JPH0742489B2 - Abrasion resistant parts with tool or hard head made of composite sintered material - Google Patents
Abrasion resistant parts with tool or hard head made of composite sintered materialInfo
- Publication number
- JPH0742489B2 JPH0742489B2 JP59163095A JP16309584A JPH0742489B2 JP H0742489 B2 JPH0742489 B2 JP H0742489B2 JP 59163095 A JP59163095 A JP 59163095A JP 16309584 A JP16309584 A JP 16309584A JP H0742489 B2 JPH0742489 B2 JP H0742489B2
- Authority
- JP
- Japan
- Prior art keywords
- sintered
- hard
- cemented carbide
- composite
- less
- 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 - Fee Related
Links
- 239000002131 composite material Substances 0.000 title claims description 87
- 239000000463 material Substances 0.000 title claims description 70
- 235000002505 Centaurea nigra Nutrition 0.000 title claims description 11
- 241001073742 Mylopharodon conocephalus Species 0.000 title claims description 11
- 238000005299 abrasion Methods 0.000 title claims 3
- 229910003460 diamond Inorganic materials 0.000 claims description 49
- 239000010432 diamond Substances 0.000 claims description 49
- 239000000843 powder Substances 0.000 claims description 37
- 238000005245 sintering Methods 0.000 claims description 27
- 229910052582 BN Inorganic materials 0.000 claims description 22
- PZNSFCLAULLKQX-UHFFFAOYSA-N Boron nitride Chemical compound N#B PZNSFCLAULLKQX-UHFFFAOYSA-N 0.000 claims description 22
- 238000000034 method Methods 0.000 claims description 15
- 229910052751 metal Inorganic materials 0.000 claims description 13
- 239000002184 metal Substances 0.000 claims description 13
- 239000002245 particle Substances 0.000 claims description 13
- 230000004323 axial length Effects 0.000 claims description 10
- 150000001247 metal acetylides Chemical class 0.000 claims description 4
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical group [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 claims 1
- 238000005520 cutting process Methods 0.000 description 32
- 239000012071 phase Substances 0.000 description 27
- 238000004519 manufacturing process Methods 0.000 description 20
- 239000011812 mixed powder Substances 0.000 description 15
- 229910045601 alloy Inorganic materials 0.000 description 12
- 239000000956 alloy Substances 0.000 description 12
- 239000013078 crystal Substances 0.000 description 12
- 229910009043 WC-Co Inorganic materials 0.000 description 11
- 238000005553 drilling Methods 0.000 description 8
- 239000000758 substrate Substances 0.000 description 8
- 238000000227 grinding Methods 0.000 description 7
- 239000004593 Epoxy Substances 0.000 description 5
- 239000000203 mixture Substances 0.000 description 5
- 239000011230 binding agent Substances 0.000 description 4
- 239000011521 glass Substances 0.000 description 4
- 238000010438 heat treatment Methods 0.000 description 4
- 238000007731 hot pressing Methods 0.000 description 4
- 238000005452 bending Methods 0.000 description 3
- 238000005219 brazing Methods 0.000 description 3
- 238000001816 cooling Methods 0.000 description 3
- 238000010894 electron beam technology Methods 0.000 description 3
- 230000005496 eutectics Effects 0.000 description 3
- 238000002474 experimental method Methods 0.000 description 3
- 230000010354 integration Effects 0.000 description 3
- 239000006104 solid solution Substances 0.000 description 3
- 238000003466 welding Methods 0.000 description 3
- 229910052782 aluminium Inorganic materials 0.000 description 2
- 230000007547 defect Effects 0.000 description 2
- 239000003365 glass fiber Substances 0.000 description 2
- 238000005304 joining Methods 0.000 description 2
- 239000007791 liquid phase Substances 0.000 description 2
- 150000004767 nitrides Chemical class 0.000 description 2
- 239000002244 precipitate Substances 0.000 description 2
- 229920005989 resin Polymers 0.000 description 2
- 239000011347 resin Substances 0.000 description 2
- 239000007787 solid Substances 0.000 description 2
- 239000002904 solvent Substances 0.000 description 2
- 101150051314 tin-10 gene Proteins 0.000 description 2
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 1
- 229910000531 Co alloy Inorganic materials 0.000 description 1
- BQCADISMDOOEFD-UHFFFAOYSA-N Silver Chemical compound [Ag] BQCADISMDOOEFD-UHFFFAOYSA-N 0.000 description 1
- 229910000831 Steel Inorganic materials 0.000 description 1
- ATJFFYVFTNAWJD-UHFFFAOYSA-N Tin Chemical compound [Sn] ATJFFYVFTNAWJD-UHFFFAOYSA-N 0.000 description 1
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 1
- 238000013459 approach Methods 0.000 description 1
- 229910052799 carbon Inorganic materials 0.000 description 1
- 229910052804 chromium Inorganic materials 0.000 description 1
- 150000001875 compounds Chemical class 0.000 description 1
- 238000009792 diffusion process Methods 0.000 description 1
- 238000009826 distribution Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 239000003822 epoxy resin Substances 0.000 description 1
- 238000011049 filling Methods 0.000 description 1
- 239000012467 final product Substances 0.000 description 1
- 229910052735 hafnium Inorganic materials 0.000 description 1
- 239000012761 high-performance material Substances 0.000 description 1
- 230000002706 hydrostatic effect Effects 0.000 description 1
- 239000012770 industrial material Substances 0.000 description 1
- 238000009776 industrial production Methods 0.000 description 1
- 230000008595 infiltration Effects 0.000 description 1
- 238000001764 infiltration Methods 0.000 description 1
- 239000013067 intermediate product Substances 0.000 description 1
- 229910052742 iron Inorganic materials 0.000 description 1
- 230000001788 irregular Effects 0.000 description 1
- 239000007769 metal material Substances 0.000 description 1
- 238000002156 mixing Methods 0.000 description 1
- 238000000465 moulding Methods 0.000 description 1
- 229910052759 nickel Inorganic materials 0.000 description 1
- 229910052755 nonmetal Inorganic materials 0.000 description 1
- 238000009931 pascalization Methods 0.000 description 1
- 230000000737 periodic effect Effects 0.000 description 1
- 229920000647 polyepoxide Polymers 0.000 description 1
- 239000011148 porous material Substances 0.000 description 1
- 238000001556 precipitation Methods 0.000 description 1
- 238000003825 pressing Methods 0.000 description 1
- 239000000047 product Substances 0.000 description 1
- 239000002994 raw material Substances 0.000 description 1
- 229910052710 silicon Inorganic materials 0.000 description 1
- 239000010703 silicon Substances 0.000 description 1
- 229910052709 silver Inorganic materials 0.000 description 1
- 239000004332 silver Substances 0.000 description 1
- 239000007779 soft material Substances 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
- 229910052719 titanium Inorganic materials 0.000 description 1
- 229910052721 tungsten Inorganic materials 0.000 description 1
- 229910052984 zinc sulfide Inorganic materials 0.000 description 1
- 229910052726 zirconium Inorganic materials 0.000 description 1
Landscapes
- Cutting Tools, Boring Holders, And Turrets (AREA)
- Powder Metallurgy (AREA)
Description
【発明の詳細な説明】 産業上の利用分野 本発明は硬質な頭部を有する複合焼結材料に関する。Description: FIELD OF THE INVENTION The present invention relates to a composite sintered material having a hard head.
更に詳細には本発明は、ダイヤモンド焼結体或いは高圧
相窒化硼素焼結体の如き硬質な頭部と、該頭部と一体に
構成される超硬合金からなる支持部とを具備する小断面
の複合焼結材料に関する。More specifically, the present invention relates to a small cross section having a hard head such as a diamond sintered body or a high-pressure phase boron nitride sintered body, and a supporting portion made of cemented carbide integrally formed with the head. Of the composite sintered material.
このような本発明の対象となる小断面の複合焼結材料
は、高性能な小径ドリルの素材或いはドットプリンタの
ヘッド部として用いることができる。The composite sintered material having a small cross section, which is the subject of the present invention, can be used as a material for a high-performance small-diameter drill or a head portion of a dot printer.
従来の技術 超硬合金よりなるドリルが金属、非金属材料の穴あけ用
に多用されている。特に近年急激に需要が伸びているプ
リント基板の穴あけには直径1mm前後或いはこれより細
い超硬合金製ドリルが使われている。プリント基板の集
積度は今後も上昇すると予想され、それに伴ないより細
径のドリルの使用割合が増えていくと考えられる。2. Description of the Related Art Drills made of cemented carbide are widely used for drilling metal and non-metal materials. In particular, cemented carbide drills with a diameter of about 1 mm or thinner are used for drilling printed circuit boards, which are in rapid demand in recent years. It is expected that the degree of integration of printed circuit boards will increase in the future, and the use rate of smaller diameter drills will increase accordingly.
一方、プリント基板には各種の材料が使われているが、
主として用いられているのはガラス繊維にエポキシ樹脂
を含浸させた強化樹脂で、一般にガラエポ基板と称され
ている。On the other hand, various materials are used for printed circuit boards,
Mainly used is a reinforced resin obtained by impregnating glass fiber with an epoxy resin, which is generally called a glass epoxy substrate.
このようなプリント基板の穴あけは剛性の高いドリルで
通常回転数5〜6万rpmの条件で行われているが、基板
に含まれるガラス繊維は超硬工具を非常に早く摩耗さ
せ、一般的に3000〜5000ヒット(ヒットとは穴あけ回数
のこと)で超硬ドリルは寿命となる。こうしたドリル盤
には自動工具交換装置がついており、寿命となったドリ
ルは自動的に交換される。しかしながら、上述のように
プリント基板の集積度が高まるにつれ、生産効率向上の
ためにはこの自動工具交換のための時間も問題であり、
ドリル寿命をのばして工具交換回数すなわち交換時間を
減少させるという要求が強い。Drilling of such a printed circuit board is usually performed with a high-rigidity drill at a rotational speed of 50,000 to 60,000 rpm, but the glass fiber contained in the circuit board causes the cemented carbide tool to wear very quickly, and generally With 3000 to 5000 hits (hits are the number of holes drilled), a carbide drill reaches its end of life. These drill machines are equipped with an automatic tool changer, which automatically replaces the drill when it reaches the end of its useful life. However, as the degree of integration of printed circuit boards increases as described above, the time for this automatic tool change is also a problem in order to improve production efficiency.
There is a strong demand to extend the drill life and reduce the number of tool changes, that is, the change time.
プリント基板の特性からみると、更に耐熱性等を向上さ
せて高機能化を計りたいという要求も強く、このような
基板材料は実際に製造可能であるが、一般にこのような
高機能材料は難削で、従来の超硬質ドリルでは非常に短
寿命となってしまい、このためこの種の基板材料の実用
化が出来ないのが実情である。Considering the characteristics of printed circuit boards, there is a strong demand for further improvement in heat resistance and other functions, and such board materials can be actually manufactured, but in general, such high-performance materials are difficult to manufacture. Due to grinding, the life of conventional ultra-hard drills becomes extremely short, and it is the actual situation that this kind of substrate material cannot be put to practical use.
更に、通常のガラエポ基板に対しても更に高能率の穴あ
けを行うため穴あけドリルの回転数の上昇が望まれてい
るが、これも従来の超硬合金製ドリルでは切削速度の上
昇と共に急激に寿命が低下してしまうのでドリル回転数
上昇による高能率化を達成できない。Furthermore, it is desired to increase the rotation speed of the drill to make even more efficient drilling for ordinary glass-epoxy substrates, but this is also the case with conventional cemented carbide drills, where the life is sharply increased with increasing cutting speed. However, it is impossible to achieve high efficiency by increasing the rotation speed of the drill.
一方、近年使用量が急激に増加しつつある焼結ダイヤモ
ンド工具は超硬工具に対して飛躍的に硬度が高く、耐摩
耗性がすぐれており、上記強化樹脂などの切削に於いて
は非常な高性能を発揮する。On the other hand, sintered diamond tools, whose usage has been increasing rapidly in recent years, have dramatically higher hardness than cemented carbide tools and have excellent wear resistance, which makes them extremely useful in cutting such reinforced resins. Demonstrate high performance.
ところが第1図に示すように、現在市販されている焼結
ダイヤモンド素材は焼結ダイヤモンド層11が超硬合金の
支持部12に14の部分で貼り合わされた形状のものであ
る。However, as shown in FIG. 1, the sintered diamond material currently on the market has a shape in which a sintered diamond layer 11 is bonded to a support portion 12 of cemented carbide at 14 portions.
この複合焼結体13を使用してドリルを作製する場合には
第2図に示すようにシャンク15の先端部に複合焼結体13
を何らかの方法により固着させて作らざるを得ない。When a drill is produced using this composite sintered body 13, the composite sintered body 13 is attached to the tip of the shank 15 as shown in FIG.
There is no choice but to fix it by some method.
ところが例えばプリント基板用に使われるドリルの径は
一般に1mm程度より細く、場合によっては0.1mm位であ
り、このような小径のものではシャンク15と余程強力な
接合強度をもたせないと接合後の刃先研削加工で接合部
16からはずれてしまい、良好なドリルが製造できない。
特に焼結ダイヤモンドは難研削であり、研削抵抗が高
く、通常の銀ロウ付け程度の強度では強度不足である。
接合強度の高い接合方法として例えば電子ビーム溶接が
考えられるが、電子ビーム溶接を実施するとなると、ド
リルの製造工程が複雑且つ原価が高くなり、高性能ドリ
ルの需要の近年の急激な増加に対応できなかった。However, for example, the diameter of the drill used for printed circuit boards is generally smaller than about 1 mm, and in some cases it is about 0.1 mm. Joined part by cutting edge grinding
It deviates from 16, and a good drill cannot be manufactured.
In particular, sintered diamond is difficult to grind, has a high grinding resistance, and is insufficient in strength at the level of ordinary silver brazing.
Electron beam welding, for example, is considered as a joining method with high joining strength, but if electron beam welding is implemented, the manufacturing process of the drill will be complicated and the cost will be high, and it will be possible to respond to the recent rapid increase in demand for high-performance drills. There wasn't.
一方、支持部について説明すると特に小径の製品の場合
には支持部の強度は非常に重要である。前に述べたよう
にプリント基板の集積度は近年上がって来ており、将来
益々この現象は加速されると考えてよい。すなわちスル
ー・ホール・メッキされる孔の径はどんどん小径へ移行
する。今後プリント基板の製造に0.1mmφとか0.3mmφの
小径のドリルの使用量は増大する。このとき特に問題と
なるのはドリルの折損であり、刃先の摩耗で寿命となる
前に折損してしまっては高価な焼結ダイヤモンドドリル
を使用する意味がなくなる。折損をさけるために軟い材
料や剛性の低い材料で支持部を製造すると屈曲し易くな
り真直な穴があかないという問題がある。又切粉による
支持部の摩耗の問題も生ずる。On the other hand, when the support portion is described, the strength of the support portion is very important especially in the case of a product having a small diameter. As described above, the degree of integration of printed circuit boards has been increasing in recent years, and it can be considered that this phenomenon will accelerate in the future. That is, the diameter of the through-hole plated hole is gradually reduced. In the future, the amount of drills with small diameters of 0.1 mmφ or 0.3 mmφ will increase in the production of printed circuit boards. At this time, a particular problem is breakage of the drill, and if it breaks before the end of its life due to wear of the cutting edge, there is no point in using an expensive sintered diamond drill. If the support portion is made of a soft material or a material having low rigidity to avoid breakage, there is a problem that the support portion is easily bent and there is no straight hole. There is also a problem of wear of the supporting portion due to cutting chips.
発明が解決しようとする問題点 本発明は、上記従来技術の問題を解決することを目的と
し、更に詳細には、硬質な頭部と強度および抗折力の高
い支持部とを有する小径の複合焼結材料を提供し、これ
より切削性、耐摩耗性および剛性が優れ且つ長寿命のド
リル等を容易に製造可能とすることを目的とする。DISCLOSURE OF THE INVENTION Problems to be Solved by the Invention The present invention aims to solve the above-mentioned problems of the prior art, and more specifically, a small-diameter composite having a hard head and a support having high strength and transverse rupture strength. An object of the present invention is to provide a sintered material, which enables easy production of a drill or the like having excellent machinability, wear resistance and rigidity and having a long life.
更に本発明の目的は、ガラエポ基板の如き難削性の基板
の穴あけを容易且つ高性能で実現する、長寿命のドリル
を低価格で提供することにある。A further object of the present invention is to provide a long-life drill at a low price, which enables easy and high-performance drilling of a difficult-to-cut substrate such as a glass epoxy substrate.
更に、本発明の目的は、ドットプリンタのヘッドの如き
超硬質の先端部を必要とする細長の部材を容易に製造し
得る中間製品としての小径の複合焼結材料を提供するこ
とにある。A further object of the present invention is to provide a small-diameter composite sintered material as an intermediate product that can easily manufacture an elongated member such as a head of a dot printer that requires an ultra-hard tip.
更に詳細には、本発明の目的は、本出願人による特願昭
59−120218号に開示した複合焼結材料の支持部の耐摩耗
性および剛性を改善することにある。More specifically, the purpose of the present invention is
It is to improve the wear resistance and rigidity of the supporting portion of the composite sintered material disclosed in 59-120218.
問題点を解決する手段 上記の目的を達成するため、本発明に従い、ダイヤモン
ド粉末または高圧相窒化硼素粉末のいずれか一方または
双方を50%以上含有する硬質焼結部と、該硬質焼結部の
1端部で該硬質焼結部と接合している超硬合金からなる
支持部とを具備する複合焼結材料であって、 該硬質焼結部と該支持部との接合は、該硬質焼結部の焼
結過程で形成されたものであり; 更に、該複合焼結材料の直径あるいは相当直径は3mm以
下であり; 該硬質焼結部の軸方向長さが0.3〜2mmであり; 該支持部の軸方向長さが該硬質焼結部の軸方向長さの5
倍以上であり; 該支持部はWCを主成分とした炭化物を鉄属金属で結合し
た超硬合金よりなり、この超硬合金中の炭化物の平均粒
度が3μm以下であり、また結合金属量が7重量%以上
であることを特徴とする硬質な頭部を有する複合焼結材
料が提供される。Means for Solving the Problems In order to achieve the above object, according to the present invention, a hard sintered portion containing 50% or more of either or both of diamond powder or high-pressure phase boron nitride powder, and the hard sintered portion. A composite sintered material comprising a support part made of a cemented carbide that is joined to the hard sintered part at one end, wherein the hard sintered part and the support part are joined by the hard sintering. Formed in the sintering process of the joint; and further, the diameter or equivalent diameter of the composite sintered material is 3 mm or less; the axial length of the hard sintered portion is 0.3 to 2 mm; The axial length of the supporting portion is 5 times the axial length of the hard sintered portion.
The supporting portion is made of a cemented carbide in which a carbide containing WC as a main component is bound by an iron-group metal, the average grain size of the carbide in the cemented carbide is 3 μm or less, and the amount of bound metal is A composite sintered material having a hard head is provided, which is characterized by being 7% by weight or more.
ダイヤモンド粉末または高圧相窒化硼素粉末の平均粒度
は好ましくは30μm以下であり、この範囲の粒度のダイ
ヤモンドまたは高圧相窒化硼素焼結体で耐摩耗性および
剛性に優れた複合焼結材料が得られる。The average particle size of the diamond powder or the high-pressure phase boron nitride powder is preferably 30 μm or less, and a diamond or high-pressure phase boron nitride sintered body having a particle size within this range can provide a composite sintered material having excellent wear resistance and rigidity.
ただし、ダイヤモンド粉末を使用して切削工具のチップ
を作製するときは、平均粒度が10μmを越えるダイヤモ
ンド粉末を原料として使用すると、この複合焼結材料を
加工して得た切削工具の切刃が鋭利に成形できず、この
ため高性能とならないので、硬質焼結部は10μm以下の
ダイヤモンドまたは高圧相窒化硼素からなるのが好まし
い。However, when making chips for cutting tools using diamond powder, if diamond powder with an average particle size of more than 10 μm is used as a raw material, the cutting edge of the cutting tool obtained by processing this composite sintered material will have a sharp edge. The hard sintered part is preferably made of diamond having a diameter of 10 μm or less or high-pressure phase boron nitride, because it cannot be formed into a compact shape and therefore does not have high performance.
硬質焼結部がダイヤモンド粉末を主成分として焼結され
たものであるときは、ダイヤモンド粉末単独、或いは70
%以上のダイヤモンドを含み、残部がFe、CoまたはNiを
主成分とする結合材により焼結したものである。このよ
うな硬質焼結部の好ましい例としては、70%以上のダイ
ヤモンドとWC−5〜15%Coとの焼結体がある。When the hard sintered part is sintered with diamond powder as the main component, the diamond powder alone or 70
% Of diamond and the balance is sintered with a binder containing Fe, Co or Ni as a main component. A preferable example of such a hard sintered part is a sintered body of 70% or more diamond and WC-5 to 15% Co.
尚、硬質焼結部の材料としてダイヤモンド単独の粉末を
使用する場合は、硬質焼結部の焼結時に支持部材料中の
結合材成分もしくはダイヤモンド粉末に隣接しておいた
溶浸材が硬質焼結部材料粉末中に溶浸することによって
硬質焼結部の焼結が達成される。When powder of diamond alone is used as the material of the hard sintered portion, the infiltrant adjoining the binder component or diamond powder in the support material at the time of sintering of the hard sintered portion is hard burned. Sintering of the hard sintered part is achieved by infiltration into the binder material powder.
硬質焼結部が高圧相窒化硼素粉末を主成分とする場合
は、高圧相窒化硼素粉末単独、或いは50%以上の高圧相
窒化硼素に4a、5a、6a族元素の炭化物、窒化物、炭窒化
物及びアルミニウムおよび/またはシリコンを結合材と
して添加して焼結したものがある。なお、高圧相窒化硼
素単独の粉末はそれに隣接して置いた溶浸材から溶浸さ
れて焼結が達成される。ここで、高圧相窒化硼素とは、
立方晶型窒化硼素およびウルツ鉱型窒化硼素を意味す
る。When the hard sintered part is mainly composed of high-pressure phase boron nitride powder, high-pressure phase boron nitride powder alone or 50% or more high-pressure phase boron nitride powder in 4a, 5a, 6a group carbides, nitrides, carbonitrides And sintered by adding aluminum and / or silicon as a binder. The powder of high-pressure phase boron nitride alone is infiltrated from the infiltrant placed adjacent to it to achieve sintering. Here, the high-pressure phase boron nitride is
It means cubic boron nitride and wurtzite boron nitride.
次に支持部について説明すると、WCを主成分とする超硬
合金は高い剛性のみならず高い耐摩耗性を有し、また高
い耐摩耗性を示す割りに強度の高い優れた工業材料であ
るため本発明に於いても支持部にはWCを主成分とする超
硬合金を採用した。Next, the support part will be explained.Because the cemented carbide containing WC as the main component has not only high rigidity but also high wear resistance, and because it is a high-strength industrial material with high wear resistance. Also in the present invention, a cemented carbide containing WC as a main component is adopted for the supporting portion.
鋼切削用の超硬合金に含まれているTiCやTaCは本発明の
支持部の場合には耐摩耗性の向上には役立たずむしろ強
度を低下するので有効でない。しかし焼結時にWCの粒成
長を抑制するに有効な数%以下程度の少量のTaC、Cr3C2
やVCは特に微細なWCを主成分とする超硬合金を得るのに
有効である。また結合金属としてCoが最も好ましく、Ni
がそれに次いで好ましい。TiC and TaC contained in the cemented carbide for steel cutting are not effective in the case of the support portion of the present invention because they do not serve to improve the wear resistance and rather reduce the strength. However, a small amount of TaC or Cr 3 C 2 of a few percent or less, which is effective in suppressing the grain growth of WC during sintering.
And VC are particularly effective for obtaining fine WC-based cemented carbide. Further, Co is most preferable as the binding metal, and Ni is
Are next preferred.
本発明の好ましい1態様に従うと、支持部を構成する超
硬合金中の炭化物の粒度が2μm以下であり、結合金属
量が12重量%以上である。According to a preferred embodiment of the present invention, the grain size of the carbide in the cemented carbide forming the support is 2 μm or less, and the amount of binding metal is 12% by weight or more.
更に、本発明の1つの態様に従うと、硬質焼結部と支持
部とは、厚さ0.5mm以下の中間接合層を介して接合され
ている。Further, according to one aspect of the present invention, the hard sintered portion and the support portion are joined together via an intermediate joining layer having a thickness of 0.5 mm or less.
中間接合層としては、70%未満の高圧相窒化硼素と残部
が周期律表第4a族のTi、Zr、Hfの炭化物、窒化物、炭窒
化物あるいはホウ化物の1種もしくはこれらの混合物ま
たは相互固溶体化合物を主体としたものと、これにAlお
よび/またはSiを0.1重量%以上含有するものが好まし
い。As the intermediate bonding layer, a high-pressure phase boron nitride of less than 70% and the balance being one of Ti, Zr, and Hf carbides, nitrides, carbonitrides, or borides of Group 4a of the Periodic Table, or a mixture thereof or mutual mutual. It is preferable to use a solid solution compound as a main component and a material containing Al and / or Si in an amount of 0.1% by weight or more.
上記した如く、本発明に於いては硬質焼結部と支持部の
接合が硬質焼結部の焼結時に形成されることが肝要であ
る。このために、硬質焼結部のホットプレス(焼結処
理)時に硬質焼結部の材料粉末を支持部材料の上に配置
してホットプレスを行うことが必要である。このとき、
支持部となる材料は、既に焼結済みの固形超硬合金であ
ってもよく、或いは超硬合金材料の粉末であってもよ
い。As described above, in the present invention, it is important that the joint between the hard sintered portion and the support portion is formed when the hard sintered portion is sintered. Therefore, at the time of hot pressing (sintering treatment) of the hard sintered portion, it is necessary to place the material powder of the hard sintered portion on the material of the supporting portion and perform hot pressing. At this time,
The material forming the supporting portion may be solid cemented carbide that has already been sintered, or may be powder of cemented carbide material.
次ぎに、本発明の複合焼結材料円柱体の寸法上の特徴を
説明する。Next, dimensional features of the composite sintered material cylindrical body of the present invention will be described.
本発明の複合焼結材料の断面は3mm以下の直径あるいは
相当直径であることが必要である。3mmを越える直径の
複合焼結材料はプリント基板の穴あけドリル用素材とし
ては不適格である。また研削して使用するにしても研削
代が大きくなり不経済である。ここで、相当直径とは断
面積の等しい円の直径に換算した値を意味する。The cross section of the composite sintered material of the present invention needs to have a diameter of 3 mm or less or an equivalent diameter. A composite sintered material with a diameter of more than 3 mm is not suitable as a material for drilling holes for printed circuit boards. Further, even if it is used after grinding, the grinding allowance is large and it is uneconomical. Here, the equivalent diameter means a value converted into the diameter of a circle having the same cross-sectional area.
また、硬質焼結部の軸方向の長さは0.3〜2mmの範囲であ
る。0.3mm未満では、ドリル先端部として使用した場合
には必要が切刃を形成できず、2mmを越える長さでは高
価なダイヤモンド粉末等を多量に使用することになり不
経済であり、また折損の危険が増加する。Moreover, the axial length of the hard sintered portion is in the range of 0.3 to 2 mm. If it is less than 0.3 mm, the cutting edge cannot be formed when it is used as the tip of the drill, and if it exceeds 2 mm, it is uneconomical because it uses a large amount of expensive diamond powder etc. The risk increases.
更に、本発明の複合焼結材料の支持部の長さは硬質焼結
部の長さの5倍以上であることが必要である。ドリルを
作製する場合に、ドリルの刃先長さを確保し、末端をシ
ャンクに埋込む必要があるので、上記の通り、硬質焼結
部の長さの5倍以上の長さの支持部が必要となる。複合
焼結材料の断面形状としては円形が一般に望ましいが、
ドリルにしても平切りドリルもあり、必ずしも円形にこ
だわらなく、角形であってもよい。これは製造上の難易
や最終製品の形状によって決められる。Further, the length of the supporting portion of the composite sintered material of the present invention needs to be 5 times or more the length of the hard sintered portion. When making a drill, it is necessary to secure the cutting edge length of the drill and to bury the end in the shank. Therefore, as mentioned above, a supporting portion having a length 5 times or more the length of the hard sintered portion is required. Becomes A circular shape is generally desirable as the cross-sectional shape of the composite sintered material,
There are flat drills as well as drills, and the shape is not limited to a circular shape and may be a square shape. This is determined by manufacturing difficulty and the shape of the final product.
作用 本発明は上述した如く特願昭59−120218号および特願昭
59−120219号に開示した複合焼結材料の支持部を改良し
たものである。すなわち、上記した如く本発明の複合焼
結材料に於いては支持部の軸方向長さは硬質焼結部の長
さの5倍以上ある。従って、ドリルとして用いられる際
には支持部の折損または屈曲の恐れがあり、更に高速回
転による摩耗を考慮する必要があり、上記の如く支持部
の成分を限定して苛酷な使用条件でも折損または屈曲の
恐れがなく、長寿命のドリルを提供することに成功した
ものである。従って、本発明による支持部の改良点およ
びその作用を以下に詳細に説明する。Function The present invention is as described above in Japanese Patent Application No. 59-120218 and Japanese Patent Application No.
This is an improvement of the supporting portion of the composite sintered material disclosed in No. 59-120219. That is, as described above, in the composite sintered material of the present invention, the axial length of the support portion is 5 times or more the length of the hard sintered portion. Therefore, when used as a drill, there is a risk of breakage or bending of the support portion, and it is necessary to consider wear due to high-speed rotation. It has succeeded in providing a long-life drill that is free from bending. Therefore, the improvement of the support portion according to the present invention and its operation will be described in detail below.
まず、本発明の複合焼結材料の1つの特徴は硬質焼結部
と支持部との接合を硬質焼結部の焼結過程で形成するこ
とにある。このため支持部が製造中にダイヤモンド又は
高圧相型窒化硼素が安定な高温でしかも超高圧下にさら
される。WC−Coの焼結は通常真空下1300〜1500℃の温度
で行われ、一方ダイヤモンド又は高圧相型窒化硼素の焼
結は温度は同程度であるが、4万〜5万気圧の超高圧下
でなされる。従ってWC−Coは予め焼結されたものが用い
られるにせよ、硬質部と同時に焼結されるにせよこの超
高圧の影響を受ける。First, one feature of the composite sintered material of the present invention is that the joint between the hard sintered portion and the support portion is formed in the sintering process of the hard sintered portion. As a result, the diamond or the high-pressure phase type boron nitride is exposed to a stable high temperature and ultrahigh pressure during manufacturing of the support part. Sintering of WC-Co is usually performed under vacuum at a temperature of 1300 to 1500 ° C, while sintering of diamond or high pressure phase type boron nitride is at the same temperature, but under ultra high pressure of 40,000 to 50,000 atm. Made in. Therefore, WC-Co is affected by this ultra-high pressure regardless of whether a pre-sintered one is used or whether it is simultaneously sintered with the hard part.
本発明の複合焼結材料を製造するには予め焼結した支持
部を用いる場合の方が容易である。従って本発明者は色
々な種類の焼結済みのWC−Co合金を上記条件にさらして
みたところ、以下の現象を見い出した。In order to manufacture the composite sintered material of the present invention, it is easier to use a pre-sintered support part. Therefore, the present inventor found the following phenomenon when exposing various kinds of sintered WC-Co alloys to the above conditions.
一般にWC−Co合金の機械的特性はCo%とWC結晶粒度で決
まる。ところで、WC結晶の粒度が3μm以上の場合に
は、このWC結晶は超高圧加工により破壊され、その機械
的特性が大幅に変わってしまい一定の機械的特性を有す
る支持部の製造が困難となる。従って、支持部の超硬合
金のWC結晶の平均粒度を3μm以下とした。Generally, the mechanical properties of WC-Co alloys are determined by Co% and WC grain size. By the way, when the grain size of the WC crystal is 3 μm or more, the WC crystal is destroyed by ultra-high pressure processing, and its mechanical properties are significantly changed, which makes it difficult to manufacture a supporting portion having constant mechanical properties. . Therefore, the average grain size of the WC crystals of the cemented carbide of the supporting portion is set to 3 μm or less.
しかしながら、ダイヤモンド又は高圧相型窒化硼素の焼
結条件に於いて、WC結晶は液相Coとの濡れ性が極めて良
いので、破壊したWC結晶中に液相Coが侵入し破壊された
WCをCoが結合した形となるので、その機械的特性はかな
らずしも低下すると限らないことが本発明者等の実験で
確認された。However, under the sintering conditions of diamond or high-pressure phase boron nitride, the WC crystal has an extremely good wettability with the liquid phase Co, so that the liquid phase Co penetrates and is destroyed in the destroyed WC crystal.
It has been confirmed by experiments by the inventors of the present invention that the mechanical properties of WC are not necessarily deteriorated because Co is bound to Co.
例えば、従来の技術知識に従うと、平均粒度1μm以下
のWC−Co合金の場合、少量の大きなWC結晶が存在すると
この大きなWC結晶が破壊の起点になり強度が低下すると
考えられた。しかしながら、本発明者等の実験による
と、逆に超高圧加圧により処理後の強度が上昇する場合
がある。こうした強度上昇の現象は超硬合金中の結合金
属の含有量によって左右される。本発明者等の実験によ
ると、この強度上昇は、ダイヤモンド又は高圧相型窒化
硼素の焼結中の超高圧加圧により大きなWC結晶が破壊さ
れ、破壊されたWC結晶間に結合金属が侵入してこれらを
結合するためと考えられる。For example, according to the conventional technical knowledge, in the case of a WC-Co alloy having an average grain size of 1 μm or less, it was considered that the presence of a small amount of large WC crystals would cause the large WC crystals to be the starting point of fracture and reduce the strength. However, according to the experiments performed by the present inventors, the strength after the treatment may be increased due to the ultrahigh pressure. The phenomenon of such strength increase depends on the content of the binding metal in the cemented carbide. According to experiments conducted by the present inventors, this increase in strength is caused by the fact that large WC crystals are destroyed by ultra-high pressure application during the sintering of diamond or high-pressure phase boron nitride, and a bond metal penetrates between the destroyed WC crystals. It is thought that this is to combine these.
一方、超高圧加圧が完全に静水圧的になされるならば問
題ないが、実際にはその加圧を静水圧に近づける工夫を
加えているというのが工業生産における実状である。従
って、超高圧加圧下の超硬合金には無理な変形が加わる
と考えてよい。例えばWC−Co合金を例に考察すると、そ
の含有Co量が多ければ、その変形に合金が追随可能であ
るが、少なければ、最も変形の著しかった部分に微細亀
裂ないしは孔などの欠陥を生ずる可能性がある。On the other hand, if the ultra-high pressure is completely hydrostatically applied, there is no problem, but in reality, industrial production is devised so that the pressurization approaches hydrostatic pressure. Therefore, it can be considered that the cemented carbide under ultrahigh pressure is subjected to an unreasonable deformation. For example, considering a WC-Co alloy as an example, if the content of Co is large, the alloy can follow the deformation, but if it is small, defects such as fine cracks or holes can occur in the most deformed part. There is a nature.
超高圧高温加熱を色々なCo量の合金に加えた後その抗折
力を測定してみたところCo量が重量で7%以下の場合に
は、超高圧高温処理前に比べ抗折力値は低下すること、
12%以上の場合にはむしろ向上することを見い出した。After applying ultra high pressure and high temperature heating to alloys with various Co contents, the transverse rupture strength was measured. When the Co content was 7% or less by weight, the transverse rupture strength value was higher than that before the ultra high pressure high temperature treatment. To fall,
It has been found that if it exceeds 12%, it will rather improve.
7%以下の場合は超高圧によりWC結晶が破壊され、これ
にCoが追随できず欠陥を生じたためと考えられる。12%
以上の場合に、むしろ抗折力が向上した理由は次のごと
くと考えられる。When the content is 7% or less, it is considered that the WC crystal was destroyed by the ultrahigh pressure, and Co could not follow this, resulting in a defect. 12%
The reason why the transverse rupture strength is improved in the above cases is considered as follows.
WC−Co合金の破壊の起点は前述のごとく粗大なWC結晶、
空孔、異相といわれる。いま、異相は存在しないことを
処理前後に顕微鏡で観察しているので問題外とする。粗
大なWC結晶については前に述べた如くである。空孔とい
うのは数μmから数百μmの孔を指すがこれが外圧によ
ってつぶれ或いはCoにより充填されることがHIPの例か
ら容易に推測出来る。HIPの場合と本発明の複合焼結材
料の製造工程では処理温度は同一であり、本発明の場合
の方が圧力が一桁以上高いのでこの傾向がより助長され
ると考えられる。The origin of fracture of WC-Co alloy is coarse WC crystal as described above,
It is said that there are vacancies and foreign phases. Since it is observed with a microscope before and after the treatment that there is no foreign phase, it is out of the question. The coarse WC crystal is as described above. Voids are pores of several μm to several hundreds μm, but it can be easily inferred from the example of HIP that they are crushed by external pressure or filled with Co. It is considered that this tendency is further promoted because the treatment temperature is the same in the case of HIP and the manufacturing process of the composite sintered material of the present invention, and the pressure is higher by one digit or more in the case of the present invention.
Co%が12%より更に高い、例えば20%のWC−Co合金では
その抗折力の増加率が30%以上と大きかった。その抗折
力の増加率の高い原因を検討した結果次のことが分っ
た。With a WC-Co alloy having a Co% higher than 12%, for example 20%, the increase in transverse rupture strength was as large as 30% or more. As a result of examining the cause of the high increase rate of the transverse rupture strength, the following was found.
すなわち、WC−CoのCo相は通常FCC構造をなし、合金の
含有炭素量が低い場合には10%近くのWを固溶している
が一般には純Coに近い組成である。従って、一般にCo量
の高いWC−Co超硬合金は容易に変形し、このため歪をか
けていくと塑性変形し、いわゆる歪−応力曲線はなだら
かに水平に寝た形となる。この曲線が寝た形とならず直
線的に上昇推移すれば強度は高くなることになる。この
観点から高温且つ超高圧の条件下での処理後のCo相を調
べたところWが15%前後固溶していることが判明し、こ
れによりCo相が変形し難くなっていることが分った。こ
の理由は次の如く考えられる。That is, the Co phase of WC-Co usually has an FCC structure, and when the carbon content of the alloy is low, nearly 10% of W is solid-dissolved, but the composition is generally close to that of pure Co. Therefore, in general, a WC-Co cemented carbide having a high Co content is easily deformed, and therefore, when strained, it is plastically deformed, and a so-called strain-stress curve has a gently horizontal shape. If this curve does not have a lying shape and rises linearly, the strength will increase. From this point of view, when the Co phase after the treatment under the conditions of high temperature and ultra high pressure was examined, it was found that W was in solid solution at about 15%, and it was found that the Co phase was not easily deformed. It was. The reason for this is considered as follows.
すなわち、Co−W−C3元共晶からその共晶温度で析出す
るCo相は約20%のWを含有する。通常の焼結後の冷却で
はWはこの3元共晶からWC相上へ析出する。しかし本発
明の複合焼結材料の製造工程では硬質部の焼結終了後ま
ず加熱電源を切って冷却したのち除圧する。すなわちW
がCo相から析出しようとする時には、まだ超高圧下にあ
り、このような超高圧下では固体中の拡散速度は著しく
低下し、WC相上への析出が阻止される。このことは本発
明の複合焼結材料の支持部のWC−Co超硬合金中のCo相が
多くのWを固溶していることからも納得できる。従っ
て、本発明に於いては、通常ではその変形により使えな
い範囲の高含有量の結合金属を含むWC超硬合金が支持部
として用いられる。That is, the Co phase that precipitates from the Co-W-C ternary eutectic at that eutectic temperature contains about 20% W. During normal cooling after sintering, W precipitates from the ternary eutectic on the WC phase. However, in the manufacturing process of the composite sintered material of the present invention, after the sintering of the hard portion is completed, the heating power source is first turned off to cool and then the pressure is released. Ie W
When it is attempting to precipitate from the Co phase, it is still under ultra-high pressure, and under such ultra-high pressure, the diffusion rate in the solid is remarkably reduced, and the precipitation on the WC phase is prevented. This can be understood from the fact that the Co phase in the WC-Co cemented carbide of the support portion of the composite sintered material of the present invention is a solid solution of a large amount of W. Therefore, in the present invention, the WC cemented carbide containing a high content of the binding metal in a range that cannot be normally used due to its deformation is used as the supporting portion.
すなわち、本発明に従うと、支持部を構成する超硬合金
中の炭化物の平均粒度が3μm以下であり、また結合金
属量が7重量%以上である。That is, according to the present invention, the average particle size of the carbide in the cemented carbide forming the support portion is 3 μm or less, and the amount of the binding metal is 7% by weight or more.
更に、本発明の好ましい態様に従うと、支持部を構成す
る超硬合金中の炭化物の粒度が2μm以下であり、結合
金属量が12重量%以上である。Further, according to a preferred embodiment of the present invention, the grain size of the carbide in the cemented carbide forming the support portion is 2 μm or less, and the amount of binding metal is 12% by weight or more.
以下、本発明を実施例により説明する。Hereinafter, the present invention will be described with reference to examples.
実施例 添付図面の第3図(a)及び(b)は、それぞれ本発明
の複合焼結材料の外観を示す。Example FIGS. 3 (a) and 3 (b) of the accompanying drawings respectively show the appearance of the composite sintered material of the present invention.
第3図(a)に示す複合焼結材料円柱体23は硬質焼結部
21と支持部22とからなり、硬質焼結部21と支持部22とは
硬質焼結部21の焼結過程で一体に接合されている。The composite sintered material cylindrical body 23 shown in FIG. 3 (a) is a hard sintered portion.
The hard sintered portion 21 and the support portion 22 are integrally joined in the sintering process of the hard sintered portion 21.
他方、第3図(b)に示す複合焼結材料円柱体23では、
硬質焼結部21と支持部22とは、それらの間に中間接合層
24を介在させて接合している。On the other hand, in the composite sintered material cylindrical body 23 shown in FIG. 3 (b),
The hard sintered part 21 and the support part 22 have an intermediate bonding layer between them.
It is joined with 24 interposed.
次に本発明の複合焼結材料円柱体の製造方法を説明す
る。Next, a method for manufacturing the composite sintered material cylindrical body of the present invention will be described.
本出願人による特願昭59−120219号に詳細に記載の如
く、本発明者らは、まず断面積の大きな複合材料ブロッ
クのホットプレスを行って複合焼結体ブロックを製造
し、これを放電ワイヤカッティングで小断面の棒状体に
切断することにより小径で細長の、硬質な頭部を有する
複合焼結材料を与えることに成功したものである。As described in detail in Japanese Patent Application No. 59-120219 filed by the present applicant, the present inventors first hot-press a composite material block having a large cross-sectional area to manufacture a composite sintered body block, and discharge this. By cutting into a rod-shaped body having a small cross section by wire cutting, it has succeeded in providing a composite sintered material having a small diameter, an elongated shape, and a hard head.
すなわち、上記特願昭59−120219号に記載の方法では、
ダイヤモンド粉末または高圧相窒化硼素粉末を50%以上
含有する硬質焼結体用の第1の材料層と、該第1の材料
層の焼結過程で該第1の材料の硬質焼結体と接合する第
2の材料層とを同一のホットプレスコンテナ内に加圧方
向に重ねて装入し、高温高圧下でホットプレスして該第
1の材料層を焼結すると同時に、得られた硬質焼結体を
該第2の材料層側と接合せしめて、所定厚さの硬質焼結
体の層を有する複合材料ブロックを形成し、該複合材料
ブロックを放電ワイヤカッティング方法により材料層厚
方向に切断して、頭部に硬質焼結体を備える細長の複合
材料棒状体を2本以上切り取る。That is, in the method described in Japanese Patent Application No. 59-120219,
Bonding a first material layer for a hard sintered body containing 50% or more of diamond powder or high-pressure phase boron nitride powder, and a hard sintered body of the first material in a sintering process of the first material layer And the second material layer to be stacked are placed in the same hot press container in the pressing direction, and hot pressed under high temperature and high pressure to sinter the first material layer and at the same time to obtain the obtained hard-baked material. The composite is bonded to the second material layer side to form a composite material block having a layer of a hard sintered body having a predetermined thickness, and the composite material block is cut in the material layer thickness direction by a discharge wire cutting method. Then, two or more elongated composite rod-shaped bodies each having a hard sintered body on its head are cut out.
この複合材料をホットプレスして焼結するに際し、本発
明に従うと、複合材料ブロックの軸方向長さはその相当
直径の3倍、好ましくは2倍以下の必要がある。3倍を
越える軸方向長さの複合材料ブロックのホットプレスを
行うと複合材料ブロック内の圧力分布が変則的となり、
曲がりなどを生ずるからである。When this composite material is hot pressed and sintered, according to the present invention, the axial length of the composite material block should be 3 times, preferably 2 times or less than its equivalent diameter. When hot pressing a composite material block with an axial length exceeding 3 times, the pressure distribution in the composite material block becomes irregular,
This is because bending or the like occurs.
第3図に示す複合材料円柱体の切り出し方法を説明す
る。上述の如くホットプレスして得られた複合焼結体ブ
ロック33は、第4図(a)に示す如く、厚さ1mmのダイ
ヤモンド焼結体層31と、これに接合した超硬合金層32と
からなり、中間接合層を含む場合では第4図(b)示す
如くダイヤモンド焼結体層31と超硬合金層32とが中間接
合層34を介して接合されている。図示の例では円柱状の
複合焼結体ブロックを示しているが、複合焼結体ブロッ
クは円柱体でも角柱体でもよいことは勿論である。A method of cutting out the composite material cylindrical body shown in FIG. 3 will be described. The composite sintered body block 33 obtained by hot pressing as described above has a diamond sintered body layer 31 having a thickness of 1 mm and a cemented carbide layer 32 bonded thereto as shown in FIG. 4 (a). When the intermediate bonding layer is included, the diamond sintered body layer 31 and the cemented carbide layer 32 are bonded via the intermediate bonding layer 34 as shown in FIG. 4 (b). In the illustrated example, a cylindrical composite sintered body block is shown, but it goes without saying that the composite sintered body block may be a cylindrical body or a prismatic body.
これらの複合焼結体ブロックを第5図に示す如く、複合
焼結体ブロックと同軸方向の相当直径3mm以下の断面の
棒状体に放電ワイヤカッティング法により切断して第3
図(a)および(b)に示す如き硬質の頭部を有する複
合材料棒状体に切断する。As shown in FIG. 5, these composite sintered body blocks were cut into rod-shaped bodies having a cross-section with an equivalent diameter of 3 mm or less in the direction coaxial with the composite sintered body blocks by a discharge wire cutting method to form a third rod.
A composite rod having a hard head as shown in FIGS. (A) and (b) is cut.
この放電ワイヤカッティング法では、ワイヤと複合焼結
体ブロックとの間に高電圧をかけ、ワイヤを緊張した状
態で走行させてブロックを切断するものであり、その方
法の詳細は例えば米国特許第4,103,137号を参照された
い。In this discharge wire cutting method, a high voltage is applied between the wire and the composite sintered body block, and the wire is run in a tensioned state to cut the block, and the details of the method are described in, for example, U.S. Patent No. 4,103,137. See issue.
以下、本発明の頭部に硬質な焼結体を有する複合焼結材
料の具体的な製造例を説明する。Hereinafter, specific production examples of the composite sintered material having a hard sintered body on the head of the present invention will be described.
製造例1 外径18mm、内径14mm、高さ15mmのWC−12%Co超硬合金製
リング、外径14mm、高さ12mmのWC−12%Co超硬合金製円
柱ブロック、外径14mm、厚さ0.5mmのWC−12%Co超硬合
金製円板と粒径0.5μmのダイヤモンド粉末85%と残余
が粒径0.5μm以下のWC−15%Co超硬合金粉末よりなる
混合粉末を用意した。Production Example 1 WC-12% Co cemented carbide ring with outer diameter 18mm, inner diameter 14mm, height 15mm, WC-12% Co cemented carbide column block with outer diameter 14mm, height 12mm, outer diameter 14mm, thickness Prepared a mixed powder consisting of a 0.5 mm thick WC-12% Co cemented carbide disc, 85% diamond powder with a particle size of 0.5 μm, and the balance WC-15% Co cemented carbide powder with a particle size of 0.5 μm or less. .
超硬合金リングの内径に超硬合金円柱ブロックを挿入
し、超硬合金リング内面と超硬合金円柱ブロックの上面
とで形成される直径14mm、深さ3mmの凹所に前記混合ダ
イヤモンド粉末を充填後加圧して、混合粉末の高さを1.
5mmとし、超硬合金円板で蓋をした後、超高圧焼結装置
中に配置し、圧力55kb、温度1370℃の条件で15分間焼結
を行った。冷却後、減圧して取り出した封入容器の上部
超硬合金円板を研削により除去すると高さ12mmの超硬合
金支持部の上面に厚さ1mmの焼結ダイヤモンド層が接合
して形成され周囲に超硬合金製リングがやはり支持部及
び焼結ダイヤモンド層に結合した複合体ブロックが得ら
れた。Insert the cemented carbide column block into the inner diameter of the cemented carbide ring, and fill the recess of 14 mm in diameter and 3 mm in depth formed by the inner surface of the cemented carbide ring and the upper surface of the cemented carbide column block with the mixed diamond powder. Post-pressurize the height of the mixed powder to 1.
After making it 5 mm and covering it with a cemented carbide disc, it was placed in an ultra-high pressure sintering apparatus and sintered under conditions of a pressure of 55 kb and a temperature of 1370 ° C. for 15 minutes. After cooling, decompressing and removing the upper cemented carbide disk of the enclosed container removed by grinding, a sintered diamond layer with a thickness of 1 mm was formed on the upper surface of the cemented carbide support with a height of 12 mm and formed around it. A composite block was obtained in which the cemented carbide ring was also bonded to the support and the sintered diamond layer.
この複合体ブロックを第5図に示すように、放電ワイヤ
カット加工機に装着し、放電ワイヤカッティングして、
複合体ブロックの軸方向より直径1mm、長さ13mmの丸棒
で支持部は平均粒度2μmのWC−12%Co超硬合金よりな
り、その一端に長さ1mmの焼結ダイヤモンド層が固着形
成された円柱体を得た。As shown in FIG. 5, this composite block is mounted on an electric discharge wire cutting machine, and electric discharge wire cutting is performed.
A round bar with a diameter of 1 mm and a length of 13 mm from the axial direction of the composite block, the support part is made of WC-12% Co cemented carbide with an average grain size of 2 μm, and a 1 mm long sintered diamond layer is firmly formed on one end I got a cylinder.
製造例2 それぞれWC−12%Co超硬合金よりなる外径18mm、内径
14mm、高さ20mmのリング、外径14mm、高さ18mmのWC−
1%Cr3C2−20%Co円柱ブロック、外径14mm、厚さ1mm
の円板と、粒径3μmのダイヤモンド粉末90%と残余が
Co粉末よりなる混合粉末、粒径3μmの高圧相窒化硼素
(以下、立方晶型窒化硼素をCBNと略記する)粉末60%
と残余が(TiN−10重量%A1)の組成の粉末よりなる混
合粉末を用意した。Production Example 2 18 mm outer diameter and 18 mm inner diameter made of WC-12% Co cemented carbide
14mm, height 20mm ring, outer diameter 14mm, height 18mm WC-
1% Cr 3 C 2 -20% Co cylinder block, an outer diameter of 14 mm, 1mm thick
Disk and 90% diamond powder with a particle size of 3 μm and the rest
Mixed powder consisting of Co powder, high-pressure phase boron nitride having a particle size of 3 μm (hereinafter cubic boron nitride is abbreviated as CBN) powder 60%
Then, a mixed powder having a composition of which the balance is (TiN-10% by weight A1) was prepared.
超硬合金製円柱ブロックの上面に前記CBN混合粉末を溶
媒に溶かしたものを厚さ50μmに塗付した後、溶媒を加
熱除去し、この処理を行った超硬合金円柱ブロックを超
硬リング内径に挿入した。The CBN mixed powder dissolved in a solvent is applied to the upper surface of a cemented carbide column block to a thickness of 50 μm, and then the solvent is removed by heating, and the cemented carbide column block that has undergone this treatment is processed into a cemented carbide ring inner diameter. Inserted in.
次に、超硬合金リング内面とCBN混合粉末を塗布した超
硬合金円柱ブロックの上面とで形成される凹所に前記ダ
イヤモンド混合粉末を充填した後、加圧成型して厚さ1m
mのダイヤモンド混合粉末層を形成した後、超硬合金円
板で蓋をした。Next, after filling the diamond mixed powder in the recess formed by the inner surface of the cemented carbide ring and the upper surface of the cemented carbide columnar block coated with CBN mixed powder, pressure molding to a thickness of 1 m
After forming a diamond mixed powder layer of m, the lid was covered with a cemented carbide disc.
次にこの容器を超高圧焼結装置中に配置し、圧力55kb、
温度1400℃で10分間焼結を行った後、冷却、減圧して容
器を取り出した。容器の上部超硬合金円板を研削除去す
ると高さ18mmの超硬合金支持体の上面に厚さ0.5mmの焼
結ダイヤモンド層が厚さ25μmの焼結CBN層を介して接
合され、周囲に超硬合金リングが支持体及び焼結ダイヤ
モンド層に結合した複合体ブロックが得られた。Next, this container was placed in an ultra-high pressure sintering machine, and the pressure was 55 kb,
After sintering at a temperature of 1400 ° C. for 10 minutes, the container was taken out by cooling and reducing the pressure. When the upper cemented carbide disk of the container is ground away, a 0.5 mm thick sintered diamond layer is bonded to the upper surface of a 18 mm high cemented carbide support through a 25 μm thick sintered CBN layer, A composite block was obtained in which the cemented carbide ring was bonded to the support and the sintered diamond layer.
この複合体ブロックを放電ワイヤカット、加工機に装着
し、放電ワイヤカッティングにより複合体の軸方向より
直径0.3mm、長さ18.5mmの丸棒で支持部は平均粒度0.7μ
mの微細なWC−1%Cr3C2−20%Co超硬合金よりなり、
その一端に長さ0.5mmの焼結ダイヤモンド層が厚さ25μ
mの焼結CBN界面層を介して接合形成された円柱体を得
た。This composite block is mounted on a discharge wire cutting and processing machine, and by discharge wire cutting, a round bar with a diameter of 0.3 mm and a length of 18.5 mm is used from the axial direction of the composite, and the average particle size of the support is 0.7 μ
fine WC-1% of m Cr 3 C 2 consists -20% Co cemented carbide,
A 0.5 mm long sintered diamond layer is 25μ thick at one end.
As a result, a cylindrical body was obtained which was joined and formed through the sintered CBN interface layer of m.
製造例3 WC−0.5%VC−13%Co超硬合金よりなり、上面に直径20m
m、深さ3mmの円形凹所を有する外径24mm、高さ25mmの円
柱ブロック、外径20mm、厚さ0.5mmのWC−12%Co超硬合
金製円板と粒径0.5μmのダイヤモンド粉末80%と残余
が粒径0.5μm以下のWC−15%Co超硬合金粉末よりなる
ダイヤモンド混合粉末を用意した。Production Example 3 WC-0.5% VC-13% Co cemented carbide with a diameter of 20m on the upper surface
m, cylindrical block with an outer diameter of 24 mm and height of 25 mm with a circular recess of 3 mm, outer diameter of 20 mm, thickness of 0.5 mm WC-12% Co cemented carbide disc and diamond powder with a particle size of 0.5 μm A diamond mixed powder consisting of WC-15% Co cemented carbide powder with a particle size of 80% and the remainder of 0.5 μm or less was prepared.
このダイヤモンド混合粉末を前記超硬合金円柱ブロック
の上面凹所に充填後加圧して高さ2.3mmのダイヤモンド
混合粉末層を形成した。次にこの上に超硬合金円板で蓋
をした後、超高圧焼結装置内に配置し、圧力55kb、温度
1400℃で15分間焼結した。This diamond mixed powder was filled in the recess in the upper surface of the cemented carbide column block and then pressed to form a diamond mixed powder layer having a height of 2.3 mm. Next, after covering with a cemented carbide disc on this, place it in the ultra-high pressure sintering equipment, pressure 55 kb, temperature
Sintered at 1400 ° C for 15 minutes.
焼結後、封入容器を取り出し、上面の超硬合金蓋を研削
除去すると上面円形凹所に厚さ1.5mmの焼結ダイヤモン
ド層を有し、これが周囲の合金容器に強固に接合した複
合体ブロックが得られた。After sintering, take out the enclosed container and grind off the cemented carbide lid on the top surface to have a sintered diamond layer with a thickness of 1.5 mm in the circular recess on the top surface, which is a composite block firmly bonded to the surrounding alloy container. was gotten.
この複合体ブロックを放電ワイヤカット加工機に装着
し、放電ワイヤカッティングにより複合体ブロックの軸
方向より直径2mm、長さ23.5mmの丸棒で支持部は平均粒
度0.7μmのWC−0.5%VC−13%Co超硬合金よりなり、そ
の一端に長さ1.5mmの焼結ダイヤモンド層が固着形成さ
れた円柱体が得られた。This composite block was mounted on an electric discharge wire cutting machine, and by discharge wire cutting, a round bar with a diameter of 2 mm and a length of 23.5 mm was used from the axial direction of the composite block, and the support part had an average grain size of 0.7 μm WC-0.5% VC- A cylindrical body made of 13% Co cemented carbide and having a 1.5 mm long sintered diamond layer fixedly formed on one end thereof was obtained.
製造例4 外径18mm、内径14mm、高さ15mmのWC−12%Co超硬合金リ
ング、外径14mm、高さ12mmのWC−2%TaC−16%Co合金
よりなる円柱ブロック、外径14mm、厚さ0.5mmのWC−12
%Co超硬合金円板と粒径3μmのCBN85%と残余がTiN
0.82粉末とAl粉末を重量比で80:20として混合した後、1
000℃で30分真空炉内で加熱処理を行った後、0.3μmに
粉砕した粉末とよりなるCBN混合粉末を用意した。Production Example 4 WC-12% Co cemented carbide ring with an outer diameter of 18 mm, an inner diameter of 14 mm, and a height of 15 mm, an outer diameter of 14 mm, a cylindrical block of WC-2% TaC-16% Co alloy with a height of 12 mm, and an outer diameter of 14 mm , 0.5 mm thick WC-12
% Co Cemented Carbide Disc, CBN85% with 3μm grain size and the balance TiN
After mixing 0.82 powder and Al powder in a weight ratio of 80:20,
After heat treatment at 000 ° C. for 30 minutes in a vacuum furnace, a CBN mixed powder consisting of powder pulverized to 0.3 μm was prepared.
超硬合金リングの内径に円柱ブロックを挿入して、超硬
合金リング内面と円柱ブロック上面とで形成される直径
14mm、深さ3mmの凹所に前記CBN混合粉末を充填し、加圧
して高さ1.7mmのCBN混合粉末層を形成した。次いで、超
硬合金円板をかぶせて蓋をし、超硬合金容器全体を超高
圧焼結装置中に配置し、しかる後圧力50kb、温度1250℃
で20分間焼結を行った。Diameter formed by the inner surface of the cemented carbide ring and the upper surface of the cylinder block by inserting the cylinder block into the inner diameter of the cemented carbide ring
The CBN mixed powder was filled in a recess having a depth of 14 mm and a depth of 3 mm and pressed to form a CBN mixed powder layer having a height of 1.7 mm. Then, cover with a cemented carbide disc and cover, place the entire cemented carbide container in the ultra-high pressure sintering device, then pressure 50 kb, temperature 1250 ℃
And sintered for 20 minutes.
焼結後、超硬合金容器を取り出し、上面のWC−12%Co超
硬合金蓋を研削除去すると高さ12mmの支持部の上面に厚
さ1mmの焼結CBN層が接合して形成され周囲に超硬合金製
リングが支持体および焼結CBN層に接合した複合体ブロ
ックが得られた。After sintering, take out the cemented carbide container and grind off the WC-12% Co cemented carbide lid on the top surface to form a 1 mm thick sintered CBN layer on the top surface of the support part with a height of 12 mm. A composite block with a cemented carbide ring bonded to the support and the sintered CBN layer was obtained.
この複合体ブロックを放電ワイヤカット加工機に装着
し、放電ワイヤカッティングにより複合体ブロックの軸
方向より一辺が1mm、長さ13mmの角棒で支持部は平均粒
度1μmのWC−2%TaC−16%Co合金よりなり、その一
端に長さ1mmの焼結CBNが固着形成された細長角棒が得ら
れた。This composite block was mounted on an electric discharge wire cutting machine, and by electric discharge wire cutting, a square bar with a side of 1 mm and a length of 13 mm from the axial direction of the composite block was used to support WC-2% TaC-16 with an average grain size of 1 μm. % Sl alloy was obtained, and a long rectangular rod with a 1 mm long sintered CBN adhered to one end was obtained.
製造例5 外径40mm、内径36mm、高さ40mmのWC−12%Co超硬合金リ
ング、外径36mm、高さ34mmのWC−12%Co超硬合金円柱ブ
ロック、外径36mm、厚さ0.5mmのWC−12%Co超硬合金円
板と粒径3μmのCBN粉末60体積%と残余(TiN−10重量
%Al)の組成の粉末よりなるCBN混合粉末を用意した。Production Example 5 WC-12% Co cemented carbide ring with outer diameter 40mm, inner diameter 36mm, height 40mm, WC-12% Co cemented carbide column block with outer diameter 36mm, height 34mm, outer diameter 36mm, thickness 0.5 A WC-12% Co cemented carbide disc having a diameter of 3 mm, a CBN powder having a composition of 60% by volume of a CBN powder having a particle diameter of 3 μm and a balance (TiN-10 wt% Al) was prepared.
まずCBN混合粉末を直径36mm、厚さ2.5mmの円板に加圧成
型し、前記超硬合金リングの内径に下部より超硬合金円
板、CBN成型体、超硬合金円柱ブロック、CBN成型体、超
硬合金円板の順に積層配置し、セットした容器全体を超
高圧焼結装置中に配置して圧力40kb、温度1200℃で20分
間焼結した。First, the CBN mixed powder is pressure-molded into a disc having a diameter of 36 mm and a thickness of 2.5 mm, and the cemented carbide ring, the CBN molded body, the cemented carbide column block, and the CBN molded body are inserted into the inner diameter of the cemented carbide ring from the bottom. Then, the cemented carbide discs were laminated in this order, and the entire set container was placed in an ultrahigh pressure sintering apparatus and sintered at a pressure of 40 kb and a temperature of 1200 ° C. for 20 minutes.
焼結後取り出し、上下の超硬合金蓋を研削除去すると高
さ34mmの超硬合金円柱ブロックの上下面に直径36mm、厚
さ1.5mmの焼結CBN層が固着形成され、更に周囲が超硬合
金リングでおおわれた複合体ブロックが得られた。After taking out after sintering and grinding and removing the upper and lower cemented carbide lids, a sintered CBN layer with a diameter of 36 mm and a thickness of 1.5 mm is fixedly formed on the upper and lower surfaces of the cemented carbide column block with a height of 34 mm. A composite block covered with an alloy ring was obtained.
次に、この複合体ブロックを放電ワイヤカット加工機に
装着し、放電ワイヤカッティングにより複合ブロック軸
方向より、直径2.5mm、長さ37mmの丸棒でその両端に長
さ1.5mmの焼結CBN層が固着形成されものが得られた。Next, this composite block was mounted on an electric discharge wire cutting machine, and by a discharge wire cutting, from the axial direction of the composite block, a 2.5 mm diameter and 37 mm long round bar was used to form a sintered CBN layer of 1.5 mm length at both ends. Was adhered and formed.
この丸棒を更に長さ方向中央部で切断2分することによ
り直径2.5mm、長さ18mmの丸棒で支持部はWC−12%Co超
硬合金よりなり一端に長さ1.5mmの焼結CBN層が固着形成
された棒状体が得られた。This round bar is further cut at the center in the length direction and cut into two parts. The round bar has a diameter of 2.5 mm and a length of 18 mm. The supporting part is made of WC-12% Co cemented carbide and has a length of 1.5 mm at one end A rod-shaped body on which the CBN layer was firmly formed was obtained.
尚、本明細書中では%の表示は、特別に示さない限り体
積パーセントで示す。In the present specification,% is shown as volume percent unless otherwise specified.
適用例 本発明の複合焼結材料をドリルに適用した例を第6図に
示す。Application Example An example in which the composite sintered material of the present invention is applied to a drill is shown in FIG.
第6図(a)に示す如く、ドリルのシャンク25の先端
に、断面円形の複合焼結材料とほゞ同一径の孔26を穿設
する。この孔26に本発明の複合焼結材料23の支持部の一
端部を押し込み、固定する。このとき、孔26内にロウ材
を滴下しておき、ロウ付けしてもよい。As shown in FIG. 6 (a), a hole 26 having a circular cross section and a diameter substantially the same as that of the composite sintered material is formed at the tip of the shank 25 of the drill. One end of the supporting portion of the composite sintered material 23 of the present invention is pushed into this hole 26 and fixed. At this time, a brazing material may be dropped into the hole 26 and then brazing.
この第6図(a)に示す如く、シャンクに固定された複
合焼結材料23を刃付け加工し、第6図(b)に示す如き
ドリルを得た。この本発明の複合焼結材料を用いて製造
したドリルは複雑な電子ビーム溶接による接合部分を含
まず、しかも全体として強固且つ堅牢な構造である。従
って、ガラエポ基板の如き高性能のプリント基板に対し
ても高能率の穴あけを行うことが可能である。As shown in FIG. 6 (a), the composite sintered material 23 fixed to the shank was bladed to obtain a drill as shown in FIG. 6 (b). The drill manufactured by using the composite sintered material of the present invention does not include a complicated joint portion by electron beam welding, and has a strong and robust structure as a whole. Therefore, it is possible to perform highly efficient drilling even for a high-performance printed circuit board such as a glass epoxy substrate.
更に、本発明の複合焼結材料は断面が任意の形状にカッ
トされているので、断面が円形の場合は第6図(a)に
示す如くドリルのシャンクの先端に穿孔された穴に押し
込む際にも特別な加工を必要とせずに取り付けることが
でき、更に刃先加工の削り代も少量であり経済的であ
る。Furthermore, since the cross section of the composite sintered material of the present invention is cut into an arbitrary shape, when the cross section is circular, when it is pushed into the hole drilled at the tip of the shank of the drill as shown in FIG. 6 (a). Also, it can be installed without requiring special processing, and the cutting allowance for cutting the cutting edge is small, making it economical.
発明の効果 以上に説明の如く本発明は、特願昭59−120218号及び特
願昭59−120219号に記載の複合焼結材料に於いてその支
持部の組成を改善して強度および抗折力の高い支持部を
提供することに成功したものである。すなわち、本出願
人は特願昭59−120218号でガラエポ基板の如き難削性の
基板の穴あけを容易且つ高性能で実現する長寿命のドリ
ル用の複合焼結材料を開示したが、これに更に支持部の
改善を行い耐摩耗性および剛性を高め高速回転等の苛酷
な使用条件でも長寿命のドリル等を容易に製造可能とし
たものである。EFFECTS OF THE INVENTION As described above, the present invention improves the strength and flexural strength by improving the composition of the supporting portion in the composite sintered materials described in Japanese Patent Application No. 59-120218 and Japanese Patent Application No. 59-120219. It succeeded in providing a strong support. That is, the applicant has disclosed in Japanese Patent Application No. 59-120218 a composite sintered material for a drill having a long life, which realizes easy and high-performance drilling of a difficult-to-cut substrate such as a glass epoxy substrate. Further, by improving the support portion, wear resistance and rigidity are improved, and a long-life drill or the like can be easily manufactured even under severe use conditions such as high-speed rotation.
【図面の簡単な説明】 第1図は従来技術の複合ダイヤモンド焼結体の構造を示
す。 第2図は従来技術の複合焼結体を刃先に固着したドリル
を示す。 第3図(a)及び(b)はそれぞれ本発明の実施例の複
合焼結材料円柱体を示す。 第4図(a)および(b)はそれぞれ本発明の複合焼結
材料円柱体を切り出す前の状態の複合焼結材料ブロック
の斜視図である。 第5図は、複合材料ブロックから小断面の円柱体を切り
出す位置を示す。 第6図(a)は本発明の複合焼結材料円柱体をドリルの
シャンクに固着した状態を示し、第6図(b)はこのよ
うにして得られたドリルを示す。 (主な参照番号) 11……従来のダイヤモンド工具の焼結ダイヤモンド層、
12……超硬合金製の支持部、 13……従来の複合焼結ダイヤモンドのチップ、 15……シャンク、 21……本発明の複合焼結材料の硬質焼結部、 22……支持部、23……本発明の複合焼結材料、 24……中間接合部、 31……複合材料ブロックの硬質焼結部、 32……支持部、33……複合材料ブロック、 34……中間接合部、BRIEF DESCRIPTION OF THE DRAWINGS FIG. 1 shows the structure of a prior art composite diamond sintered body. FIG. 2 shows a drill in which a composite sintered body of the prior art is fixed to the cutting edge. 3 (a) and 3 (b) respectively show a composite sintered material cylinder according to an embodiment of the present invention. 4 (a) and 4 (b) are perspective views of the composite sintered material block before cutting out the composite sintered material columnar body of the present invention. FIG. 5 shows a position where a cylindrical body having a small cross section is cut out from the composite material block. FIG. 6 (a) shows the composite sintered material cylindrical body of the present invention fixed to the shank of the drill, and FIG. 6 (b) shows the drill thus obtained. (Main reference number) 11 …… Sintered diamond layer of conventional diamond tool,
12 …… Cemented Carbide Support, 13 …… Conventional Composite Sintered Diamond Tip, 15 …… Shank, 21 …… Hard Sintered Part of Composite Sintered Material of the Present Invention, 22 …… Support, 23 …… Composite sintered material of the present invention, 24 …… Intermediate joint, 31 …… Hard sintered portion of composite material block, 32 …… Support portion, 33 …… Composite material block, 34 …… Intermediate joint,
Claims (3)
末のいずれか一方または双方を50%以上含有する硬質焼
結部(21)と、この硬質焼結部の1端部に接合された支
持部(22)とで構成される複合焼結材料(23)からなる
工具または硬質頭部を有する耐磨耗性部品において、 硬質焼結部(21)と支持部(22)との接合は硬質焼結部
(21)の焼結過程で形成されたものであり、 複合焼結材料(23)の直径あるいは相当直径は3mm以下
であり、硬質焼結部(21)の軸方向長さは0.3〜2mmであ
り、支持部(22)の軸方向長さは硬質焼結部(21)の軸
方向長さの5倍以上であり、 支持部(22)はWCを主成分とした炭化物を鉄族金属で結
合した超硬合金からなり、この超硬合金中の炭化物の平
均粒度は3μm以下であり、また、結合金属はCoであ
り、その量は7重量%以上であり、 硬質焼結部(21)のダイヤモンド粉末または高圧相窒化
硼素粉末の平均粒度は10μm以下である、 ことを特徴とする工具または硬質頭部を有する耐磨耗性
部品。1. A hard sintered part (21) containing 50% or more of either or both of diamond powder and high-pressure phase boron nitride powder, and a support part (1) joined to one end of the hard sintered part (21). 22) and a tool made of a composite sintered material (23) composed of and a wear-resistant component having a hard head, the hard sintered part (21) and the support part (22) are joined together by hard sintering. It was formed during the sintering process of the part (21), the composite sintered material (23) has a diameter or equivalent diameter of 3 mm or less, and the hard sintered part (21) has an axial length of 0.3 to 2 mm. The axial length of the supporting portion (22) is 5 times or more the axial length of the hard sintered portion (21), and the supporting portion (22) is made of a carbide containing WC as an iron group metal. Made of cemented carbide, the average grain size of carbides in this cemented carbide is 3 μm or less, and the bonding metal is Co. Not less than%, diamond powder or average particle size of the high-pressure phase boron nitride powder is 10μm or less, abrasion resistant component with a tool or a hard head, characterized in that the hard sintered section (21).
あり、結合金属の量が12重量%以上である特許請求の範
囲第1項に記載の工具または硬質頭部を有する耐磨耗性
部品。2. A tool according to claim 1, wherein the grain size of carbides in the cemented carbide is 2 μm or less, and the amount of binding metal is 12% by weight or more, or wear resistance having a hard head. Sex parts.
が厚さが0.5mm以下の中間接合層を介してなされている
特許請求の範囲第1項または第2項に記載の工具または
硬質頭部を有する耐磨耗性部品。3. The method according to claim 1 or 2, wherein the hard sintered part (21) and the supporting part (22) are bonded to each other through an intermediate bonding layer having a thickness of 0.5 mm or less. Abrasion resistant component having the described tool or hard head.
Priority Applications (7)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP59163095A JPH0742489B2 (en) | 1984-08-02 | 1984-08-02 | Abrasion resistant parts with tool or hard head made of composite sintered material |
| CA000483612A CA1286510C (en) | 1984-06-12 | 1985-06-11 | Stick of composite materials and process for preparation thereof |
| AT85304135T ATE49147T1 (en) | 1984-06-12 | 1985-06-11 | ROD MADE OF COMPOSITE MATERIALS AND METHOD FOR ITS MANUFACTURE. |
| EP85304135A EP0168953B2 (en) | 1984-06-12 | 1985-06-11 | Stick of composite materials and process for preparation thereof |
| KR1019850004091A KR920001585B1 (en) | 1984-06-12 | 1985-06-11 | Stick compositie materials and process for preparation thereof |
| DE8585304135T DE3575092D1 (en) | 1984-06-12 | 1985-06-11 | ROD FROM COMPOSITE MATERIALS AND METHOD FOR THEIR PRODUCTION. |
| US07/231,644 US4880707A (en) | 1984-06-12 | 1988-08-10 | Stick of composite materials and process for preparation thereof |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP59163095A JPH0742489B2 (en) | 1984-08-02 | 1984-08-02 | Abrasion resistant parts with tool or hard head made of composite sintered material |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS6141703A JPS6141703A (en) | 1986-02-28 |
| JPH0742489B2 true JPH0742489B2 (en) | 1995-05-10 |
Family
ID=15767084
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP59163095A Expired - Fee Related JPH0742489B2 (en) | 1984-06-12 | 1984-08-02 | Abrasion resistant parts with tool or hard head made of composite sintered material |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPH0742489B2 (en) |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB201010061D0 (en) | 2010-06-16 | 2010-07-21 | Element Six Ltd | Rotary machine tools |
Family Cites Families (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS567603U (en) * | 1979-06-25 | 1981-01-23 | ||
| JPS5672105A (en) * | 1979-11-13 | 1981-06-16 | Toshiba Tungaloy Co Ltd | Composite cutting body |
| JPS5681605A (en) * | 1979-12-06 | 1981-07-03 | Toshiba Tungaloy Co Ltd | Production of composite cutting body |
| JPS5681606A (en) * | 1979-12-06 | 1981-07-03 | Toshiba Tungaloy Co Ltd | Production of composite cutting body |
| JPS58120406A (en) * | 1982-01-14 | 1983-07-18 | Nippon Oil & Fats Co Ltd | High hardness sintered tool |
-
1984
- 1984-08-02 JP JP59163095A patent/JPH0742489B2/en not_active Expired - Fee Related
Also Published As
| Publication number | Publication date |
|---|---|
| JPS6141703A (en) | 1986-02-28 |
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