JPH0474314B2 - - Google Patents
Info
- Publication number
- JPH0474314B2 JPH0474314B2 JP15953388A JP15953388A JPH0474314B2 JP H0474314 B2 JPH0474314 B2 JP H0474314B2 JP 15953388 A JP15953388 A JP 15953388A JP 15953388 A JP15953388 A JP 15953388A JP H0474314 B2 JPH0474314 B2 JP H0474314B2
- Authority
- JP
- Japan
- Prior art keywords
- tungsten
- molybdenum
- crystal
- multilayer
- producing
- 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
Links
- 239000013078 crystal Substances 0.000 claims description 39
- ZOKXTWBITQBERF-UHFFFAOYSA-N Molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 claims description 29
- 229910052750 molybdenum Inorganic materials 0.000 claims description 29
- 239000011733 molybdenum Substances 0.000 claims description 29
- WFKWXMTUELFFGS-UHFFFAOYSA-N tungsten Chemical compound [W] WFKWXMTUELFFGS-UHFFFAOYSA-N 0.000 claims description 28
- 229910052721 tungsten Inorganic materials 0.000 claims description 28
- 239000010937 tungsten Substances 0.000 claims description 28
- 239000000843 powder Substances 0.000 claims description 16
- 229910052751 metal Inorganic materials 0.000 claims description 13
- 239000002184 metal Substances 0.000 claims description 12
- 239000000292 calcium oxide Substances 0.000 claims description 11
- ODINCKMPIJJUCX-UHFFFAOYSA-N calcium oxide Inorganic materials [Ca]=O ODINCKMPIJJUCX-UHFFFAOYSA-N 0.000 claims description 11
- 239000000395 magnesium oxide Substances 0.000 claims description 11
- CPLXHLVBOLITMK-UHFFFAOYSA-N magnesium oxide Inorganic materials [Mg]=O CPLXHLVBOLITMK-UHFFFAOYSA-N 0.000 claims description 11
- BRPQOXSCLDDYGP-UHFFFAOYSA-N calcium oxide Chemical compound [O-2].[Ca+2] BRPQOXSCLDDYGP-UHFFFAOYSA-N 0.000 claims description 8
- AXZKOIWUVFPNLO-UHFFFAOYSA-N magnesium;oxygen(2-) Chemical compound [O-2].[Mg+2] AXZKOIWUVFPNLO-UHFFFAOYSA-N 0.000 claims description 8
- 239000002131 composite material Substances 0.000 claims description 7
- 238000000137 annealing Methods 0.000 claims description 6
- 239000000654 additive Substances 0.000 claims description 5
- 238000004519 manufacturing process Methods 0.000 claims description 5
- 230000000996 additive effect Effects 0.000 claims description 4
- 239000002994 raw material Substances 0.000 claims description 3
- 238000005245 sintering Methods 0.000 claims description 3
- 238000000465 moulding Methods 0.000 claims description 2
- 238000003475 lamination Methods 0.000 claims 1
- 238000002360 preparation method Methods 0.000 claims 1
- 239000000463 material Substances 0.000 description 10
- 238000000034 method Methods 0.000 description 9
- 238000001953 recrystallisation Methods 0.000 description 5
- 230000000052 comparative effect Effects 0.000 description 4
- 229910052739 hydrogen Inorganic materials 0.000 description 4
- 239000001257 hydrogen Substances 0.000 description 4
- 238000002844 melting Methods 0.000 description 4
- 230000008018 melting Effects 0.000 description 4
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 description 3
- 230000000694 effects Effects 0.000 description 3
- 238000004663 powder metallurgy Methods 0.000 description 3
- 239000003779 heat-resistant material Substances 0.000 description 2
- 238000010030 laminating Methods 0.000 description 2
- 239000007769 metal material Substances 0.000 description 2
- 150000002739 metals Chemical class 0.000 description 2
- 229910000476 molybdenum oxide Inorganic materials 0.000 description 2
- QGLKJKCYBOYXKC-UHFFFAOYSA-N nonaoxidotritungsten Chemical compound O=[W]1(=O)O[W](=O)(=O)O[W](=O)(=O)O1 QGLKJKCYBOYXKC-UHFFFAOYSA-N 0.000 description 2
- PQQKPALAQIIWST-UHFFFAOYSA-N oxomolybdenum Chemical compound [Mo]=O PQQKPALAQIIWST-UHFFFAOYSA-N 0.000 description 2
- 238000005096 rolling process Methods 0.000 description 2
- 238000007665 sagging Methods 0.000 description 2
- 229910001930 tungsten oxide Inorganic materials 0.000 description 2
- 238000003776 cleavage reaction Methods 0.000 description 1
- 230000006378 damage Effects 0.000 description 1
- 230000004927 fusion Effects 0.000 description 1
- 150000002431 hydrogen Chemical class 0.000 description 1
- 230000001590 oxidative effect Effects 0.000 description 1
- 230000000737 periodic effect Effects 0.000 description 1
- 238000010298 pulverizing process Methods 0.000 description 1
- 230000007017 scission Effects 0.000 description 1
- 230000007704 transition Effects 0.000 description 1
- 229910052723 transition metal Inorganic materials 0.000 description 1
- 150000003624 transition metals Chemical class 0.000 description 1
Landscapes
- Powder Metallurgy (AREA)
- Crystals, And After-Treatments Of Crystals (AREA)
Description
[産業上の利用分野]
本発明はタングステンまたはモリブデン多重層
結晶に関するものである。
[従来の技術]
タングステン及びモリブデンは周期律表a族
に属し、第3及び第2長周期に位置する原子番号
がそれぞれ74及び42の体心立方格子の遷移金属で
ある。タングステンは金属元素中最も高い融点
3380℃を有し、一方、モリブデンは2615℃の融点
を有し、それぞれ高融点希金属の代表である。
又、タングステン及びモリブデンの金属学的性
質として、第1に挙げられる性質は、非酸化性の
雰囲気中で、2000℃以上の高温に耐えられる性質
即ち、優れた高温強度を示す超耐熱金属材料とし
て知られている。
しかしながら、両金属共に現時点では線材を除
いて有効な用途開発及び実用化が十分に成されて
いない典型的な金属材料である。その原因はタン
グステン及びモリブデンが多結晶の状態では、室
温以下で成形加工性が極めて悪く、また、
DBTT(延性、脆性遷移温度)以上でそれぞれ3
%、20%以下の伸びを示すことに起因する。
更に、高温での使用時において、多結晶のタン
グステン及びモリブデンは結晶粒の粗大化及び再
結晶脆性を引き起こすため上に述べた超耐熱材料
としての特性を十分に発揮することができないこ
とも、用途が制限される一因となつている。
[発明が解決しようとする課題]
一般にモリブデン及びタングステン材料は、高
温で長時間の苛酷な条件下で使用されているた
め、一旦、破壊亀裂が発生した場合、多結晶状態
では、再結晶脆性により結晶粒界で急激に破壊す
る。
一方、上記した多結晶モリブデン及びタングス
テンの欠点を除去するために、再結晶法により、
結晶を粗大化したタングステン(特開昭61−6197
号公報)および単結晶化したモリブデン(特許第
1420928号)が知られている。この様に、単結晶
化さされたタングステン及びモリブデンでは、へ
き開破壊が、一度に生じることがあり、このため
に、材料としての信頼性の面で十分とはいい難
い。
そこで、本発明の技術課題は、高温における再
結晶脆性を生ずることなく強度、特に耐垂下性及
び信頼性を有するタングステン及びモリブデン材
料を提供することにある。ここで、これらモリブ
デン及びタングステン材料を多層化した、多重層
結晶の場合、破壊切裂が、結晶表面に生じても各
層の結晶粒間に結晶粒界を有し、結晶方位を異に
するための破壊が、各層結晶で拘束を生じ急激な
破壊につながるとことなく、材料の強度と信頼性
を高める結果となる。このため、結晶粒界を板に
平行に存在する多重結晶を提供することができれ
ば、高温強度と信頼性を必要とする原子路材料を
初めとする一般炉材に使用が可能となり、利用分
野が、著しく拡大される。
従つて、本発明の他の技術課題は、上記タング
ステンまたはモリブデン多重結晶を容易にして製
造できるタングステンまたはモリブデン多重結晶
の製造方法を提供することにある。
[課題を解決するための手段]
本発明によれば、板面に平行な結晶粒界を有す
る2層以上の多重層から構成され、これら多重層
の中で互いに重なる各層は互いに結晶学的方位を
異にした単結晶状態を有することを特徴とするタ
ングステン又はモリブデン多重層結晶が得られ
る。
本発明によれば、タングステン又はモリブデン
多結晶体を積層成形して成形体を形成し、この成
形体を焼鈍して隣接する層に互いに結晶方位をこ
とにした結晶状態を呈する多重層結晶の製造方法
が得られる。
具体的に言えば、タングステン又はモリブデン
多重層結晶の製造する場合、CaO又はMgOを重
量で0.03〜1.55wt%含む酸化タングステン又は酸
化モリブデン粉末を還元雰囲気中にて、粉末冶金
法により、直接的に多結晶の金属粉末を生成する
方法又は粉末冶金法により焼結体を生成し、この
焼結体を粉砕して多結晶の金属粉末を生成する方
法等により作製する。次に、この多結晶の金属粉
末を加圧成形して、圧粉体とする。この様な圧粉
体を重ね合わせて、水素等の還元雰囲気中にて、
焼結して各層が互いに結晶学的方位を異にした焼
結体を得る。続いて、この焼結体を、熱間及び温
間等で圧延加工を施して、板状の複合体を水素等
の還元雰囲気中で1800〜2300℃の範囲内の温度
で、好ましくは1〜3時間焼鈍して、互いに重な
る各層が結晶学的方位を異にした単結晶状態を持
つ多層結晶体を得ることが確認された。
更に、本発明においては、モリブデン又はタグ
ステンへの金属粉末への添加量が0.003wt%以下
の場合には、多重層結晶体には粒界は存在しな
い。更に、添加量が0.232wt%以上の場合には、
単結晶層及び多結晶層の複合体が得られるので、
添加量が0.003〜0.115wt%の範囲内であることが
好ましい。
[実施例]
以下本発明を実施例に基づいて説明する。
本発明は、タングステン、モリブデンの双方に
同様に適用できるから、以下の実施例では、いず
れかに限定しないで、説明する。先ず、タングス
テン酸化物あるいはモリブデン酸化物の粉末に、
カルシウム酸化物及びマグネシウム酸化物を種々
の割合いで湿式法によつて添加し、複数種類の原
料粉末を用意した。次に、この原料粉末を粉末冶
金法を用いて、多結晶の金属粉末とした。この添
加量の異なる金属粉末を、板状に成形した後、積
層し、圧力3ton/cm2でプレス成形し第1図に示す
ような、多層構造の成形体を得た。この図のよう
な成形体の各層は、カルシウム酸化物及びマグネ
シウム酸化物の添加濃度が互いに等しく、各層
2,4は、層1,3及び5と異なる添加物濃度を
有し、且つ相互に等しい添加物濃度を有してい
る。この様にして、多層構造を有する複合圧粉体
が得られた。
次に、1800〜2300℃にて水素雰囲気中で、この
複合圧粉体を焼結して、多層構造の焼結体を得
た。更に、この焼結体に1200〜1600℃の範囲内の
温度にて熱間加工を施し、続いて、500〜1000℃
の温度にて、温間加工を施し、最終圧延率が、70
%以上となるようにして、厚さが2〜5mm、幅が
20mm、長さが150mmの圧延品を得た。この圧延品
を、1800〜2300℃の範囲内の温度にて水素雰囲気
中で、1〜3時間焼鈍を行つた。その時の結晶状
態及び温度を第1表に示す。
第1表において、C0は各層1,3,5のCaO
及びMgOの金属粉末への添加量を示し、重量%
0.003wt%と一定である。一方、C1は各層2,4
のCaO及びMgOの金属粉末への添加量を示し、
0.012〜0.155wt%の範囲で変化されている。第1
表では比較のために、C1が0.05〜0.08wt%(比較
例1)、及び0.232〜0.310wt%(比較例2)の試
料も同様に示されている。その結果、比較例1に
示すように、C1が0.005〜0.008wt%である場合、
積層体の結晶状態は、結晶粒界のない単結晶とな
り、所望の多重層結晶とすることが、難しいこと
が、判明した。
[Industrial Field of Application] The present invention relates to tungsten or molybdenum multilayer crystals. [Prior Art] Tungsten and molybdenum belong to group a of the periodic table, and are body-centered cubic lattice transition metals with atomic numbers of 74 and 42, located in the third and second long periods, respectively. Tungsten has the highest melting point of all metal elements
It has a melting point of 3380℃, while molybdenum has a melting point of 2615℃, respectively, which are representative of high melting point rare metals. In addition, the first metallurgical property of tungsten and molybdenum is the ability to withstand high temperatures of 2000°C or higher in a non-oxidizing atmosphere, that is, they are super heat-resistant metal materials that exhibit excellent high-temperature strength. Are known. However, both metals are typical metal materials that have not yet been developed for effective use or put into practical use, except for wire rods. The reason for this is that when tungsten and molybdenum are in a polycrystalline state, their moldability is extremely poor below room temperature.
DBTT (ductile, brittle transition temperature) or higher, each 3
%, due to showing an elongation of 20% or less. Furthermore, when used at high temperatures, polycrystalline tungsten and molybdenum cause coarsening of crystal grains and recrystallization embrittlement, making it impossible to fully demonstrate the characteristics as super heat-resistant materials mentioned above. This is one of the reasons why it is restricted. [Problems to be Solved by the Invention] Generally, molybdenum and tungsten materials are used under harsh conditions at high temperatures and for long periods of time, so once a fracture crack occurs, the polycrystalline state may suffer from recrystallization embrittlement. Rapid destruction occurs at grain boundaries. On the other hand, in order to eliminate the drawbacks of polycrystalline molybdenum and tungsten mentioned above, the recrystallization method is used to
Tungsten with coarse crystals (Japanese Patent Application Laid-Open No. 61-6197
Patent No.) and single crystallized molybdenum (Patent No.
No. 1420928) is known. In this way, single crystallized tungsten and molybdenum may undergo cleavage fracture all at once, and therefore cannot be said to be sufficiently reliable as a material. SUMMARY OF THE INVENTION It is therefore an object of the present invention to provide tungsten and molybdenum materials that have strength, particularly sagging resistance and reliability, without recrystallization brittleness at high temperatures. In the case of a multilayer crystal made of these molybdenum and tungsten materials, even if fracture fracture occurs on the crystal surface, there are grain boundaries between the crystal grains of each layer and the crystal orientation is different. This results in increased strength and reliability of the material, without causing confinement in the crystals in each layer and leading to rapid fracture. Therefore, if it is possible to provide multiple crystals with grain boundaries parallel to the plates, it will be possible to use them in general reactor materials such as atomic route materials that require high-temperature strength and reliability, and the field of application will expand. , significantly expanded. Therefore, another technical object of the present invention is to provide a method for manufacturing tungsten or molybdenum multiple crystals that can easily manufacture the tungsten or molybdenum multiple crystals. [Means for Solving the Problems] According to the present invention, it is composed of two or more multilayers having crystal grain boundaries parallel to the plate plane, and the layers that overlap each other in these multilayers have crystallographic orientations that are different from each other. A tungsten or molybdenum multilayer crystal is obtained, which is characterized by having single crystal states with different tungsten or molybdenum crystals. According to the present invention, a multilayer crystal is manufactured by laminating and molding tungsten or molybdenum polycrystals to form a molded body, and annealing the molded body to exhibit a crystal state in which adjacent layers have mutually aligned crystal orientations. method is obtained. Specifically, when producing tungsten or molybdenum multilayer crystals, tungsten oxide or molybdenum oxide powder containing 0.03 to 1.55 wt% of CaO or MgO is directly processed by powder metallurgy in a reducing atmosphere. It is produced by a method of producing polycrystalline metal powder, or by a method of producing a sintered body using a powder metallurgy method, and pulverizing the sintered body to produce polycrystalline metal powder. Next, this polycrystalline metal powder is pressure-molded to form a green compact. Such compacted powder bodies are stacked one on top of the other, and in a reducing atmosphere such as hydrogen,
By sintering, a sintered body in which each layer has a different crystallographic orientation is obtained. Subsequently, this sintered body is subjected to hot and warm rolling processing to form a plate-shaped composite in a reducing atmosphere such as hydrogen at a temperature within the range of 1800 to 2300°C, preferably 1 to 2300°C. It was confirmed that by annealing for 3 hours, a multilayered crystal body having a single crystal state in which the layers overlapped with each other had different crystallographic orientations was obtained. Furthermore, in the present invention, if the amount of molybdenum or tagsten added to the metal powder is 0.003 wt% or less, no grain boundaries exist in the multilayer crystal. Furthermore, if the amount added is 0.232wt% or more,
Since a composite of single crystal and polycrystalline layers is obtained,
It is preferable that the amount added is within the range of 0.003 to 0.115 wt%. [Examples] The present invention will be described below based on Examples. Since the present invention can be similarly applied to both tungsten and molybdenum, the following examples will be described without limiting to either of them. First, tungsten oxide or molybdenum oxide powder is
Calcium oxide and magnesium oxide were added in various proportions by a wet method to prepare a plurality of types of raw material powders. Next, this raw material powder was made into polycrystalline metal powder using a powder metallurgy method. These metal powders with different amounts added were formed into plate shapes, then laminated and press-molded at a pressure of 3 tons/cm 2 to obtain a molded body with a multilayer structure as shown in FIG. Each layer of the molded body as shown in this figure has the same additive concentration of calcium oxide and magnesium oxide, and each layer 2, 4 has a different additive concentration than layers 1, 3, and 5, and is mutually equal. It has an additive concentration. In this way, a composite green compact having a multilayer structure was obtained. Next, this composite powder compact was sintered in a hydrogen atmosphere at 1800 to 2300°C to obtain a multilayered sintered body. Furthermore, this sintered body is subjected to hot working at a temperature within the range of 1200 to 1600℃, and then heated to 500 to 1000℃.
The final rolling reduction was 70.
% or more, with a thickness of 2 to 5 mm and a width of
A rolled product with a length of 20 mm and a length of 150 mm was obtained. This rolled product was annealed in a hydrogen atmosphere at a temperature in the range of 1800 to 2300°C for 1 to 3 hours. Table 1 shows the crystal state and temperature at that time. In Table 1, C 0 is CaO of each layer 1, 3, and 5.
and the amount of MgO added to the metal powder, weight%
It is constant at 0.003wt%. On the other hand, C 1 is each layer 2, 4
Indicates the amount of CaO and MgO added to the metal powder,
It is varied in the range of 0.012 to 0.155wt%. 1st
For comparison, samples with C1 of 0.05 to 0.08 wt% (Comparative Example 1) and 0.232 to 0.310 wt% (Comparative Example 2) are also shown in the table. As a result, as shown in Comparative Example 1, when C 1 is 0.005 to 0.008 wt%,
It has been found that the crystalline state of the laminate is a single crystal without grain boundaries, and that it is difficult to form the desired multilayer crystal.
【表】
これは、カルシウム酸化物、マグネシウム酸化
物の含有量が0.008wt%以下の場合にはC0層とC1
層の結晶粒成長に対するピンニング効果の差が小
さいために層境界で粒成長を抑制できないためで
ある。
更に、比較例2として、C0が0.03wt%でC1が
0.232wt%以上の層は、単結晶層及び多結晶層の
複合体が形成された。
このように、カルシウム酸化物及びマグネシウ
ム酸化物の添加量が0.232wt%以上の場合には、
カルシウム酸化物、マグネシウム酸化物の添加量
が多いので、結晶粒成長に対するピンニング効果
が強力となり、粒成長を抑制するためであると推
測できる。
一方、実施例として上げられているC0が
0.03wt%及びC1が0.012〜0.155wt%の範囲内にお
いては、5重層の各層が単結晶であり、しかも、
各層内には、結晶粒界が、存在することが、確認
された。この様な実施例に係る試料は高温におい
ても再結晶脆性を引き起こすことなく、耐垂下性
を有し、また破壊時にも急激な破壊伝播を引き起
こすことなく高い信頼性を有することが判明し
た。
[発明の効果]
以上説明したように、本発明によれば、カルシ
ウム酸化物又はマグネシウム酸化物の少くとも一
方を総量で0.003〜0.115wt%を含むタングステン
又はモリブデン多重層結晶は、耐垂下性及び急激
な破壊伝播を持たず、原子炉、核融合炉材、及び
一般炉材等の超高温耐熱材料としての用途は実に
幅広い。
更に、本発明によれば、カルシウム酸化物又は
マグネシウム酸化物の少くとも一方を総量で
0.003〜0.115wt%含むタングステン又はモリブデ
ン圧粉体を積層成形させた後焼鈍させることによ
り、板面な平行な1つ以上の結晶粒界を有するタ
ングステンまたはモリブデン多重層結晶材料を得
るタングステン又はモリブデン多重層結晶の製造
方法を提供することである。[Table] This shows that when the content of calcium oxide and magnesium oxide is 0.008wt% or less, the C0 layer and C1
This is because grain growth cannot be suppressed at layer boundaries because the difference in pinning effect on grain growth between layers is small. Furthermore, as Comparative Example 2, C 0 is 0.03wt% and C 1 is
A composite of a single crystal layer and a polycrystalline layer was formed in the layer containing 0.232 wt% or more. In this way, when the amount of calcium oxide and magnesium oxide added is 0.232wt% or more,
It can be inferred that this is because the addition amount of calcium oxide and magnesium oxide is large, so the pinning effect on crystal grain growth is strong, and grain growth is suppressed. On the other hand, C 0 given as an example is
Within the range of 0.03 wt% and C1 of 0.012 to 0.155 wt%, each layer of the 5-layer is single crystal, and
It was confirmed that grain boundaries existed within each layer. It has been found that the samples according to these examples have sag resistance without causing recrystallization embrittlement even at high temperatures, and have high reliability without causing rapid fracture propagation even at the time of fracture. [Effects of the Invention] As explained above, according to the present invention, a tungsten or molybdenum multilayer crystal containing at least one of calcium oxide and magnesium oxide in a total amount of 0.003 to 0.115 wt% has excellent sagging resistance and It does not have rapid fracture propagation and has a wide range of uses as an ultra-high temperature heat-resistant material for nuclear reactors, fusion reactor materials, general reactor materials, etc. Furthermore, according to the present invention, the total amount of at least one of calcium oxide and magnesium oxide is
A tungsten or molybdenum multilayer crystal material having one or more parallel crystal grain boundaries on a plate surface is obtained by laminating and annealing a tungsten or molybdenum green compact containing 0.003 to 0.115 wt%. An object of the present invention is to provide a method for manufacturing a multilayer crystal.
第1図は本発明の実施例に係るモリブデン又は
タングステン多結晶を示す斜視図である。
図中、1,3,5はC0層、2及び4はC1層で
ある。
FIG. 1 is a perspective view showing a molybdenum or tungsten polycrystal according to an embodiment of the present invention. In the figure, 1, 3, and 5 are C 0 layers, and 2 and 4 are C 1 layers.
Claims (1)
重層から構成され、該多重層のうちで互いに隣接
する各層は互いに結晶学的方位を異にした単結晶
状態を有することを特徴とするタングステン又は
モリブデン多重層結晶。 2 互いに異なる両の添加物を含むタングステン
及びモリブデンのいずれか一方の多結晶体を複数
層積層して成形し、次に互いに隣接する層が互い
に結晶学的方位の異なる単結晶状態を形成するよ
うに、焼鈍することを特徴とするタングステンま
たはモリブデンの多重層結晶の製造方法。 3 タングステン又はモリブデンに、添加物とし
て酸化カルシウム及び酸化マグネシウムの少くと
も1種を重量で0.03〜0.155wt%含む多結晶の金
属粉末を生成する原料準備工程と、上記金属粉末
を加圧成形して多層構造の複合圧粉体を成形する
積層工程と、上記複合圧粉体を還元雰囲気中で焼
結して多層構造の焼結体を得る焼結工程と、上記
焼結体を加工の後、還元雰囲気中で1800〜2300℃
の範囲内の温度で、焼鈍を行う焼鈍工程を有する
ことを特徴とするタングステン又はモリブデン多
重層結晶の製造方法。[Claims] 1. Consisting of two or more multilayers having grain boundaries parallel to the plate surface, each adjacent layer among the multilayers is in a single crystal state with mutually different crystallographic orientations. A tungsten or molybdenum multilayer crystal comprising: 2 Multiple layers of polycrystals of either tungsten or molybdenum containing different additives are laminated and molded, and then adjacent layers are formed in a single crystal state with different crystallographic orientations. A method for producing a multilayer crystal of tungsten or molybdenum, which comprises annealing the crystal. 3. A raw material preparation step of producing a polycrystalline metal powder containing 0.03 to 0.155 wt% by weight of at least one of calcium oxide and magnesium oxide as an additive to tungsten or molybdenum, and press molding the metal powder. a lamination step of forming a multi-layered composite compact; a sintering step of sintering the composite compact in a reducing atmosphere to obtain a multi-layered compact; and after processing the sintered compact, 1800~2300℃ in reducing atmosphere
A method for producing a tungsten or molybdenum multilayer crystal, comprising an annealing step of performing annealing at a temperature within the range of .
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP15953388A JPH029786A (en) | 1988-06-29 | 1988-06-29 | Tungsten or molybdenum multilayer crystal and manufacturing method thereof |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP15953388A JPH029786A (en) | 1988-06-29 | 1988-06-29 | Tungsten or molybdenum multilayer crystal and manufacturing method thereof |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPH029786A JPH029786A (en) | 1990-01-12 |
| JPH0474314B2 true JPH0474314B2 (en) | 1992-11-25 |
Family
ID=15695848
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP15953388A Granted JPH029786A (en) | 1988-06-29 | 1988-06-29 | Tungsten or molybdenum multilayer crystal and manufacturing method thereof |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPH029786A (en) |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN120210624A (en) * | 2021-04-06 | 2025-06-27 | 联合材料公司 | Tungsten Material |
-
1988
- 1988-06-29 JP JP15953388A patent/JPH029786A/en active Granted
Also Published As
| Publication number | Publication date |
|---|---|
| JPH029786A (en) | 1990-01-12 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US6444049B1 (en) | Method for producing high silicon steel, and silicon steel | |
| US4025379A (en) | Method of making laminated magnetic material | |
| JP2001518681A (en) | Substrate with improved oxidation resistance | |
| CN105264100B (en) | The method for preparing metal foil | |
| CN105209188B (en) | The method for preparing metal foil | |
| JP2000509438A (en) | Thin-walled monolithic metal oxide structures made from metal and methods of making such structures | |
| JP5581505B2 (en) | Magnesium alloy sheet | |
| JP4591900B2 (en) | Method for producing Ti-Al intermetallic compound plate | |
| EP0261063B1 (en) | Method for producing self-supporting ceramic bodies with graded properties | |
| JPH0474314B2 (en) | ||
| KR101231936B1 (en) | Nickel-based semifinished product having a cube recrystallization texture, corresponding method of production and use | |
| KR101568493B1 (en) | Magnesium alloys plate and method for manufacturing the same | |
| US5284823A (en) | Superplastic forming of YBa2 Cu3 O7-x ceramic superconductors with or without silver addition | |
| JP2005097671A (en) | Ti-Al intermetallic compound and method for producing the same | |
| US4428778A (en) | Process for producing metallic chromium plates and sheets | |
| KR100288270B1 (en) | Manufacturing method for multi-layered titanium-aluminide intermetallic compound sheet | |
| Bordeaux et al. | Formation of amorphous phase by solid state reaction in elemental composites prepared by cold rolling | |
| JPH024398B2 (en) | ||
| CN113246558A (en) | Copper-aluminum alloy with layered structure and gradient stacking fault energy and preparation method thereof | |
| JP3621294B2 (en) | Oxide superconducting compression molded conductor and manufacturing method thereof | |
| JPH0119458B2 (en) | ||
| US3501277A (en) | Ductile cobalt strip | |
| JPH0279310A (en) | Manufacture of oxide superconductive wire | |
| JPH0359137B2 (en) | ||
| JP2003220663A (en) | Composite heat-resistant plate and its manufacturing method |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| EXPY | Cancellation because of completion of term |