JPH02268909A - Plug for manufacturing seamless steel tube - Google Patents
Plug for manufacturing seamless steel tubeInfo
- Publication number
- JPH02268909A JPH02268909A JP9065289A JP9065289A JPH02268909A JP H02268909 A JPH02268909 A JP H02268909A JP 9065289 A JP9065289 A JP 9065289A JP 9065289 A JP9065289 A JP 9065289A JP H02268909 A JPH02268909 A JP H02268909A
- Authority
- JP
- Japan
- Prior art keywords
- plug
- molybdenum
- core material
- particles
- life
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
- 229910000831 Steel Inorganic materials 0.000 title claims abstract description 23
- 239000010959 steel Substances 0.000 title claims abstract description 23
- 238000004519 manufacturing process Methods 0.000 title claims abstract description 19
- 229910052750 molybdenum Inorganic materials 0.000 claims abstract description 53
- 239000011162 core material Substances 0.000 claims abstract description 45
- 239000002245 particle Substances 0.000 claims abstract description 42
- 239000000463 material Substances 0.000 claims abstract description 32
- 239000000919 ceramic Substances 0.000 claims abstract description 20
- 239000002344 surface layer Substances 0.000 claims abstract description 14
- 239000000956 alloy Substances 0.000 claims abstract description 12
- 239000002131 composite material Substances 0.000 claims abstract description 10
- ZOKXTWBITQBERF-UHFFFAOYSA-N Molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 claims description 55
- 239000011733 molybdenum Substances 0.000 claims description 52
- 229910045601 alloy Inorganic materials 0.000 claims description 10
- 238000005096 rolling process Methods 0.000 abstract description 7
- 229910052751 metal Inorganic materials 0.000 abstract description 5
- 239000002184 metal Substances 0.000 abstract description 5
- 229910001315 Tool steel Inorganic materials 0.000 abstract description 3
- 230000003628 erosive effect Effects 0.000 abstract description 3
- 229910001182 Mo alloy Inorganic materials 0.000 abstract description 2
- 238000013329 compounding Methods 0.000 abstract 1
- 238000005553 drilling Methods 0.000 description 23
- 238000000034 method Methods 0.000 description 20
- 239000011247 coating layer Substances 0.000 description 13
- 239000010410 layer Substances 0.000 description 8
- 239000000843 powder Substances 0.000 description 8
- 229910000851 Alloy steel Inorganic materials 0.000 description 7
- 230000000694 effects Effects 0.000 description 6
- UQSXHKLRYXJYBZ-UHFFFAOYSA-N Iron oxide Chemical compound [Fe]=O UQSXHKLRYXJYBZ-UHFFFAOYSA-N 0.000 description 4
- 238000002156 mixing Methods 0.000 description 4
- 239000002775 capsule Substances 0.000 description 3
- 239000011651 chromium Substances 0.000 description 3
- 230000007423 decrease Effects 0.000 description 3
- 230000001788 irregular Effects 0.000 description 3
- 238000003754 machining Methods 0.000 description 3
- 238000000465 moulding Methods 0.000 description 3
- PXHVJJICTQNCMI-UHFFFAOYSA-N nickel Substances [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 3
- -1 061 Inorganic materials 0.000 description 2
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 description 2
- GWEVSGVZZGPLCZ-UHFFFAOYSA-N Titan oxide Chemical compound O=[Ti]=O GWEVSGVZZGPLCZ-UHFFFAOYSA-N 0.000 description 2
- 238000005422 blasting Methods 0.000 description 2
- 229910052804 chromium Inorganic materials 0.000 description 2
- 239000006185 dispersion Substances 0.000 description 2
- 230000005484 gravity Effects 0.000 description 2
- 238000010438 heat treatment Methods 0.000 description 2
- 238000005304 joining Methods 0.000 description 2
- 238000002844 melting Methods 0.000 description 2
- 230000008018 melting Effects 0.000 description 2
- 229910052759 nickel Inorganic materials 0.000 description 2
- 238000007751 thermal spraying Methods 0.000 description 2
- 229910052772 Samarium Inorganic materials 0.000 description 1
- 230000002411 adverse Effects 0.000 description 1
- 229910000963 austenitic stainless steel Inorganic materials 0.000 description 1
- 239000010953 base metal Substances 0.000 description 1
- 238000005266 casting Methods 0.000 description 1
- 239000003795 chemical substances by application Substances 0.000 description 1
- UOUJSJZBMCDAEU-UHFFFAOYSA-N chromium(3+);oxygen(2-) Chemical class [O-2].[O-2].[O-2].[Cr+3].[Cr+3] UOUJSJZBMCDAEU-UHFFFAOYSA-N 0.000 description 1
- 238000000576 coating method Methods 0.000 description 1
- 238000009694 cold isostatic pressing Methods 0.000 description 1
- 238000005336 cracking Methods 0.000 description 1
- 239000013078 crystal Substances 0.000 description 1
- 238000005520 cutting process Methods 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000007872 degassing Methods 0.000 description 1
- 238000009826 distribution Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 239000002360 explosive Substances 0.000 description 1
- 238000005242 forging Methods 0.000 description 1
- 108010061175 high potential iron-sulfur protein Proteins 0.000 description 1
- 150000001247 metal acetylides Chemical class 0.000 description 1
- 229910001235 nimonic Inorganic materials 0.000 description 1
- 150000004767 nitrides Chemical class 0.000 description 1
- 238000007517 polishing process Methods 0.000 description 1
- 238000004663 powder metallurgy Methods 0.000 description 1
- 238000010008 shearing Methods 0.000 description 1
- 238000005245 sintering Methods 0.000 description 1
- 238000007711 solidification Methods 0.000 description 1
- 230000008023 solidification Effects 0.000 description 1
- 239000007921 spray Substances 0.000 description 1
- 229910000601 superalloy Inorganic materials 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21B—ROLLING OF METAL
- B21B25/00—Mandrels for metal tube rolling mills, e.g. mandrels of the types used in the methods covered by group B21B17/00; Accessories or auxiliary means therefor ; Construction of, or alloys for, mandrels or plugs
Abstract
Description
【発明の詳細な説明】
〔産業上の利用分野〕
この発明は継目無し鋼管の製造に使用されるプラグに関
するものである。DETAILED DESCRIPTION OF THE INVENTION [Field of Industrial Application] This invention relates to a plug used in the manufacture of seamless steel pipes.
継目無し鋼管の製造工程においては、穿孔工程、圧延工
程(エロンゲータ、プラグミル)、磨管工程(リーラ)
で、各種の形状のプラグが用いられている。これらのプ
ラグの表面は穿孔あるいは圧延の際、高温下で高圧力や
高剪断力を受けるため、しばしば摩耗、溶損、焼付き等
を起こしていた。In the manufacturing process of seamless steel pipes, the drilling process, rolling process (elongator, plug mill), polishing process (reeler)
Various shapes of plugs are used. During drilling or rolling, the surfaces of these plugs are subjected to high pressure and high shear forces at high temperatures, which often causes wear, erosion, seizure, etc.
この結果、プラグの寿命(耐用度)を縮めて耐用度に問
題があるばかりでなく、得られた鋼管の内面品質に悪影
響を及ぼしていた。そこで、プラグの耐用度向上のため
に、いくつかの発明がなされている。As a result, not only the life (durability) of the plug was shortened and there was a problem with its durability, but also the quality of the inner surface of the obtained steel pipe was adversely affected. Therefore, several inventions have been made to improve the durability of plugs.
一般に、継目無し鋼管の材料としての綱片には低合金鋼
と高合金鋼がある。低合金鋼の穿孔には、従来から0.
3%C−3%Cr−1%Ni系低合金鋼からなるプラグ
本体の表面に、酸化物層を生成させたプラグが使用され
ている。In general, the steel pieces used as materials for seamless steel pipes include low-alloy steel and high-alloy steel. Conventionally, 0.
A plug is used in which an oxide layer is formed on the surface of a plug body made of 3%C-3%Cr-1%Ni-based low alloy steel.
例えば、特公昭5B−19363号公報においては熱処
理を施すことにより、そして、特公昭59−13924
号公報においては鉄酸化物を主体とした粉末を溶射する
ことによりプラグ本体の表面に、酸化物層を生成させて
いる。前記プラグによれば、クロム含有量が2.25w
t%までの低合金鋼からなる鋼片から4〜8mのホロー
ピースを調製する場合、500〜1500回の穿孔に耐
えられ、プラグ寿命を延長することができる。For example, in Japanese Patent Publication No. 5B-19363, by applying heat treatment, and in Japanese Patent Publication No. 59-13924,
In the publication, an oxide layer is formed on the surface of the plug body by thermal spraying a powder mainly composed of iron oxide. According to the plug, the chromium content is 2.25w.
When preparing a 4-8 m hollow piece from a steel billet made of low-alloy steel up to t%, it can withstand 500-1500 drillings and extend the plug life.
しかしながら、クロム含有1113wt%以上のCr鋼
、オーステナイト系ステンレス鋼のような高合金鋼の綱
片を穿孔する場合には、これらの鋼片の高温強度が高い
ことや、鋼片表面にクロム酸化物が生成し綱片からプラ
グ表面への鉄酸化物の供給が断たれることから、プラグ
の焼付きが著しくなり、第4図に示すようにプラグ1の
溶損、焼付きが激しい。従って、プラグの寿命は長いも
のでも5回程度であり、場合によっては1回の穿孔で使
用を中止しなければならないことも少なくなかった。However, when drilling a piece of high-alloy steel such as Cr steel with a chromium content of 1113 wt% or more or austenitic stainless steel, it is important to note that these steel pieces have high high-temperature strength and that chromium oxides are present on the surface of the steel piece. As a result, the supply of iron oxide from the rope to the plug surface is cut off, resulting in severe seizure of the plug, and as shown in FIG. 4, the plug 1 undergoes severe melting and seizure. Therefore, the lifespan of a plug is only about five times at most, and in some cases, it is often necessary to stop using it after one puncture.
さらに、プラグは穿孔における材料のメタルフローに対
し理想的な形に設計されているにもかかわらず、穿孔中
にプラグ先端部が消耗してプラグの先端の後退を生じて
いた。その結果、プラグ先端に材料が当接するまでの時
間が延び、これによってプラグ先端圧下率が増大し、材
料が回転鍛造割れを起こす可能性が増して、ホローピー
スの内面品質低下を招来していた。Furthermore, although the plug is designed to be ideal for metal flow of material during drilling, the plug tip wears out during drilling, resulting in retraction of the plug tip. As a result, the time it takes for the material to come into contact with the plug tip increases, which increases the plug tip reduction ratio, increases the possibility that the material will cause rotary forging cracks, and causes a decline in the inner surface quality of the hollow piece.
最近、これらの高合金鋼の鋼片を穿孔するために、各種
の耐熱合金製のプラグを使用する動きがある。このプラ
グの材料には高温強度で耐焼付き性の高い材料である、
モリブデンを適用することが多い。Recently, there has been a movement to use plugs made of various heat-resistant alloys to drill holes in these high-alloy steel billets. The material of this plug is a material with high temperature strength and high seizure resistance.
Molybdenum is often applied.
しかしながら、モリブデン類のプラグの場合には、その
材料費が高価であるばかりでな(、難削材料であること
、プラグ形状が複雑であることなどにより機械加工費が
高くなり、プラグ製作費が非常に高くつくという問題が
あった。さらに、モリブデンは、鋼の1.3倍の比重を
有するために、モリブデンからなるプラグは重くなり、
作業性の低下を招く。その上、モリブデンは鋼の3倍以
上の熱伝導率を有するために、プラグ後部でプラグにか
かる力を支持するためのマンドレルバ−またはその装着
部において多大な温度上昇を招き、マンドレルバ−の変
形やプラグとの焼付きなどの弊害を生じた。However, in the case of plugs made of molybdenum, not only are the material costs expensive (the machining costs are high due to the difficult-to-cut materials and the complicated shape of the plugs, resulting in high plug production costs). There was a problem that it was very expensive.Furthermore, molybdenum has a specific gravity 1.3 times that of steel, so a plug made of molybdenum is heavy.
This leads to a decrease in work efficiency. Furthermore, because molybdenum has a thermal conductivity more than three times that of steel, it causes a large temperature rise in the mandrel bar that supports the force applied to the plug at the rear of the plug, or in its mounting area, causing deformation of the mandrel bar. This caused problems such as seizure with the plug.
この問題点を解決する方法の一つにプラグ表面にモリブ
デン層を被覆する手法がある。例えば、特開昭61−2
86077号公報においては溶射と熱間等方圧加圧処理
により、特開昭62−50009号公報、特開昭62−
238011号公報においてはカプセルに封入後熱間等
方圧加圧処理により、モリブデン溶射層や粉末層をプラ
グ表面に被覆させることを提案している。One method for solving this problem is to coat the plug surface with a molybdenum layer. For example, JP-A-61-2
In JP-A No. 86077, thermal spraying and hot isostatic pressure treatment were used to obtain the results of JP-A-62-50009 and JP-A-62-
Publication No. 238011 proposes that the surface of the plug be coated with a molybdenum thermal spray layer or powder layer by hot isostatic pressure treatment after being encapsulated in a capsule.
[発明が解決しようとする課題]
これらの提案は、先に示したモリブデンプラグの問題点
を解決をしている。しかし、モリブデン及びモリブデン
合金は室温で非常に脆弱なため、穿孔初期にかかる衝撃
力により簡単に破壊したり、穿孔作業を進めているうち
に被穿孔材から伝わる熱による組織の粗大化が強度低下
につながり、遂には破壊してしまうという問題点があっ
た。[Problems to be Solved by the Invention] These proposals solve the problems of the molybdenum plugs mentioned above. However, molybdenum and molybdenum alloys are very brittle at room temperature, so they can easily break due to the impact force applied during the initial stage of drilling, and as the drilling process progresses, the structure becomes coarser due to heat transmitted from the material to be drilled, reducing its strength. There was a problem in that it led to this, and eventually it was destroyed.
発明者らもモリブデンプラグの研究の中でこの室温で脆
性な点を問題視しており、いくつかの改善策をとったが
、デイメリットも多かった。In their research on molybdenum plugs, the inventors also recognized this brittleness at room temperature as a problem, and took several measures to improve it, but there were many disadvantages as well.
本発明は、低合金鋼や耐熱鋼製のプラグにみられる溶損
や焼付き、モリブデン類のプラグにみられるマンドレル
バ−への熱影響や高比重による作業性の低下、モリブデ
ン層を有するプラグにみられる室温における脆性や組織
の粗大化により生ずる割れといった問題点を解決し、高
寿命で、しかも、内面品質が良好なホローピースを安定
して製造することができる継目無し鋼管製造用プラグを
提供することを目的としている。The present invention addresses the problems of melting damage and seizure seen in plugs made of low-alloy steel and heat-resistant steel, thermal effects on the mandrel bar and reduction in workability due to high specific gravity seen in plugs made of molybdenum, and plugs with a molybdenum layer. To provide a seamless steel pipe manufacturing plug that solves problems such as brittleness at room temperature and cracks caused by coarsening of the structure, and can stably manufacture hollow pieces with a long life and good inner surface quality. The purpose is to
(課題を解決するための手段〕
本発明はかかる目的を達成するべくなされたものであり
、本発明者らはプラグをモリブデンまたはモリブデン基
合金にセラミック粒子を分散させた複合材よりなる被穿
孔物と接触する表面層と、他の材料よりなる芯材より構
成することによりこの目的を達成することに成功したも
のである。(Means for Solving the Problems) The present invention has been made to achieve the above object, and the present inventors have developed a plug made of a composite material in which ceramic particles are dispersed in molybdenum or a molybdenum-based alloy. This goal was successfully achieved by comprising a surface layer in contact with the core material and a core material made of another material.
プラグの形状は通常は略弾頭形状であり、底面にはマン
ドレルを取り付ける嵌合穴、嵌合突起等が設けられる。The shape of the plug is usually approximately bullet-shaped, and the bottom surface is provided with a fitting hole, a fitting protrusion, etc. for attaching a mandrel.
頭部は半球形のばか傘形等のものも知られている。本発
明のプラグの形状はこれらに限定されるものではなく公
知の如何なる形状であってもよい。It is also known that the head is hemispherical or umbrella-shaped. The shape of the plug of the present invention is not limited to these, and may be any known shape.
このプラグは少なくとも、被穿孔物と接触する表面層と
該表面層の内面側において接触している芯材よりなって
いる。表面層はプラグの外表面全体に設けられていても
よく、穿孔によって損傷を生じやすい部分のみに設けら
れていてもよい。This plug consists of at least a surface layer that contacts the object to be drilled, and a core material that is in contact with the inner surface of the surface layer. The surface layer may be provided over the entire outer surface of the plug or only in areas susceptible to damage by perforation.
芯材の表面層と接する面に凹凸を設けることによって穿
孔中に被穿孔物の回転力から受ける反力による剪断を凹
凸部分に持たせてプラグの先端変形、割れ等を防止する
ことができる。この凹凸形状はショツトブラスト面のよ
うな浅い凹凸では不十分で、ある程度の深さを持った丸
や三角や四角のクレータ−状や円形や三角や四角の溝形
状が好ましい。上記の凹みや溝でなく突起や突条であっ
てもよいがその場合表面層の厚みを増加させるデメリッ
トがある。凹凸の大きさすなわち径や巾や深さはプラグ
の大きさにも依存するが、プラグ径に対する相対値は0
.005〜0,5程度で十分効果が見出せるが実用上は
0.05〜0.2程度が好ましい。By providing unevenness on the surface that contacts the surface layer of the core material, the uneven portion can absorb shear due to the reaction force received from the rotational force of the object to be drilled during drilling, thereby preventing deformation and cracking of the tip of the plug. A shallow unevenness such as a shot blast surface is insufficient for this uneven shape, and a round, triangular or square crater shape or a circular, triangular or square groove shape with a certain depth is preferable. Protrusions or protrusions may be used instead of the above-mentioned depressions and grooves, but in this case there is a disadvantage of increasing the thickness of the surface layer. The size of the unevenness, that is, the diameter, width, and depth, also depends on the size of the plug, but the relative value to the plug diameter is 0.
.. Although a sufficient effect can be found at about 0.005 to 0.5, it is practically preferable to use about 0.05 to 0.2.
凹凸の分布は不規則であってもよいが、等間隔に並んで
いる状態が好ましい。また、溝のコーナー部は応力集中
を避けるためにアールを設けるのが好ましい。Although the distribution of the unevenness may be irregular, it is preferable that the unevenness be arranged at equal intervals. Further, it is preferable that the corner portions of the grooves be rounded to avoid stress concentration.
芯材は室温から1300°Cの線膨張係数が3.5X1
0−’〜13X10−6/’Cであれば金属、合金、セ
ラミックスの別を問わないが、芯材に凹凸形状を施す場
合はモリブデンまたはモリブデン基合金よりも熱膨張係
数の高い、つまり20°Cで4.8xlO−6/’C以
上、1300°Cで7.4xlO−”/”C以上の熱膨
張係数を有した材料を用いるのが好ましい。例えば5K
061等に代表される熱間工具鋼やNimonicやN
imoiyal等の超合金や更に高温強度の高いTiB
t、 Zr0t等のセラミックスがある。モリブデンよ
りも熱膨張係数の大きな材質を芯材に適用し、かつ凹凸
形状を四角い溝状とした場合には、溝に径方向の切込が
あるため製作時の)TIP後の冷却の際にモリブデンと
芯材の熱膨張係数の差により溝側面の両者界面に圧縮応
力が働き、両者が強固に焼嵌め接合される利点がある。The core material has a linear expansion coefficient of 3.5X1 from room temperature to 1300°C.
It does not matter whether it is a metal, alloy, or ceramic as long as it is 0-' to 13X10-6/'C, but if the core material is to have an uneven shape, use a material with a higher coefficient of thermal expansion than molybdenum or molybdenum-based alloys, that is, 20° It is preferable to use a material having a thermal expansion coefficient of 4.8xlO-6/'C or higher at C and 7.4xlO-"/"C or higher at 1300°C. For example, 5K
Hot work tool steels such as 061, Nimonic and N
Superalloys such as imoiyal and TiB with even higher high temperature strength
There are ceramics such as Zr0t and Zr0t. If a material with a larger coefficient of thermal expansion than molybdenum is used for the core material and the uneven shape is made into a square groove, the groove will have radial cuts, so it will be difficult to cool down after TIP (during production). Due to the difference in thermal expansion coefficient between molybdenum and the core material, compressive stress acts on the interface between the two on the side surfaces of the groove, which has the advantage of firmly shrink-fitting the two.
これらを凹凸形状の芯材に仕上げる方法には、単にビレ
ットから切り出す機械加工法のほかに、鋳造法や、これ
らの材質の粉末を成形後焼結する粉末冶金法がある。Methods for finishing these materials into uneven core materials include a machining method in which the billet is simply cut out, a casting method, and a powder metallurgy method in which powders of these materials are molded and then sintered.
次に、このようにして製作した芯材の表面にモリブデン
またはモリブデン基合金にセラミ・ンク粒子を分散した
複合材を被覆する。母材のモリブデンまたはモリブデン
基合金は高温における潤滑性及び強度特性に優れたもの
であればよく、純モリブデンのほか例えば、TZM(0
,5朽tχTi−0,07れχZr−0.05wtXC
−Ba1.Mo)、 TZC(1,0朽tχTi−0
,14ivtχZr−0,1wtχC−Ba1.Mo)
、 ZtlM(0,72wtXZr−0,14wtX
tlf−0,05wtχC−Ba1.Mo)、 Ml
(C(1,OwtχHf−0,05WtχC−Ba1.
Mo)等も利用できる。Next, the surface of the core material thus produced is coated with a composite material in which ceramic ink particles are dispersed in molybdenum or a molybdenum-based alloy. The base material molybdenum or molybdenum-based alloy may be any material that has excellent lubricity and strength properties at high temperatures, and in addition to pure molybdenum, for example, TZM (0
,5 decaytχTi-0,07reχZr-0.05wtXC
-Ba1. Mo), TZC (1,0 decaytχTi-0
, 14ivtχZr-0, 1wtχC-Ba1. Mo)
, ZtlM(0,72wtXZr-0,14wtX
tlf-0,05wtχC-Ba1. Mo), Ml
(C(1, OwtχHf-0,05WtχC-Ba1.
Mo) etc. can also be used.
セラミック粒子は各種酸化物、炭化物、窒化物、硼化物
のうちの一種もしくは二種以上の組み合せが可能である
が、周期律表のma族またはIVa族の元素の酸化物の
中から選出するのが好ましい。Ceramic particles can be made of one or a combination of various oxides, carbides, nitrides, and borides; is preferred.
好ましいセラミック粒子の例として、ZrO□、Ce、
Oly、o、、Ah(h、TiO2,Lag’s、Sm
103などを挙げることができる。粒形は一般の粒状の
ばか繊維状等であってもよい。セラミック粒子の粒径は
粒状の場合には0.01〜5n程度、好ましくは0.0
2〜1n程度が適当である。また、分散量は体積%で1
〜20%程度がよく、好ましくは5〜10%程度である
。Examples of preferred ceramic particles include ZrO□, Ce,
Oly, o,, Ah(h, TiO2, Lag's, Sm
103, etc. The particle shape may be general granular, fibrous, or the like. The particle size of ceramic particles is about 0.01 to 5n in the case of granular particles, preferably 0.0
Approximately 2 to 1n is appropriate. In addition, the amount of dispersion is 1% by volume.
It is preferably about 20%, preferably about 5 to 10%.
セラミックのモリブデンまたはモリブデン基台金へのセ
ラミック粒子の分散はモリブデンまたはモリブデン基合
金の粒子と均一混合することによって行なう。モリブデ
ンまたはモリブデン基合金の粒径は0.5〜10−程度
が適当であり、1〜5μm程度が好ましい。Dispersion of the ceramic particles in the ceramic molybdenum or molybdenum base metal is carried out by homogeneous mixing with particles of molybdenum or molybdenum-based alloy. The grain size of the molybdenum or molybdenum-based alloy is suitably about 0.5 to 10 μm, preferably about 1 to 5 μm.
被覆方法には、ビレットから機械加工により切り出した
のち、芯材にHIPIP処理嵌め等により接合させたり
する方法のほかに、セラミック粒子を分散させたモリブ
デンまたはモリブデン基合金の粉末を固化接合する焼結
HIP法、キャニングHIP法、爆発成形法(衝撃成形
法)等があるが、他のいかなる固化技術を応用してもよ
い。このうちキャニングHIP法を簡単に説明すると次
のようになる。まず、粉末を冷間静水圧加圧(CIP)
等の成形方法で成形する。次にこれをメタルカプセルに
挿入し、真空加熱脱気により十分乾燥した後、カプセル
内に真空封入し、)(IP処理を施す方法である。Coating methods include cutting the billet by machining and then joining it to the core material by HIPIP fitting, as well as sintering, which solidifies and joins molybdenum or molybdenum-based alloy powder in which ceramic particles are dispersed. Examples include the HIP method, the Canning HIP method, and the explosive molding method (impact molding method), but any other solidification techniques may be applied. Among these methods, the Canning HIP method is briefly explained as follows. First, the powder is subjected to cold isostatic pressing (CIP).
Molded using a molding method such as Next, this is inserted into a metal capsule, thoroughly dried by vacuum heating and degassing, and then vacuum sealed in the capsule and subjected to IP treatment.
接合後は必要により外表面を仕上げ加工して使用に供す
る。After joining, the outer surface is finished if necessary and the parts are ready for use.
なお、本発明のプラグは、前述した鋼片の穿孔に対する
プラグのみならず、エロンゲータ、プラグミル、リーラ
等に用いられるプラグに対しても適用することができる
。The plug of the present invention can be applied not only to a plug for drilling a steel billet as described above, but also to a plug used for an elongator, a plug mill, a reeler, etc.
〔作用]
モリブデンは一般に室温で脆性なため穿孔初期に破壊し
たり、穿孔中に粒成長し強度が低下し遂には破壊してし
まうのに対し、本発明のプラグにおいてはセラミックス
との複合化により室温での脆性を回避したり、粒成長を
抑え脆弱化を防止している。[Function] Molybdenum is generally brittle at room temperature, so it may break at the initial stage of drilling, or grains grow during drilling, resulting in a decrease in strength and eventually breakage. It avoids brittleness at room temperature and suppresses grain growth to prevent brittleness.
実施例1
本発明の一実施例であるプラグ1をマンドレルバ−2に
装着した状態を第2図(a)(b)に示す。これは、ピ
アサ−プラグの場合を例に示したものであり、(a)は
その側面図、(b)は第1図(a)における八−A部所
面図である。Embodiment 1 A state in which a plug 1 according to an embodiment of the present invention is attached to a mandrel bar 2 is shown in FIGS. 2(a) and 2(b). This shows the case of a piercer plug as an example; (a) is a side view thereof, and (b) is a side view of section 8-A in FIG. 1(a).
このプラグ1は被穿孔物と接触する表面層3がZrO□
粒子やY2O3粒子やAh03粒子を分散したモリブデ
ンの複合組織となっており、内部の芯材は熱間工具鋼(
SKD61)で構成されている。プラグ形状は円錐体の
先端部が略半球状に丸められた弾頭形状をしている。In this plug 1, the surface layer 3 that contacts the object to be drilled is ZrO□
It has a composite structure of molybdenum in which particles, Y2O3 particles, and Ah03 particles are dispersed, and the internal core material is hot work tool steel (
SKD61). The plug has a warhead shape with the tip of a cone rounded into a substantially hemispherical shape.
プラグ1は円柱形状のマンドレルバ−2の先端に装着さ
れている。プラグIの底面には、マンドレルバ−2へ取
り付ける所定深さの嵌合穴5が穿設されている。一方、
マンドレルバ−2の先端には凸部6が設けられ、プラグ
1とマンドレルバ−2とは嵌合穴5と凸部6とにより嵌
着されている。The plug 1 is attached to the tip of a cylindrical mandrel bar 2. A fitting hole 5 of a predetermined depth for attachment to the mandrel bar 2 is bored in the bottom of the plug I. on the other hand,
A protrusion 6 is provided at the tip of the mandrel bar 2, and the plug 1 and the mandrel bar 2 are fitted through the fitting hole 5 and the protrusion 6.
本実施例では、被覆層をZrot粒子やY2O3粒子や
A1z03粒子を分散したモリブデンの複合材とした場
合と比べどの程度改善されるかを試験した。In this example, a test was conducted to see how much improvement there would be compared to a case where the coating layer was a composite material of molybdenum in which Zrot particles, Y2O3 particles, and A1z03 particles were dispersed.
外径φ32価、長さ76a+mのモデル試験用プラグに
対し、外径φ26mm、長さ60n+mの芯材を準備し
た。A core material with an outer diameter of 26 mm and a length of 60 n+m was prepared for a model test plug with an outer diameter of 32 mm and a length of 76 a+m.
被覆層は平均粒径0.02μmの各種セラミック粒子を
平均粒径1nのモリブデン粉末に体積%でlO%湿式混
合した後乾燥した粉末をキャニングHIP法により固化
接合することにより芯材の表面に張り付けた。The coating layer is pasted on the surface of the core material by wet mixing various ceramic particles with an average particle size of 0.02 μm with molybdenum powder with an average particle size of 1N in 10% by volume, and then solidifying and bonding the dried powder using the Canning HIP method. Ta.
プラグの製作条件の詳細を第1表に示す。Details of the manufacturing conditions of the plug are shown in Table 1.
第1表
プラグ製作条件
これら4つのプラグにつき小型穿孔機でモデル穿孔試験
を行った。被穿孔材は13%CrtFflからなる直径
φ40rtm、長さ200−1温度1250℃の丸鋼片
で、直径φ42+ma、厚さ6an、長さ400鴫のホ
ローピースに加工した。なお、プラグの予熱は行われず
に試験を行った。モデル穿孔試験の結果として、プラグ
の耐用回数および損傷状態を第2表に示す。Table 1 Plug Manufacturing Conditions Model drilling tests were conducted on these four plugs using a small drilling machine. The material to be drilled was a round steel piece made of 13% CrtFfl with a diameter of 40 rtm and a length of 200° C. and a temperature of 1250° C., and was processed into a hollow piece with a diameter of 42+ ma, a thickness of 6 ann, and a length of 400 rtm. Note that the test was conducted without preheating the plug. Table 2 shows the service life and damage state of the plug as a result of the model drilling test.
第2表
モデル穿孔試験結果
第2表に示すように、本発明の供試体は予熱を行わなく
ても十数口の穿孔に成功した。Table 2 Model drilling test results As shown in Table 2, the specimen of the present invention succeeded in drilling more than ten holes without preheating.
このようにセラミック粒子でモリブデンを複合化する効
果が十分証明された。In this way, the effect of compositing molybdenum with ceramic particles has been fully demonstrated.
実施例2
本発明の他の実施例であるプラグIをマンドレルバ−2
に装着した状態を第2図に(a)(b)に示す。Embodiment 2 A plug I, which is another embodiment of the present invention, is connected to a mandrel bar 2.
Figures 2 (a) and (b) show the state in which it is installed.
これは、プアサープラグの場合を例にしたのであり、(
a)はその側面図、(b)は第2図(a)におけるAA
部断面図である。This is an example of the case of a poorer plug (
a) is its side view, (b) is the AA in Fig. 2 (a)
FIG.
このプラグ1は被穿孔物と接触する表面層3がZrot
粒子やY2O1粒子やAhOs粒子を分散したモリブデ
ンの複合組織となっており、内部の芯材4がモリブデン
よりも熱膨張係数の高い材料より構成されている。また
、穿孔時の被穿孔物の回転力から受ける反力による剪断
に対し接合界面が十分な接合強度を持つように、芯材4
の表面には第2図(b)に示す凹凸状の溝7が形成され
ている。プラグ形状は円錐体の先端部が略半球状に丸め
られた弾頭形状をしている。プラグlは円柱形状のマン
ドレルバ−2の先端に装着されている。プラグ1の底面
には、マンドレルバ−2へ取付ける所定深さの嵌合穴5
が穿設されている。一方、マンドレルバ−2の先端には
凸部6が設けられ、プラグ1とマンドレルバ−2とは嵌
合穴5と凸部6とにより嵌着されている。This plug 1 has a surface layer 3 that contacts the object to be drilled.
It has a composite structure of molybdenum in which particles, Y2O1 particles, and AhOs particles are dispersed, and the internal core material 4 is made of a material with a higher coefficient of thermal expansion than molybdenum. In addition, the core material 4 is
A groove 7 having an uneven shape as shown in FIG. 2(b) is formed on the surface. The plug has a warhead shape with the tip of a cone rounded into a substantially hemispherical shape. The plug l is attached to the tip of a cylindrical mandrel bar 2. The bottom of the plug 1 has a fitting hole 5 of a predetermined depth for attaching to the mandrel bar 2.
is drilled. On the other hand, a protrusion 6 is provided at the tip of the mandrel bar 2, and the plug 1 and the mandrel bar 2 are fitted through the fitting hole 5 and the protrusion 6.
プラグの製造方法は次の通りである。この例においては
、芯材4の形状もプラグと同様に弾頭形状をしているが
、軸方向に数本の溝7が施されている。The method for manufacturing the plug is as follows. In this example, the shape of the core material 4 is also bullet-shaped like the plug, but several grooves 7 are formed in the axial direction.
本実施例では、被覆層をZrO1粒子やYzOs粒子や
AhO:+粒子を分散したモリブデンの複合材とじた場
合、純モリブデンを被覆した場合と比べどの程度改善さ
れるのか、芯材に溝を施した場合どの程度改善されるの
かを試験した。In this example, we investigated how much improvement is achieved when the coating layer is made of a composite material of molybdenum in which ZrO1 particles, YzOs particles, and AhO:+ particles are dispersed, compared to the case where pure molybdenum is coated. We tested to see how much improvement there would be if we did so.
外径φ32mm、長さ76fflffiのモデル試験用
プラグに対し、外径φ26mm、長さ60mmの芯材を
準備した。A core material with an outer diameter of 26 mm and a length of 60 mm was prepared for a model test plug with an outer diameter of 32 mm and a length of 76 fflffi.
芯材には、その外周に幅2.5mm、長さ60III[
Ilの溝6本等間隔に溝彫加工し、コーナーにはアール
を設けた。The core material has a width of 2.5 mm and a length of 60 mm on its outer circumference.
Six Il grooves were carved at equal intervals, and the corners were rounded.
被覆層は平均粒径0.02Qの各種セラミック粒子を平
均粒径1μmのモリブデン粉末に体積%で10Q湿式混
合した後乾燥した粉末をキャニングHIP法により固化
接合することにより芯材の表面に被覆した後、仕上げ加
工によりプラグ1を製作した。The coating layer was coated on the surface of the core material by wet mixing various ceramic particles with an average particle size of 0.02Q with molybdenum powder with an average particle size of 1 μm at a volume percent of 10Q, and then solidifying and bonding the dried powder using the Canning HIP method. After that, plug 1 was manufactured by finishing processing.
なお、比較のように芯材に溝加工を施さない代わりに、
被覆層と芯材の間にニッケルの中間層を設けたものや、
芯材表面にショツトブラスト処理を施しモリブデン被覆
層と芯材の界面を不規則にしたものを作製し、本発明プ
ラグと比較した。In addition, instead of grooving the core material as in the comparison,
Those with a nickel intermediate layer between the coating layer and the core material,
A core material whose surface was subjected to shot blasting treatment to make the interface between the molybdenum coating layer and the core material irregular was prepared and compared with the plug of the present invention.
第3表
プラグ製作条件
これら7つのプラグにつき小型穿孔機でモデル穿孔試験
を行った。被穿孔材は13%Crjilからなる直径φ
40M、長さ200mm、温度1250°Cの丸鋼片で
、直径φ42胴、厚さ6飾、長さ400鵬のホローピー
スに加工した。なお、プラグの予熱は行われずに試験を
行った。モデル穿孔試験の結果として、プラグの耐用回
数および損傷状態を第4表に示す。Table 3 Plug Manufacturing Conditions A model drilling test was conducted on these seven plugs using a small drilling machine. The material to be drilled is made of 13% Crjil and has a diameter φ
A round steel piece measuring 40M, length 200mm, and temperature 1250°C was processed into a hollow piece with diameter φ42, thickness 6 ornaments, and length 400mm. Note that the test was conducted without preheating the plug. Table 4 shows the service life and damage state of the plug as a result of the model drilling test.
第4表
モデル穿孔試験結果
第4表に示すように、本発明の供試体は使用前に予熱し
なくても非常に長寿命でNα10やNα11の数十倍の
穿孔に成功した。Table 4 Model Drilling Test Results As shown in Table 4, the specimen of the present invention had a very long life without being preheated before use, and was able to successfully drill tens of times as many holes as Nα10 and Nα11.
このようにセラミック粒子でモリブデンを複合化し、か
つ、芯材に溝加工を施す効果が十分証明された。In this way, the effectiveness of compositing molybdenum with ceramic particles and grooving the core material was fully demonstrated.
実施例3
次に、本発明をプラグミルプラグに適用した例を第3図
(a) (b)に示す、(a)はプラグの側面図、(b
)はその芯材4の側断面図である。Example 3 Next, an example in which the present invention is applied to a plug mill plug is shown in FIGS. 3(a) and 3(b). (a) is a side view of the plug, and (b)
) is a side sectional view of the core material 4.
このプラグ1もピアサ−プラグと同様に被圧延物と接触
する表面層3がモリブデン、そして内部の芯材4がモリ
ブデンよりも熱膨張係数の高い材料より構成されている
。また、圧延時の被圧延物から受ける軸力による剪断に
対し接合界面が十分な接合強度を持つように芯材4の表
面には第3図(b)に示す凹凸状の溝7が形成されてい
る。プラグ1は略円錐台形状をしている。Like the piercer plug, this plug 1 also has a surface layer 3 in contact with the rolled material made of molybdenum, and an internal core material 4 made of a material having a higher coefficient of thermal expansion than molybdenum. In addition, uneven grooves 7 shown in FIG. 3(b) are formed on the surface of the core material 4 so that the bonding interface has sufficient bonding strength against shearing due to the axial force received from the rolled object during rolling. ing. The plug 1 has a substantially truncated conical shape.
プラグ1は円柱形状のマンドレルバ−2の先端に装着さ
れている。プラグ1の中心には、マンドレルバ−2へ取
り付ける所定径が貫通穴8が穿設されている。一方、マ
ンドレルバ−2の先端にはネジが切ってありプラグ1と
マンドレルバ−2をボルト9により固定することができ
ようになっている。The plug 1 is attached to the tip of a cylindrical mandrel bar 2. A through hole 8 of a predetermined diameter is bored in the center of the plug 1 to be attached to the mandrel bar 2. On the other hand, the tip of the mandrel bar 2 is threaded so that the plug 1 and the mandrel bar 2 can be fixed with bolts 9.
プラグの製造方法は次の通りである。この例においても
、芯材4は熱間工具鋼(SKD61)又はTiBz系セ
ラミックスで構成されている。The method for manufacturing the plug is as follows. In this example as well, the core material 4 is made of hot work tool steel (SKD61) or TiBz ceramics.
芯材4には、径方向に数本の溝7が設けられている。The core material 4 is provided with several grooves 7 in the radial direction.
本実施例では、被覆層をZrO,粒子やy、o:1粒子
やAlt03粒子を分散したモリブデンの複合材とした
場合、純モリブデンを被覆した場合と比べどの程度改善
されるのかを試験した。In this example, when the coating layer is a composite material of molybdenum in which ZrO, particles, y, o: 1 particles, and Alt03 particles are dispersed, it was tested to see how much improvement is achieved compared to the case where pure molybdenum is coated.
外径φ164M、長さ120o++nの実機用プラグに
対し、外周にモリブデンを20no++の厚みで盛れる
ように外周加工を施した芯材を準備した。特にこの部分
には、周方向に幅10印、深さ5印の四角い溝を2本等
間隔に溝彫加工し、コーナーにはアールを設けた。For a plug for actual use with an outer diameter of φ164M and a length of 120o++n, a core material was prepared in which the outer periphery was processed so that molybdenum could be applied to the outer periphery to a thickness of 20no++. In particular, in this part, two square grooves with a width of 10 marks and a depth of 5 marks were carved at equal intervals in the circumferential direction, and the corners were rounded.
被覆層は平均粒径0.02μmの各種セラミック粒子を
平均粒径1μmのモリブデン粉末に体積%で10%湿式
混合した後乾燥した粉末をキャニングHIP法により固
化接合することにより芯材の表面に被覆した後、仕上げ
加工によりプラグ1を製作した。The coating layer is coated on the surface of the core material by wet mixing various ceramic particles with an average particle size of 0.02 μm with molybdenum powder with an average particle size of 1 μm at 10% by volume, and then solidifying and bonding the dried powder using the Canning HIP method. After that, plug 1 was manufactured by finishing processing.
なお、比較のように芯材に溝加工を施さない代わりに、
被覆層と芯材の間に二・νケルの中間層を設けたものや
、芯材表面にショツトブラスト処理を施しモリブデン被
覆層と芯材の界面を不規則にしたものを作製し、本発明
プラグと比較した。In addition, instead of grooving the core material as in the comparison,
The present invention was produced by providing an intermediate layer of 2.ν Kel between the coating layer and the core material, or by subjecting the surface of the core material to shot blasting to make the interface between the molybdenum coating layer and the core material irregular. compared to plug.
プラグの製作条件を第5表に示す。Table 5 shows the manufacturing conditions of the plug.
第5表 プラグ製作条件
これら6つのプラグにつき実穿孔機で圧延試験を行った
。被圧延材は13%Cr1ilからなる円筒鋼片でホロ
ーピースに加工したもので、温度はあらかじめ1100
°Cに加熱し使用した。実機試験の結果とし、阻17プ
ラグの耐用限界での圧延回数費および損傷状態を第6表
に示す。Table 5: Plug manufacturing conditions A rolling test was conducted on these six plugs using an actual drilling machine. The material to be rolled is a cylindrical steel piece made of 13% Cr1il processed into a hollow piece, and the temperature was set to 1100 in advance.
It was heated to ℃ and used. Table 6 shows the rolling cost and damage condition of the 17 plug at its service life limit, as a result of the actual machine test.
第6表
実機試験結果
第6表に示すように、本発明の供試体は使用前に予熱し
なくとも非常に長寿命でNo、 17の数十倍の圧延に
成功した。Table 6 Actual machine test results As shown in Table 6, the specimen of the present invention had a very long life without being preheated before use, and was successfully rolled several tens of times as much as No. 17.
このようにセラミック粒子でモリブデンを複合化し、か
つ、芯材に溝加工を施す効果が十分ありプラグミルプラ
グにも適用可能であることが証明された。In this way, it has been proven that combining molybdenum with ceramic particles and grooving the core material is sufficiently effective and can also be applied to plug mill plugs.
以上説明したように、この発明のプラグによれば、次の
効果がもたらされる。As explained above, the plug of the present invention provides the following effects.
(1)モリブデンを主とした被覆層の室温における脆性
が回避されたため、本発明のプラグでは予熱が不要とな
り作業性が良くなった。(1) Since the brittleness of the molybdenum-based coating layer at room temperature was avoided, the plug of the present invention did not require preheating, resulting in improved workability.
また、被覆層の結晶粒成長も抑制されるためプラグの寿
命が大幅に向上した。In addition, since the growth of crystal grains in the coating layer is also suppressed, the life of the plug is greatly improved.
(2)高合金材料の穿孔や圧延に対し、極めて優れた耐
摩耗性、耐溶損性、耐焼付き性等を具備し、しかも破壊
することなく、その寿命は大幅に向上した。(2) It has extremely excellent wear resistance, erosion resistance, seizure resistance, etc. against drilling and rolling of high alloy materials, does not break, and has a significantly extended lifespan.
更に、被穿孔材料や被圧延材料の理想的なメタルフロー
を維持でき、焼付き疵等が生じないため、内面品質が良
好なホローピースを安定して製造することができる。Further, since the ideal metal flow of the material to be drilled and the material to be rolled can be maintained and seizure defects etc. do not occur, hollow pieces with good inner surface quality can be stably manufactured.
(3)全体がモリブデンから成るものに比べ、軽量化が
図れ、かつ、マンドレルバ−への熱影舌も回避できる。(3) Compared to a structure made entirely of molybdenum, the weight can be reduced, and heat shadows on the mandrel bar can also be avoided.
(4)芯材に凹凸形状を施すことにより、被覆層と芯材
の接合性が良くなり、寿命の大幅な向上につながった。(4) By providing the core material with an uneven shape, the bondability between the coating layer and the core material was improved, leading to a significant improvement in the lifespan.
したがって、継目無し鋼管製造の作業能率向上および大
幅な経費節減が達成され、産業上有用な効果が得られた
。Therefore, it has been possible to improve the working efficiency of seamless steel pipe manufacturing and to significantly reduce costs, resulting in industrially useful effects.
第1図は及び第2図はそれぞれ本発明をピアサ−プラグ
に適用した実施例を示す図であり、図(a)はいずれも
その側面図そして(b)は(21図におけるA−A部所
面図を示している。第3図は本発明をプラグミルプラグ
に適用した実施例を示す図であり、同図(a)はその側
面図そして(b)はその芯材の側断面図である。第4図
は従来のプラグの使用による損傷状態の例を示す側面図
である。
1・・・プラグ、2・・・マンドレルバ−3・・・表面
層、4・・・芯材、5・・・嵌合穴、6・・・凸部、7
・・・溝、8・・・貫通穴、9・・・ボルト
特許出願人 日本鋼管株式会社
代 理 人 弁理士 国中 政情
(a)
(b)
第
夏
図
(a)
(b)
第2
図
(a)
第3図
第4図FIGS. 1 and 2 are views showing an embodiment in which the present invention is applied to a piercer plug, and FIG. 1A is a side view thereof, and FIG. Fig. 3 shows an embodiment in which the present invention is applied to a plug mill plug, in which (a) is a side view thereof and (b) is a side sectional view of its core material. 4 is a side view showing an example of damage caused by use of a conventional plug. 1... Plug, 2... Mandrel bar, 3... Surface layer, 4... Core material, 5... Fitting hole, 6... Convex part, 7
...Groove, 8...Through hole, 9...Bolt Patent applicant Nihon Kokan Co., Ltd. Agent Patent attorney Kuninaka Political Affairs (a) (b) Summer figure (a) (b) Fig. 2 (a) Figure 3 Figure 4
Claims (2)
粒子を分散させた複合材よりなる被穿孔物と接触する表
面層と、他の材料よりなる芯材からなっている継目無し
鋼管製造用プラグ(1) Plug for seamless steel pipe manufacturing consisting of a surface layer in contact with the object to be drilled, which is made of a composite material made of molybdenum or a molybdenum-based alloy with ceramic particles dispersed therein, and a core material made of another material.
れていることを特徴とする請求項(1)に記載の継目無
し鋼管製造用プラグ(2) The plug for seamless steel pipe manufacturing according to claim (1), wherein the surface with which the surface layer of the core material contacts is provided with an uneven shape.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP9065289A JPH02268909A (en) | 1989-04-12 | 1989-04-12 | Plug for manufacturing seamless steel tube |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP9065289A JPH02268909A (en) | 1989-04-12 | 1989-04-12 | Plug for manufacturing seamless steel tube |
Publications (1)
Publication Number | Publication Date |
---|---|
JPH02268909A true JPH02268909A (en) | 1990-11-02 |
Family
ID=14004452
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP9065289A Pending JPH02268909A (en) | 1989-04-12 | 1989-04-12 | Plug for manufacturing seamless steel tube |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPH02268909A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0743106A1 (en) * | 1995-05-19 | 1996-11-20 | Nkk Corporation | Method for manufacturing seamless pipe |
WO1998029204A1 (en) * | 1996-12-27 | 1998-07-09 | Kawasaki Steel Corporation | Plug and mandrel bar for rolling of seamless steel pipe and method of manufacturing seamless steel pipe |
KR102384019B1 (en) * | 2020-12-21 | 2022-04-08 | (주)세창스틸 | Piercing plug assembly for manufacturing seamless tube with heat resistance |
-
1989
- 1989-04-12 JP JP9065289A patent/JPH02268909A/en active Pending
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0743106A1 (en) * | 1995-05-19 | 1996-11-20 | Nkk Corporation | Method for manufacturing seamless pipe |
US5778714A (en) * | 1995-05-19 | 1998-07-14 | Nkk Corporation | Method for manufacturing seamless pipe |
US6073331A (en) * | 1995-05-19 | 2000-06-13 | Nkk Corporation | Method for manufacturing seamless pipe |
WO1998029204A1 (en) * | 1996-12-27 | 1998-07-09 | Kawasaki Steel Corporation | Plug and mandrel bar for rolling of seamless steel pipe and method of manufacturing seamless steel pipe |
US6202463B1 (en) | 1996-12-27 | 2001-03-20 | Kawasaki Steel Corporation | Plug and mandrel bar for seamless steel pipe rolling operation for manufacturing seamless steel pipe |
KR100403061B1 (en) * | 1996-12-27 | 2003-10-24 | 제이에프이 스틸 가부시키가이샤 | Plug and mandrel bar for rolling of seamless steel pipe and method of manufacturing seamless steel pipe |
KR102384019B1 (en) * | 2020-12-21 | 2022-04-08 | (주)세창스틸 | Piercing plug assembly for manufacturing seamless tube with heat resistance |
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