JPH0196358A - Composite molybdenum plate and its manufacture - Google Patents
Composite molybdenum plate and its manufactureInfo
- Publication number
- JPH0196358A JPH0196358A JP25152287A JP25152287A JPH0196358A JP H0196358 A JPH0196358 A JP H0196358A JP 25152287 A JP25152287 A JP 25152287A JP 25152287 A JP25152287 A JP 25152287A JP H0196358 A JPH0196358 A JP H0196358A
- Authority
- JP
- Japan
- Prior art keywords
- molybdenum
- layer
- pure
- composite
- purity
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
- 229910052750 molybdenum Inorganic materials 0.000 title claims abstract description 65
- 239000002131 composite material Substances 0.000 title claims abstract description 12
- 238000004519 manufacturing process Methods 0.000 title claims abstract description 7
- 239000011733 molybdenum Substances 0.000 title claims description 62
- ZOKXTWBITQBERF-UHFFFAOYSA-N Molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 title claims description 61
- MRELNEQAGSRDBK-UHFFFAOYSA-N lanthanum oxide Inorganic materials [O-2].[O-2].[O-2].[La+3].[La+3] MRELNEQAGSRDBK-UHFFFAOYSA-N 0.000 claims abstract description 48
- 229910052746 lanthanum Inorganic materials 0.000 claims abstract description 7
- 238000010438 heat treatment Methods 0.000 claims abstract description 4
- FZLIPJUXYLNCLC-UHFFFAOYSA-N lanthanum atom Chemical compound [La] FZLIPJUXYLNCLC-UHFFFAOYSA-N 0.000 claims description 6
- 239000000654 additive Substances 0.000 claims 2
- 230000000996 additive effect Effects 0.000 claims 2
- 238000002360 preparation method Methods 0.000 claims 1
- 238000000034 method Methods 0.000 abstract description 6
- 238000001953 recrystallisation Methods 0.000 abstract description 4
- KTUFCUMIWABKDW-UHFFFAOYSA-N oxo(oxolanthaniooxy)lanthanum Chemical compound O=[La]O[La]=O KTUFCUMIWABKDW-UHFFFAOYSA-N 0.000 abstract 2
- 238000005096 rolling process Methods 0.000 description 13
- 239000000463 material Substances 0.000 description 7
- 239000002019 doping agent Substances 0.000 description 6
- 230000000052 comparative effect Effects 0.000 description 5
- 150000002751 molybdenum Chemical class 0.000 description 5
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 description 4
- 239000013078 crystal Substances 0.000 description 4
- 229910052739 hydrogen Inorganic materials 0.000 description 4
- 239000001257 hydrogen Substances 0.000 description 4
- 239000002245 particle Substances 0.000 description 4
- 239000000843 powder Substances 0.000 description 4
- 238000005097 cold rolling Methods 0.000 description 3
- 230000000694 effects Effects 0.000 description 3
- 230000015572 biosynthetic process Effects 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 238000005242 forging Methods 0.000 description 2
- 238000005098 hot rolling Methods 0.000 description 2
- 238000005245 sintering Methods 0.000 description 2
- 101100145155 Escherichia phage lambda cIII gene Proteins 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 230000004927 fusion Effects 0.000 description 1
- 239000012535 impurity Substances 0.000 description 1
- 229910000476 molybdenum oxide Inorganic materials 0.000 description 1
- 238000000465 moulding Methods 0.000 description 1
- 239000003758 nuclear fuel Substances 0.000 description 1
- PQQKPALAQIIWST-UHFFFAOYSA-N oxomolybdenum Chemical compound [Mo]=O PQQKPALAQIIWST-UHFFFAOYSA-N 0.000 description 1
- 238000004663 powder metallurgy Methods 0.000 description 1
- 239000007858 starting material Substances 0.000 description 1
Landscapes
- Manufacture Of Alloys Or Alloy Compounds (AREA)
- Powder Metallurgy (AREA)
Abstract
Description
【発明の詳細な説明】
〔産業上の利用分野〕
本発明は、−殻構造材、高温炉用、核燃料焼結用ボート
、核融合炉用材料、電子管材料等に使用されるモリブデ
ン板とその製造方法に関する。[Detailed Description of the Invention] [Field of Industrial Application] The present invention relates to a molybdenum plate used for shell structural materials, high temperature reactors, boats for nuclear fuel sintering, materials for nuclear fusion reactors, materials for electron tubes, etc. Regarding the manufacturing method.
一般に、粉末冶金法で製造されるモリブデン板は、純モ
リブデンによって製造される。Generally, molybdenum plates manufactured by powder metallurgy are made of pure molybdenum.
このモリブデン板の再結晶開始温度は1000℃である
。よって、斯るモリブデンからなるモリブデン板は、1
000℃以上で使用すると、再結晶粒子の成長によって
、板の脆化が生じ、また高温状態の荷重負荷に対して容
易に変形してしまうという問題があった。そこで、上述
の欠点を補うモリプデン材料として、従来は、色々なド
ープ材を添加してモリブデンを強化する方法が行われて
いた゛。The recrystallization start temperature of this molybdenum plate is 1000°C. Therefore, a molybdenum plate made of molybdenum is 1
When used at temperatures above 000° C., there is a problem in that the plate becomes brittle due to the growth of recrystallized particles and is easily deformed under high-temperature loads. Therefore, as a molybdenum material that compensates for the above-mentioned drawbacks, a method has conventionally been used in which molybdenum is strengthened by adding various dopants.
しかしながら、従来のドープモリブデン材料は、その製
造過程において、高い加工率を必要とし、しかも、加工
性も悪いという製造上の欠点があった。However, conventional doped molybdenum materials require a high processing rate in the manufacturing process and have poor processability.
また、高温での使用においては、再結晶組織がドープ剤
の配列によりコントロールされる為、圧延方向には長大
に、また、圧延方向と直角方向には、短い再結晶組織と
なる。その為短い再結晶組織の方に負荷が掛かる様な使
用方法を行うと、容易に変形してしまうという欠点があ
った。Furthermore, when used at high temperatures, the recrystallized structure is controlled by the arrangement of the dopant, so the recrystallized structure becomes long in the rolling direction and short in the direction perpendicular to the rolling direction. Therefore, when used in a manner that places a load on the short recrystallized structure, it has the disadvantage that it easily deforms.
一方、純度99.95%以上のモリブデン板の結晶粒構
成を選定することにより、使用方向の制限を有さす高温
強度に優れた板にする方法等も行われているがこの方法
でも、小さい負荷に対しては著しい効果を示すが、大き
い負荷に対しては、容易に変形してしまうという欠点が
あった。On the other hand, by selecting the crystal grain structure of a molybdenum plate with a purity of 99.95% or more, a method is being used to create a plate with excellent high-temperature strength that has restrictions on the direction of use. However, it has the disadvantage that it easily deforms under large loads.
そこで、本発明の技術的課題は、上記欠点に鑑み、高温
状態下における荷重負荷に対しても、変形量の少ない使
用性の優れたモリブデン板とその製造方法を提供するこ
とである。SUMMARY OF THE INVENTION In view of the above-mentioned drawbacks, it is a technical object of the present invention to provide a molybdenum plate that is easy to use and has a small amount of deformation even when subjected to loads under high temperature conditions, and a method for manufacturing the same.
本発明によれば、モリブデン板を製造する場合の出発原
料となるインゴットは、例えば、0.1%以上〜1.0
%以下のランタン又は酸化ランタンをドープしたドープ
モリブデン粉末より形成されたドープモリブデン層と、
純度99.95%以上のモリブデンより形成された純モ
リブデン層との2種の層のおのおの1層以上の組合せよ
り形成される。According to the present invention, the ingot serving as the starting material for producing a molybdenum plate is, for example, 0.1% or more to 1.0%
% or less of lanthanum or lanthanum oxide;
It is formed from a combination of one or more layers of each of the two types of layers, including a pure molybdenum layer made of molybdenum with a purity of 99.95% or more.
次に、この多層を有するインゴットをその厚さ方向に8
0%以上の総加工率で熱間鍛造及び圧延加工のどちらか
一方又はその組合せた加工を施す。Next, the ingot with this multilayer is
Hot forging, rolling, or a combination thereof is performed at a total processing rate of 0% or more.
次に、この繊維状組織からなるモリブデン板にさらに、
再結晶温度以上で熱処理による粗大化処理を施し、結晶
粒子を再結晶させ、内部歪を解放する。Next, on the molybdenum plate made of this fibrous structure,
A coarsening treatment is performed by heat treatment at a temperature higher than the recrystallization temperature to recrystallize the crystal grains and release internal strain.
このとき、純度99.95%以上の純モリブデン層はド
ープ剤あるいは不純物による粒成長抑制作用かない為に
直径の平均の大きさが10mm〜150nの円板状組織
となる。At this time, the pure molybdenum layer with a purity of 99.95% or more has a disk-like structure with an average diameter of 10 mm to 150 nm because there is no effect of suppressing grain growth due to dopants or impurities.
一方、ランタンをドープしたドープモリブデン層は圧延
方向に沿ってドープ剤が配列している為に、板厚方向へ
の粒成長は抑制されることから、板厚方向には粗大化せ
ず、圧延方向に沿って伸長したいわゆるインターロッキ
ング構造を呈する。On the other hand, in the doped molybdenum layer doped with lanthanum, the dopant is arranged along the rolling direction, so grain growth in the thickness direction is suppressed, so the layer does not become coarse in the thickness direction, and rolling It exhibits a so-called interlocking structure that extends along the direction.
即ち、酸化ランタン粒によって分散強化されたインター
ロッキング層と、方向性を持たない粒界の辷りが発生し
にくい円板状組織を有する層とによって形成された複合
モリブデン板が得られる。That is, a composite molybdenum plate is obtained, which is formed by an interlocking layer that is dispersion-strengthened by lanthanum oxide grains and a layer that has a disk-like structure that is less likely to cause grain boundary sliding without directionality.
従って、高温下におかれた場合でも変形量の非常に少な
い高品質のモリブデン板材が得られる。Therefore, a high-quality molybdenum plate material with very little deformation even when exposed to high temperatures can be obtained.
ここで、酸化ランタンを含有したドープモリブデン層の
酸化ランタン添加量を1.0%以下としたのは添加量が
1.0%を越えると、焼結時の酸化ランタンの蒸発量が
多くなり、純度99.95%の純モリブデン層を汚染さ
せ、結晶粒粗大化処理工程における純度99.95%の
純モリブデン層の円板状組織の形成が疎外されるからで
ある。Here, the addition amount of lanthanum oxide in the doped molybdenum layer containing lanthanum oxide was set to 1.0% or less because if the addition amount exceeds 1.0%, the amount of lanthanum oxide evaporated during sintering increases. This is because the pure molybdenum layer with a purity of 99.95% will be contaminated and the formation of a disk-like structure in the pure molybdenum layer with a purity of 99.95% in the crystal grain coarsening process will be hindered.
また0、1%以上としたのはO,1%未満ではランタン
のドープ剤としての効果が薄く、十分なインターロッキ
ング層の形成が望めないからである。The reason why the content is set to 0.1% or more is that if O is less than 1%, the effect of lanthanum as a doping agent is weak, and formation of a sufficient interlocking layer cannot be expected.
次に、本発明の実施例に係る複合モリブデン板材につい
て図面を参照して説明する。Next, a composite molybdenum plate material according to an example of the present invention will be described with reference to the drawings.
まず始めに、純99.95%以上の平均粒径3〜5μm
の純モリブデン粉末を準備した。First of all, the average particle size of 99.95% pure or more is 3 to 5 μm.
Pure molybdenum powder was prepared.
次に、それぞれ0.01. 0.1. 0.5. 1.
0重量%の酸化ランタンをドープしたモリブデン酸化物
粉末に水素還元を施し、酸化ランタンがドープされた平
均粒径2〜5μmのドープモリブデン粉末を準備した。Next, each 0.01. 0.1. 0.5. 1.
Molybdenum oxide powder doped with 0% by weight of lanthanum oxide was subjected to hydrogen reduction to prepare doped molybdenum powder doped with lanthanum oxide and having an average particle size of 2 to 5 μm.
次に、粉末を成形する為の金型を準備し、まず、酸化ラ
ンタンがドープされたドープモリブデン粉末を充填し金
型の底面と平行となる様に粉末を均した。Next, a mold for molding the powder was prepared, and first, doped molybdenum powder doped with lanthanum oxide was filled and the powder was leveled so that it was parallel to the bottom of the mold.
次に、純度99.95%以上の純モリブデン粉末を充填
し、同様に、均し作業を行った。最後に再び酸化ランタ
ンをドープした粉末を充填し、均し、作業を行い、油圧
プレス機にて、2ton/cIIIの圧力でプレス体を
成形し、水素気流中で1900℃で5時間の焼結を行い
、約30m1厚の3N構造から成るインゴットを得た。Next, pure molybdenum powder with a purity of 99.95% or more was filled, and the same leveling operation was performed. Finally, the powder doped with lanthanum oxide is again filled, leveled and worked, and a pressed body is formed using a hydraulic press at a pressure of 2 tons/cIII, and sintered at 1900°C for 5 hours in a hydrogen stream. An ingot having a 3N structure and having a thickness of about 30 m1 was obtained.
このインゴットを最高温度1300℃で加熱し熱間鍛造
を行い徐々に加熱温度を下げながら圧延加工を繰り返し
、温間圧延加工、冷間圧延加工を加えて2龍厚のモリブ
デン板を得た。This ingot was heated at a maximum temperature of 1300° C., hot forged, and rolled repeatedly while gradually lowering the heating temperature, followed by warm rolling and cold rolling to obtain a molybdenum plate with a thickness of 2 times.
次に、この板を水素気流中、2250℃にて結晶粒粗大
化処理を行った後、最終圧延方向及び最終圧延方向と直
角方向より2%重×20mmX 15 Qmmの試片を
切り出した。これらの本発明に係る試片1〜4と他の同
様なサイズの比較試片5〜8とを用いて、スパン10
Q +nで負荷500gと1000 gとで、1800
℃で10時間の変形試験を行い、変形量の比較を行った
。尚、変形試験は第2図に示す態様で行った。Next, this plate was subjected to grain coarsening treatment at 2250° C. in a hydrogen stream, and then test pieces of 2% weight x 20 mm x 15 Q mm were cut from the final rolling direction and the direction perpendicular to the final rolling direction. Using these specimens 1 to 4 according to the present invention and other comparison specimens 5 to 8 of similar size, a span of 10
Q +n with loads of 500g and 1000g, 1800
A deformation test was conducted at ℃ for 10 hours, and the amount of deformation was compared. Incidentally, the deformation test was conducted in the manner shown in FIG.
ここで、比較用とした試験片とは、純度99.95%の
モリブデンからなり、耐高温変形性に効果のある円板状
の粒構造を有する板8と、0.1%。Here, the test pieces used for comparison are Plate 8, which is made of molybdenum with a purity of 99.95% and has a disk-shaped grain structure that is effective in high-temperature deformation resistance, and Molybdenum with a purity of 0.1%.
0.5%、1.0%の比率で酸化ランタンを含有したモ
リブデン板5〜7である。Molybdenum plates 5 to 7 contain lanthanum oxide at a ratio of 0.5% and 1.0%.
尚、第1図に、本発明に係る試験片1〜4と比較用試験
片5〜8との組織構造の概念を示す。In addition, FIG. 1 shows the concept of the structure of test pieces 1 to 4 according to the present invention and comparison test pieces 5 to 8.
Vノ、下しjミ白
表−1
※ 〉20 治具に接地
その結果、表−1に示す通り、ランタンを0.1〜1.
0%含有させたモリブデン層と純度99.95%以上の
モリブデン層によって形成された本発明に係わる複合モ
リブデン板(1〜4)は、圧延方向と圧延方向と直角の
変形量の差が他の比較例5〜8よりも小さく、また変形
量も少ないことが認められる。V-no, lower j-white Table-1 *〉20 Grounded on the jig As a result, as shown in Table-1, the lantern was 0.1 to 1.
The composite molybdenum plates (1 to 4) according to the present invention formed by a molybdenum layer containing 0% and a molybdenum layer with a purity of 99.95% or more have a difference in deformation in the rolling direction and at right angles to the rolling direction. It is observed that the amount of deformation is smaller than that of Comparative Examples 5 to 8, and the amount of deformation is also smaller.
〔実施例2〕
実施例1と同様な方法で、それぞれ0.1.0.5゜1
.0重量%の酸化ランタンを含有したモリブデン層の間
に純度99.95%のモリブデンより形成された層がサ
ンドインチされ、しかも最終圧延でそれぞれの加工度が
65%、80%、93%になる様に、インゴットを準備
した。[Example 2] In the same manner as in Example 1, 0.1 and 0.5゜1, respectively.
.. A layer made of molybdenum with a purity of 99.95% is sandwiched between molybdenum layers containing 0% by weight of lanthanum oxide, and furthermore, the degree of working becomes 65%, 80%, and 93% in the final rolling. I prepared an ingot.
次に、そのインゴットを最高1300℃で加熱し、加工
度がそれぞれ65%、80%、93%になる様に熱間鍛
造と熱間圧延さらに温間圧延、冷間圧延を加え、所定の
加工率の加工が施された板を製作した。そこから、2u
+x 2 Qmsx 150mmの試片を切り出した。Next, the ingot is heated to a maximum temperature of 1300°C, and subjected to hot forging and hot rolling, as well as warm rolling and cold rolling, so that the degree of working becomes 65%, 80%, and 93%, respectively. A plate with a certain ratio was manufactured. From there, 2u
+x 2 Qmsx A 150 mm specimen was cut out.
次に、この試片を水素気流中2250℃で結晶粒粗大化
処理を行った。この試片をスパン100璽朧で負荷10
00gで1800℃で10時間の変形試験を行い変形量
の比較を行った。その結果を表−2に示す。Next, this specimen was subjected to crystal grain coarsening treatment at 2250° C. in a hydrogen stream. This test piece was applied with a span of 100 and a load of 10.
A deformation test was conducted at 1800° C. for 10 hours using 00g to compare the amount of deformation. The results are shown in Table-2.
以下余白
表−2
※〉20 治具に接地
その結果、表−2に示されたとおり、加工率が80%を
越えた試験片2,3.5,6,8.9の方が、加工率が
65%の試験片1,4.7に比べて、その変形量が少な
くなることが認められる。Margin Table-2 below *〉20 Grounding on the jig As a result, as shown in Table-2, test pieces 2, 3.5, 6, and 8.9 with a processing rate exceeding 80% were more processed. It is recognized that the amount of deformation is smaller than that of test specimens 1 and 4.7 with a ratio of 65%.
以上の説明のとおり、本発明によれば0.1%以上〜1
.0%以下のランタンを含有したドープモリブデン層と
純度99.95%以上の純モリブデン層とを少なくとも
おのおの一層以上より形成されたインゴットを、その厚
さ方向に80%以上の加工率で熱間鍛造又は熱間圧延加
工、さらに温間圧延および冷間圧延を施して、酸化ラン
タンを含有したドープモリブデン層のドープ剤を板厚と
垂直方向に配列させた後、再結晶温度以上に加熱して、
粗大化処理を施すことにより、酸化ランタンを含有した
ドープモリブデン層は、酸化ランタンの粒により分散強
化されたインターロッキング層となり、一方、純度99
.95%以上の純モリブデン層は粒界のすべりの少ない
大きな円板状組織を有する層を形成する。As explained above, according to the present invention, 0.1% or more to 1%
.. An ingot formed of at least one doped molybdenum layer containing 0% or less lanthanum and at least one pure molybdenum layer having a purity of 99.95% or more is hot forged at a processing rate of 80% or more in the thickness direction. Alternatively, hot rolling, further warm rolling and cold rolling are performed to align the dopant of the doped molybdenum layer containing lanthanum oxide in the direction perpendicular to the plate thickness, and then heated to a temperature higher than the recrystallization temperature.
By performing the coarsening treatment, the doped molybdenum layer containing lanthanum oxide becomes an interlocking layer that is dispersed and strengthened by the lanthanum oxide particles, while the purity is 99%.
.. A 95% or more pure molybdenum layer forms a layer having a large disk-like structure with little slippage at grain boundaries.
従って、高温状態の荷重負荷に対しても変形量の少ない
使用性の優れた複合モリブデン板とその製造方法を提供
することが出来る。Therefore, it is possible to provide a composite molybdenum plate with excellent usability that exhibits little deformation even under high-temperature loads, and a method for manufacturing the same.
第1図の1〜8は下記の構造を示す概念図である。
1は、0.01%酸化ランタン含をモリブデン層と純度
99.95%のモリブデン層の本発明に係る三層構造組
織、
2は、0.1%酸化ランタン含有モリブデン層と純度9
9.95%のモリブデン層の本発明に係る三層構造組織
、
3は、0.5%酸化ランタン含有モリブデン層と純度9
9.95%のモリブデン層の本発明に係る三層構造組織
、
4は、1.0%酸化ランタン含有モリブデン層と純度9
9.95%のモリブデン層の本発明に係る三層構造組織
、
5は比較例としての0.1%酸化ランタン含有モリブデ
ン板の組織、
6は比較例としての0.5%酸化ランタン含有モリブデ
ン板の組織、
7は比較例としての1.0%酸化ランタン含有モリブデ
ン板の組織、
8は比較例としての純度99.95%のモリブデン板の
組織である。
第2図は、高温変形試験の態様を示す図である。
第1図1 to 8 in FIG. 1 are conceptual diagrams showing the following structure. 1 is a three-layer structure according to the present invention of a molybdenum layer containing 0.01% lanthanum oxide and a molybdenum layer with a purity of 99.95%; 2 is a molybdenum layer containing 0.1% lanthanum oxide and a purity of 9
Three-layer structure according to the invention of 9.95% molybdenum layer, 3 is a molybdenum layer containing 0.5% lanthanum oxide and purity 9
Three-layer structure according to the present invention of 9.95% molybdenum layer, 4 is a molybdenum layer containing 1.0% lanthanum oxide and purity 9
9.95% molybdenum layer three-layer structure according to the present invention, 5 is a structure of a molybdenum plate containing 0.1% lanthanum oxide as a comparative example, 6 is a molybdenum plate containing 0.5% lanthanum oxide as a comparative example 7 is the structure of a molybdenum plate containing 1.0% lanthanum oxide as a comparative example, and 8 is the structure of a molybdenum plate with a purity of 99.95% as a comparative example. FIG. 2 is a diagram showing an aspect of a high temperature deformation test. Figure 1
Claims (1)
純モリブデン層と、重量比で0.1%以上〜1.0%以
下のランタン又は酸化ランタンを含み残部がモリブデン
からなるドープモリブデン層とを少なくともおのおの一
層以上を有することを特徴とする複合モリブデン板。 2)特許請求の範囲第1項記載の複合モリブデン板にお
いて、前記純モリブデン層は円板状組織を呈し、前記ド
ープモリブデン層はインターロッキング組織を呈するこ
とを特徴とする複合モリブデン板。 3)微量添加元素を含まない、純度99.95%以上の
純モリブデン層と、重量比で、0.1%以上〜1.0%
以下のランタン又は酸化ランタンを含み、残部がモリブ
デンからなるドープモリブデン層とを少なくともおのお
の一層以上組合せて形成された複合インゴットを準備す
る準備工程と、該インゴットの厚みに対して80%以上
の総加工率で加工する加工工程と、該加工物が少なくと
も再結晶化する温度で加熱する粗大化処理工程とを有す
ることを特徴とする耐衝撃性と耐高温変形性に優れた複
合モリブデン板の製造方法。[Scope of Claims] 1) A pure molybdenum layer with a purity of 99.95% or more and containing no trace additive elements, and a layer containing lanthanum or lanthanum oxide in a weight ratio of 0.1% to 1.0%, with the remainder being 1. A composite molybdenum board comprising at least one doped molybdenum layer made of molybdenum. 2) A composite molybdenum plate according to claim 1, wherein the pure molybdenum layer has a disk-like structure, and the doped molybdenum layer has an interlocking structure. 3) A pure molybdenum layer with a purity of 99.95% or more, which does not contain trace additive elements, and a weight ratio of 0.1% or more to 1.0%.
A preparation process of preparing a composite ingot formed by combining at least one layer of each of the following lanthanum or lanthanum oxide with a doped molybdenum layer with the remainder being molybdenum, and total processing of 80% or more with respect to the thickness of the ingot. A method for producing a composite molybdenum plate having excellent impact resistance and high-temperature deformation resistance, comprising a processing step of processing the workpiece at a high temperature and a coarsening step of heating the workpiece at a temperature at least at which it recrystallizes. .
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP25152287A JPH0196358A (en) | 1987-10-07 | 1987-10-07 | Composite molybdenum plate and its manufacture |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP25152287A JPH0196358A (en) | 1987-10-07 | 1987-10-07 | Composite molybdenum plate and its manufacture |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPH0196358A true JPH0196358A (en) | 1989-04-14 |
| JPH0359137B2 JPH0359137B2 (en) | 1991-09-09 |
Family
ID=17224064
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP25152287A Granted JPH0196358A (en) | 1987-10-07 | 1987-10-07 | Composite molybdenum plate and its manufacture |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPH0196358A (en) |
-
1987
- 1987-10-07 JP JP25152287A patent/JPH0196358A/en active Granted
Also Published As
| Publication number | Publication date |
|---|---|
| JPH0359137B2 (en) | 1991-09-09 |
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