JPS62992B2 - - Google Patents
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- Publication number
- JPS62992B2 JPS62992B2 JP53058887A JP5888778A JPS62992B2 JP S62992 B2 JPS62992 B2 JP S62992B2 JP 53058887 A JP53058887 A JP 53058887A JP 5888778 A JP5888778 A JP 5888778A JP S62992 B2 JPS62992 B2 JP S62992B2
- Authority
- JP
- Japan
- Prior art keywords
- amount
- less
- corrosion resistance
- wear
- 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.)
- Expired
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- 229910045601 alloy Inorganic materials 0.000 claims description 25
- 239000000956 alloy Substances 0.000 claims description 25
- 229910052750 molybdenum Inorganic materials 0.000 claims description 4
- 229910052759 nickel Inorganic materials 0.000 claims description 4
- 229910052721 tungsten Inorganic materials 0.000 claims description 2
- 239000000463 material Substances 0.000 description 26
- PXHVJJICTQNCMI-UHFFFAOYSA-N nickel Substances [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 21
- 239000011651 chromium Substances 0.000 description 20
- 238000005260 corrosion Methods 0.000 description 17
- 230000007797 corrosion Effects 0.000 description 17
- 239000010936 titanium Substances 0.000 description 14
- 230000000694 effects Effects 0.000 description 9
- 229910052782 aluminium Inorganic materials 0.000 description 8
- 150000001247 metal acetylides Chemical class 0.000 description 7
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 7
- 229910001566 austenite Inorganic materials 0.000 description 6
- 229910052799 carbon Inorganic materials 0.000 description 6
- 230000007423 decrease Effects 0.000 description 6
- 238000005482 strain hardening Methods 0.000 description 6
- 229910052719 titanium Inorganic materials 0.000 description 6
- 229910052804 chromium Inorganic materials 0.000 description 5
- 238000010586 diagram Methods 0.000 description 4
- 229910000765 intermetallic Inorganic materials 0.000 description 4
- 239000011159 matrix material Substances 0.000 description 4
- 230000003647 oxidation Effects 0.000 description 4
- 238000007254 oxidation reaction Methods 0.000 description 4
- 239000002244 precipitate Substances 0.000 description 4
- 238000001556 precipitation Methods 0.000 description 4
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 3
- 238000005520 cutting process Methods 0.000 description 3
- 239000000446 fuel Substances 0.000 description 3
- 238000000034 method Methods 0.000 description 3
- 239000003758 nuclear fuel Substances 0.000 description 3
- 238000004881 precipitation hardening Methods 0.000 description 3
- 229910000601 superalloy Inorganic materials 0.000 description 3
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 description 2
- 239000000654 additive Substances 0.000 description 2
- 230000000996 additive effect Effects 0.000 description 2
- 229910017052 cobalt Inorganic materials 0.000 description 2
- 239000010941 cobalt Substances 0.000 description 2
- GUTLYIVDDKVIGB-UHFFFAOYSA-N cobalt atom Chemical compound [Co] GUTLYIVDDKVIGB-UHFFFAOYSA-N 0.000 description 2
- 230000000052 comparative effect Effects 0.000 description 2
- 238000005336 cracking Methods 0.000 description 2
- 239000006104 solid solution Substances 0.000 description 2
- 239000010935 stainless steel Substances 0.000 description 2
- 229910001220 stainless steel Inorganic materials 0.000 description 2
- 229910019589 Cr—Fe Inorganic materials 0.000 description 1
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 1
- 238000005299 abrasion Methods 0.000 description 1
- 239000011358 absorbing material Substances 0.000 description 1
- 230000002411 adverse Effects 0.000 description 1
- 238000003483 aging Methods 0.000 description 1
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 1
- 239000003795 chemical substances by application Substances 0.000 description 1
- 238000002425 crystallisation Methods 0.000 description 1
- 230000008025 crystallization Effects 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 238000002844 melting Methods 0.000 description 1
- 230000008018 melting Effects 0.000 description 1
- 229910052751 metal Inorganic materials 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 150000002736 metal compounds Chemical class 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 239000000843 powder Substances 0.000 description 1
- 239000011253 protective coating Substances 0.000 description 1
- 230000005855 radiation Effects 0.000 description 1
- 238000005728 strengthening Methods 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
- 238000003466 welding Methods 0.000 description 1
Classifications
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E30/00—Energy generation of nuclear origin
- Y02E30/30—Nuclear fission reactors
Landscapes
- Laminated Bodies (AREA)
Description
〔産業上の利用分野〕
本発明は、摺動構造物に係り、特に原子炉の炉
心制御棒に使用するために優れた耐食性および耐
摩耗性が要求される燃料制御棒用ピンとローラの
ような摺動構造物に関する。
〔従来の技術〕
原子炉燃料制御棒の一例を第1図に示す。
図において、1は燃料制御棒の把手、2は本発
明の対象となるピンとローラとからなるガイドロ
ーラ、3は中性子吸収材を入れたステンレス管、
4はステンレス管3を内包するブレードである。
ガイドローラ2は、第2図に示すように、コバ
ルト(Co)基超合金製のローラ5と、同じくCo
基の鍛造材製のピン6とからなる。
〔発明が解決しようとする問題点〕
このローラに使用されているCo基合金は、高
い炭素(C1.0%)と高いクロム(Cr28%)を含
んでいる。そのため炭化物が多く、従つて硬さが
高く、また高いクロム含量ゆえに高温高圧の純水
への耐腐食性にも優れ、ローラ材として優れた特
性を有している。一方、ピン材に使用されている
Co基鍛造合金は、鍛造性、加工性、溶接性が要
求されるので、Cが0.1%低く、またCrも20%と
低いが、やはり優れた耐摩耗性、耐食性を有す
る。
しかし、これらの合金は、ローラ材で約65%の
Coを、またピン材で約50%のCoを含むため、使
用中に両者の摩耗により摩耗粉を生じ、それが放
射化されて系内を循環し、また高温高圧の純水に
よる腐食で溶出したCoがやはり放射能により汚
染されて循環するという問題を生ずる。
本発明の目的は、耐摩耗性および耐食性が良好
で、かつCoの誘導放射能による問題を生じない
摺動構造物を提供することである。
〔問題点を解決するための手段〕
上記目的を達成するためには、摺動側部材と固
定側部材の材料が、Coを含まず、耐摩耗性に優
れ、かつ高温高圧の純水に対する耐食性に優れて
いること、さらにピン材は鍛造可能であること、
およびブレードに溶接固定するので溶接性にも優
れていることが要求される。
耐摩耗性を得るには合金が一定の硬さを有する
ことが要求される。合金の硬さは、(イ)析出物によ
る析出硬化、(ロ)基地の固溶硬化によつて得られ
る。(イ)の方法においては、炭化物によるものと金
属間化合物によるものが代表的であり、(ロ)の方法
においては、Mo、W等の固溶強化型元素が多く
含有させること、さらには冷間加工等による加工
硬化が効果的である。
また、高温高圧水に対する耐食性の点からは、
Cr量およびNi量、さらにはMo量が最も重要であ
り、またCの量も重要となる。以上の点から、
Coを含まない適当な合金を選ぶ必要がある。
本発明者らは、上記のような観点から、
(1) ニツケル(Ni)基でチタン(Ti)とアルミ
ニウム(Al)を多く含み、かつCr量の多い、
いわゆるγ′強析出型超合金(Ni3(Al、Ti)
を析出させた合金)、
(2) Ni基で炭化物の晶出または析出による硬化
型合金でCが高く、かつCrがさらに高いも
の、
(3) Ni基でB型なる金属間化合物を析出、晶出
させたCの高い合金、
(4) Ni―Cr―Fe基合金にMoを多く含有させ、さ
らに冷間加工を与えた合金、
(5) Fe基合金にTiとAlを含有させ、かつCrを充
分高く含有させた合金、
を選び、ローラ材として4種の合金とピン材とし
て3種の合金とを組合わせた場合について、それ
ぞれ純水中で摺動摩耗試験を行なつた。このよう
にしたのは、摺動側となるローラ材に適していて
も、固定側となるピン材には不適当な材料もあ
り、また摩耗特性上も両者の組合わせが重要とな
るからである。
その結果、ピン材としては、(5)のFe基合金に
TiとAlを含有させかつCr量を充分に高く含有さ
せた合金と、ローラ材としては、(4)のNi―Cr―
Fe基合金にMoを多く含有させかつ冷間加工を与
えた合金との組合わせが、最も優れていることを
見出した。
そこで、本発明は、上記目的を達成するため
に、C0.01〜0.3%、Ni30〜50%、Cr18〜24%、
Mo7〜10%、W3%以下、および残部Feからなる
合金に5〜40%の冷間加工を施した摺動側部材
と、重量でC0.01〜0.3%、Ni20〜30%、Cr15〜
20%、Mo0.5〜2%、Ti1〜3%、Al 0.1〜0.5
%、B0.2%以下、V1%以下、残部Feからなる固
定側部材との組合せからなる摺動構造物を提案す
るものである。
〔作 用〕
摺動側部材(ローラ材)および固定側部材(ピ
ン材)の成分限定理由は下記の通りである。
<摺動側部材>
C:0.01〜0.3%
CはCrと結合して炭化物を形成し強度を向上
させる重要な元素である。しかし、C量が0.3%
を越えると、マトリツクスの耐食性が劣り、また
加工性も悪く、冷間加工、熱間加工で割れが生じ
る。また、0.01%未満では硬さが低下する場合が
あるので、C量は0.01〜0.3%の範囲に限定し
た。
Ni:30〜50%
Niはオーステナイト組織を形成し、耐食性を
改善する重要な成分である。Ni量が多いほど耐
食性が改善される。とくにNi量30%以上耐食性
が良い。30%以下では耐食性の効果が十分でな
い。一方、50%を越えると熱間加工性を低めると
共に材料原価が上昇するので、30〜50%の範囲で
添加する必要がある。
Cr:18〜24%
Crは強度、耐食性、耐酸化性を向上させる重
要な添加元素である。Cr量が18%未満であれ
ば、その効果が少なく、24%を越えると炭素との
結合が多くなつて脆化するので、Cr含有量は18
〜24%の範囲に限定した。
Mo:7〜10%
Moはオーステナイト基地を強化すると共に、
炭化物を形成して引張り強度等を向上させる元素
である。7%未満では、その効果が少なく、10%
を越えると、延性が低下し切削加工が困難になる
ため、Mo量を7〜10%の範囲に限定した。
W:3%以下
WはMoと同様、オーステナイト基地を強化す
ると共に、炭化物を形成して引張り強度等を向上
させる元素である。しかし、W量が3%を越える
と延性が低下し切削加工が困難になるため、その
上限値を3%とする。
加工度:5〜40%
冷間加工は、その度合を40%越えて行なつても
加工度の割りに硬度が上昇しない。また、5%未
満の加工度では硬化が促進されないので、加工度
を5〜40%の範囲に限定した。
<固定側部材>
C:0.01〜0.3%
CはCrと結合して炭化物を形成し強度を向上
させる重要な元素である。しかし、C量が0.3%
を越えると、マトリツクスの耐食性が劣り、ま
た、加工性も悪く冷間加工、熱間加工で割れが生
じる。0.01%未満では硬さが低下する場合がある
ので、C量は0.01〜0.3%の範囲に限定した。
Ni:20〜30%
Niはオーステナイト組織を形成し、耐食性を
改善する重要な成分である。しかし、20以下では
その効果が十分でない。一方、30%を越えると、
熱間加工性を低める。さらに溶接割れを高めるの
で、Ni量は20〜30%の範囲に限定した。
Cr:15〜20%
Crは強度、耐食性、耐酸化性を向上させる重
要な添加元素である。Cr量が15%未満であれ
ば、その効果が少なく、20%を越えると炭素との
結合が多くなつて脆化するので、Cr含有量は15
〜20%の範囲に限定した。
Mo:0.5〜2%
Moはオーステナイト基地を強化すると共に、
炭化物を形成して引張り強度等を向上させる元素
である。0.5%未満ではその効果が少なく、2%
を越えると延性が低下し切削加工が困難になるた
め、Mo量は0.5〜2%の範囲に限定した。
Ti:1〜3%及びAl:0.1〜0.5%
Ti及びAlはNiと化合して金属間化合物である
γ′相〔Ni3(Al、Ti)〕を形成する析出硬化元素
である。このγ′相はオーステナイト基地との整
合性がよく、格子ひずみを生ずるので、強度の改
善に有効である。また、Tiは脱酸剤として作用
すると共に、上記のように強度、延性を向上させ
るに有効なγ′相を析出させる重要な元素であつ
て、1%未満ではその効果が少なく、3%を越え
ると、延性を低下させるη相が析出し易くなるた
め、Ti量を1〜3%の範囲に限定した。
一方、AlはTiと結合して金属化合物γ′相を析
出して強度を向上させる元素であるが、0.1%未
満ではこの効果が少なく、0.5%を越えると、か
えつて強度を低下させるため、単独添加のAl量
を0.1〜0.5%の範囲に限定した。
B:0.2%以下
Bは結晶粒界を著しく強化ししかも延性を改善
する元素であるが、多量に添加すると、鍛造性及
び耐酸化性に悪影響を及びすため、上限を0.2%
以下とした。
V:1%以下
VはVC等の析出物を生成する元素である。VC
は時効硬化性があるため、引張強さを向上させる
のに有効である。しかし、V量が増加すると、V
はCr2O3等の金属保護被覆に拡散して、その融点
を低めるため低酸化性に悪影響を及ぼす。そこで
V量は1%以下とした。
なお、前記(1)のNi基のγ′型、あるいは(2)の炭
化物析出型、さらには(3)のNi3B金属間化合物析
出合金は、硬さは充分で耐食性にも優れていた
が、耐摩耗性は劣つていた。
〔実施例〕
以下、本発明を実施例および比較例によりさら
に詳細に説明する。
第1表に摺動摩耗試験に供した材料の化学成分
(重量%)を示す。第2表には材料に施した熱処
理と硬さを示す。ローラ材としてNo.1〜5の5
種、ピン材としてNo.6〜9の4種について試験し
た。ローラ材は摺動側に、ピン材は固定側に置い
て、純水中で摺動摩耗試験を行なつた。試験条件
は、室温と70℃の高温大気圧下で行なつたが、室
温と70℃との差はみられない。摺動サイクル28
回/min、摺動距離60mm/回、面圧25Kg/cm2で、
500回、2000回、5000回後にそれぞれの摩耗量を
測定した。
第3図〜第5図に試験結果を示す。
第3図においてローラ材No.1およびNo.2とピン
材No.8との組合わせの結果を示す。
No.1は、第1表に示すように、Niをベースと
し、Ti+Alを7.5%と多くしたγ′析出硬化型合金
で、硬さは500Hである。No.8はFe基合金で、Ti
+Alが2.2%とNo.1よりは低く、Niも26%で硬さ
は260Hと低い。この組合わせでは、No.1(ロー
ラ材)の摩耗量は比較的少ないが、No.8の固定側
(ピン材)の摩耗量が大きい。
No.2はNi基でCとCrを多くした炭化物による
硬化合金であるが、No.8との組合わせの結果では
No.1の場合よりもやや摩耗量が多い。なお、No.8
の摩耗も大きいが、No.1の場合と変わらない。
[Industrial Application Field] The present invention relates to sliding structures, particularly for use in nuclear reactor core control rods such as pins and rollers for fuel control rods that require excellent corrosion resistance and wear resistance. Regarding sliding structures. [Prior Art] Fig. 1 shows an example of a nuclear reactor fuel control rod. In the figure, 1 is a handle of a fuel control rod, 2 is a guide roller consisting of a pin and a roller, which is the object of the present invention, 3 is a stainless steel pipe containing a neutron absorbing material,
4 is a blade that encloses the stainless steel tube 3. As shown in FIG. 2, the guide roller 2 includes a roller 5 made of a cobalt (Co)-based superalloy and a cobalt (Co)-based superalloy.
It consists of a pin 6 made of forged material. [Problems to be Solved by the Invention] The Co-based alloy used in this roller contains high carbon (C1.0%) and high chromium (Cr28%). Therefore, it contains many carbides, and therefore has high hardness, and because of its high chromium content, it has excellent corrosion resistance to high-temperature, high-pressure pure water, and has excellent properties as a roller material. On the other hand, it is used for pin material.
Co-based forged alloys require forgeability, workability, and weldability, so although the C content is 0.1% low and the Cr content is low at 20%, it still has excellent wear resistance and corrosion resistance. However, these alloys have approximately 65%
Since the pin material contains about 50% Co, abrasion powder is generated by the wear of both during use, which is activated and circulates within the system, and is also eluted by corrosion caused by high-temperature and high-pressure pure water. This poses a problem in that the Co that has been removed is contaminated with radioactivity and circulates. An object of the present invention is to provide a sliding structure that has good wear resistance and corrosion resistance and does not cause problems due to Co-induced radioactivity. [Means for solving the problem] In order to achieve the above objective, the materials of the sliding side member and the fixed side member must not contain Co, have excellent wear resistance, and have corrosion resistance against high temperature and high pressure pure water. In addition, the pin material can be forged.
Since it is fixed to the blade by welding, it is also required to have excellent weldability. To obtain wear resistance, the alloy is required to have a certain hardness. The hardness of the alloy is obtained by (a) precipitation hardening due to precipitates and (b) solid solution hardening of the matrix. In the method (a), methods using carbides and intermetallic compounds are typical, and in the method (b), it is necessary to contain a large amount of solid solution strengthening elements such as Mo and W, and furthermore, Work hardening by temporary processing etc. is effective. In addition, in terms of corrosion resistance against high temperature and high pressure water,
The amount of Cr, the amount of Ni, and furthermore the amount of Mo are the most important, and the amount of C is also important. From the above points,
It is necessary to select a suitable alloy that does not contain Co. From the above-mentioned viewpoints, the present inventors have developed (1) a nickel (Ni)-based material containing a large amount of titanium (Ti) and aluminum (Al), and a large amount of Cr;
The so-called γ′ strong precipitation superalloy (Ni 3 (Al, Ti)
(2) Ni-based hardening alloys with high C and even higher Cr by crystallization or precipitation of carbides; (3) Ni-based alloys with B-type intermetallic compounds precipitated; Alloys with high C crystallized; (4) Ni-Cr-Fe-based alloys containing a large amount of Mo and further cold-worked; (5) Fe-based alloys containing Ti and Al; An alloy with a sufficiently high Cr content was selected, and a sliding wear test was conducted in pure water using a combination of four types of alloys as roller materials and three types of alloys as pin materials. This was done because there are materials that are suitable for the roller material on the sliding side but unsuitable for the pin material on the stationary side, and the combination of the two is important in terms of wear characteristics. be. As a result, the Fe-based alloy (5) was used as the pin material.
An alloy containing Ti and Al and a sufficiently high Cr content, and (4) Ni-Cr-
It has been found that the combination of an Fe-based alloy containing a large amount of Mo and an alloy that has been subjected to cold working is the most excellent. Therefore, in order to achieve the above-mentioned object, the present invention provides C0.01~0.3%, Ni30~50%, Cr18~24%,
The sliding side member is made of an alloy consisting of Mo7~10%, W3% or less, and the balance Fe, which has been subjected to 5~40% cold working, and the weight is C0.01~0.3%, Ni20~30%, Cr15~
20%, Mo0.5~2%, Ti1~3%, Al 0.1~0.5
%, B0.2% or less, V1% or less, and the remainder is Fe. [Function] The reasons for limiting the components of the sliding side member (roller material) and fixed side member (pin material) are as follows. <Sliding side member> C: 0.01 to 0.3% C is an important element that combines with Cr to form carbide and improve strength. However, the amount of C is 0.3%
If it exceeds this value, the corrosion resistance of the matrix will be poor, and the workability will be poor, resulting in cracking during cold working and hot working. Moreover, since hardness may decrease if it is less than 0.01%, the amount of C is limited to a range of 0.01 to 0.3%. Ni: 30-50% Ni is an important component that forms an austenite structure and improves corrosion resistance. The higher the amount of Ni, the better the corrosion resistance. Particularly good corrosion resistance with Ni content of 30% or more. If it is less than 30%, the corrosion resistance effect will not be sufficient. On the other hand, if it exceeds 50%, hot workability decreases and material cost increases, so it is necessary to add it in a range of 30 to 50%. Cr: 18-24% Cr is an important additive element that improves strength, corrosion resistance, and oxidation resistance. If the Cr content is less than 18%, the effect will be small, and if it exceeds 24%, the bond with carbon will increase and become brittle, so the Cr content should be 18%.
Limited to a range of ~24%. Mo: 7-10% Mo strengthens the austenite base and
It is an element that forms carbides and improves tensile strength etc. If it is less than 7%, the effect is small, and 10%
If it exceeds this amount, the ductility decreases and cutting becomes difficult, so the amount of Mo was limited to a range of 7 to 10%. W: 3% or less W, like Mo, is an element that strengthens the austenite base and forms carbides to improve tensile strength and the like. However, if the amount of W exceeds 3%, the ductility decreases and cutting becomes difficult, so the upper limit is set at 3%. Working degree: 5-40% Even if cold working is performed to a degree exceeding 40%, the hardness does not increase in proportion to the working degree. Further, since hardening is not promoted with a working degree of less than 5%, the working degree was limited to a range of 5 to 40%. <Fixed side member> C: 0.01 to 0.3% C is an important element that combines with Cr to form carbide and improve strength. However, the amount of C is 0.3%
If it exceeds this value, the corrosion resistance of the matrix will be poor, and the workability will also be poor, causing cracks during cold working and hot working. If it is less than 0.01%, the hardness may decrease, so the amount of C was limited to a range of 0.01 to 0.3%. Ni: 20-30% Ni is an important component that forms an austenite structure and improves corrosion resistance. However, if it is less than 20, the effect is not sufficient. On the other hand, if it exceeds 30%,
Reduces hot workability. Furthermore, the amount of Ni was limited to a range of 20 to 30% because it would increase weld cracking. Cr: 15-20% Cr is an important additive element that improves strength, corrosion resistance, and oxidation resistance. If the Cr content is less than 15%, the effect will be small, and if it exceeds 20%, the bond with carbon will increase and become brittle, so the Cr content should be 15%.
Limited to ~20% range. Mo: 0.5-2% Mo strengthens the austenite base and
It is an element that forms carbides and improves tensile strength etc. If it is less than 0.5%, the effect is small, and 2%
The amount of Mo was limited to a range of 0.5 to 2% since ductility decreases and cutting becomes difficult when it exceeds this amount. Ti: 1-3% and Al: 0.1-0.5% Ti and Al are precipitation hardening elements that combine with Ni to form a γ' phase [Ni 3 (Al, Ti)] which is an intermetallic compound. This γ' phase has good consistency with the austenite matrix and causes lattice strain, so it is effective in improving strength. In addition, Ti is an important element that acts as a deoxidizing agent and precipitates the γ' phase, which is effective in improving strength and ductility as mentioned above. If it exceeds the Ti content, the η phase, which reduces ductility, tends to precipitate, so the amount of Ti was limited to a range of 1 to 3%. On the other hand, Al is an element that combines with Ti and precipitates a metal compound γ' phase to improve strength, but if it is less than 0.1%, this effect is small, and if it exceeds 0.5%, it will actually reduce the strength. The amount of Al added alone was limited to a range of 0.1 to 0.5%. B: 0.2% or less B is an element that significantly strengthens grain boundaries and improves ductility, but when added in large amounts, it has a negative effect on forgeability and oxidation resistance, so the upper limit is set at 0.2%.
The following was made. V: 1% or less V is an element that generates precipitates such as VC. V.C.
Since it has age hardening properties, it is effective in improving tensile strength. However, when the amount of V increases, V
diffuses into metal protective coatings such as Cr 2 O 3 and lowers its melting point, thereby adversely affecting low oxidation properties. Therefore, the amount of V was set to 1% or less. In addition, the Ni-based γ' type (1), the carbide precipitation type (2), and the Ni 3 B intermetallic compound precipitation alloy (3) had sufficient hardness and excellent corrosion resistance. However, the wear resistance was poor. [Examples] Hereinafter, the present invention will be explained in more detail with reference to Examples and Comparative Examples. Table 1 shows the chemical components (% by weight) of the materials subjected to the sliding wear test. Table 2 shows the heat treatments applied to the materials and their hardness. No. 1 to 5 as roller materials
Four types of seed and pin materials, Nos. 6 to 9, were tested. A sliding wear test was conducted in pure water with the roller material placed on the sliding side and the pin material placed on the stationary side. The test conditions were at room temperature and 70°C under high temperature and atmospheric pressure, but no difference was observed between room temperature and 70°C. Sliding cycle 28
times/min, sliding distance 60mm/times, surface pressure 25Kg/ cm2 ,
The amount of wear was measured after 500, 2000, and 5000 times. The test results are shown in FIGS. 3 to 5. FIG. 3 shows the results of the combination of roller materials No. 1 and No. 2 and pin material No. 8. As shown in Table 1, No. 1 is a γ' precipitation hardening alloy based on Ni with a high Ti+Al content of 7.5%, and has a hardness of 500H. No. 8 is an Fe-based alloy, with Ti
+Al is 2.2%, lower than No. 1, Ni is also 26%, and hardness is low at 260H. In this combination, the amount of wear on No. 1 (roller material) is relatively small, but the amount of wear on the fixed side (pin material) of No. 8 is large. No. 2 is a Ni-based hardened alloy made of carbides with a high content of C and Cr, but the result of the combination with No. 8 is
The amount of wear is slightly greater than that of No. 1. In addition, No. 8
Although the wear of No. 1 is also large, it is no different from that of No. 1.
【表】【table】
本発明による摺動構造物は、合金組成として
Coを含まないので、例えば高温高圧の純水にさ
らされる原子炉炉心燃料制御棒に装備されるロー
ラおよびピンに使用した場合に、Coの誘導放射
のおそれがなく、また耐摩耗性と耐食性の両方に
優れており、構造上の信頼性が高くなる等の利点
がある。
The sliding structure according to the present invention has an alloy composition of
Since it does not contain Co, there is no risk of induced Co radiation when used, for example, in rollers and pins installed in nuclear reactor core fuel control rods that are exposed to high-temperature, high-pressure pure water. It is excellent in both, and has advantages such as increased structural reliability.
第1図は原子炉燃料制御棒の構成を示す図、第
2図はそのガイドローラの構成を示す図、第3
図、第4図、第5図、および第6図はそれぞれ本
発明の実施例および比較例における摩耗試験の結
果を示す図である。
5…摺動側部材(ローラ)、6…固定側部材
(ピン)。
Figure 1 is a diagram showing the configuration of the reactor fuel control rod, Figure 2 is a diagram showing the configuration of its guide roller, and Figure 3 is a diagram showing the configuration of the reactor fuel control rod.
FIG. 4, FIG. 5, and FIG. 6 are diagrams showing the results of wear tests in Examples and Comparative Examples of the present invention, respectively. 5... Sliding side member (roller), 6... Fixed side member (pin).
Claims (1)
24%、Mo7〜10%、W3%以下、および残部Feか
らなる合金に5〜40%の冷間加工を施した摺動側
部材と、重量でC0.01〜0.3%、Ni20〜30%、
Cr15〜20%、Mo0.5〜2%、Ti1〜3%、Al0.1〜
0.5%、B0.2%以下、V1%以下、残部Feからなる
固定側部材とからなることを特徴とする摺動構造
物。1 C0.01~0.3%, Ni30~50%, Cr18~ by weight
The sliding side member is made of an alloy consisting of 24% Mo, 7 to 10% W, 3% or less W, and the balance Fe, which is cold-worked to 5 to 40%, C0.01 to 0.3%, Ni 20 to 30% by weight,
Cr15~20%, Mo0.5~2%, Ti1~3%, Al0.1~
A sliding structure comprising a fixed side member consisting of 0.5% B, 0.2% or less, V1% or less, and the remainder Fe.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP5888778A JPS54150317A (en) | 1978-05-19 | 1978-05-19 | Sliding structure |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP5888778A JPS54150317A (en) | 1978-05-19 | 1978-05-19 | Sliding structure |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS54150317A JPS54150317A (en) | 1979-11-26 |
| JPS62992B2 true JPS62992B2 (en) | 1987-01-10 |
Family
ID=13097279
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP5888778A Granted JPS54150317A (en) | 1978-05-19 | 1978-05-19 | Sliding structure |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS54150317A (en) |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS54160993A (en) * | 1978-06-12 | 1979-12-20 | Toshiba Corp | Control-rod drive mechanism |
-
1978
- 1978-05-19 JP JP5888778A patent/JPS54150317A/en active Granted
Also Published As
| Publication number | Publication date |
|---|---|
| JPS54150317A (en) | 1979-11-26 |
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