JPS62177155A - Fe-base alloy excellent in stress corrosion cracking resistance and its production - Google Patents
Fe-base alloy excellent in stress corrosion cracking resistance and its productionInfo
- Publication number
- JPS62177155A JPS62177155A JP1785386A JP1785386A JPS62177155A JP S62177155 A JPS62177155 A JP S62177155A JP 1785386 A JP1785386 A JP 1785386A JP 1785386 A JP1785386 A JP 1785386A JP S62177155 A JPS62177155 A JP S62177155A
- Authority
- JP
- Japan
- Prior art keywords
- less
- stress corrosion
- corrosion cracking
- cracking resistance
- base alloy
- 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
- 238000005260 corrosion Methods 0.000 title claims abstract description 41
- 230000007797 corrosion Effects 0.000 title claims abstract description 41
- 238000005336 cracking Methods 0.000 title claims abstract description 40
- 229910045601 alloy Inorganic materials 0.000 title claims abstract description 30
- 239000000956 alloy Substances 0.000 title claims abstract description 30
- 238000004519 manufacturing process Methods 0.000 title claims abstract description 7
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims abstract description 9
- 238000001816 cooling Methods 0.000 claims abstract description 8
- 229910052804 chromium Inorganic materials 0.000 claims abstract description 6
- 229910052717 sulfur Inorganic materials 0.000 claims abstract description 6
- 229910052750 molybdenum Inorganic materials 0.000 claims abstract description 5
- 229910052759 nickel Inorganic materials 0.000 claims abstract description 5
- 229910052710 silicon Inorganic materials 0.000 claims abstract 4
- 238000005096 rolling process Methods 0.000 claims description 3
- 239000006104 solid solution Substances 0.000 claims description 3
- 238000010438 heat treatment Methods 0.000 abstract description 8
- 229910052748 manganese Inorganic materials 0.000 abstract description 4
- 239000000203 mixture Substances 0.000 abstract description 4
- 229910052799 carbon Inorganic materials 0.000 abstract description 3
- 229910052742 iron Inorganic materials 0.000 abstract description 2
- 239000007787 solid Substances 0.000 abstract 1
- 239000000463 material Substances 0.000 description 9
- 238000012360 testing method Methods 0.000 description 9
- 238000012545 processing Methods 0.000 description 6
- 230000000694 effects Effects 0.000 description 5
- 229910001293 incoloy Inorganic materials 0.000 description 5
- 239000000243 solution Substances 0.000 description 5
- 239000003795 chemical substances by application Substances 0.000 description 3
- 238000000034 method Methods 0.000 description 3
- 239000000126 substance Substances 0.000 description 3
- 238000005275 alloying Methods 0.000 description 2
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 2
- 229910052760 oxygen Inorganic materials 0.000 description 2
- 239000001301 oxygen Substances 0.000 description 2
- 238000003672 processing method Methods 0.000 description 2
- 206010023204 Joint dislocation Diseases 0.000 description 1
- 101150063599 Rtn2 gene Proteins 0.000 description 1
- KGBXLFKZBHKPEV-UHFFFAOYSA-N boric acid Chemical compound OB(O)O KGBXLFKZBHKPEV-UHFFFAOYSA-N 0.000 description 1
- 230000007423 decrease Effects 0.000 description 1
- 239000012535 impurity Substances 0.000 description 1
- 238000011160 research Methods 0.000 description 1
- 239000000523 sample Substances 0.000 description 1
- 238000005204 segregation Methods 0.000 description 1
- 238000007711 solidification Methods 0.000 description 1
- 230000008023 solidification Effects 0.000 description 1
- 238000005482 strain hardening Methods 0.000 description 1
- 238000005728 strengthening Methods 0.000 description 1
- 238000010998 test method Methods 0.000 description 1
- 238000012546 transfer Methods 0.000 description 1
Classifications
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D8/00—Modifying the physical properties by deformation combined with, or followed by, heat treatment
- C21D8/005—Modifying the physical properties by deformation combined with, or followed by, heat treatment of ferrous alloys
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Crystallography & Structural Chemistry (AREA)
- Mechanical Engineering (AREA)
- Materials Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Heat Treatment Of Steel (AREA)
Abstract
Description
【発明の詳細な説明】
〔産業上の利用分野〕
本発明は耐応力腐食割れ性に優れたFe基合金及びその
製造方法に関し、特に軽水炉あるいは高速増殖炉の蒸気
発生器伝熱管材や熱交換器用支持構造部材等及び配管材
等に適用されるFe基合金及びその製造方法に関する。[Detailed Description of the Invention] [Industrial Application Field] The present invention relates to an Fe-based alloy with excellent stress corrosion cracking resistance and a method for producing the same, particularly for use in steam generator heat transfer tube materials and heat exchange materials for light water reactors or fast breeder reactors. The present invention relates to an Fe-based alloy that is applied to dexterous support structural members, piping materials, etc., and a method for producing the same.
従来、耐応力腐食割れ性に優れたFe基合金としては、
インコロイ(Incoloy) 800 (商品名)と
称するNi: 5 Q、O〜35.0%、Cr: 19
.0〜2五〇チ、Fe:残部を有するIPe基合金が用
いられて来たが、インコロイ800は加工条件によって
は応力腐食割れ感受性が高く、上記伝熱管や構造部材等
で応力腐食割れを生じることがある。Conventionally, Fe-based alloys with excellent stress corrosion cracking resistance include:
Incoloy 800 (trade name) Ni: 5 Q, O ~ 35.0%, Cr: 19
.. IPe-based alloys with 0 to 250% Fe: balance have been used, but Incoloy 800 is highly susceptible to stress corrosion cracking depending on processing conditions, causing stress corrosion cracking in the heat exchanger tubes and structural members, etc. Sometimes.
インコロイ800は、酸素を含まない高温高圧水中では
比較的耐応力腐食割れ性に優れていると言われているが
、冷間加工を受けた場合には、応力腐食割れが発生する
ことがあった。Incoloy 800 is said to have relatively excellent stress corrosion cracking resistance in high temperature, high pressure water that does not contain oxygen, but stress corrosion cracking may occur when subjected to cold working. .
本発明は上述のような応力腐食割れの発生がないFθ基
合金及びその製造方法を提供しようとするものである。The present invention aims to provide an Fθ-based alloy that does not cause stress corrosion cracking as described above, and a method for manufacturing the same.
従来用いてきたインコロイ800を用いた部材で応力腐
食割れを生じたのは、インコロイ800の化学成分加工
条件等によシ材料の金属組織が変化し、材料の応力腐食
割れ感受性が高くなるとの知見に基き、本発明者らは材
料の応力腐食割れ感受性を低減するような化学成分、加
工条件につき鋭意研究の結果、本発明を完成するに至っ
た。The reason why stress corrosion cracking occurred in parts using Incoloy 800, which has been used in the past, was due to the knowledge that the chemical composition of Incoloy 800 and the processing conditions change the metallographic structure of the material, increasing the material's susceptibility to stress corrosion cracking. Based on this, the present inventors have completed the present invention as a result of intensive research into chemical components and processing conditions that reduce the stress corrosion cracking susceptibility of materials.
すなわち本発明は、
(1)重量比でC:α04チ以下、Si: 1%以下、
Mn:2%以下、Ni: 25%以上、45チ以下、C
r: 25%以上35チ以下、Mo: 6 %以下、P
、S:[101%以下、残部F’s よりなる耐応力
腐食割れ性に優れたFθ基合金及び(2)重量比でC:
Q、04チ以下、Sl:1%以下、Mn: 2%以下、
Ni: 25%以上45%以下、Or: 25%以上3
5%以下、Mo:6%以下、P、S:0.01%以下、
残部F’s よりなるFe午
基合金を、850〜1250で、圧下率にして、20%
以上の熱間加工を施した後、900〜1150℃で2分
〜5時間保持してから空冷以上の速い冷却速度で冷却す
ることを特徴、とする室温下のα2%耐力が21 kg
/rtn2以上、引張強さが53kg/rnrn2以上
の強度を有し、かつ高温高圧水中での耐応力腐食割れ性
の優れた固溶強化型Fe基合金の製造方法
である。That is, the present invention provides: (1) C: α04 or less, Si: 1% or less in weight ratio;
Mn: 2% or less, Ni: 25% or more, 45% or less, C
r: 25% or more and 35% or less, Mo: 6% or less, P
, S: [101% or less, the balance F's, an Fθ-based alloy with excellent stress corrosion cracking resistance, and (2) C: by weight ratio
Q, 04chi or less, Sl: 1% or less, Mn: 2% or less,
Ni: 25% or more and 45% or less, Or: 25% or more3
5% or less, Mo: 6% or less, P, S: 0.01% or less,
A Fe base alloy consisting of the balance F's was rolled at a rolling reduction rate of 20% at a rolling stock of 850 to 1250.
After the above hot working, it is held at 900-1150℃ for 2 minutes to 5 hours and then cooled at a faster cooling rate than air cooling.The α2% yield strength at room temperature is 21 kg.
/rtn2 or more, a tensile strength of 53kg/rnrn2 or more, and a solid solution strengthened Fe-based alloy that has excellent stress corrosion cracking resistance in high-temperature, high-pressure water.
本発明Fe基合金の各合金元素の限定理由及び熱処理、
加工条件の限定理由は以下のとおりである。Reasons for limiting each alloying element of the present invention Fe-based alloy and heat treatment,
The reasons for limiting the processing conditions are as follows.
各合金元素の限定理由
C;Cは固溶強化型元素であシ所定の強度を得るには、
ある程度の量が必要である。しかし、多く含むと、溶体
化処理後の冷却過程で鋭敏化し、耐応力腐食割れ性を低
下させるので0.04チ以下とする。Reason for limiting each alloying element C; C is a solid solution strengthening element. To obtain the specified strength,
A certain amount is required. However, if it is included in a large amount, it will become sensitive during the cooling process after solution treatment and reduce stress corrosion cracking resistance, so the content should be 0.04 inches or less.
81、Mn ;81.Mnは合金中の不純物としての酸
素を取除く作用をもつが、反面多くなると、応力腐食割
れ性を低下させる。従ってSi#Mntは低い方が良(
Si: 1 %以下、Mn: 2 %以下とする。81, Mn;81. Mn has the effect of removing oxygen as an impurity in the alloy, but on the other hand, when the amount increases, it reduces stress corrosion cracking resistance. Therefore, the lower Si#Mnt is, the better (
Si: 1% or less, Mn: 2% or less.
P、S;P、8は粒界に偏析し、粒界結合力を低下させ
るのみでなく、電気化学的に有害な元素であり、低い方
が好ましい(101%以下)。P, S; P, 8 segregates at grain boundaries and not only reduces grain boundary bonding strength, but is also an electrochemically harmful element, and the lower the content, the better (101% or less).
Ni; Ni は合金の耐すラクセーション性ヲ保持
させるとともに、C2−を含むような環境下での耐応力
腐食割れ性を向上させるので、多く含有する方が良いが
、多量に含んだ場合には、脱気高温高圧水中での耐応力
腐食割れ性が低下するため、25チ以上、45%以下と
する。Ni: Ni maintains the luxation resistance of the alloy and improves stress corrosion cracking resistance in environments containing C2-, so it is better to contain a large amount, but if it is contained in a large amount, Since the stress corrosion cracking resistance in deaerated high temperature and high pressure water decreases, it should be set at 25% or more and 45% or less.
Or; Orは耐応力腐食割れ性を保持させる上で最も
重要な元素でろD、25%以上添加することが良い。し
かしあまシ多量に添加すると凝固偏析が著しく鍛造しに
くくなるばかシか、均質なインゴットができにくいので
35−以下とする。Or; Or is the most important element for maintaining stress corrosion cracking resistance, and is preferably added in an amount of 25% or more. However, if a large amount of slender is added, solidification segregation will occur and it will be difficult to forge, or it will be difficult to form a homogeneous ingot, so it should be set at 35- or less.
MO; MOは耐食性を向上させるが、多くなると熱間
加工性を著しく劣化させるため6%以下とする。MO: MO improves corrosion resistance, but if too much MO deteriorates hot workability significantly, it should be kept at 6% or less.
本発明Fa 基合金の熱処理・加工方法の限定理由
本発明Fe基合金の熱間加工性を保持するには比較的高
温で加工する必要があシ、加工条件は850〜1250
℃で行う必要がおる。また耐応力腐食割れ性を保持する
Kは均質かつ大きな加工率を与えることが望ましく、熱
間加工としては圧下率で20%以上にする。Reasons for limiting the heat treatment/processing method for the Fe-based alloy of the present invention In order to maintain the hot workability of the Fe-based alloy of the present invention, it is necessary to process it at a relatively high temperature, and the processing conditions are 850-1250.
It is necessary to do it at ℃. Further, K, which maintains stress corrosion cracking resistance, is desirably given a homogeneous and large working rate, and for hot working, the reduction rate is 20% or more.
熱処理条件としては、高強度を保持し、かつ高い耐応力
腐食割れ性を保持させるには、900℃以上1150℃
以下で溶体化処理を施す。溶体化処理温度が1150℃
を越えると耐応力腐食割れ性が劣化するとともに高強度
が保持できなくなる。The heat treatment conditions are 900°C or higher and 1150°C to maintain high strength and high stress corrosion cracking resistance.
Solution treatment is performed below. Solution treatment temperature is 1150℃
If the stress corrosion cracking resistance is exceeded, stress corrosion cracking resistance deteriorates and high strength cannot be maintained.
本発明のFθ基合金の効果を立証するために下記のよう
な試験を行った。In order to prove the effects of the Fθ-based alloy of the present invention, the following tests were conducted.
0応力腐食割れ試験
軽水炉環境下で蒸気発生器伝熱管等に本発四Fθ基合金
が用いられた場合の耐応力腐食割わ性を評価するため、
PWR−次系水を模擬し六下記の表1に示す環境下で、
第1図に示すUAンド試験片を浸漬し、高応力を負荷し
た各供斜材の応力腐食割れ試験を5oooh迄実施し、
割れの有無を調査した。0-stress corrosion cracking test In order to evaluate the stress corrosion cracking resistance when the present four Fθ-based alloy is used for steam generator heat exchanger tubes etc. in a light water reactor environment,
Under the environment shown in Table 1 below, simulating PWR-order system water,
A stress corrosion cracking test was carried out on each diversion member by immersing the UA-and test piece shown in Fig. 1 and applying high stress up to 5oooh.
The presence or absence of cracks was investigated.
表1試験条件
(1)温度 360℃
(2) 圧 力 2 1 4 kg/cm
2G(3) 水 質
pH(at2S℃)約7
H3BO3濃度(asB) 約500 ppmLi0
1(d度(asLi) 約 2 ppmH,約
30cc−8TP/に9 ” H20DO2< 5 p
pb
OL−< 0.1 ppm
0供試材
本試験に用いた供試材(代表例)の化学成分を表2に、
表2の/166の供試材の熱処理・加工: 条件の例
を表3に示す。Table 1 Test conditions (1) Temperature 360℃ (2) Pressure 2 1 4 kg/cm
2G (3) Water quality pH (at2S℃) approx. 7 H3BO3 concentration (asB) approx. 500 ppmLi0
1 (d degree (asLi) approx. 2 ppmH, approx. 30cc-8TP/9''H20DO2<5p
pb OL-< 0.1 ppm 0 Test material Table 2 shows the chemical composition of the test material (representative example) used in this test.
Heat treatment/processing of sample material /166 in Table 2: Examples of conditions are shown in Table 3.
表 2
表 5 7166(D供試材の熱処理、加工方法と耐応
力腐食割れ性×;割れるり
01割れなし
0試験結果
合金成分を変化させて耐応力屑食割れ性を検討した結果
は次のとおり。Table 2 Table 5 7166 (Heat treatment, processing method and stress corrosion cracking resistance of test material D Street.
a)C2Cr社、熱処理条件と耐応力腐食割れ性
第2図に示すように、ciは0.04%以下、Cr量は
25%以上で、1250℃以下で溶体化処理?施したも
のが耐応力腐食割れ性に優れて優れている。a) C2Cr Co., heat treatment conditions and stress corrosion cracking resistance As shown in Figure 2, ci is 0.04% or less, Cr content is 25% or more, and solution treatment is performed at 1250°C or less. The treated products have excellent stress corrosion cracking resistance.
b) Si、Mni熱処理条件と耐応力腐食割れ性第
3図に示すように、Si 量は1チ以下、Mn量は2%
以下で900℃以上で溶体化処理を施したものが耐応力
腐食割れ性に優れている。b) Si, Mni heat treatment conditions and stress corrosion cracking resistance As shown in Figure 3, the amount of Si is 1% or less, and the amount of Mn is 2%.
Those subjected to solution treatment at 900° C. or higher have excellent stress corrosion cracking resistance.
C)熱間加工条件と耐応力腐食割れ性
前掲の表3に示すように熱間加工は所定の温度(この種
合金では900〜1200℃が良い)で圧下率20チ以
上の熱間加工を施すと耐応力腐食割れ性が良い。C) Hot working conditions and stress corrosion cracking resistance As shown in Table 3 above, hot working is carried out at a specified temperature (900 to 1200°C is good for this type of alloy) and at a reduction rate of 20 inches or more. When applied, it has good stress corrosion cracking resistance.
本発明の合金組成及び製造方法によシ耐応力腐食割れ性
に漬れたFe基合金が得られる。The alloy composition and manufacturing method of the present invention provide an Fe-based alloy with excellent stress corrosion cracking resistance.
第1図は本発明Fe基合金の耐応力腐食割れ性を評価す
るための試験方法を示し図、第2図はFe基合金の耐応
力腐食割れ性に及ぼすC2Or量の影響を示す図表、第
5図はFe基合金の耐応力腐食割れ性に及ばすSi、M
n量の影響2示す図表である。
復代理人 内 1) 明
復代理人 萩 原 亮 −
復代理人 安 西 篤 夫
第1図Figure 1 shows a test method for evaluating the stress corrosion cracking resistance of the Fe-based alloy of the present invention, and Figure 2 is a chart showing the influence of the amount of C2Or on the stress corrosion cracking resistance of the Fe-based alloy. Figure 5 shows the effects of Si and M on the stress corrosion cracking resistance of Fe-based alloys.
It is a chart showing the influence of n amount 2. Sub-Agents 1) Meifuku Agent Ryo Hagiwara - Sub-Agent Atsuo Anzai Figure 1
Claims (1)
n:2%以下、Ni:25%以上、45%以下、Cr:
25%以上、35%以下、Mo:6%以下、P、S、:
0.01%以下、残部Feよりなる耐応力腐食割れ性に
優れたFe基合金。 2)重量比でC:0.04%以下、Si:1%以下、M
n:2%以下、Ni:25%以上45%以下、Cr:2
5%以上35%以下、Mo:6%以下、P、S:0.0
1%以下、残部FeよりなるFe基合金を、850〜1
250℃で、圧下率にして、20%以上の熱間加工を施
した後、900〜1150℃で2分〜5時間保持してか
ら空冷以上の速い冷却速度で冷却することを特徴とする
室温下の0.2%耐力が21kg/mm^2以上、引張
強さが53kg/mm^2以上の強度を有し、かつ高温
高圧水中での耐応力腐食割れ性の優れた固溶強化型Fe
基合金の製造方法。[Claims] 1) Weight ratio: C: 0.04% or less, Si: 1% or less, M
n: 2% or less, Ni: 25% or more, 45% or less, Cr:
25% or more, 35% or less, Mo: 6% or less, P, S,:
An Fe-based alloy with excellent stress corrosion cracking resistance consisting of 0.01% or less and the balance being Fe. 2) Weight ratio: C: 0.04% or less, Si: 1% or less, M
n: 2% or less, Ni: 25% or more and 45% or less, Cr: 2
5% or more and 35% or less, Mo: 6% or less, P, S: 0.0
Fe-based alloy consisting of 1% or less and the balance Fe, 850-1
Room temperature characterized by hot working at 250°C with a rolling reduction of 20% or more, holding at 900-1150°C for 2 minutes to 5 hours, and then cooling at a faster cooling rate than air cooling. Solid solution strengthened Fe with a lower 0.2% yield strength of 21 kg/mm^2 or more, a tensile strength of 53 kg/mm^2 or more, and excellent stress corrosion cracking resistance in high-temperature, high-pressure water.
Method of manufacturing base alloy.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP1785386A JPS62177155A (en) | 1986-01-31 | 1986-01-31 | Fe-base alloy excellent in stress corrosion cracking resistance and its production |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP1785386A JPS62177155A (en) | 1986-01-31 | 1986-01-31 | Fe-base alloy excellent in stress corrosion cracking resistance and its production |
Publications (1)
Publication Number | Publication Date |
---|---|
JPS62177155A true JPS62177155A (en) | 1987-08-04 |
Family
ID=11955219
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP1785386A Pending JPS62177155A (en) | 1986-01-31 | 1986-01-31 | Fe-base alloy excellent in stress corrosion cracking resistance and its production |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPS62177155A (en) |
-
1986
- 1986-01-31 JP JP1785386A patent/JPS62177155A/en active Pending
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