JP2000015632A - Method for boring prepreg - Google Patents

Method for boring prepreg

Info

Publication number
JP2000015632A
JP2000015632A JP18349498A JP18349498A JP2000015632A JP 2000015632 A JP2000015632 A JP 2000015632A JP 18349498 A JP18349498 A JP 18349498A JP 18349498 A JP18349498 A JP 18349498A JP 2000015632 A JP2000015632 A JP 2000015632A
Authority
JP
Japan
Prior art keywords
prepreg
drill bit
blade
drilling
hole
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.)
Granted
Application number
JP18349498A
Other languages
Japanese (ja)
Other versions
JP3853074B2 (en
Inventor
Shoichi Tsutsui
章市 筒井
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.)
Panasonic Electric Works Co Ltd
Original Assignee
Matsushita Electric Works 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 Matsushita Electric Works Ltd filed Critical Matsushita Electric Works Ltd
Priority to JP18349498A priority Critical patent/JP3853074B2/en
Publication of JP2000015632A publication Critical patent/JP2000015632A/en
Application granted granted Critical
Publication of JP3853074B2 publication Critical patent/JP3853074B2/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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Abstract

PROBLEM TO BE SOLVED: To provide a method for boring a prepreg with a backing impregnated with a thermosetting resin composition in which boring can be done many times continuously with the use of a drill bit. SOLUTION: A prepreg 20 is bored with the use of a drill bit 10 which has a blade 12 at the end part and a notch shaped recessed part 18 communicating with a prepreg in the axial direction from a noncontact part to a blade 12 part in boring in a shaft part 14 and in which a through hole 16 in the axial direction is exposed to the recessed part 18, while the blade 12 and the shaft part 14 being cooled by ejecting gas A from the through hole 16 to the blade 12 part.

Description

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

【0001】[0001]

【発明の属する技術分野】本発明は、積層板の製造に使
用されるプリプレグの、穴あけ方法に関するものであ
る。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a method for drilling a prepreg used for manufacturing a laminate.

【0002】[0002]

【従来の技術】従来、プリント配線板の製造に用いられ
る積層板は、例えばガラスクロス等の空隙を有する基材
に、エポキシ樹脂等の熱硬化性樹脂組成物を含浸した
後、乾燥して含浸した熱硬化性樹脂組成物を半硬化(B
ステージ)状に固化させることによってプリプレグを作
製し、次いでこのプリプレグを所要枚数重ねるととも
に、必要に応じて銅箔等の金属箔をその片側又は両側に
配して積層して積層物を形成した後、その積層物を加熱
・加圧することにより成形して製造されている。
2. Description of the Related Art Conventionally, a laminated board used in the production of a printed wiring board is impregnated with a thermosetting resin composition such as an epoxy resin, which is impregnated into a base material having voids such as a glass cloth. The cured thermosetting resin composition is semi-cured (B
After preparing a prepreg by solidifying into a (stage) shape, and then stacking the required number of prepregs, and arranging a metal foil such as a copper foil on one or both sides thereof as necessary, forming a laminate It is manufactured by molding the laminate by heating and pressing.

【0003】上記プリプレグは、熱硬化性樹脂組成物を
基材に含浸して半硬化させたものであるため、この樹脂
は、加熱するといったん粘度が低下して流動し、更に加
熱すると硬化して流動しなくなる挙動を示す。そのた
め、積層時の取り扱いにおいては半硬化しているため取
り扱いやすく、また、加熱・加圧して成形する途中で
は、ある程度流動性を有するため、多少の樹脂量のばら
つきがあってもほぼ均一の厚みの積層板が得られるとい
う特徴があり一般に用いられている。
[0003] Since the prepreg is obtained by impregnating a thermosetting resin composition into a substrate and semi-curing the resin, the resin decreases in viscosity as soon as it is heated, and flows when it is further heated. It shows the behavior that it does not flow. Therefore, it is easy to handle because it is semi-cured when handling at the time of lamination, and has a certain degree of fluidity during molding by heating and pressing, so that even if there is some variation in the amount of resin, the thickness is almost uniform Is generally used because of the feature that a laminated plate of

【0004】しかし、プリプレグを用いて積層板を製造
する場合、加熱して樹脂の粘度が低下したときに、その
樹脂の流動によってプリプレグがずれてしまい、所望の
大きさの積層板が得られない場合があるという問題があ
った。そのため、プリプレグに予め穴を形成しておき、
その穴にピンを挿入してプリプレグを固定した状態で加
熱して成形する、一般にピンラミネーション法と呼ばれ
る方法も行われている。
However, in the case of manufacturing a laminate using a prepreg, when the viscosity of the resin is reduced by heating, the prepreg is displaced by the flow of the resin, and a laminate having a desired size cannot be obtained. There was a problem that sometimes. Therefore, a hole is formed in the prepreg in advance,
A method generally called a pin lamination method, in which a pin is inserted into the hole to heat and mold the prepreg in a fixed state, is also performed.

【0005】従来、このプリプレグに穴を形成する方法
としては、図3に示すような、先端部に刃42を有する
と共に、軸の側面にねじれ溝44を有するドリルビット
40を用いて、プリプレグを複数重ねたプリプレグの積
載物にドリリングにより穴を形成する方法が行われてい
る。しかし、この方法の場合、穴あけを繰り返すことに
よってドリルビット40の温度が次第に高くなり樹脂の
融点を越えた場合、刃42の部分やねじれ溝44の部分
に樹脂が多量に付着してしまい、ドリルマシンのスピン
ドル等にかかる負荷が大きくなって穴あけが困難となり
やすく、穴あけを連続して行える回数が少ないという問
題があった。
Conventionally, as a method of forming a hole in the prepreg, as shown in FIG. 3, a prepreg is formed by using a drill bit 40 having a blade 42 at a tip end and a twist groove 44 on a side surface of a shaft. 2. Description of the Related Art A method of forming a hole in a load of a plurality of prepregs by drilling has been performed. However, in the case of this method, when the temperature of the drill bit 40 gradually increases due to repeated drilling and exceeds the melting point of the resin, a large amount of the resin adheres to the blade 42 and the torsion groove 44, and the drill bit is removed. There is a problem that the load on the spindle and the like of the machine becomes large and it becomes difficult to make a hole, and the number of times that a hole can be made continuously is small.

【0006】そのため、図4(a)及び(b)に示すよ
うな、先端部に刃52を有すると共に、軸方向に貫通す
る穴54を有するドリルビット50を用いて、図4
(c)に示すように、その貫通する穴54から刃52の
部分に気体Aを吹き出して刃52の部分を冷却しなが
ら、プリプレグ20の積載物に穴あけする方法が検討さ
れている。なお、図4(b)は、図4(a)のドリルビ
ット50を側方から見た図である。しかし、この方法の
場合であっても、穴あけを連続して行える回数の向上は
不十分であり、更に穴あけを連続して行える回数が多い
プリプレグの穴あけ方法が望まれている。
For this reason, a drill bit 50 having a blade 52 at the tip and a hole 54 penetrating in the axial direction as shown in FIGS.
As shown in (c), a method is being considered in which gas A is blown out from the penetrating hole 54 to the blade 52 to cool the blade 52 while drilling a load on the prepreg 20. FIG. 4B is a view of the drill bit 50 of FIG. 4A as viewed from the side. However, even in the case of this method, the improvement of the number of times that drilling can be continuously performed is insufficient, and a method of drilling a prepreg that can frequently perform drilling continuously is desired.

【0007】[0007]

【発明が解決しようとする課題】本発明は、上記問題点
を改善するために成されたもので、その目的とするとこ
ろは、ドリルビットを用いて、熱硬化性樹脂組成物を基
材に含浸したプリプレグを複数重ねたプリプレグの積載
物に穴あけするプリプレグの穴あけ方法であって、穴あ
けを連続して行える回数が優れたプリプレグの穴あけ方
法を提供することにある。
SUMMARY OF THE INVENTION The present invention has been made to solve the above problems, and an object of the present invention is to use a drill bit to apply a thermosetting resin composition to a substrate. An object of the present invention is to provide a method for drilling a prepreg in which a plurality of impregnated prepregs are drilled in a pile of prepregs in which a plurality of impregnated prepregs are stacked.

【0008】[0008]

【課題を解決するための手段】本発明の請求項1に係る
プリプレグの穴あけ方法は、先端部に刃を有すると共
に、軸方向に貫通する穴を有するドリルビットを用い
て、その貫通する穴から刃の部分に気体を吹き出しなが
ら、熱硬化性樹脂組成物を基材に含浸したプリプレグを
複数重ねたプリプレグの積載物に穴あけするプリプレグ
の穴あけ方法において、ドリルビットが、穴あけすると
きプリプレグの積載物に非接触の部分から、刃の部分に
まで軸方向に連通する切り欠き形状の凹部を軸部に有
し、その凹部に上記貫通する穴が露出するドリルビット
であることを特徴とする。
According to a first aspect of the present invention, there is provided a prepreg drilling method using a drill bit having a blade at a tip end and having a hole penetrating in the axial direction. In the prepreg boring method, in which a plurality of prepregs impregnated with a thermosetting resin composition are impregnated into a base material while blowing a gas to the blade portion, a drill bit is drilled when the prepreg is pierced. The shaft portion has a cutout-shaped concave portion communicating in the axial direction from the non-contact portion to the blade portion, and the through-hole is exposed in the concave portion.

【0009】本発明の請求項2に係るプリプレグの穴あ
け方法は、請求項1記載のプリプレグの穴あけ方法にお
いて、ドリルビットが、一枚刃のドリルビットであるこ
とを特徴とする。
According to a second aspect of the present invention, there is provided a prepreg drilling method according to the first aspect, wherein the drill bit is a single-flute drill bit.

【0010】本発明の請求項3に係るプリプレグの穴あ
け方法は、請求項1又は請求項2記載のプリプレグの穴
あけ方法において、ドリルビットの刃が、その刃を支持
する部分の軸部より、軸の半径方向に0.2〜1mm突
出して配設されていることを特徴とする。
According to a third aspect of the present invention, there is provided the prepreg drilling method according to the first or second aspect, wherein the blade of the drill bit has an axial portion closer to a shaft portion of a portion supporting the blade. Are protruded in the radial direction by 0.2 to 1 mm.

【0011】本発明によると、貫通する穴から吹き出し
た気体は、凹部を介して刃の部分及びプリプレグの積載
物の下面側に到達すると共に、プリプレグの積載物の上
面側にも到達する。そのため、この気体によってドリル
ビットのうちプリプレグと接触する部分全体を冷却する
ことができると共に、この気体によってプリプレグを切
削することによって生じた切り粉を効率的に排出するこ
とができ、ドリルビットに切り粉や樹脂が付着すること
が生じ難くなって、穴あけを連続して行える回数が優れ
たプリプレグの穴あけ方法となる。
According to the present invention, the gas blown out from the through hole reaches the blade portion and the lower surface side of the load of the prepreg via the recess, and also reaches the upper surface side of the load of the prepreg. Therefore, the entire portion of the drill bit that comes into contact with the prepreg can be cooled by the gas, and the chips generated by cutting the prepreg can be efficiently discharged by the gas, so that the drill bit can be cut. Powder and resin are less likely to adhere to the prepreg, and the prepreg drilling method is excellent in the number of times that drilling can be continuously performed.

【0012】[0012]

【発明の実施の形態】本発明に係るプリプレグの穴あけ
方法を図面に基づいて説明する。図1は本発明に係るプ
リプレグの穴あけ方法の一実施の形態を説明する図であ
り、(a)は用いるドリルビットを示す正面図、(b)
は用いるドリルビットを示す側面図、(c)は穴あけし
ている状態を破断して示した正面図である。また、図2
は本発明に係るプリプレグの穴あけ方法の他の実施の形
態に用いるドリルビットを示す正面図である。
DESCRIPTION OF THE PREFERRED EMBODIMENTS A method for drilling a prepreg according to the present invention will be described with reference to the drawings. FIG. 1 is a view for explaining an embodiment of a prepreg drilling method according to the present invention, wherein (a) is a front view showing a drill bit to be used, and (b).
FIG. 2 is a side view showing a drill bit to be used, and FIG. 2C is a front view showing a state in which a drill bit is drilled. FIG.
FIG. 4 is a front view showing a drill bit used in another embodiment of the prepreg drilling method according to the present invention.

【0013】本発明に係るプリプレグの穴あけ方法の一
実施の形態は、図1(a)及び(b)に示すような、先
端部に刃12を有すると共に、軸部14にその軸の方向
に連通する切り欠き形状の凹部18を有し、その凹部1
8に軸方向に貫通する穴16が露出しているドリルビッ
ト10を用いる。
One embodiment of the method for drilling a prepreg according to the present invention has a blade 12 at a tip end and a shaft 14 in the direction of the shaft as shown in FIGS. 1 (a) and 1 (b). It has a notch-shaped recess 18 communicating therewith, and the recess 1
8 uses a drill bit 10 in which a hole 16 penetrating in the axial direction is exposed.

【0014】そして、穴あけを行う場合には、図1
(c)に示すように、上記貫通する穴16から凹部18
を介して刃12の部分に気体Aを吹き出しながら、プリ
プレグ20の積載物に穴あけを行う。なおこのとき、凹
部18の上側の部分は、プリプレグ20の積載物より上
側に突出した状態に保持されるように、切り込み深さが
設定されており、ドリルビット10に形成された凹部1
8は、穴あけするときプリプレグ20の積載物に非接触
の部分から、刃12の部分にまで軸方向に連通する凹部
18となっている。
In the case of drilling, FIG.
As shown in (c), the through hole 16 is inserted into the recess 18.
While the gas A is blown out to the blade 12 through the hole, the load of the prepreg 20 is perforated. At this time, the depth of the cut is set so that the upper portion of the concave portion 18 is held in a state of protruding above the load of the prepreg 20, and the concave portion 1 formed in the drill bit 10 is formed.
Reference numeral 8 denotes a concave portion 18 which communicates in the axial direction from a portion not in contact with the load of the prepreg 20 to a portion of the blade 12 when drilling.

【0015】そのため、貫通する穴16から吹き出した
気体Aは、凹部18を介して刃12の部分及びプリプレ
グ20の積載物の下面側に到達すると共に、プリプレグ
20の積載物の上面側にも到達する。そのため、この気
体によってドリルビット10のうちプリプレグ20と接
触する部分全体を冷却することができ、ドリルビット1
0の温度を低く保つことができるため、ドリルビット1
0に溶融した樹脂が付着することが生じ難くなってお
り、穴あけを連続して行える回数が多くなっている。更
に、この気体Aによってプリプレグ20を切削すること
によって生じた切り粉を効率的に排出することができる
ため、ドリルビット10に切り粉が付着することも生じ
難くなっており、穴あけを連続して行える回数が多くな
っている。
Therefore, the gas A blown out from the through hole 16 reaches the blade 12 and the lower surface side of the load of the prepreg 20 via the concave portion 18 and also reaches the upper surface side of the load of the prepreg 20. I do. Therefore, the entire part of the drill bit 10 that comes into contact with the prepreg 20 can be cooled by this gas, and the drill bit 1 can be cooled.
0 can be kept low, so drill bit 1
It is difficult for the molten resin to adhere to zero, and the number of times that drilling can be continuously performed is increased. Further, since the chips generated by cutting the prepreg 20 with the gas A can be efficiently discharged, the chips are less likely to adhere to the drill bit 10, and the drilling is continuously performed. The number of operations that can be performed is increasing.

【0016】なお、凹部18の大きさは、貫通する穴1
6から吹き出した気体Aが、凹部18を介して刃12の
部分及びプリプレグ20の積載物の下面側や上面側に到
達することが可能な大きさであれば特に限定するもので
はないが、軸部14のほぼ半分程度が切り欠き状態の場
合、特に穴あけを連続して行える回数が優れ好ましい。
この大きさが小さ過ぎる場合、気体Aが通過しにくくな
るため、穴あけを連続して行える回数が低下する場合が
あり、大き過ぎる場合、ドリルビット10の強度が低下
しやすくなる。
The size of the recess 18 is determined by the size of the through hole 1.
The size of the shaft A is not particularly limited as long as the gas A blown out from the cylinder 6 can reach the blade 12 and the lower surface side or the upper surface side of the load of the prepreg 20 via the recess 18. When about half of the portion 14 is notched, the number of continuous drilling operations is particularly excellent, which is preferable.
If the size is too small, the gas A becomes difficult to pass, so that the number of times that drilling can be continuously performed may decrease. If the size is too large, the strength of the drill bit 10 tends to decrease.

【0017】また、凹部18は、切り欠き形状である
が、これは軸部14をあらかじめ円柱状に形成してお
き、そこから切り欠いて形成したものに限定するもので
はなく、切り欠いた形状になるように注型して形成した
もの等でも良い。また、この切り欠きの形状は断面D字
状に切り欠くことに限定するものではなく、切り欠いた
部分が曲線状や凹凸線状でも良く、切り欠いた部分が複
数あっても良い。なお、ドリルビット10が、切り欠い
た部分が1ヶ所のドリルビット10であり、その切り欠
いた部分の先端に1枚の刃12を形成したドリルビット
10の場合、強度と気体Aの通過しやすさのバランスが
優れ好ましい。
The concave portion 18 has a notched shape, but this is not limited to the shaft portion 14 previously formed in a cylindrical shape and cut out therefrom. It may be formed by casting such that Further, the shape of the cutout is not limited to the cutout having a D-shaped cross section, and the cutout portion may have a curved shape or an uneven line shape, or may have a plurality of cutout portions. In the case of the drill bit 10 in which the notched portion is one drill bit 10 and the drill bit 10 having one blade 12 formed at the tip of the notched portion, the strength and the passage of the gas A are obtained. The balance of ease is excellent and preferable.

【0018】また、図2に示すように、刃12が、その
刃12を支持する部分の軸部14より、軸部14の半径
方向に、Lの長さとして0.2〜1mm突出して配設さ
れていると、プリプレグ20の積載物に穴あけすると
き、この刃12の突出によって生じる軸部14とプリプ
レグ20の積載物との隙間にも、気体Aが通過するよう
になるため、特に穴あけを連続して行える回数が優れ好
ましい。
As shown in FIG. 2, the blade 12 is disposed so as to protrude 0.2 to 1 mm as a length L in the radial direction of the shaft portion 14 from the shaft portion 14 which supports the blade 12. When the prepreg 20 is provided, the gas A passes through the gap between the shaft portion 14 and the prepreg 20 caused by the protrusion of the blade 12 when the prepreg 20 is pierced. The number of times that this can be continuously performed is excellent and preferable.

【0019】なお、この刃12の材質としては、軸部1
4と同じ材質で形成されていても良く、異なった材質で
形成し接合して形成されていても良く、例えば、焼き入
れ処理した鉄や、超硬ステンレスや、ダイヤモンド等が
一般的に用いられる。なお、ダイヤモンドで形成した
り、表面にダイヤモンド層を形成した複合材で形成した
場合、特に穴あけを連続して行える回数が優れ好まし
い。
The material of the blade 12 is as follows.
4 may be formed of the same material, or may be formed of a different material and joined together. For example, quenched iron, super hard stainless steel, diamond, or the like is generally used. . In addition, when it is formed of diamond or formed of a composite material having a diamond layer formed on the surface, the number of times that drilling can be continuously performed is particularly excellent.

【0020】また、ドリルビット10の径は、形成しよ
うとする穴の大きさに合わせて調整すれば良いが、一般
的には3〜10mm程度である。また、穴あけするとき
の回転数や送り速度は、穴あけした穴の外観等により適
宜調整して穴あけする。
The diameter of the drill bit 10 may be adjusted according to the size of the hole to be formed, but is generally about 3 to 10 mm. The number of revolutions and the feed rate at the time of drilling are appropriately adjusted according to the appearance of the drilled hole and the like, and drilling is performed.

【0021】また、貫通する穴16から吹き出す気体A
は、一般的には空気が用いられるが、炭酸ガス等を吹き
出すようにしても良い。また、この気体Aは、冷却処理
されていると、ドリルビット10の温度が特に上昇しに
くくなるため、特に穴あけを連続して行える回数が優れ
好ましい。また、この気体Aが除湿処理されていると、
穴あけ時のプリプレグ20の吸湿を減らすことができる
ため、このプリプレグ20を用いて製造した積層板の特
性が優れ好ましい。
The gas A blown out from the through hole 16
In general, air is used, but carbon dioxide gas or the like may be blown out. In addition, when the gas A is subjected to the cooling treatment, the temperature of the drill bit 10 becomes particularly difficult to rise, so that the number of times that the drilling can be continuously performed is particularly excellent and preferable. Also, if this gas A is subjected to dehumidification processing,
Since the moisture absorption of the prepreg 20 at the time of drilling can be reduced, the characteristics of the laminate manufactured using the prepreg 20 are excellent and preferable.

【0022】なお、本発明に用いるプリプレグ20は、
熱硬化性樹脂組成物を基材に含浸したものであり、例え
ば、熱硬化性樹脂組成物を溶剤で粘度調整したワニス
に、基材を浸漬して含浸した後、必要に応じて加熱乾燥
して半硬化して製造したり、室温で液状又は加熱溶融さ
せて液状とした熱硬化性樹脂組成物を、基材の一方の面
に塗布した後、加熱して粘度を低下させて含浸して得ら
れるものである。なお、プリプレグ20の樹脂比率は、
熱硬化性樹脂組成物及び基材の合計100重量部に対
し、40〜200重量部が一般的である。
The prepreg 20 used in the present invention comprises:
The thermosetting resin composition is obtained by impregnating a base material.For example, the thermosetting resin composition is impregnated by immersing the base material in a varnish having a viscosity adjusted with a solvent, and then dried by heating if necessary. The semi-cured or manufactured at room temperature, the liquid or heat-melted liquid thermosetting resin composition, after applying to one surface of the substrate, heated to reduce the viscosity and impregnated It is obtained. The resin ratio of the prepreg 20 is
It is generally 40 to 200 parts by weight based on 100 parts by weight of the total of the thermosetting resin composition and the base material.

【0023】このプリプレグ20に用いる熱硬化性樹脂
組成物としては、エポキシ樹脂系、フェノール樹脂系、
ポリイミド樹脂系、不飽和ポリエステル樹脂系、ポリフ
ェニレンエーテル樹脂系等の単独、変性物、混合物のよ
うに、熱硬化性樹脂組成物全般を用いることができる。
この熱硬化性樹脂組成物中には、熱硬化性樹脂を必須と
して含有し、必要に応じてその熱硬化性樹脂の硬化剤、
硬化促進剤及び無機充填材等を含有することができる。
The thermosetting resin composition used for the prepreg 20 includes epoxy resin, phenol resin,
The thermosetting resin composition in its entirety can be used, such as a polyimide resin, an unsaturated polyester resin, a polyphenylene ether resin, or the like alone, a modified product, or a mixture.
The thermosetting resin composition contains a thermosetting resin as an essential component and, if necessary, a curing agent for the thermosetting resin,
A curing accelerator and an inorganic filler can be contained.

【0024】また、プリプレグ20に用いる基材として
は、ガラス等の無機質繊維やポリエステル、ポリアミ
ド、ポリアクリル、ポリイミド等の有機質繊維や、木綿
等の天然繊維の織布、不織布、紙等を用いることができ
る。なお、ガラス繊維製の織布(ガラスクロス)を用い
ると、得られる積層板の耐熱性、耐湿性に優れ好まし
い。
The base material used for the prepreg 20 is a woven fabric, nonwoven fabric, paper, or the like of inorganic fibers such as glass, organic fibers such as polyester, polyamide, polyacryl, and polyimide, and natural fibers such as cotton. Can be. In addition, it is preferable to use a woven fabric (glass cloth) made of glass fiber because the obtained laminate has excellent heat resistance and moisture resistance.

【0025】また、プリプレグ20の積載物は、上記プ
リプレグ20を複数重ねたものであれば特に限定するも
のではなく、必要に応じて上下や間に、プラスチック板
等を重ねていても良い。
The load of the prepreg 20 is not particularly limited as long as a plurality of the prepregs 20 are stacked, and a plastic plate or the like may be stacked above, below, or between them as necessary.

【0026】[0026]

【実施例】(実施例1)ドリルビットとして、図1に示
すような、先端部に刃12を有すると共に、軸部14に
その軸の方向に連通する切り欠き形状の凹部18を有
し、その凹部18に軸方向に貫通する穴16が露出して
いる直径6mmのドリルビット10を用いた。なおこの
ドリルビット10の刃12は、ダイヤモンドの一枚刃で
形成されており、凹部18の大きさは、軸部14のほぼ
半分程度が切り欠き形状であるドリルビット10を用い
た。
(Embodiment 1) As a drill bit, as shown in FIG. 1, a notch-shaped concave portion 18 communicating with the shaft portion 14 in the direction of the axis is provided on the shaft portion 14 in addition to having a blade 12 at a tip portion. A drill bit 10 having a diameter of 6 mm in which a hole 16 penetrating in the axial direction was exposed in the concave portion 18 was used. The blade 12 of the drill bit 10 is formed by a single diamond blade, and the size of the concave portion 18 is a drill bit 10 in which approximately half of the shaft portion 14 has a cutout shape.

【0027】また、プリプレグとしてエポキシ樹脂系樹
脂組成物をガラスクロス(基材)に含浸した厚み0.1
mmのプリプレグ[松下電工株式会社製、品名 R16
61]を用いた。そして、このプリプレグを50枚重ね
てプリプレグ20の積載物を形成した。
A glass cloth (substrate) impregnated with an epoxy resin-based resin composition as a prepreg has a thickness of 0.1%.
mm prepreg [R16, manufactured by Matsushita Electric Works, Ltd.
61] was used. Then, 50 prepregs were stacked to form a load of the prepreg 20.

【0028】そして、上記ドリルビット10を用いて、
上記プリプレグ20の積載物に、貫通する穴16から除
湿処理した空気を吹き出しながら、送り速度20秒/ヒ
ットで、プリプレグ20の積載物に穴あけを行った。な
おこのとき、凹部18の上側の部分が、プリプレグ20
の積載物より上側に突出した状態に保持されるように、
切り込み深さを設定することにより、凹部18が、穴あ
けするときプリプレグ20の積載物に非接触の部分か
ら、刃12の部分にまで軸方向に連通するように調整し
て穴あけを行った。その結果、1万ヒット連続して穴あ
けをした時点で刃12にピッチングが発生して、穴あけ
が困難となった。
Then, using the above drill bit 10,
Drilling was performed on the load of the prepreg 20 at a feed rate of 20 seconds / hit while blowing dehumidified air through the hole 16 penetrating the load of the prepreg 20. At this time, the upper part of the recess 18 is
So that it is held in a state protruding above the load of
By setting the depth of cut, drilling was performed by adjusting the concave portion 18 so that it communicated in the axial direction from the portion not in contact with the load of the prepreg 20 to the portion of the blade 12 when drilling. As a result, pitching occurred on the blade 12 when drilling was performed continuously for 10,000 hits, making drilling difficult.

【0029】(実施例2)ドリルビットとして、図2に
示すような、先端部に刃12を有すると共に、軸部14
にその軸の方向に連通する切り欠き形状の凹部18を有
し、その凹部18に軸方向に貫通する穴16が露出して
おり、且つ、刃12が、その刃12を支持する部分の軸
部14より、軸部14の半径方向に0.5mm突出して
配設されている直径6mmのドリルビット10を用いた
こと以外は実施例1と同様にして穴あけを行った。その
結果、2.3万ヒット連続して穴あけをした時点で刃1
2にピッチングが発生して、穴あけが困難となった。
(Embodiment 2) As a drill bit, as shown in FIG.
Has a notch-shaped concave portion 18 communicating with the direction of the axis, a hole 16 penetrating in the axial direction is exposed in the concave portion 18, and the blade 12 has a shaft that supports the blade 12. Drilling was performed in the same manner as in Example 1 except that a drill bit 10 having a diameter of 6 mm was provided so as to protrude from the part 14 by 0.5 mm in the radial direction of the shaft part 14. As a result, when 23,000 hits were continuously drilled, blade 1
Pitching occurred in No. 2, making drilling difficult.

【0030】(比較例1)ドリルビットとして、図4に
示すような、先端部に刃52を有すると共に、軸方向に
貫通する穴54を有する直径6mmのドリルビット50
を用いて、その貫通する穴54から除湿処理した空気を
吹き出しながら、プリプレグ20の積載物に穴あけを行
ったこと以外は実施例1と同様にして穴あけを行った。
なお、この場合、図4(c)に示すように、ドリルビッ
ト50の軸部が、プリプレグ20の積載物の内部まで侵
入しており、貫通する穴54から吹き出した気体Aは、
プリプレグ20の積載物の上面側には到達しない状態に
なっていた。その結果、5千ヒット連続して穴あけをし
た時点で刃52にピッチングが発生して、穴あけが困難
となった。
(Comparative Example 1) As shown in FIG. 4, a drill bit 50 having a diameter of 6 mm and having a blade 52 at the tip and a hole 54 penetrating in the axial direction as shown in FIG.
The hole was drilled in the same manner as in Example 1 except that the load on the prepreg 20 was drilled while blowing the dehumidified air through the hole 54 through which the air was blown.
In this case, as shown in FIG. 4C, the shaft of the drill bit 50 has penetrated to the inside of the load of the prepreg 20, and the gas A blown out from the through hole 54 is
The prepreg 20 did not reach the upper surface of the load. As a result, pitching occurred in the blade 52 when drilling was performed continuously for 5,000 hits, making drilling difficult.

【0031】(結果のまとめ)本発明に係るプリプレグ
の穴あけ方法で穴あけを行った各実施例は、比較例1と
比べて、穴あけを連続して行える回数が優れていること
が確認された。また、刃が、その刃を支持する部分の軸
部より、軸の半径方向に0.2〜1mm突出して配設さ
れている実施例2は、実施例1と比べて、特に穴あけを
連続して行える回数が優れていることが確認された。
(Summary of Results) It was confirmed that, in each of the examples in which the prepreg was drilled according to the present invention, the number of times of continuous drilling was excellent as compared with Comparative Example 1. Further, in the second embodiment, in which the blade is disposed so as to protrude from the shaft portion of the portion supporting the blade in the radial direction of the shaft by 0.2 to 1 mm, the drilling is particularly continuous compared to the first embodiment. It was confirmed that the number of times that it could be performed was excellent.

【0032】[0032]

【発明の効果】本発明に係るプリプレグの穴あけ方法
は、用いるドリルビットが、穴あけするときプリプレグ
の積載物に非接触の部分から、刃の部分にまで軸方向に
連通する切り欠き形状の凹部を軸部に有し、その凹部に
気体を吹き出す貫通する穴が露出するドリルビットであ
るため、穴あけを連続して行える回数が優れたプリプレ
グの穴あけ方法である。
According to the method for drilling a prepreg according to the present invention, the drill bit used has a notch-shaped concave portion communicating in the axial direction from a portion not in contact with a load of the prepreg to a blade portion when drilling. Since the drill bit has a shaft portion and a through hole that blows out gas into the concave portion is exposed, the method is a method for drilling a prepreg excellent in the number of times that drilling can be continuously performed.

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

【図1】本発明に係るプリプレグの穴あけ方法の一実施
の形態を説明する図であり、(a)は用いるドリルビッ
トを示す正面図、(b)は用いるドリルビットを示す側
面図、(c)は穴あけしている状態を破断して示した正
面図である。
FIG. 1 is a view for explaining an embodiment of a prepreg drilling method according to the present invention, wherein (a) is a front view showing a drill bit to be used, (b) is a side view showing a drill bit to be used, and (c). () Is a cutaway front view showing the state of drilling.

【図2】本発明に係るプリプレグの穴あけ方法の他の実
施の形態に用いるドリルビットを示す正面図である。
FIG. 2 is a front view showing a drill bit used in another embodiment of the prepreg drilling method according to the present invention.

【図3】従来のプリプレグの穴あけ方法に用いるドリル
ビットを示す正面図である。
FIG. 3 is a front view showing a drill bit used in a conventional prepreg drilling method.

【図4】従来のプリプレグの穴あけ方法の他の方法を説
明する図であり、(a)は用いるドリルビットを示す正
面図、(b)は用いるドリルビットを示す側面図、
(c)は穴あけしている状態を破断して示した図であ
る。
4A and 4B are diagrams illustrating another conventional prepreg drilling method, wherein FIG. 4A is a front view showing a drill bit to be used, FIG. 4B is a side view showing a drill bit to be used,
(C) is the figure which fractured and showed the state which perforated.

【符号の説明】[Explanation of symbols]

10,40,50 ドリルビット 12,42,52 刃 14 軸部 16,54 貫通する穴 18 凹部 20 プリプレグ A 気体 10, 40, 50 Drill bit 12, 42, 52 Blade 14 Shaft 16, 54 Hole penetrating 18 Recess 20 Prepreg A Gas

Claims (3)

【特許請求の範囲】[Claims] 【請求項1】 先端部に刃を有すると共に、軸方向に貫
通する穴を有するドリルビットを用いて、その貫通する
穴から刃の部分に気体を吹き出しながら、熱硬化性樹脂
組成物を基材に含浸したプリプレグを複数重ねたプリプ
レグの積載物に穴あけするプリプレグの穴あけ方法にお
いて、ドリルビットが、穴あけするときプリプレグの積
載物に非接触の部分から、刃の部分にまで軸方向に連通
する切り欠き形状の凹部を軸部に有し、その凹部に上記
貫通する穴が露出するドリルビットであることを特徴と
するプリプレグの穴あけ方法。
1. A thermosetting resin composition is formed on a base material by using a drill bit having a blade at a tip portion and having a hole penetrating in an axial direction, while blowing gas from the penetrating hole to a blade portion. In a method of drilling a prepreg loaded with a plurality of prepregs impregnated with a prepreg, a drill bit is formed so that when drilling, a cutting portion communicating in the axial direction from a portion not in contact with the prepreg loaded material to a blade portion. A method for drilling a prepreg, characterized in that the drill bit is a drill bit having a notch-shaped concave portion in a shaft portion and exposing the through hole in the concave portion.
【請求項2】 ドリルビットが、一枚刃のドリルビット
であることを特徴とする請求項1記載のプリプレグの穴
あけ方法。
2. The method for drilling a prepreg according to claim 1, wherein the drill bit is a single-flute drill bit.
【請求項3】 ドリルビットの刃が、その刃を支持する
部分の軸部より、軸の半径方向に0.2〜1mm突出し
て配設されていることを特徴とする請求項1又は請求項
2記載のプリプレグの穴あけ方法。
3. The drill bit according to claim 1, wherein a blade of the drill bit protrudes from a shaft portion of a portion supporting the blade by 0.2 to 1 mm in a radial direction of the shaft. 2. The method for drilling a prepreg according to 2.
JP18349498A 1998-06-30 1998-06-30 How to drill prepreg Expired - Fee Related JP3853074B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP18349498A JP3853074B2 (en) 1998-06-30 1998-06-30 How to drill prepreg

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP18349498A JP3853074B2 (en) 1998-06-30 1998-06-30 How to drill prepreg

Related Child Applications (1)

Application Number Title Priority Date Filing Date
JP2004031020A Division JP3966291B2 (en) 2004-02-06 2004-02-06 Drill bit for drilling prepreg

Publications (2)

Publication Number Publication Date
JP2000015632A true JP2000015632A (en) 2000-01-18
JP3853074B2 JP3853074B2 (en) 2006-12-06

Family

ID=16136812

Family Applications (1)

Application Number Title Priority Date Filing Date
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Country Status (1)

Country Link
JP (1) JP3853074B2 (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2008120989A (en) * 2006-10-17 2008-05-29 Hitachi Chem Co Ltd Prepreg and laminate
JP2012228884A (en) * 2006-10-17 2012-11-22 Hitachi Chemical Co Ltd Prepreg, and laminate

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103573185A (en) * 2013-07-16 2014-02-12 昆山巨德泰精密机械有限公司 Drilling bit with radiating hole in center of bottom part

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2008120989A (en) * 2006-10-17 2008-05-29 Hitachi Chem Co Ltd Prepreg and laminate
JP2012228884A (en) * 2006-10-17 2012-11-22 Hitachi Chemical Co Ltd Prepreg, and laminate

Also Published As

Publication number Publication date
JP3853074B2 (en) 2006-12-06

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