JPH0459923A - Production of maraging steel excellent in strength, toughness, and ductility - Google Patents

Production of maraging steel excellent in strength, toughness, and ductility

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Publication number
JPH0459923A
JPH0459923A JP16980790A JP16980790A JPH0459923A JP H0459923 A JPH0459923 A JP H0459923A JP 16980790 A JP16980790 A JP 16980790A JP 16980790 A JP16980790 A JP 16980790A JP H0459923 A JPH0459923 A JP H0459923A
Authority
JP
Japan
Prior art keywords
less
solution treatment
ductility
toughness
maraging steel
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
Application number
JP16980790A
Other languages
Japanese (ja)
Inventor
Akihiro Matsuzaki
明博 松崎
Yoshiyuki Saito
斉藤 良行
Osamu Tanigawa
谷川 治
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
JFE Steel Corp
Original Assignee
Kawasaki Steel Corp
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Kawasaki Steel Corp filed Critical Kawasaki Steel Corp
Priority to JP16980790A priority Critical patent/JPH0459923A/en
Publication of JPH0459923A publication Critical patent/JPH0459923A/en
Pending legal-status Critical Current

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  • Heat Treatment Of Steel (AREA)

Abstract

PURPOSE:To stably produce a maraging steel excellent in strength, toughness, and ductility by subjecting a steel having a specific composition containing C, Si, Mn, P, S, Ni, Co, Mo, Ti, Al, and B to specific recrystallization solution treatment. CONSTITUTION:A hot forged maraging steel having a composition containing, by weight, <=0.05% C, <=0.2% Si, <=0.2% Mn, <=0.05% P, <=0.05% S, 10.0-21.0% Ni, 5.0-<9.5% Co, 3.0-12.0% Mo, 0.2-1.6% Ti, <=0.30% Al, and 0.0005-0.0020% B is subjected to recrystallization solution treatment, unrecrystallization solution treatment, and aging heat treatment. At this time, a two-times recrystallization solution treatment consisting of heating up to 1000-1300 deg.C for >=1min, cooling at >=20 deg.C/min cooling rate, further heating up to 800-950 deg.C for >=1min, and cooling is carried out. By this method, the maraging steel excellent in strength, toughness, and ductility can be obtained.

Description

【発明の詳細な説明】 〈産業上の利用分野〉 この発明は、高強度でかつ優れた靭性や延性を必要とす
るロケットモーターケース、圧力容器、ローラ類、シャ
フト類等の構造部材に通用されるマルエージング鋼の製
造方法に関するものである。
[Detailed Description of the Invention] <Industrial Application Field> This invention is applicable to structural members such as rocket motor cases, pressure vessels, rollers, shafts, etc. that require high strength and excellent toughness and ductility. The present invention relates to a method for producing maraging steel.

〈従来の技術〉 現在実用化されているマルエージング鋼の中心的な鋼種
はCOを含有するマルエージング鋼(Fe−18%Ni
 −Co−Mo−Ti−Al)である。マルエージング
鋼は熱間加工による成形加工後、800〜950℃のオ
ーステナイト温度域に加熱後冷却する溶体化処理を施し
て、合金元素の固溶およびオーステナイト粒の微細化を
図るとともに、その後の冷却によりマルテンサイト組織
を得ている。そして260〜650℃の温度域で0.5
〜24時間の時効処理を施すことによってNf、 Mo
、 Ti等の金属間化合物を析出させ硬化を図っている
<Conventional technology> The main type of maraging steel currently in practical use is CO-containing maraging steel (Fe-18%Ni).
-Co-Mo-Ti-Al). After forming by hot working, maraging steel is subjected to solution treatment in which it is heated to an austenitic temperature range of 800 to 950°C and then cooled to dissolve the alloying elements and refine the austenite grains. A martensitic structure is obtained. and 0.5 in the temperature range of 260-650℃
By aging for ~24 hours, Nf, Mo
, hardening is attempted by precipitating intermetallic compounds such as Ti.

また“日1本金属学会会報第25巻第6号(1986)
第550〜552頁”には、マルエージング鋼の基本成
分以外に硼素を添加し、未再結晶溶体化処理を施し強靭
化を図る技術が報告されている。未再結晶域溶体化処理
とは、溶体化処理において未再結晶域のオーステナイト
即ちまだ転位密度の高いオーステナイトから冷却しマル
テンサイト組織を得る熱処理手法であり、これによりマ
ルテンサイトの下部組織が微細化され強靭化が実現され
る0通常のマルエージング鋼ではこのような未再結晶域
のオーステナイト温度Mは非常に狭(、工業的には適用
できない、しかし硼素を添加するとオーステナイトの再
結晶温度が上昇し、未再結晶温度域が拡大されるため工
業的な適用が可能となるものである。このように硼素の
添加は優れた効果を発揮するが、硼素の過剰添加は靭性
や延性の低下をもたらすことも報告されている。
Also, “Japan Institute of Metals Bulletin Volume 25 No. 6 (1986)
On pages 550-552, there is a report on a technology in which boron is added to maraging steel in addition to its basic components, and a non-recrystallized solution treatment is applied to strengthen the maraging steel.What is non-recrystallized solution treatment? , is a heat treatment method in which a martensite structure is obtained by cooling the austenite in the unrecrystallized region, that is, austenite that still has a high dislocation density, during solution treatment to obtain a martensite structure. In maraging steel, the austenite temperature M in such a non-recrystallized region is very narrow (and cannot be applied industrially, but when boron is added, the austenite recrystallization temperature increases and the non-recrystallized temperature range expands. This makes it possible to apply it industrially.As described above, the addition of boron exhibits excellent effects, but it has also been reported that excessive addition of boron causes a decrease in toughness and ductility.

しかし、一方、硼素−t−適量添加した場合でも圧延や
熱処理条件によっては脆化の要因となり得ること、また
その回避手段として圧延と熱処理条件の適切な組合せに
より製造手法が特開昭61−15917号公報に報告さ
れている。
However, even if an appropriate amount of boron is added, it may cause embrittlement depending on the rolling and heat treatment conditions, and as a means to avoid this, a manufacturing method using an appropriate combination of rolling and heat treatment conditions has been proposed. It is reported in the No.

しかしながら、現実には鋼材の形状、板厚等によっては
適切な圧延、熱処理条件を確保することは困難である場
合も多い。
However, in reality, it is often difficult to ensure appropriate rolling and heat treatment conditions depending on the shape, plate thickness, etc. of the steel material.

また硼素含有マルエージング鋼では、熱間加工中に生成
する(あるいはその後の熱処理過程での生成の核となる
)析出物はその後の800〜950 ’Cの通常の溶体
化処理では完全には固溶しないため、破壊靭性を低下さ
せる。また1000℃以上の高温溶体化後に徐冷すると
冷却中にオーステナイト粒界に析出物を生成し、これが
その後の800〜950℃での溶体化処理時の再結晶を
抑制するため結晶粒が微細化されず、延性やンヤルピー
吸収エネルギー値が低くなる。
In addition, in boron-containing maraging steel, precipitates that form during hot working (or become the nucleus of formation during the subsequent heat treatment process) are not completely solidified during the subsequent normal solution treatment at 800 to 950'C. Because it does not dissolve, it reduces fracture toughness. In addition, when slowly cooling after high-temperature solution treatment at 1000°C or higher, precipitates are generated at austenite grain boundaries during cooling, which suppresses recrystallization during subsequent solution treatment at 800 to 950°C, resulting in finer grains. ductility and absorbed energy values are low.

そこで硼素を含有するマルエージング鋼において強度、
靭性、延性の優れた鋼を安定して製造できる手法の開発
が強く望まれていた。
Therefore, in maraging steel containing boron, the strength
There was a strong desire to develop a method that could stably produce steel with excellent toughness and ductility.

〈発明が解決しようとする課題〉 本発明は以上の諸点に鑑みてなされたもので熱間加工条
件を限定することな(、熱処理方法のみの工夫により容
品に従来鋼と同等もしくはそれよりも強度、靭性及び延
性に優れるマルエージング鋼の製造方法を提供すること
を目的とするものである。
<Problems to be Solved by the Invention> The present invention has been made in view of the above points, and does not limit the hot working conditions (by devising only the heat treatment method) The object of the present invention is to provide a method for producing maraging steel that has excellent strength, toughness, and ductility.

〈課題を解決するための手段〉 本発明は、重!%で、 C: 0.05%以下、 Si : 0.2%以下、M
n : 0.2%以下、 P:0.05%以下、s:o
、os%以下、 Ni : 10゜0%以上21,0%以下、Co : 
5.0%以上9,5%未満、Mo : 3.0%以上1
2.0%以下、ri : 0.2%以上1.6%以下、
A7 : 0.30%以下、 B : 0.0005%以上0.0020%以下を含有
する熱開成形したマルエージング鋼に再結晶溶体化処理
、未再結晶溶体化処理および時効熱処理を施すマルエー
ジング鋼の製造方法において、1000〜1300℃の
温度範囲に1分以上加熱したのちに20℃/分以上の冷
却速度で冷却し、さらに800〜950 ’Cの温度範
囲に1分以上加熱後冷却することからなる2回の再結晶
溶体化処理を行うことを特徴とする強度、靭性および延
性に優れたマルエージング鋼の製造方法である。
<Means for Solving the Problems> The present invention is a heavy! %, C: 0.05% or less, Si: 0.2% or less, M
n: 0.2% or less, P: 0.05% or less, s: o
, os% or less, Ni: 10°0% or more and 21.0% or less, Co:
5.0% or more and less than 9.5%, Mo: 3.0% or more 1
2.0% or less, ri: 0.2% or more and 1.6% or less,
A7: 0.30% or less, B: Maraging that performs recrystallization solution treatment, non-recrystallization solution treatment, and aging heat treatment on heat-opened maraging steel containing 0.0005% or more and 0.0020% or less. In the method of manufacturing steel, the steel is heated to a temperature range of 1000 to 1300°C for 1 minute or more, then cooled at a cooling rate of 20°C/min or more, and further heated to a temperature range of 800 to 950'C for 1 minute or more and then cooled. This is a method for producing maraging steel with excellent strength, toughness, and ductility, which is characterized by performing recrystallization solution treatment twice.

〈作 用〉 まず本発明の成分限定理由について説明する。<For production> First, the reason for limiting the components of the present invention will be explained.

C,Si、 Mn、  P、 Sはマルエージング鋼で
は靭性を低下させるために極力低く抑える必要があり、
それぞれの上限を0.05.0.2.0.2.0.05
、O,OS%とした。
C, Si, Mn, P, and S must be kept as low as possible in maraging steel to reduce toughness.
Each upper limit is 0.05.0.2.0.2.0.05
, O,OS%.

Niはマルエージング鋼においては靭性に優れるマルテ
ンサイト母相を形成するために必要な元素であり、その
ためには10%以上が必要である。しかし21%を超え
ると残留オーステナイトを生成し強度の確保が困難とな
るため上限は21%とした。
Ni is an element necessary for forming a martensitic matrix having excellent toughness in maraging steel, and for this purpose, Ni is required to be present in an amount of 10% or more. However, if it exceeds 21%, residual austenite will be generated and it will be difficult to ensure strength, so the upper limit was set at 21%.

COは析出硬化に寄与する一〇の固溶度を低下させてN
1Joなとの析出を促進させ、これにより強度の上昇を
図る有効な元素である。そのためには5.0%以上が必
要である。しかし9.5%以上添加すると強度は上昇す
るものの靭性の低下が著しく、しかもコストを上昇させ
るため9.5%未満とした。
CO reduces the solid solubility of 10, which contributes to precipitation hardening, and N
It is an effective element that promotes the precipitation of 1Jo and thereby increases strength. For that purpose, 5.0% or more is required. However, if 9.5% or more is added, the strength increases but the toughness decreases significantly, and the cost increases, so the content was set to be less than 9.5%.

Moはマルエージング鋼の時効硬化に寄与する重要な元
素であり、そのためには3%以上が必要であるが、過剰
に添加すると残留オーステナイトの生成による強度低下
、あるいは粗大析出物による脆化を来すため上限は12
.0%とした。
Mo is an important element that contributes to age hardening of maraging steel, and for this purpose 3% or more is required, but if added in excess, it may cause strength reduction due to the formation of retained austenite or embrittlement due to coarse precipitates. The upper limit is 12
.. It was set to 0%.

T4はFIoと同様に析出硬化元素であるが0.2%未
満ではその効果が少なく、また1、6%を超えると脆化
するため上限は1.6%とした。
T4 is a precipitation hardening element like FIo, but if it is less than 0.2%, its effect is small, and if it exceeds 1.6%, it becomes brittle, so the upper limit was set at 1.6%.

Mも時効硬化に寄与する元素であるが、0.30%を超
えると脆化するため上限を0.30%とした。
M is also an element that contributes to age hardening, but if it exceeds 0.30%, it becomes brittle, so the upper limit was set at 0.30%.

Bは未再結晶域溶体化処理に有効な元素であり、そのた
めには0.0005%以上が必要である。しかし0.0
02Q%を超えると脆化をもたらすため上限は0.00
20%とした。
B is an effective element for solution treatment in the non-recrystallized region, and for this purpose, 0.0005% or more is required. But 0.0
If it exceeds 02Q%, it will cause embrittlement, so the upper limit is 0.00.
It was set at 20%.

次に再結晶溶体化熱処理条件の限定理由は次の通りであ
る。
Next, the reasons for limiting the recrystallization solution heat treatment conditions are as follows.

まず熱間加工中に析出した(あるいはその後の溶体化処
理時の析出の核となる)析出物の完全固溶を図るために
は1000℃以上で1分以上の加熱が必要である。また
加熱温度が1300℃を超えると鋼材表面性状の悪化を
招くとともに熱処理コストが嵩むため上限は1300℃
とした。
First, in order to completely dissolve the precipitates that precipitate during hot working (or become the nucleus of precipitation during subsequent solution treatment), heating at 1000° C. or higher for 1 minute or more is necessary. Furthermore, if the heating temperature exceeds 1300°C, the surface quality of the steel material will deteriorate and the heat treatment cost will increase, so the upper limit is 1300°C.
And so.

また加熱後の冷却速度が20℃/分よりも小さいと冷却
中にオーステナイト粒界上に析出が生じ、後述の低温域
での溶体化処理時にオーステナイトの再結晶が著しく抑
制されるためオーステナイト結晶粒が微細化されず、引
張延性やシャルピー吸収エネルギーが低下する。そのた
め?に温溶体化後は20’C/分以上の冷却速度が必要
である。
In addition, if the cooling rate after heating is lower than 20°C/min, precipitation will occur on the austenite grain boundaries during cooling, and austenite recrystallization will be significantly suppressed during solution treatment at low temperatures, which will be described later. is not refined, and tensile ductility and Charpy absorbed energy decrease. Therefore? After hot solution treatment, a cooling rate of 20'C/min or more is required.

ところで析出物の固溶のために行った上記の高温溶体化
後は結晶粒が粗大化しているためこのままでは引張延性
、シャルピー衝撃特性が低い、そこでさらに結晶粒を細
かくするために800〜950℃の温度範囲で1分以上
の溶体化処理を行う必要がある。オーステナイト相を再
結晶させ細粒化させるためには800℃以上で1分以上
加熱する必要がある。また950’Cを趙えると逆にオ
ーステナイト粒が粗大化し過ぎるため上限は950’C
とした。
By the way, after the above-mentioned high-temperature solution treatment, which was carried out to dissolve the precipitates, the crystal grains have become coarse and the tensile ductility and Charpy impact properties are low. It is necessary to perform solution treatment for 1 minute or more at a temperature range of . In order to recrystallize the austenite phase and refine the grains, it is necessary to heat the material at 800° C. or higher for 1 minute or more. In addition, if the temperature exceeds 950'C, the austenite grains will become too coarse, so the upper limit is 950'C.
And so.

以上の高温および低温の2回にわたる再結晶溶体化処理
を施すことにより、従来よりも格段に破壊靭性、延性、
シャルピー衝撃特性に優れるマルエージング鋼を得るこ
とが可能となる。
By performing recrystallization solution treatment twice at high and low temperatures, fracture toughness, ductility, and
It becomes possible to obtain maraging steel with excellent Charpy impact properties.

〈実施例〉 表1に示す鋼を溶製後熱間加工により厚さ2On+mノ
w4vi、トじた。A−E鋼は本発明の対象となる組成
である。またFおよびG鋼はそれぞれ硼素が本発明の対
象外の組成である。さらに表2に示ず熱処理を施した後
に引張特性、シャルピー吸収エネルギーおよび平面歪み
破壊靭性を調べた。引張特性および破壊靭性は室温で測
定した。またシャルピー吸収エネルギーはO′Cでのv
ノツチフルサイズ試験片を用いて測定した。測定結果を
表2に合わせて示す。
<Example> The steel shown in Table 1 was heated to a thickness of 2On+m w4vi after melting. A-E steel is the composition that is the object of the present invention. In addition, F and G steels each have boron compositions that are outside the scope of the present invention. Further, the tensile properties, Charpy absorbed energy, and plane strain fracture toughness were examined after heat treatment, which is not shown in Table 2. Tensile properties and fracture toughness were measured at room temperature. Also, the Charpy absorbed energy is v at O'C
Measurement was performed using a Notti full size test piece. The measurement results are also shown in Table 2.

本発明によるものはいずれも引張特性、シャルピー衝撃
特性および破壊靭性が良好であることは明らかである。
It is clear that all the materials according to the invention have good tensile properties, Charpy impact properties and fracture toughness.

Nα4111は高温溶体化後の冷却速度が本発明の下限
を下回るものであるが、延性、靭性が低くなっている。
Although the cooling rate of Nα4111 after high-temperature solution treatment is below the lower limit of the present invention, the ductility and toughness are low.

Nα5鋼は従来の熱処理条件即ち高温溶体化を適用して
いない鋼であるが、本発明鋼に比べて延性、シャルピー
吸収エネルギーおよび破壊靭性が低いことは明らかであ
る。隘6鋼は細粒化溶体化処理を省いたものであるが、
Nα414と同様に延性、シャルピー吸収エネルギーが
低くなっている9階11綱は本発明法によるものである
が、未再結晶域溶体化処理を省略したものである。 k
lotHに比べるとやや強度が低いものの優れた特性を
有しており、本発明法の効果が未再結晶域溶体化処理の
有無に依らないことは明らかである。胤12および13
鋼は硼素含有量が本発明を逸脱した綱であるが、本発明
の熱処理条件を適用しても効果は認められない。
Although Nα5 steel is a steel to which conventional heat treatment conditions, that is, high temperature solution treatment is not applied, it is clear that the ductility, Charpy absorbed energy, and fracture toughness are lower than the steel of the present invention.隘6 steel does not require solution treatment to refine grains,
The 9th grade 11 steel, which has low ductility and low Charpy absorbed energy like Nα414, is produced by the method of the present invention, but the solution treatment in the non-recrystallized region is omitted. k
Although the strength is slightly lower than that of lotH, it has excellent properties, and it is clear that the effect of the method of the present invention does not depend on the presence or absence of solution treatment in the non-recrystallized region. Seeds 12 and 13
Steel is a steel whose boron content deviates from the present invention, but no effect is observed even if the heat treatment conditions of the present invention are applied.

〈発明の効果〉 本発明の熱処理により、従来よりも格段に破壊靭性、引
張延性およびシャルピー衝撃特性に優れたマルエージン
グ鋼の提供が可能となり、構造物の軽量化および信転性
の向上を実現することができる。
<Effects of the Invention> The heat treatment of the present invention makes it possible to provide maraging steel with far superior fracture toughness, tensile ductility, and Charpy impact properties than conventional maraging steels, resulting in lighter structures and improved reliability. can do.

Claims (1)

【特許請求の範囲】 重量%で、 C:0.05%以下、Si:0.2%以下、Mn:0.
2%以下、P:0.05%以下、S:0.05%以下、 Ni:10.0%以上21.0%以下、 Co:5.0%以上9.5%未満、 Mo:3.0%以上12.0%以下、 Ti:0.2%以上1.6%以下、 Al:0.30%以下、 B:0.0005%以上0.0020%以下を含有する
熱間成形したマルエージング鋼に再結晶溶体化処理、未
再結晶溶体化処理および時効熱処理を施すマルエージン
グ鋼の製造方法において、1000〜1300℃の温度
範囲に1分以上加熱したのちに20℃/分以上の冷却速
度で冷却し、さらに800〜950℃の温度範囲に1分
以上加熱後冷却することからなる2回の再結晶溶体化処
理を行うことを特徴とする強度、靭性および延性に優れ
たマルエージング鋼の製造方法。
[Claims] In weight %, C: 0.05% or less, Si: 0.2% or less, Mn: 0.
2% or less, P: 0.05% or less, S: 0.05% or less, Ni: 10.0% or more and 21.0% or less, Co: 5.0% or more and less than 9.5%, Mo: 3. Hot-formed maru containing 0% or more and 12.0% or less, Ti: 0.2% or more and 1.6% or less, Al: 0.30% or less, and B: 0.0005% or more and 0.0020% or less. In a method for manufacturing maraging steel in which aging steel is subjected to recrystallization solution treatment, non-recrystallization solution treatment, and aging heat treatment, heating to a temperature range of 1000 to 1300℃ for 1 minute or more and then cooling at 20℃/minute or more Maraging steel with excellent strength, toughness and ductility, characterized by being subjected to recrystallization solution treatment twice, which consists of cooling at a high speed, heating to a temperature range of 800 to 950°C for 1 minute or more, and then cooling. manufacturing method.
JP16980790A 1990-06-29 1990-06-29 Production of maraging steel excellent in strength, toughness, and ductility Pending JPH0459923A (en)

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JP16980790A JPH0459923A (en) 1990-06-29 1990-06-29 Production of maraging steel excellent in strength, toughness, and ductility

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JP16980790A JPH0459923A (en) 1990-06-29 1990-06-29 Production of maraging steel excellent in strength, toughness, and ductility

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JPH0459923A true JPH0459923A (en) 1992-02-26

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2005303001A (en) * 2004-04-12 2005-10-27 Mitsuo Ebisawa Core for toroidal coil

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2005303001A (en) * 2004-04-12 2005-10-27 Mitsuo Ebisawa Core for toroidal coil

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