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JPH0431790B2 - - Google Patents
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JPH0431790B2 - - Google Patents

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Publication number
JPH0431790B2
JPH0431790B2 JP59010331A JP1033184A JPH0431790B2 JP H0431790 B2 JPH0431790 B2 JP H0431790B2 JP 59010331 A JP59010331 A JP 59010331A JP 1033184 A JP1033184 A JP 1033184A JP H0431790 B2 JPH0431790 B2 JP H0431790B2
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Japan
Prior art keywords
steel
welding
strength
welded
point
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 - Lifetime
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JP59010331A
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Japanese (ja)
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JPS60154886A (en
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Priority to JP1033184A priority Critical patent/JPS60154886A/en
Publication of JPS60154886A publication Critical patent/JPS60154886A/en
Publication of JPH0431790B2 publication Critical patent/JPH0431790B2/ja
Granted legal-status Critical Current

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Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23KSOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K15/00Electron-beam welding or cutting
    • B23K15/0046Welding
    • B23K15/0093Welding characterised by the properties of the materials to be welded

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Arc Welding In General (AREA)
  • Welding Or Cutting Using Electron Beams (AREA)

Description

【発明の詳細な説明】[Detailed description of the invention]

本発明は超高強力マルエージング鋼の溶接に関
するもので、さらに詳しくは、高い継手効率を得
るための18%Niマルエージング鋼の電子ビーム
溶接法またはTIG溶接法に関するものである。 18%Niマルエージング鋼は通常重量比にて C:0.03%以下、 Si:0.10%以下、 Mn:0.010%以下、 P:0.010%以下、 S:0.010%以下、 Ni:17.0〜19.0%、 Co:7.0〜15.0%、 Mo:3.0〜6.5%、 Ti:0.2〜1.5%、 Al:0.3%以下 を含み、さらに必要に応じて、B、CaまたはZr
等を含有する析出強化鋼である。この鋼は比較的
簡単な熱処理により、高い強度と良好な靱性を併
せ有するため、固体燃料ロケツトモーターケー
ス、深海潜水艇、ウラン遠心分離機回転胴筒など
に用いられている。 これらの用途においては、強度/密度比が重要
な要素となるため、高強度化の要求が強く、これ
に応えるため当初開発された 18%Ni−8〜9%Co−3〜5%Mo−0.4〜0.5
%Ti から成る引張強さ180〜210Kgf/mm2級鋼に加え
て、さらに高強度のマルエージング鋼が開発され
ている。すなわち、 18%Ni−12.5%Co−3%Mo−1.2%Ti鋼や、 18%Ni−15〜20%Co−5〜6.5%Mo−1%Ti
−0.05〜0.3%Al(特開昭58−25457) 等がそれで、それぞれ、245Kgf/mm2および270
Kgf/mm2の引張強さを有する。 これらの超高強度マルエージング鋼開発の考え
方は以下の通りである。 マルエージング鋼の時効処理後の強度には
Mo、CoおよびTiが主として寄与し、これらの元
素含有量が増加するほど強度が増加する。 一方、これらの元素のうちMoおよびTiは溶体
化処理後の冷却時のオーステナイト相からマルテ
ンサイト相への変態を開始する温度(以下この温
度をMs点という)を大きく低下させる元素であ
り、これらの元素含有量が多くなるとMs点が常
温近傍まで低下するため、時効処理による硬化を
得るために必要なマルテンサイト相中に多量のオ
ーステナイト相が残留し(以下これを残留オース
テナイト相という)十分な硬化が得られなくな
る。またMoは、これを多量に含有させると、製
造時にさらされる高温において粗大な金属間化合
物を形成し、靱性を害する。 以上の観点から、Ms点を低下させる作用の小
さいCo含有量を多くし、Mo含有量を低目に抑え
ることにより、強度の上昇を確保するとともに靱
性の低下を抑えている。 さて、上記用途の多くにおいて、工場で製造さ
れた鋼板を、必要な形状に加工後溶接した後、溶
体化処理を施し、対で時効処理するか、あるい
は、溶接後直接時効処理を施して、使用する。こ
の場合通常、TIG溶接法が採用されるが、溶接部
には溶接金属の凝固時に生ずる濃化偏析に起因す
る強度低下が生ずる。すなわち、溶接金属の凝固
相は基本的には通常の鋼塊の凝固相と同様、樹枝
状に発達するが、樹枝状晶間の最終凝固相には
Ni、Mo、Tiが濃化するため、その部分のMs点
が低下し、冷却後残留オーステナイト相となる。
このオーステナイト相は安定で、溶接後の800℃
〜900℃での溶体化処理によつては消滅しないた
め、溶接金属の強度は鋼板強度より低くなる。 ところが、鋼板の強度を増加させるためには、
前述のごとく、Co、Mo、Tiの含有量を増加する
ことが必要であり、Mo、Tiの添加を抑えてMs
点の低下を抑えてはいるものの、鋼板の強度が増
加するほど、溶接金属中の残留オーステナイト相
が増え、強度の低下が著しくなる。構造物の設計
は、強度の最も低い部分の強度を基準にしてなさ
れるため、溶接継手の強度が低い場合には鋼板自
体の強度が増加してもこれが設計に反映されない
ことになる。 上記問題点を解決する方策として、溶接後、溶
接部を含めて冷間加工を加えるという技術が特開
昭51−122616に開示されている。これは、溶接後
溶体化処理して、その後60〜85%の冷間加工を加
えた時効処理を施すことにより、溶接継手の強度
および靱性を母材のそれと同等にし得るというも
のである。しかし、溶接された構造物を冷間加工
するのは、非常に特殊な構造物に限られ、全ての
溶接構造物に適用することはできない。 一法、溶接後溶接金属のみあるいは構造物全体
を、溶接金属中の濃化偏析部が十分拡散、均一化
する温度にまで加熱する方法も考えられるが、そ
のためには1000℃以上に加熱することが必要であ
り、この場合高温加熱による母材特性の劣化が避
けられない。 本発明者らは、このような難点を克服すべく、
強度およびMs点に及ぼすこられの元素の影響、
凝固時の偏析度などを詳細に検討した結果、電子
ビーム溶接におけるインサートメタルまたはTIG
溶接における溶加棒の成分を適切に定めることに
よつて、溶接金属の組成をある範囲内に調整する
ことにより優れた継手効率を得る本発明を成しと
げるに至つた。 以下、本発明者らが行つた試験について詳細に
説明する。 17〜19%Ni−7〜15%Co−4〜6.5%Mo−0.3
〜1.5%Tiの組成を有するマルエージング鋼を実
験炉で溶製し、十分な均熱した後厚さ15mmの鋼板
に圧延した。これらの鋼板について、850℃〜900
℃での溶体化処理後Ms点を測定するとともに、
480℃、5時間の時効処理後引張試験を行つた。 また、一部については、入熱6000〜8000J/cm
の条件で電子ビーム溶接、または共金溶接棒で
20000J/cm、15パスの条件でTIG溶接を行い、鋼
板と同様の溶体化処理、時効処理の後、溶接金属
の残留オーステナイト量を測定するとともに
EPMA(エレクトロンプローベマイクロアナライ
ザ)により濃化偏析量を測定した。 第1図は、鋼板の強度とMo、CoおよびTi含有
量との関係を示すもので、 Mo当量=(%Mo)+1/3×(%Co) +3×(%Ti) ……(1) と定義すると、 引張強さ=9.7×(Mo当量)+117 ……(2) の関係があることが分る。 第2図は鋼板のMs点と合金元素含有率との関
係を示すもので、鋼板のMs点の計算値を、 Ms=941−26×(%Ni)−1.7 ×(%Co)−51×(%Mo) −18×(%Ti) ……(3) で表わし、Ms点の実測値と対比したもので、極
めて良好な一致が見られる。 一方EPMAによる溶接金属の偏析度、すなわ
ち、偏析部含有率/平均含有率は以下のように測
定された。 Ni:1.1、Co:1.0、 Mo:1.5、Ti:2.0、 この偏析度は、電子ビーム溶接およびTIG溶接
に限つて見れば、入熱量に関係なくほぼ一定であ
つた。 この偏析度を上記(3)式の各々の元素の係数に掛
けることにより、溶接金属の濃化偏析部のMs点
を次の(4)式のように推定するこができる。 Ms=941−28×(%Ni) −1.7×(%Co) −71(%Mo) −38(%Ti) ……(4) ただし、(%Ni)、(%Co)、(%Mo)、および
(%Ti)は溶接金属中のそれぞれの元素の平均含
有率である。 第3図は、電子ビーム溶接金属組織中の残留オ
ーステナイト相の割合と溶接金属濃化偏析部の推
定Ms点との関係を示したもので、推定Ms点が約
110℃以下になるとオーステナイトが残留し始め、
推定Ms点が低下するにつれて残留オーステナイ
ト相の割合が増えることがわかる。 本発明は以上の示したように、溶接金属におい
て、 () 最大濃化偏析部のMs点が110℃以上にな
るように組成を限定することにより、強度低下
の原因となる残留オーステナイトを実質的に0
にすること () それに加えて、Mo当量を母材のMo当
量以上に限定することにより、実質的にマルテ
ンサイト単相の時効により母材以上の強度を保
障すること の2条件を確保することによつて高い溶接継手効
率を得るものであり、上述のようにその硬化はあ
きらかである。 なお、最大濃化偏析部のMs点が200をこえると
上記(1)、(2)および(4)式の関係より、Mo当量が小
さくなりマルエージング鋼として十分な強度が得
られないため、Ms点の上限を200以下に限定す
る。また、溶接部のMo当量が(母材のMo当量
+1)を越えると溶接金属の強度が必要以上に上
りすぎて脆化するので好ましくない。 上記知見はインサートメタルあるいは溶加棒を
使用しない、いわゆるビードオンプレートの継手
について得られたものであるが、インサートメタ
ルあるいは溶加棒を使用する電子ビーム溶接ある
いはTIG溶接においては、母材の溶込み量を考慮
したうえ、溶接金属組成が上記()および
()で限定する組成になるようにインサートメ
タルあるいは溶加棒の組成を設計する必要があ
る。母材の溶込み量は、溶接方法、溶接条件によ
つて異なるが、インサートメタルを使用した電子
ビーム溶接の場合は40〜60%、溶加棒を使用した
TIG溶接の場合は20〜40%が正常である。 次に実施例を挙げて本発明の硬化を具体的に説
明する。 実施例 第1表に示す組成の18%Niマルエージング鋼
No.1、No.2の50Kg鋼塊を真空中で溶製した。 鋼No.1は210Kgf/mm2、鋼No.2は245Kgf/mm2
のマルエージング鋼である。 1200℃で24時間均質化したのち、熱間鍛造、圧
延により厚さ15mmの鋼板に仕上げ、900℃で溶体
化した。 一方、溶加棒またはインサートメタル用に供す
るため、第2表に示す組成の18%Niマルエージ
ング鋼の10Kg鋼塊A,B,C,Dを真空中で溶製
した。1200℃で24時間均質化した後、熱間鍛造、
圧延により3mmの鋼板に仕上げた、900℃溶体化
の後、一部は厚さ2mmに、他の厚さ1mmに冷間圧
延した。これらの冷延板を900℃で溶体化し、酸
洗したのち、厚さ2mmの鋼板は2mm角の棒に仕上
げた。 鋼Aは鋼No.1と組合わせることにより、また鋼
Cは鋼No.2と組み合わせることにより、本発明の
限定範囲を満足するものである。鋼Bおよび鋼D
はそれぞれ鋼No.1および鋼No.2と組合わされるも
のであるが、鋼Bは被溶接鋼である鋼No.1に比べ
てMo当量の小さいもの、鋼DはMo当量が被溶
接鋼である鋼No.2のそれより大であるが、Ms点
が低く、溶接金属のMs点が本発明の限定簡易か
ら外れるものである。 以上の熱延板および冷延板ならびに角棒を用い
て以下の試験を行つた。 (1) 15mm熱延板について480℃、5時間の時効処
理後引張試験を行つた。 (2) 第4図に示すように、15mm熱延板1の圧延方
向に直角に、板面に垂直な開先を加工し、 (a) そのまま2枚を突合わせて溶接部2を電子
ビーム溶接 (b) 開先の間に厚さ1mmの冷延板4をはさみ電
子ビーム溶接 して継手を製作し、900℃で溶体処理した。第4
図で3は電子ビームを示し、溶接入熱は8000J/
cmとした。これらの継手の溶接金属について組織
観察により残留オーステナイト相の割合を測定す
るとともに、ビードに直角かつ溶接金属が試験片
平行部の中央になるように平行部径10mm、平行部
長さ50mmの引張試験片を加工し、480℃、5時間
の時効処理後引張試験を行つた。また溶接金属の
組成分析も行つた。 (3) 第5図に示すように、15mm熱延板1の圧延方
向に直角に板面に対して75度の角度を持つたV
型開先を加工し、共金または前記2mm角の棒を
溶加棒とし母材と同材の裏当金5を用いてTIG
溶接によつて継手を製作し、900℃で溶体化処
理した。溶接は溶接速度150mm/分で18パスと
し、電流120〜210A、電圧11〜13Vで行つた。
これらの継手について上記(2)と同様の試験を行
つた。 第3表に試験結果をまとめて示した。 鋼No.1を被溶接鋼板とし、鋼Aを電子ビーム溶
接におけるインサートメタルまたはTIG溶接にお
ける溶加棒とした組合せ、ならびに鋼No.2を被溶
接鋼板とし、鋼Cを電子ビーム溶接におけるイン
サートメタルまたはTIG溶接における溶加棒とし
た組合せの場合、Ms点は本発明の限定範囲内に
入り、継手効率99〜100%を示している。 一方、鋼No.1と鋼Bとの組合せ、鋼No.2と鋼D
との組合せ、または鋼No.1および鋼No.2のそれぞ
れのインサートメタルなしの電子ビーム溶接、共
金溶加棒によるTIG溶接の場合は、Mo当量が被
溶接鋼板のそれよりも小さいかまたはMs点が100
℃より低くなり、継手効率は84〜96%と低かつ
た。 以上の通り、本発明の方法により、18%Niマ
ルエージング鋼の溶接部の継手効率が大きく改善
されることが明らかである。 なお、上記実施例では主として18%Niマルエ
ージング鋼について述べたが、本発明の方法は他
のマルエージング鋼にも同様に適用することがで
きる。
The present invention relates to welding ultra-high strength maraging steel, and more particularly to electron beam welding or TIG welding of 18% Ni maraging steel to obtain high joint efficiency. 18%Ni maraging steel usually has the following weight ratio: C: 0.03% or less, Si: 0.10% or less, Mn: 0.010% or less, P: 0.010% or less, S: 0.010% or less, Ni: 17.0-19.0%, Co : 7.0 to 15.0%, Mo: 3.0 to 6.5%, Ti: 0.2 to 1.5%, Al: 0.3% or less, and further contains B, Ca or Zr as necessary.
It is a precipitation-strengthened steel containing Because this steel has both high strength and good toughness through relatively simple heat treatment, it is used in solid fuel rocket motor cases, deep-sea submersibles, and uranium centrifuge rotating barrels. In these applications, the strength/density ratio is an important factor, so there is a strong demand for higher strength, and to meet this demand, 18%Ni-8-9%Co-3-5%Mo- 0.4~0.5
In addition to class 2 steel with a tensile strength of 180 to 210 Kgf/mm, which consists of %Ti, even higher strength maraging steels have been developed. That is, 18%Ni-12.5%Co-3%Mo-1.2%Ti steel, 18%Ni-15~20%Co-5~6.5%Mo-1%Ti
−0.05 to 0.3% Al (Japanese Unexamined Patent Publication No. 58-25457) etc. are 245Kgf/ mm2 and 270Kgf/mm2, respectively.
It has a tensile strength of Kgf/ mm2 . The concept behind the development of these ultra-high strength maraging steels is as follows. The strength of maraging steel after aging treatment is
Mo, Co and Ti mainly contribute, and the strength increases as the content of these elements increases. On the other hand, among these elements, Mo and Ti are elements that significantly lower the temperature at which the transformation from austenite phase to martensite phase starts (hereinafter referred to as the Ms point) during cooling after solution treatment. When the element content of Hardening cannot be obtained. Furthermore, when Mo is contained in a large amount, it forms coarse intermetallic compounds at high temperatures exposed during manufacturing, impairing toughness. From the above viewpoint, by increasing the Co content, which has a small effect of lowering the Ms point, and keeping the Mo content low, an increase in strength is ensured and a decrease in toughness is suppressed. Now, in many of the above applications, steel plates manufactured in a factory are processed into the required shape and then welded, then subjected to solution treatment and aged in pairs, or directly aged after welding. use. In this case, TIG welding is usually used, but the strength of the welded part is reduced due to concentration segregation that occurs during solidification of the weld metal. In other words, the solidification phase of weld metal basically develops into a dendritic shape, similar to the solidification phase of a normal steel ingot, but the final solidification phase between the dendrites is
Since Ni, Mo, and Ti are concentrated, the Ms point of that part decreases and becomes a retained austenite phase after cooling.
This austenite phase is stable and can be heated up to 800℃ after welding.
Since it is not eliminated by solution treatment at ~900°C, the strength of the weld metal becomes lower than the strength of the steel sheet. However, in order to increase the strength of steel plates,
As mentioned above, it is necessary to increase the content of Co, Mo, and Ti, and by suppressing the addition of Mo and Ti, Ms.
Although the decrease in the point is suppressed, as the strength of the steel sheet increases, the amount of retained austenite phase in the weld metal increases, and the decrease in strength becomes more significant. Since the design of a structure is based on the strength of the lowest strength part, if the strength of the welded joint is low, even if the strength of the steel plate itself increases, this will not be reflected in the design. As a measure to solve the above-mentioned problems, a technique is disclosed in JP-A-51-122616 in which cold working is applied to the welded part after welding. This means that the strength and toughness of the welded joint can be made equivalent to that of the base metal by performing a solution treatment after welding and then an aging treatment with 60 to 85% cold working. However, cold working of welded structures is limited to very specific structures and cannot be applied to all welded structures. One method is to heat only the weld metal or the entire structure after welding to a temperature at which the concentrated segregated parts in the weld metal are sufficiently diffused and homogenized, but for this purpose, it is necessary to heat the weld metal to a temperature of 1000℃ or higher. In this case, deterioration of the base material properties due to high temperature heating is unavoidable. The present inventors, in order to overcome such difficulties,
The influence of these elements on the strength and Ms point,
As a result of a detailed study of the degree of segregation during solidification, we found that insert metal or TIG in electron beam welding
By appropriately determining the components of the filler rod in welding, we have achieved the present invention, which achieves excellent joint efficiency by adjusting the composition of the weld metal within a certain range. Hereinafter, the tests conducted by the present inventors will be explained in detail. 17~19%Ni-7~15%Co-4~6.5%Mo-0.3
Maraging steel with a composition of ~1.5% Ti was melted in an experimental furnace, thoroughly soaked, and then rolled into a 15 mm thick steel plate. For these steel plates, 850℃~900℃
In addition to measuring the Ms point after solution treatment at °C,
After aging at 480°C for 5 hours, a tensile test was conducted. In addition, for some parts, the heat input is 6000 to 8000 J/cm.
Electron beam welding under the conditions of
TIG welding was performed under the conditions of 20,000 J/cm and 15 passes, and after solution treatment and aging treatment similar to steel plates, the amount of retained austenite in the weld metal was measured.
The amount of concentrated segregation was measured using an electron probe microanalyzer (EPMA). Figure 1 shows the relationship between the strength of a steel plate and the Mo, Co, and Ti contents. Mo equivalent = (%Mo) + 1/3 x (%Co) + 3 x (%Ti) ... (1) When defined as , it can be seen that there is a relationship as follows: tensile strength = 9.7 x (Mo equivalent) + 117... (2). Figure 2 shows the relationship between the Ms point of the steel plate and the alloying element content. It is expressed as (%Mo) −18×(%Ti) (3) and is compared with the actual measured value at the Ms point, and an extremely good agreement can be seen. On the other hand, the degree of segregation of weld metal by EPMA, that is, the segregation content ratio/average content ratio, was measured as follows. Ni: 1.1, Co: 1.0, Mo: 1.5, Ti: 2.0. This degree of segregation was almost constant regardless of the heat input when looking only at electron beam welding and TIG welding. By multiplying the coefficient of each element in the above equation (3) by this segregation degree, the Ms point of the concentrated segregation part of the weld metal can be estimated as shown in the following equation (4). Ms=941−28×(%Ni) −1.7×(%Co) −71(%Mo) −38(%Ti) ……(4) However, (%Ni), (%Co), (%Mo) , and (%Ti) are the average content of each element in the weld metal. Figure 3 shows the relationship between the proportion of retained austenite phase in the electron beam weld metal structure and the estimated Ms point of the weld metal concentrated and segregated area.
When the temperature drops below 110℃, austenite begins to remain,
It can be seen that as the estimated Ms point decreases, the proportion of retained austenite phase increases. As shown above, the present invention substantially eliminates retained austenite, which causes strength reduction, by limiting the composition of the weld metal so that the Ms point of the maximum concentration segregation zone is 110°C or higher. to 0
() In addition, by limiting the Mo equivalent to more than the Mo equivalent of the base material, the two conditions of ensuring strength greater than that of the base material due to aging of the martensite single phase can be ensured. High welded joint efficiency is obtained by this method, and as mentioned above, its hardening is obvious. Furthermore, if the Ms point of the maximum concentration segregation part exceeds 200, the Mo equivalent will become small and sufficient strength as a maraging steel will not be obtained, according to the relationships in equations (1), (2), and (4) above. Limit the upper limit of Ms points to 200 or less. Furthermore, if the Mo equivalent of the weld exceeds (Mo equivalent of the base metal + 1), the strength of the weld metal increases more than necessary and becomes brittle, which is not preferable. The above findings were obtained for so-called bead-on-plate joints that do not use insert metal or filler rods, but in electron beam welding or TIG welding that uses insert metals or filler rods, the In addition to considering the amount of filler metal, it is necessary to design the composition of the insert metal or filler rod so that the weld metal composition is as limited by () and () above. The amount of base metal penetration varies depending on the welding method and welding conditions, but it is 40 to 60% in the case of electron beam welding using insert metal, and 40% to 60% in the case of electron beam welding using insert metal, and
For TIG welding, 20-40% is normal. Next, the curing of the present invention will be specifically explained with reference to Examples. Example 18% Ni maraging steel with the composition shown in Table 1
50Kg steel ingots No. 1 and No. 2 were melted in vacuum. Steel No. 1 is a 210Kgf/mm 2 maraging steel, and Steel No. 2 is a 245Kgf/mm 2 grade maraging steel. After homogenizing at 1200℃ for 24 hours, it was hot forged and rolled into a 15mm thick steel plate, which was then solution-treated at 900℃. On the other hand, 10 kg steel ingots A, B, C, and D of 18% Ni maraging steel having the composition shown in Table 2 were melted in vacuum to be used as filler rods or insert metals. After homogenization at 1200℃ for 24 hours, hot forging,
A steel plate of 3 mm was finished by rolling, and after solution treatment at 900°C, some were cold rolled to a thickness of 2 mm and others to a thickness of 1 mm. These cold-rolled sheets were solution-treated at 900°C and pickled, and then the 2-mm-thick steel sheets were finished into 2-mm square bars. By combining steel A with steel No. 1, and by combining steel C with steel No. 2, the limited range of the present invention is satisfied. Steel B and Steel D
are combined with steel No. 1 and steel No. 2, respectively, but steel B has a lower Mo equivalent than steel No. 1, which is the steel to be welded, and steel D has a Mo equivalent that is lower than that of the steel to be welded. However, the Ms point is lower than that of Steel No. 2, which is a weld metal, and the Ms point of the weld metal deviates from the limitation and simplicity of the present invention. The following tests were conducted using the above hot-rolled sheets, cold-rolled sheets, and square bars. (1) Tensile tests were conducted on 15 mm hot rolled sheets after aging treatment at 480°C for 5 hours. (2) As shown in Figure 4, a groove is machined perpendicular to the rolling direction of the 15 mm hot-rolled plate 1 and perpendicular to the plate surface. Welding (b) A cold-rolled plate 4 with a thickness of 1 mm was sandwiched between the grooves, electron beam welding was performed to fabricate a joint, and solution treatment was performed at 900°C. Fourth
In the figure, 3 indicates the electron beam, and the welding heat input is 8000J/
cm. The proportion of retained austenite phase was measured by microstructural observation of the weld metal of these joints, and a tensile test piece with a parallel part diameter of 10 mm and a parallel part length of 50 mm was prepared at right angles to the bead and with the weld metal at the center of the parallel part of the test piece. After processing and aging at 480°C for 5 hours, a tensile test was conducted. We also conducted a compositional analysis of the weld metal. (3) As shown in Figure 5, the V
Process the mold groove, use the same metal or the 2 mm square rod mentioned above as a filler rod, and use a backing metal 5 made of the same material as the base material to perform TIG.
The joint was manufactured by welding and solution-treated at 900℃. Welding was performed in 18 passes at a welding speed of 150 mm/min, at a current of 120 to 210 A, and a voltage of 11 to 13 V.
The same tests as in (2) above were conducted on these joints. Table 3 summarizes the test results. Combinations in which Steel No. 1 is the steel plate to be welded and Steel A is the insert metal in electron beam welding or filler rod in TIG welding, and Steel No. 2 is the steel plate to be welded and Steel C is the insert metal in electron beam welding. Alternatively, in the case of a combination as a filler rod in TIG welding, the Ms point falls within the limited range of the present invention, showing a joint efficiency of 99 to 100%. On the other hand, the combination of steel No. 1 and steel B, steel No. 2 and steel D
or in the case of electron beam welding without insert metal for Steel No. 1 and Steel No. 2, or TIG welding using a matching metal filler rod, the Mo equivalent is smaller than that of the steel plate to be welded or Ms score is 100
℃, and the joint efficiency was as low as 84-96%. As described above, it is clear that the method of the present invention greatly improves the joint efficiency of welded parts of 18% Ni maraging steel. In addition, although the above examples mainly described 18% Ni maraging steel, the method of the present invention can be similarly applied to other maraging steels.

【表】【table】

【表】【table】

【表】【table】

【表】【table】 【図面の簡単な説明】[Brief explanation of drawings]

第1図は18%Niマルエージング鋼板の組成と
引張強さとの関係を示すグラフ、第2図は18%
Niマルエージング鋼板の組成とMs点との関係を
示すグラフ、第3図は18%Niマルエージング鋼
電子ビーム溶接溶接金属の濃化偏析部推定Ms点
と組織中の残留オーステナイト相の割合の関係を
示すグラフ、第4図a,bはいずれも電子ビーム
溶接方法における突合せ状態を示す説明図、第5
図はTIG溶接における開先形状を示す説明図であ
る。 1……被溶接鋼板、2……溶接部、3……電子
ビーム、4……インサートメタル、5……裏金。
Figure 1 is a graph showing the relationship between the composition and tensile strength of 18% Ni maraging steel sheets, and Figure 2 is a graph showing the relationship between the composition and tensile strength of 18% Ni maraging steel sheets.
A graph showing the relationship between the composition of Ni maraging steel sheet and the Ms point. Figure 3 shows the relationship between the estimated Ms point of the enriched segregated part of electron beam welded weld metal of 18% Ni maraging steel and the proportion of retained austenite phase in the structure. 4a and 4b are both explanatory diagrams showing the butt state in the electron beam welding method.
The figure is an explanatory diagram showing the groove shape in TIG welding. 1... Steel plate to be welded, 2... Welding part, 3... Electron beam, 4... Insert metal, 5... Backing metal.

Claims (1)

【特許請求の範囲】 1 18%Niマルエージング鋼を溶接後、該溶接
部を時効処理およびまたは溶体化処理をする電子
ビームまたはTIGによる溶接において、溶接金属
の平均組成が、下記(1)式で表わされるそのMs点
の値が110〜200であつて、かつ下記(2)式であらわ
されるそのMo当量の値が母材のMo当量以上に
なるように、インサートメタルまたは溶加棒の組
成を調整することを特徴とする継手効率の優れた
溶接方法。 (1) 式 Ms点 =941−28×(%Ni)−1.7×(%Co) −71(%Mo)−38(%Ti) (2) 式 Mo当量 =(%Mo)+1/3×(%Co)+3×(%Ti) ただし(%Ni)、(%Co)、(%Mo)および(%
Ti)は溶着鋼中の各元素の平均含有量。
[Claims] 1. In electron beam or TIG welding in which 18% Ni maraging steel is welded and then the welded part is subjected to aging treatment and/or solution treatment, the average composition of the weld metal is determined by the following formula (1). The composition of the insert metal or filler rod should be adjusted so that the value of the Ms point, expressed by A welding method with excellent joint efficiency characterized by adjusting. (1) Formula Ms point = 941−28×(%Ni)−1.7×(%Co) −71(%Mo)−38(%Ti) (2) Formula Mo equivalent =(%Mo)+1/3×( %Co)+3×(%Ti) However, (%Ni), (%Co), (%Mo) and (%
Ti) is the average content of each element in the welded steel.
JP1033184A 1984-01-25 1984-01-25 Welding method of 18% marageing steel Granted JPS60154886A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP1033184A JPS60154886A (en) 1984-01-25 1984-01-25 Welding method of 18% marageing steel

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP1033184A JPS60154886A (en) 1984-01-25 1984-01-25 Welding method of 18% marageing steel

Publications (2)

Publication Number Publication Date
JPS60154886A JPS60154886A (en) 1985-08-14
JPH0431790B2 true JPH0431790B2 (en) 1992-05-27

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Application Number Title Priority Date Filing Date
JP1033184A Granted JPS60154886A (en) 1984-01-25 1984-01-25 Welding method of 18% marageing steel

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Country Link
JP (1) JPS60154886A (en)

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JP6707965B2 (en) * 2016-04-14 2020-06-10 日油株式会社 Ammunition container

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JPS60154886A (en) 1985-08-14

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