the movement of chips caused by the drill.
The chips 18 cut out from the cutting edges 6 and 9 are formed in a curled shape along the groove wall 7 and flow from the center side to the outer circumferential side of the drill. At this time,
If the distance between the cutting edge 6 and the groove wall 7 is large, chips 1
8 becomes larger, and the chips 18 tend to become clogged in the groove 2. Also, the chips 18 are removed from the hole wall 1.
It breaks when it hits point 9, making the finished surface rough. One of the important factors governing the movement of the chips 18 is the relative relationship between the shape (curvature) of the cutting edge 6 and the shape (curvature) of the groove wall 7. Therefore, in order for the chips 18 to pass through the groove portion 2 and be smoothly discharged, there is an appropriate shape relationship between the cutting edge 6, the groove walls 6, and the groove walls 7. If the shape is expressed using some index, the relative positional relationship of the groove wall 7 to the cutting edge 6 or the cutting edge 6 to the groove wall 7 can be expressed by the distance (relative distance) between them. Expression is effective as one display method. Therefore, it is possible to define the relative distance L as one index, and express the quality of the chip evacuation function by the ratio of the relative distance L to the drill diameter D. That is, in the example shown in FIG. 9, the relative distance L is large, so that the narrow groove portion 2 cannot sufficiently perform the chip discharge function. Next, the performance will be compared among three types: the conventional drill shown in FIG. 3, the conventional drill 1 shown in Table 1, and the drill of the present invention. In this case, the thinning shown in Figure 3 was also the same as for the other drills. As shown in Table 1, the torque and thrust of the Conventional-1 drill are almost stable. In the conventional drill shown in Figure 3, the normal torque is 85Kgfcm and the thrust is 330Kgf, but when the hole depth is near 30mm, the torque increases to 130Kgfcm and 380Kgf, respectively.
It becomes Kgf. In contrast, with the drill of the present invention,
As shown in Table 1, it is stable at a low value. Next, as a result of a continuous drilling test, the resistance of the conventional drill shown in Figure 3 increased as the hole depth increased, and the drill broke at the 33rd hole. The conventional-1 drill in Table 1 was able to cut stably, but it broke at the 350th hole. Observation of the drill revealed that the maximum wear width on the flank surface reached 0.7mm, and it was assumed that the breakage occurred due to increased resistance. On the other hand, Table 1
The drill of the present invention experienced the same level of wear as the conventional -1 drill after drilling 400 holes, and had the same strength as the conventional -1 drill. FIG. 10 is a schematic diagram showing the movement of chips by the drill of the present invention. The relative distance L is the drill diameter D.
Since it is set to 47% or less, the chips 18 are curled along the groove wall 7, broken into short pieces, and formed into a shape that is easy to flow in the groove 2, that is, easily discharged. Furthermore, by setting the angle θ 2 shown in FIG. The parts to be curled are formed in different directions, and are cut into a shape that is easy to curl.
If this angle θ 2 is too small, the chip 18 will have a nearly flat shape and will be difficult to curl, while if it is too large, the proportion of the area cut by the cutting blade 9 to the whole will be small and the chip will not be curled. It becomes difficult. The angle θ 3 corresponds to the rake angle at the center, and as is well known, the larger the angle is positive, the less the resistance will be, but the strength will also be lower, and if it is negative, the opposite effect will occur. If the angle θ 3 is in the range of −5° to +5°, the sharpness and strength can be maintained. Further, if the angle θ 3 is not close to 0°, the amount of re-grinding per time during re-grinding will become large. The angle θ 4 influences the evacuation of chips in the center and the magnitude of the resistance. That is, if the angle θ 4 is small, the resistance will be small, but the chip breaking effect will be poor, and if the angle θ 4 is large, the opposite effect will occur. Experimentally, the angle θ 4 is 25
It can be set within the range of 35° to 41°.
° is desirable. The angle θ 5 , together with the angle θ 4 , influences the chip evacuation performance. The setting range of angle θ 5 is 90
It is possible within a range of 110°, but 100° is preferable.
As is well known, the chisel is the part to be cut, and the key is how narrow it is to make the cutting edge all the way to the center.
The chisel width is preferably in the range of 0 to 0.4 mm. Next, the effect when the cutting oil supply hole 14 is formed will be explained. Suction port 1 of oil supply hole 14
When cutting oil is press-fitted from 6 through the drill holder, the cutting oil is supplied to the cutting edge 6 from the outlet 15 at the tip through the oil supply hole 14, and the cutting edge can be effectively cooled. Further, the returning cutting oil passes through the groove 2 and is discharged to the outside of the hole, and at this time, it promotes the discharge of chips and also cools the workpiece. Therefore, cutting resistance is stable and breakage accidents can be prevented. As for the size of the oil hole, the larger the hole, the more effective the oil discharge will be, but if it is too large, the cross-sectional area of the drill will become smaller, resulting in a decrease in strength. A few percent of the drill diameter
~20% is desirable, but since the groove width is set narrow and the core thickness is set large, the area of the land portion 3 becomes larger than that of a conventional drill. Therefore, even if a large oil supply hole is made, there will be less decrease in strength. Furthermore, although these drills may be made only of high-speed steel, TiC,
By forming a coating layer made of one or a combination of two or more of TiCN, TiN, and Al 2 O 3 , the heat resistance of the drill itself can be increased and its wear can be further prevented. Further, since these coating materials have a small coefficient of friction, the thrust and torque can be further reduced. In addition, when the drill wears out, it is re-ground to regenerate the cutting edge. However, even if the base material is exposed on the flank 8 of the drill during this regrinding, the outer circumferential surface of the rake face and margin area is coated. The layer remains and the cutting forces can remain small. [Effects of the Invention] As is clear from the above description, the present invention provides the following excellent effects. In other words, by increasing the core thickness ratio and decreasing the groove width ratio, the strength of the drill can be increased, and by increasing the radial rake angle of the cutting edge, an increase in cutting resistance can be suppressed, and the relative distance can be reduced. By reducing the size, it is possible to suppress the deterioration of the chip evacuation function.

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

第1図は従来のドリルの切刃端面直視形状を示
す側面図、第2図はドリルのねじれ剛性比と芯厚
比および溝幅比との関係を示すグラフ図、第3図
は他の従来例のドリルの切刃端面直視形状を示す
側面図、第4図は本発明のドリルの一実施例にお
ける切刃端面直視形状を示す側面図、第5図は本
発明のドリルの一実施例における先端部分の概略
構成を示す斜視図、第6図は第5図の矢印の方
向から見た側面図、第7図は第5図の矢印の方
向から見た側面図、第8図は本発明のドリルの他
の一実施例を示す斜視図、第9図は従来のドリル
の切屑の動きを示す模式図、第10図は本考案の
ドリルの切屑の動きを示す模式図である。 なお、図中1は芯厚部、2は溝部、3は陸部、
6は切刃、7は溝壁、9は芯厚部の切刃、10は
芯厚部の切刃のすくい面、11は隣接研ぎ出し
面、12は谷線、14は給油孔、P1は切刃の最外
周端の点、P2は切刃上の点であつて中心から半径
の2/3の長さ外周寄りの点、P3は溝壁の最外周端
の点、は仮想基準線である。
Figure 1 is a side view showing the shape of a conventional drill when viewed directly from the cutting edge, Figure 2 is a graph showing the relationship between the torsional rigidity ratio, core thickness ratio and groove width ratio of the drill, and Figure 3 is another conventional drill. FIG. 4 is a side view showing the shape of the cutting edge of the drill as viewed directly from the cutting edge of the example drill, FIG. A perspective view showing a schematic configuration of the tip portion, FIG. 6 is a side view as seen from the direction of the arrow in FIG. 5, FIG. 7 is a side view as seen from the direction of the arrow in FIG. 5, and FIG. FIG. 9 is a schematic diagram showing the movement of chips in the conventional drill, and FIG. 10 is a schematic diagram showing the movement of chips in the drill of the present invention. In addition, in the figure, 1 is the core thick part, 2 is the groove part, 3 is the land part,
6 is the cutting edge, 7 is the groove wall, 9 is the cutting edge in the core thickness section, 10 is the rake face of the cutting edge in the core thickness section, 11 is the adjacent ground surface, 12 is the valley line, 14 is the oil supply hole, P 1 is The point at the outermost edge of the cutting edge, P 2 is a point on the cutting edge that is 2/3 of the radius from the center and closer to the outer periphery, P 3 is the point at the outermost edge of the groove wall, is a virtual reference It is a line.

Claims (1)

【特許請求の範囲】 1 高速度鋼製ドリルであつて、 芯厚部の直径がドリル直径の25%〜35%に、か
つ溝幅比が0.4:1〜0.8:1の範囲内にそれぞれ
設定され、 切刃端面直視形状において、ドリル直径の少な
くとも2/3より外周側に位置する切刃の半径方向
のすくい角が−5゜〜正に設定され、 前記切刃端面直視形状における切刃の最外周端
の点と、該切刃上の点であつて中心から半径の2/
3の長さ外周よりの点とを直線で結ぶ仮想基準線
に対して、前記切刃の最外周端の点を通る垂線ま
で、前記切刃に溝部の空間を隔てて臨む溝壁の最
外周端の点からの距離がドリル直径の47%以下に
設定されることを特徴とするドリル。 2 前記切刃端面直視形状において、ドリル直径
の少なくとも2/3より外周側に位置する切刃は、
その半径方向のすくい角が0゜〜正に設定される
べく凹状円弧に形成される特許請求の範囲第1項
記載のドリル。 3 シンニングによつて形成される前記芯厚部の
形状は、チゼル幅が0mm〜0.4mmの範囲内に設定
され、 前記切刃端面直視形状において、前記芯厚部の
軸心から径方向外方へ延びるそれぞれの切刃を互
いに直線状に形成し、かつ該芯厚部の切刃が延び
る方向と、該芯厚部の切刃の外周側の端部からさ
らに外周側へ延びる切刃の最外周端の点に前記軸
心から至る方向とが互いに軸心上で交差してなす
角が35゜〜45゜の範囲内に設定される特許請求の
範囲第1項または第2項記載のドリル。 4 シンニングによつて形成される前記芯厚部の
切刃のすくい面は、軸方向のすくい角が−5゜〜
+5゜の範囲内に設定され、かつ軸方向への長さ
をドリルの軸心位置で0mmとして、該すくい面
と、これと同時にシンニングによつて形成される
隣接研ぎ出し面とが交わつてなす谷線を、ドリル
の軸心に対して25゜〜60゜の範囲内の傾斜角で形
成する特許請求の範囲第3項記載のドリル。 5 前記芯厚部のすくい面と前記隣接研ぎ出し面
とのなす角が90゜〜110゜の範囲内に設定される
特許請求の範囲第4項記載のドリル。 6 ドリルの後端部から先端部までのシヤンク内
および本体の陸部内に、ねじれ角に沿つてねじれ
た切削油の給油孔を有する特許請求の範囲第1項
記載のドリル。 7 少なくとも前記切刃のすくい面およびマージ
ンの外周面を含むドリルの表面の一部または全部
がTiC,TiCN,TiNおよびAl2O3からなる群より
選ばれた1種または2種以上の組合わせによつて
被覆される特許請求の範囲第1項記載のドリル。
[Claims] 1. A drill made of high-speed steel, wherein the diameter of the core thickness is set to 25% to 35% of the drill diameter, and the groove width ratio is set within the range of 0.4:1 to 0.8:1. and the rake angle in the radial direction of the cutting edge located at least 2/3 of the drill diameter on the outer peripheral side is set to −5° to positive in the shape of the cutting edge when viewed directly from the cutting edge, and The outermost point and the point on the cutting edge that is 2/2 of the radius from the center.
The outermost periphery of the groove wall facing the cutting blade across the space of the groove from the virtual reference line connecting the points from the outer periphery with a straight line to the perpendicular line passing through the point at the outermost periphery of the cutting blade. A drill characterized in that the distance from the end point is set to 47% or less of the drill diameter. 2 In the shape of the cutting edge when viewed directly from the end surface, the cutting edge located on the outer peripheral side of at least 2/3 of the drill diameter is
The drill according to claim 1, wherein the drill is formed into a concave arc so that the rake angle in the radial direction is set between 0° and positive. 3. The shape of the thick core portion formed by thinning is such that the chisel width is set within the range of 0 mm to 0.4 mm, and in the shape viewed directly from the end surface of the cutting blade, the shape is radially outward from the axis of the thick core portion. The respective cutting edges extending toward each other are formed linearly with respect to each other, and the direction in which the cutting edge of the core thickness section extends and the outermost edge of the cutting edge extending further toward the outer periphery from the outer circumferential end of the cutting edge of the core thickness section are formed. The drill according to claim 1 or 2, wherein an angle formed by a point on the outer peripheral end and a direction extending from the axis intersects each other on the axis is set within a range of 35° to 45°. . 4. The rake face of the cutting edge of the core thick portion formed by thinning has an axial rake angle of −5° to
The valley formed by the intersection of the rake face and the adjacent ground surface formed by thinning at the same time, with the length in the axial direction set within the range of +5° and 0 mm at the axial center position of the drill. 4. A drill according to claim 3, wherein the line is formed at an angle of inclination within the range of 25° to 60° with respect to the axis of the drill. 5. The drill according to claim 4, wherein the angle between the rake face of the thick core portion and the adjacent ground surface is set within a range of 90° to 110°. 6. The drill according to claim 1, which has a cutting oil supply hole twisted along a helix angle in the shank from the rear end to the tip of the drill and in the land portion of the main body. 7. Part or all of the surface of the drill, including at least the rake face of the cutting edge and the outer peripheral surface of the margin, is one or a combination of two or more selected from the group consisting of TiC, TiCN, TiN, and Al 2 O 3 . A drill according to claim 1, which is coated with.
JP59033671A 1984-02-23 1984-02-23 Drill Granted JPS60177809A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP59033671A JPS60177809A (en) 1984-02-23 1984-02-23 Drill

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP59033671A JPS60177809A (en) 1984-02-23 1984-02-23 Drill

Publications (2)

Publication Number Publication Date
JPS60177809A JPS60177809A (en) 1985-09-11
JPS6260202B2 true JPS6260202B2 (en) 1987-12-15

Family

ID=12392913

Family Applications (1)

Application Number Title Priority Date Filing Date
JP59033671A Granted JPS60177809A (en) 1984-02-23 1984-02-23 Drill

Country Status (1)

Country Link
JP (1) JPS60177809A (en)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS6399112A (en) * 1986-10-15 1988-04-30 Kobe Steel Ltd Drill
US5230593A (en) * 1987-12-14 1993-07-27 Mitsubishi Kinzoku Kabushiki Kaisha Twist drill
EP0320881B2 (en) * 1987-12-14 2003-10-22 Mitsubishi Materials Corporation Twist drill
DE19961586A1 (en) * 1999-12-21 2001-07-05 Bosch Gmbh Robert Impact-assisted hand drill
US9199315B2 (en) 2000-06-02 2015-12-01 Kennametal Inc. Twist drill and method for producing a twist drill which method includes forming a flute of a twist drill
DE10027544A1 (en) * 2000-06-02 2001-12-13 Kennametal Inc Drill tip for a twist drill and method for producing a flute in the area of a drill tip for a twist drill
JP4694702B2 (en) * 2001-01-17 2011-06-08 ダイジ▲ェ▼ット工業株式会社 Drill for heat-resistant metal
GB201706687D0 (en) 2017-04-27 2017-06-14 Rolls Royce Plc A cutting tool
EP3401042B1 (en) * 2017-05-11 2020-07-22 Sandvik Intellectual Property AB Drill body and drill

Also Published As

Publication number Publication date
JPS60177809A (en) 1985-09-11

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