JPH0459924A - Production of maraging steel excellent in strength, toughness, and ductility - Google Patents
Production of maraging steel excellent in strength, toughness, and ductilityInfo
- Publication number
- JPH0459924A JPH0459924A JP16981390A JP16981390A JPH0459924A JP H0459924 A JPH0459924 A JP H0459924A JP 16981390 A JP16981390 A JP 16981390A JP 16981390 A JP16981390 A JP 16981390A JP H0459924 A JPH0459924 A JP H0459924A
- Authority
- JP
- Japan
- Prior art keywords
- solution treatment
- maraging steel
- ductility
- toughness
- 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
Links
- 229910001240 Maraging steel Inorganic materials 0.000 title claims abstract description 23
- 238000004519 manufacturing process Methods 0.000 title claims description 7
- 238000011282 treatment Methods 0.000 claims abstract description 33
- 238000010438 heat treatment Methods 0.000 claims abstract description 20
- 238000001816 cooling Methods 0.000 claims abstract description 17
- 238000001953 recrystallisation Methods 0.000 claims abstract description 16
- 229910052796 boron Inorganic materials 0.000 claims abstract description 12
- 229910052748 manganese Inorganic materials 0.000 claims abstract description 5
- 229910052710 silicon Inorganic materials 0.000 claims abstract description 5
- 229910052717 sulfur Inorganic materials 0.000 claims abstract description 5
- 230000032683 aging Effects 0.000 claims abstract description 4
- 229910052799 carbon Inorganic materials 0.000 claims abstract description 4
- 229910052698 phosphorus Inorganic materials 0.000 claims abstract description 4
- 239000000203 mixture Substances 0.000 claims description 3
- 229910000831 Steel Inorganic materials 0.000 abstract description 21
- 239000010959 steel Substances 0.000 abstract description 21
- 238000000034 method Methods 0.000 abstract description 7
- 239000000243 solution Substances 0.000 description 24
- 229910001566 austenite Inorganic materials 0.000 description 11
- 229910001000 nickel titanium Inorganic materials 0.000 description 8
- ZOXJGFHDIHLPTG-UHFFFAOYSA-N Boron Chemical compound [B] ZOXJGFHDIHLPTG-UHFFFAOYSA-N 0.000 description 7
- 239000002244 precipitate Substances 0.000 description 6
- 230000000694 effects Effects 0.000 description 5
- 229910000734 martensite Inorganic materials 0.000 description 5
- 239000000463 material Substances 0.000 description 3
- 238000001556 precipitation Methods 0.000 description 3
- 241000473391 Archosargus rhomboidalis Species 0.000 description 2
- 238000005098 hot rolling Methods 0.000 description 2
- 239000006104 solid solution Substances 0.000 description 2
- 238000005275 alloying Methods 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 150000001639 boron compounds Chemical class 0.000 description 1
- 238000012733 comparative method Methods 0.000 description 1
- 238000007796 conventional method Methods 0.000 description 1
- 239000013078 crystal Substances 0.000 description 1
- 239000000835 fiber Substances 0.000 description 1
- KHYBPSFKEHXSLX-UHFFFAOYSA-N iminotitanium Chemical compound [Ti]=N KHYBPSFKEHXSLX-UHFFFAOYSA-N 0.000 description 1
- 239000004615 ingredient Substances 0.000 description 1
- 229910000765 intermetallic Inorganic materials 0.000 description 1
- 239000011159 matrix material Substances 0.000 description 1
- 238000005259 measurement Methods 0.000 description 1
- 238000002844 melting Methods 0.000 description 1
- 230000008018 melting Effects 0.000 description 1
- 229910052758 niobium Inorganic materials 0.000 description 1
- 229910052757 nitrogen Inorganic materials 0.000 description 1
- 230000001376 precipitating effect Effects 0.000 description 1
- 238000004881 precipitation hardening Methods 0.000 description 1
- 238000011160 research Methods 0.000 description 1
- 238000005728 strengthening Methods 0.000 description 1
- 229910052715 tantalum Inorganic materials 0.000 description 1
- 238000012360 testing method Methods 0.000 description 1
Landscapes
- Heat Treatment Of Steel (AREA)
Abstract
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適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> The present invention is applied 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 −]88%
Ni−Co−Mo−Ti−A/)である、しかしこの鋼
は高価なCoを含有するために鋼のコストが著しく高く
、その用途はかなり限定されているのが現状である。そ
こで高価なCOを含有しないマルエージング鋼として2
0%Ni系(特公昭39−19885号公報)および2
5%Ni系(特公昭39.19886号公報)等のFe
Ni−Ti系マルエージング鋼が開発されている。<Conventional technology> The main type of maraging steel currently in practical use is maraging steel containing CO (Fe - 88%).
However, since this steel contains expensive Co, the cost of the steel is extremely high, and its uses are currently quite limited. Therefore, as a maraging steel that does not contain expensive CO2
0% Ni system (Japanese Patent Publication No. 39-19885) and 2
Fe such as 5% Ni type (Special Publication No. 39.19886)
Ni-Ti based maraging steels have been developed.
Fe−Ni−Ti系マルエージング鋼は熱間加工による
成形加工後、800〜950 ’Cのオーステナイ1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、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
この際必要によっては深冷処理が施され、その後260
〜650 ℃の温度域で0.5〜24時間の時効処理に
よってN、i、Ti等の金属間化合物を析出させ硬化を
図るものである。After forming by hot working, Fe-Ni-Ti maraging steel is subjected to solution treatment in which it is heated to an austenite 1 temperature range of 800 to 950'C and then cooled to form a solid solution of alloying elements and fine austenite grains. At the same time, a martensitic structure was obtained through subsequent cooling. At this time, if necessary, deep cooling treatment is performed, and then 260
Hardening is achieved by precipitating intermetallic compounds such as N, i, and Ti by aging treatment for 0.5 to 24 hours in a temperature range of ~650°C.
またFe Ni−Ti系マルエージング鋼では基本成
分以外にB(硼素)とNbを複合添加し、未再結晶溶体
化処理による強靭化を図る技術(特開昭64−4783
4号公報)が知られている。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る。これによりマルテ
ンサイトの下部組繊が微細化され強靭化が実現される。In addition, in Fe-Ni-Ti maraging steel, in addition to the basic ingredients, B (boron) and Nb are added in combination to strengthen the steel through non-recrystallization solution treatment (Japanese Unexamined Patent Publication No. 64-4783).
4) is known. The unrecrystallized region solution treatment is a heat treatment method in which the austenite in the unrecrystallized region, that is, the austenite that still has a high dislocation density, is cooled to obtain a martensitic structure in the solution treatment. As a result, the lower fibers of martensite are made finer and stronger.
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
ーステナイト温度域は非常に狭く、工業的には適用でき
ない。しかし硼素とNb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。In ordinary maraging steel, the austenite temperature range in the non-recrystallized region is very narrow and cannot be applied industrially. However, when boron and Nb are added, the recrystallization temperature of austenite increases and the non-recrystallization temperature range is expanded, making industrial application possible.
さらに未再結晶温度域の拡大のためにはBとNbとの複
合添加でなくともBの単独添加あるいはBとMOやTa
等との複合添加によっても可能であることも公知となっ
ている(CAMP、 I S I J Vol。Furthermore, in order to expand the non-recrystallization temperature range, instead of adding B and Nb in combination, it is necessary to add B alone or add B and MO or Ta.
It is also known that it is possible to make it possible by combined addition with etc. (CAMP, ISIJ Vol.
2 (1989)−1806、(702) l 。2 (1989)-1806, (702) l.
しかし硼素を含有するFe−Ni−Ti系マルエージン
グ鋼では、熱間圧延条件によっては熱間圧延中あるいは
その後の溶体化処理時に硼素の化合物を析出し、そのた
めに所朋の特性が得られないことが本発明者らの研究に
より明らかとなった。However, in Fe-Ni-Ti maraging steel containing boron, depending on the hot rolling conditions, boron compounds may precipitate during hot rolling or during subsequent solution treatment, making it impossible to obtain the desired properties. This has become clear through research conducted by the present inventors.
硼素を含有するFe−Ni−Ti系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800〜95
0°Cの通常の溶体化処理では完全には固溶しないため
、破壊靭性が低下する。また】000°C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°C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、延性やンヤルビー吸収エネルギー値が低くなる。In Fe-Ni-Ti maraging steel containing boron, the precipitates that are generated during hot working (or become the nucleus of formation during the subsequent heat treatment process) are
A normal solution treatment at 0°C does not completely form a solid solution, resulting in a decrease in fracture toughness. In addition, when slowly cooling after high-temperature solution treatment at 800 to 950°C, precipitates are formed at the austenite grain boundaries during cooling, and this suppresses recrystallization during the subsequent solution treatment at 800 to 950°C. is not refined, resulting in low ductility and Nyarby absorbed energy values.
そこで硼素を含有するFe−Ni−Ti系マルエージン
グ鋼において強靭性に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, there has been a strong desire to develop a method for stably producing Fe-Ni-Ti maraging steel containing boron and having excellent toughness.
〈発明が解決しようとする!Is>
そこで本発明は従来の強度あるいはそれ以上の強度を確
保し、さらに引張延性、シャルピー衝撃値、破壊靭性と
もバランスのとれた機械的特性を有するマルエージング
鋼を得るための製造方法を提供することを目的とするも
のである。<Invention tries to solve! Is> Therefore, the present invention provides a manufacturing method for obtaining maraging steel that secures conventional strength or higher strength and also has mechanical properties that are well-balanced in tensile ductility, Charpy impact value, and fracture toughness. The purpose is to
〈課題を解決するための手段〉
本発明は、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 : 16.5%以上26.0%以下、Ti :
1.0%以上2.5%以下、B : 0.0005%以
上0.0020%以下を基本組成として含有する熱間成
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°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 provides, in weight percent, 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: 16.5% or more and 26.0% or less, Ti:
Recrystallization solution treatment, non-recrystallization solution treatment and In a method for manufacturing maraging steel that performs aging heat treatment, it 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 then heated to a temperature range of 800 to 950°C for 1 minute or more. This is a method for producing maraging steel having excellent strength, toughness, and ductility, which is characterized by performing recrystallization solution treatment twice, which consists of heating for at least 1 minute and then cooling.
〈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.
0,05%とした。C, Si, Mn, P, and S need to be kept as low as possible in maraging steel in order to reduce toughness, and the upper limit of each is set to 0.05.0.2.0.2.0.05.
It was set to 0.05%.
NiはFe−Ni−Ti系マlレ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しかつN1d
iの析出により強化に寄与する元素である。Ni forms a martensitic matrix with excellent toughness in Fe-Ni-Ti system maraging steel, and N1d
It is an element that contributes to strengthening through the precipitation of i.
そのためには16.5%以上が必要であるが、26%を
超えると深冷処理によっても完全なマルテンサイト組織
とはならないため上限は26%とした。For this purpose, a content of 16.5% or more is required, but if it exceeds 26%, a complete martensitic structure cannot be obtained even by deep cooling treatment, so the upper limit was set at 26%.
TiはNiと同様に析出硬化元素であるが1.0%未満
ではその効果が少なく、また2、5%を超えると脆化す
るため上限は2.5%とした。Ti is a precipitation hardening element like Ni, but if it is less than 1.0%, its effect is small, and if it exceeds 2.5%, it becomes brittle, so the upper limit was set to 2.5%.
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
020%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 0.020%, it will cause embrittlement, so the upper limit is 0.00%.
It was set at 20%.
なお本発明の効果には影響を与えない範囲においてこれ
ら以外の元素MO1Nb、 AZ等を添加してもよい。Note that elements other than these, such as MO1Nb and AZ, may be added within a range that does not affect the effects of the present invention.
次に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 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°C以上で1分以上の加熱が必要である。ま
た加熱温度が7300℃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
’C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 longer is necessary. Furthermore, if the heating temperature exceeds 7300°C, the surface quality of the steel material will deteriorate and the heat treatment cost will increase, so the upper limit is 1300°C.
'C.
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し、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
め高温溶体化後は20℃/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. Grains are not refined and tensile ductility and Charpy absorbed energy decrease. Therefore, after high-temperature solution treatment, a cooling rate of 20° C./min or higher 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V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゛C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°C以上で1分
以上加熱する必要がある。また950℃を超えると逆に
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 V properties are low. It is necessary to carry out solution treatment for 1 minute or more in a temperature range of ゛C. 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. Moreover, if the temperature exceeds 950°C, the austenite grains will become too coarse, so the upper limit is 950°C.
It was set as C.
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Fe −Ni−Ti系マル
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 a Fe-Ni-Ti maraging steel having 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20mの鋼板
とした。A鋼は本発明の基本組成に該当する鋼である。<Example> The steel shown in Table 1 was made into a steel plate with a thickness of 20 m by hot working after melting. Steel A is a steel that corresponds to the basic composition of the present invention.
またB−D鋼はさらにMOlNb、 AIを添加した綱
である。またEおよびF綱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に示す熱処理を施した後
にり1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。In addition, BD steel is a steel that further contains MOINb and AI. Furthermore, classes E and F each have compositions in which boron is not covered by the present invention. Further, after the heat treatments shown in Table 2 were performed, the tensile properties, Charpy absorbed energy, and plane strain fracture toughness were examined.
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0°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
。Tensile properties and fracture toughness were measured at room temperature. Charpy absorbed energy was measured using a V-notch full-size test piece at 0°C. 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.
Nn4鯛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0階5
鯛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。阻
6鋼は細粒化溶体化処理を省いたものであるが、随4綱
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。胤7.8.9mはそれぞれFIo、Nb、 A7
を添加した鋼に本発明の熱処理を施した鋼であるが、い
ずれも引張特性、シャルピー衝撃特性および破壊靭性は
良好である。Nα10鋼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1強度、
靭性がやや低いものの、従来法や比較法に比べると格段
に優れており、本発明法の効果が未再結晶域溶体化処理
の存無に依らないことは明らかである0階11および1
2鋼は硼素含有量が本発明を逸脱した鋼であるが、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 the cooling rate of Nn4 sea bream after high-temperature solution treatment is below the lower limit of the present invention, it has low ductility and toughness.
Although sea bream is a steel to which conventional heat treatment conditions, ie, high-temperature solution treatment, are not applied, it is clear that the ductility, Charpy absorbed energy, and fracture toughness are lower than the steel of the present invention. Although No. 6 steel does not require solution treatment to refine the grain, it has low ductility and Charpy absorbed energy, similar to No. 4 steel. Seeds 7, 8, and 9m are respectively FIo, Nb, and A7.
These steels are obtained by applying the heat treatment of the present invention to the steel to which the above-mentioned is added, and all of them have good tensile properties, Charpy impact properties, and fracture toughness. Nα10 steel is produced by the method of the present invention, but has a strength of 1, which is obtained by omitting the solution treatment in the non-recrystallized region.
Although the toughness is somewhat low, it is significantly superior to conventional methods and comparative methods, and it is clear that the effect of the present method does not depend on the presence or absence of solution treatment in the non-recrystallized region.
Steel No. 2 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
張延性およびツヤルビー衝撃特性に優れたFe−Ni−
Ti系マルエージング鋼の提供が可能となり、構造物の
軽量化および信較性の向上を実現することができる。<Effects of the Invention> By the heat treatment of the present invention, Fe-Ni-
It becomes possible to provide Ti-based maraging steel, which makes it possible to reduce the weight of structures and improve reliability.
Claims (1)
2%以下、P:0.05%以下、S:0.05%以下、 Ni:16.5%以上26.0%以下、 Ti:1.0%以上2.5%以下、 B:0.0005%以上0.0020%以下を基本組成
として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、1000〜1
300℃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: 16.5% or more and 26.0% or less, Ti: 1.0% or more and 2.5% or less, B: 0. 0.0005% or more and 0.0020% or less as a basic composition, the hot-formed maraging steel is subjected to recrystallization solution treatment, non-recrystallization solution treatment, and aging heat treatment.
After heating to a temperature range of 300℃ for more than 1 minute, heat to 20℃/
Excellent strength, toughness, and ductility, characterized by performing recrystallization solution treatment twice, which consists of cooling at a cooling rate of 1 minute or more, and then cooling after heating to a temperature range of 800 to 950 °C for 1 minute or more. A method for producing maraging steel.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP16981390A JPH0459924A (en) | 1990-06-29 | 1990-06-29 | Production of maraging steel excellent in strength, toughness, and ductility |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP16981390A JPH0459924A (en) | 1990-06-29 | 1990-06-29 | Production of maraging steel excellent in strength, toughness, and ductility |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPH0459924A true JPH0459924A (en) | 1992-02-26 |
Family
ID=15893377
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP16981390A Pending JPH0459924A (en) | 1990-06-29 | 1990-06-29 | Production of maraging steel excellent in strength, toughness, and ductility |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPH0459924A (en) |
-
1990
- 1990-06-29 JP JP16981390A patent/JPH0459924A/en active Pending
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