JPH11335757A - High-strength, high-ductility titanium alloy with excellent resistance to high-temperature atmospheric oxidation - Google Patents
High-strength, high-ductility titanium alloy with excellent resistance to high-temperature atmospheric oxidationInfo
- Publication number
- JPH11335757A JPH11335757A JP14645698A JP14645698A JPH11335757A JP H11335757 A JPH11335757 A JP H11335757A JP 14645698 A JP14645698 A JP 14645698A JP 14645698 A JP14645698 A JP 14645698A JP H11335757 A JPH11335757 A JP H11335757A
- Authority
- JP
- Japan
- Prior art keywords
- alloy
- strength
- content
- oxidation resistance
- ductility
- 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
- 230000003647 oxidation Effects 0.000 title claims abstract description 48
- 238000007254 oxidation reaction Methods 0.000 title claims abstract description 48
- 229910001069 Ti alloy Inorganic materials 0.000 title claims abstract description 19
- 229910045601 alloy Inorganic materials 0.000 claims abstract description 39
- 239000000956 alloy Substances 0.000 claims abstract description 39
- 229910052760 oxygen Inorganic materials 0.000 claims abstract description 18
- 229910052742 iron Inorganic materials 0.000 claims abstract description 13
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 claims abstract description 11
- 239000001301 oxygen Substances 0.000 claims abstract description 11
- 229910052726 zirconium Inorganic materials 0.000 claims abstract description 11
- 239000000203 mixture Substances 0.000 claims description 4
- 239000006104 solid solution Substances 0.000 abstract description 8
- 239000002994 raw material Substances 0.000 abstract description 2
- 239000000243 solution Substances 0.000 abstract 1
- 229910052845 zircon Inorganic materials 0.000 abstract 1
- 230000000694 effects Effects 0.000 description 14
- 238000010438 heat treatment Methods 0.000 description 11
- 229910052804 chromium Inorganic materials 0.000 description 6
- 230000007423 decrease Effects 0.000 description 6
- 238000012360 testing method Methods 0.000 description 6
- 238000005259 measurement Methods 0.000 description 5
- 229910052759 nickel Inorganic materials 0.000 description 5
- 229910052757 nitrogen Inorganic materials 0.000 description 5
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 4
- 229910052799 carbon Inorganic materials 0.000 description 4
- 229910052748 manganese Inorganic materials 0.000 description 4
- 238000004519 manufacturing process Methods 0.000 description 4
- 239000000126 substance Substances 0.000 description 4
- 229910052719 titanium Inorganic materials 0.000 description 4
- 239000010936 titanium Substances 0.000 description 4
- 229910052782 aluminium Inorganic materials 0.000 description 3
- 238000010586 diagram Methods 0.000 description 3
- 238000011156 evaluation Methods 0.000 description 3
- 238000009864 tensile test Methods 0.000 description 3
- 238000000137 annealing Methods 0.000 description 2
- 230000000052 comparative effect Effects 0.000 description 2
- 229910052750 molybdenum Inorganic materials 0.000 description 2
- 238000005728 strengthening Methods 0.000 description 2
- 229910052720 vanadium Inorganic materials 0.000 description 2
- 229910000640 Fe alloy Inorganic materials 0.000 description 1
- 229910000831 Steel Inorganic materials 0.000 description 1
- 229910010340 TiFe Inorganic materials 0.000 description 1
- 229910006501 ZrSiO Inorganic materials 0.000 description 1
- 239000002253 acid Substances 0.000 description 1
- 239000000654 additive Substances 0.000 description 1
- 230000000996 additive effect Effects 0.000 description 1
- 238000005275 alloying Methods 0.000 description 1
- PNEYBMLMFCGWSK-UHFFFAOYSA-N aluminium oxide Inorganic materials [O-2].[O-2].[O-2].[Al+3].[Al+3] PNEYBMLMFCGWSK-UHFFFAOYSA-N 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 210000000988 bone and bone Anatomy 0.000 description 1
- 239000002131 composite material Substances 0.000 description 1
- 238000005260 corrosion Methods 0.000 description 1
- 230000007797 corrosion Effects 0.000 description 1
- 238000002474 experimental method Methods 0.000 description 1
- 238000005242 forging Methods 0.000 description 1
- 239000007789 gas Substances 0.000 description 1
- 238000005098 hot rolling Methods 0.000 description 1
- 238000007373 indentation Methods 0.000 description 1
- 239000003112 inhibitor Substances 0.000 description 1
- 238000002844 melting Methods 0.000 description 1
- 230000008018 melting Effects 0.000 description 1
- 230000035515 penetration Effects 0.000 description 1
- 238000012545 processing Methods 0.000 description 1
- 238000001953 recrystallisation Methods 0.000 description 1
- 238000005096 rolling process Methods 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
- 238000010998 test method Methods 0.000 description 1
- 229910052718 tin Inorganic materials 0.000 description 1
- 230000004584 weight gain Effects 0.000 description 1
- 235000019786 weight gain Nutrition 0.000 description 1
Landscapes
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
Description
【0001】[0001]
【発明の属する技術分野】本発明は、高温の大気中にお
ける耐酸化性(以下、耐高温大気酸化性と記す)に優れ
た高強度、高延性チタン合金に関する。BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a high-strength, high-ductility titanium alloy having excellent oxidation resistance in a high-temperature atmosphere (hereinafter referred to as high-temperature atmospheric oxidation resistance).
【0002】[0002]
【従来の技術】チタン合金は、軽量であるにもかかわら
ず高強度で、耐疲労特性や耐食性に優れているという特
長を有している。そのため、航空機部品、自動車部品、
スポーツやレジャー用具、人工骨などの医療用品および
化学工業の設備用部品など種々の用途に利用されてい
る。2. Description of the Related Art Titanium alloys are characterized by high strength despite being lightweight, and excellent fatigue resistance and corrosion resistance. Therefore, aircraft parts, automobile parts,
It is used for various purposes such as sports and leisure tools, medical supplies such as artificial bones, and parts for equipment in the chemical industry.
【0003】高強度で延性に優れたチタン合金として
は、「α+β型」および「β型」があり、いずれもチタ
ンにV、Al、Mo、Cr、SnおよびFeなどの成分
を添加することによって機械特性を改善した合金であ
る。[0003] Titanium alloys having high strength and excellent ductility include "α + β type" and "β type". Both of them are obtained by adding components such as V, Al, Mo, Cr, Sn and Fe to titanium. An alloy with improved mechanical properties.
【0004】Ti−5%Al−2.5%Fe合金は、高
価な添加成分であるVを、比較的安価で人体に無害な元
素であるFeで代替することによって製造コストを低減
した合金として知られている。[0004] The Ti-5% Al-2.5% Fe alloy is an alloy whose production cost has been reduced by substituting V which is an expensive additive component with Fe which is an element which is relatively inexpensive and harmless to the human body. Are known.
【0005】特開平1−252747号公報に、多量の
合金成分を含有させることなく強度と延性を改善した、
Fe:0.1〜0.8%とO(酸素)、Nを含有するチ
タン合金が開示されている。Japanese Patent Application Laid-Open No. 1-252747 discloses that strength and ductility are improved without containing a large amount of alloy components.
A titanium alloy containing 0.1 to 0.8% of Fe, O (oxygen) and N is disclosed.
【0006】国際公開WO96/33292号公報に、
Al、VおよびMo等の製造コスト高める合金元素を含
有させないで強度と高延性を改善した、Fe:0.9〜
2.3%とO(酸素)、Nさらに必要によりCr、Ni
を含有させたチタン合金が開示されている。[0006] International Publication WO96 / 33292 discloses that
Fe: 0.9 to Fe and 0.9 with improved strength and high ductility without containing alloying elements such as Al, V and Mo that increase the production cost.
2.3% with O (oxygen), N and Cr and Ni if necessary
Is disclosed.
【0007】しかし、これらの新しく開発された合金
は、高温での大気中で酸化し易いFeを多量に含んでい
る。そのため、耐高温大気酸化性に欠けている。[0007] However, these newly developed alloys contain a large amount of Fe which is easily oxidized in the atmosphere at high temperatures. Therefore, it lacks high-temperature atmospheric oxidation resistance.
【0008】ここでいう「高温」とは、「400〜11
00℃」のことであり、熱間加工および熱処理のための
加熱温度に相当している。[0008] The term "high temperature" used herein means "400 to 11".
00 ° C. ”, which corresponds to the heating temperature for hot working and heat treatment.
【0009】耐高温大気酸化性が劣る場合、熱間圧延あ
るいは熱間鍛造などの熱間加工工程、あるいは、焼鈍や
再結晶を目的とした熱処理工程において、酸化スケール
の生成による歩留りの低下、加工製品の寸法精度の低
下、加工中の酸化スケールの巻き込みによる表面キズの
発生等の問題が生じる。When the high-temperature atmospheric oxidation resistance is inferior, in a hot working step such as hot rolling or hot forging, or in a heat treatment step for annealing or recrystallization, the yield is reduced due to the formation of oxide scale, and the working is reduced. Problems such as a decrease in the dimensional accuracy of the product and the occurrence of surface flaws due to entrapment of the oxide scale during processing are caused.
【0010】大気酸化を抑制するための対策としては、
加熱前の合金表面への酸化抑制剤の塗布や、Arガスな
どの不活性雰囲気中での加熱等があるが、いずれも労力
や設備を必要とし、製造コストを増大させるため実用的
ではない。[0010] Measures for suppressing atmospheric oxidation include:
Application of an oxidation inhibitor to the surface of the alloy before heating, heating in an inert atmosphere such as Ar gas, etc., are all impractical because they require labor and equipment and increase manufacturing costs.
【0011】TITANIUM '80、Proceedings of the Fourth
International Conference on Titanium、P.2755には、
チタンへのZrおよびSiの添加は大気酸化の抑制に有
効であることが報告されている。しかし、酸化し易いF
eを含有させた場合のZrやSiの酸化抑制効果は知ら
れていなかった。[0011] TITANIUM '80, Proceedings of the Fourth
International Conference on Titanium, P.2755,
It has been reported that the addition of Zr and Si to titanium is effective in suppressing atmospheric oxidation. However, F which is easily oxidized
The effect of suppressing the oxidation of Zr and Si when e is contained has not been known.
【0012】[0012]
【発明が解決しようとする課題】本発明の課題は、酸化
し易いFeを含有する耐高温大気酸化性にすぐれた高強
度、高延性チタン合金を提供することにある。SUMMARY OF THE INVENTION An object of the present invention is to provide a high-strength, high-ductility titanium alloy containing Fe that is easily oxidized and having excellent resistance to high-temperature atmospheric oxidation.
【0013】[0013]
【課題を解決するための手段】耐高温大気酸化性にすぐ
れた高強度、高延性チタン合金に係わる本発明の要旨は
以下の通りである。The gist of the present invention relating to a high-strength, high-ductility titanium alloy excellent in high-temperature atmospheric oxidation resistance is as follows.
【0014】(1)質量%で、Fe:0.2〜5%、O
(酸素):0.05〜0.75%を含み、さらにZrを
下記の範囲内で含有していること特徴とする高温の大気
中における耐酸化性に優れた高強度、高延性チタン合
金。(1) In mass%, Fe: 0.2 to 5%, O
(Oxygen): A high-strength, high-ductility titanium alloy containing 0.05 to 0.75% and further containing Zr in the following range and having excellent oxidation resistance in high-temperature air.
【0015】Zr(質量%):0.01・e0.7[Fe]〜
20・e-0.2[Fe] ここで、[Fe]は合金中の含有量(質量%)を示し、
eは自然対数の底数を示す (2)質量%で、Fe:0.2〜5%、O(酸素):
0.05〜0.75%を含み、さらにZrとSiとを下
記の範囲内で含有していること特徴とする高温の大気中
における耐酸化性に優れた高強度、高延性チタン合金。Zr (% by mass): 0.01 · e 0.7 [Fe]
20 · e −0.2 [Fe] Here, [Fe] indicates the content (% by mass) in the alloy,
e indicates the base of the natural logarithm. (2) In mass%, Fe: 0.2 to 5%, O (oxygen):
A high-strength, high-ductility titanium alloy excellent in oxidation resistance in a high-temperature atmosphere, containing 0.05 to 0.75%, and further containing Zr and Si in the following range.
【0016】Zr(質量%):0.01・e0.7[Fe]〜
20・e-0.2[Fe] Si(質量%):0.01・e0.5[Fe]〜5・e
-0.5[Fe] ここで、[Fe]は合金中の含有量(質量%)を示し、
eは自然対数の底数を示す本発明者らは、酸化し易いF
eを含有するチタン合金の耐高温大気酸化性を改善する
ため種々実験検討をおこなた結果、下記の知見を得た。Zr (% by mass): 0.01 · e 0.7 [Fe]
20 · e -0.2 [Fe] Si (mass%): 0.01 · e 0.5 [Fe] to 5 · e
-0.5 [Fe] where [Fe] indicates the content (% by mass) in the alloy,
e indicates the base of the natural logarithm.
As a result of conducting various experimental studies to improve the high-temperature atmospheric oxidation resistance of a titanium alloy containing e, the following findings were obtained.
【0017】a)Fe含有チタン合金にZrを含有させ
た場合、Zrの耐高温大気酸化性向上効果は、Fe含有
量に影響される。A) When Zr is contained in an Fe-containing titanium alloy, the effect of improving the high-temperature atmospheric oxidation resistance of Zr is affected by the Fe content.
【0018】b)耐高温大気酸化性を改善する効果を得
るに必要なZrの下限量は、Fe含有が増加するにした
がって増加する。しかし、Zrの含有量の上限は、Fe
含有量が増加するにしたがい低減させなければ延性が劣
化する。B) The lower limit of Zr required to obtain the effect of improving the high-temperature atmospheric oxidation resistance increases as the Fe content increases. However, the upper limit of the Zr content is Fe
If the content is not reduced as the content increases, the ductility deteriorates.
【0019】c)すなわち、Zrの含有量を0.01・
e0.7[Fe]〜 20・e-0.2[Fe]の範囲とすることにより
耐高温大気酸化性が得られ、かつ延性も確保できる。C) That is, when the content of Zr is 0.01
By setting the range of e 0.7 [Fe] to 20 · e −0.2 [Fe] , high-temperature atmospheric oxidation resistance can be obtained and ductility can be ensured.
【0020】d)FeおよびZr含有チタン合金に、さ
らにSiを含有させると一層耐高温大気酸化性が向上す
ると共に強度も向上する。D) If the titanium alloy containing Fe and Zr further contains Si, the high-temperature atmospheric oxidation resistance is further improved and the strength is also improved.
【0021】e)耐高温大気酸化性を改善する効果を得
るのに必要なSiの下限量は、Fe含有量が増加するに
したがって増加させる必要がある。しかし、Siの含有
量の上限はFe含有量が増加するにつれ低減させなけれ
ば延性および大気酸化特性が劣化する。E) The lower limit of the amount of Si required to obtain the effect of improving the resistance to high-temperature atmospheric oxidation must be increased as the Fe content increases. However, if the upper limit of the Si content is not reduced as the Fe content increases, the ductility and atmospheric oxidation characteristics deteriorate.
【0022】f)すなわち、Siを含有させる場合、そ
の含有量は0.01・e(0.5[Fe]〜5・e-0.5[Fe]の範
囲内としなければならない。F) That is, when Si is contained, its content must be in the range of 0.01 · e (0.5 [Fe] to 5 · e −0.5 [Fe]) .
【0023】[0023]
【発明の実施の形態】本発明のチタン合金について化学
組成を限定した理由について以下に説明する。なお、化
学組成の%表示は質量%を示す。DESCRIPTION OF THE PREFERRED EMBODIMENTS The reasons for limiting the chemical composition of the titanium alloy of the present invention will be described below. In addition,% display of a chemical composition shows mass%.
【0024】Fe:Feは、欠くことのできない重要な
合金元素である。Feは、母相であるα相中にβ相ある
いはTiFe相を形成する作用があり、合金の組織を多
相化することによって強度を高める。Fe: Fe is an indispensable important alloy element. Fe has an action of forming a β phase or a TiFe phase in the α phase which is a parent phase, and increases the strength by making the structure of the alloy polyphase.
【0025】この効果を発揮させるためには、0.2%
以上含有させる必要がある。一方、Fe含有量が5%を
超えると延性が著しく低下する。したがって、Fe含有
量は、0.2〜5%とした。強度と延性のバランスを考
慮すれば、好ましくは0.2〜3.5%である。In order to exhibit this effect, 0.2%
It is necessary to contain the above. On the other hand, if the Fe content exceeds 5%, the ductility is significantly reduced. Therefore, the Fe content is set to 0.2 to 5%. Taking into account the balance between strength and ductility, the content is preferably 0.2 to 3.5%.
【0026】O(酸素):OもFeと同様に欠くことの
できない重要な元素である。Oは、固溶強化作用によっ
て合金の強度を向上させる作用がある。その効果を得る
ためには、O含有量を0.05%以上とする必要があ
る。しかし、0.75%を超えると、Oの固溶量が過剰
となり延性が低下する。したがって、O含有量は0.0
5〜0.75%とした。強度と延性のバランスを考慮す
れば、好ましくは0.1〜0.6%である。O (oxygen): O is also an important element indispensable like Fe. O has a function of improving the strength of the alloy by a solid solution strengthening function. To obtain the effect, the O content needs to be 0.05% or more. However, if it exceeds 0.75%, the amount of solid solution of O becomes excessive and ductility decreases. Therefore, the O content is 0.0
5 to 0.75%. In consideration of the balance between strength and ductility, the content is preferably 0.1 to 0.6%.
【0027】Zr:Zrは、本発明の合金において重要
な元素であり、緻密なZr酸化物層を合金表面に形成
し、酸素の合金への侵入を抑制して耐高温大気酸化性の
向上に寄与する。また、合金に固溶して強度を向上させ
る作用がある。Zr: Zr is an important element in the alloy of the present invention, and forms a dense Zr oxide layer on the surface of the alloy to prevent oxygen from entering the alloy and improve the high-temperature atmospheric oxidation resistance. Contribute. Further, it has the effect of improving the strength by forming a solid solution in the alloy.
【0028】高温大気酸化を抑制するためには、強固な
Zr酸化物層を合金表面に生成させて、酸素が合金に浸
入するのを防止しなければならない。Fe含有量の増加
に比例してFe酸化物の生成も活発となるため、Fe含
有量の増加に伴いてZr含有量の下限値を増加させる必
要がある。Zrの耐高温大気酸化性および強度の向上効
果を得るためには、Zr含量を0.01・e0.7[Fe]%
以上とする必要がある。 一方、Zr含有量が20・e
-0.2[Fe]%を超えると合金の延性が低下する。したがっ
て、Zr含有量は0.01・e0.7[Fe]〜20・e
-0.2[Fe]%とした。In order to suppress high-temperature atmospheric oxidation, a strong Zr oxide layer must be formed on the surface of the alloy to prevent oxygen from entering the alloy. Since the generation of Fe oxides becomes active in proportion to the increase in the Fe content, it is necessary to increase the lower limit of the Zr content as the Fe content increases. In order to obtain the effect of improving the high-temperature atmospheric oxidation resistance and strength of Zr, the Zr content must be 0.01 · e 0.7 [Fe] %.
It is necessary to do above. On the other hand, when the Zr content is 20 · e
If the content exceeds -0.2 [Fe] %, the ductility of the alloy decreases. Therefore, the Zr content is 0.01 · e 0.7 [Fe] to 20 · e.
-0.2 [Fe] %.
【0029】図1は、本発明で規定するZr含有量の範
囲を示す図である。FIG. 1 is a diagram showing the range of the Zr content specified in the present invention.
【0030】この上下限量は、種々実験を重ねて求めた
ものである。Fe含有量に応じた上記のZr含有量の許
容範囲内では、Zr含有量が多いほど耐高温大気酸化性
および強度の改善効果は大きい。しかし、Zrの過剰な
添加は原料コストを増大させるので、Zr含有量は製造
条件および製品規格において必要とされる耐高温大気酸
化性および強度が得られる量までに抑え、過剰な添加を
避けるのがよい。The upper and lower limits are obtained by repeating various experiments. Within the allowable range of the Zr content according to the Fe content, the higher the Zr content, the greater the effect of improving high-temperature atmospheric oxidation resistance and strength. However, since excessive addition of Zr increases the cost of raw materials, the Zr content should be reduced to an amount that provides high-temperature atmospheric oxidation resistance and strength required in manufacturing conditions and product specifications, and excessive addition should be avoided. Is good.
【0031】Si:Siは、より優れた耐高温大気酸化
性および強度を必要とする場合に含有させる元素であ
る。Si: Si is an element to be contained when more excellent high-temperature atmospheric oxidation resistance and strength are required.
【0032】Siは、安定で緻密なZrSiO4 を合金
表面に形成し、酸素の合金への侵入を抑制して耐高温大
気酸化性の向上に寄与する。また、合金に固溶して合金
の強度を向上させる作用がある。Si forms stable and dense ZrSiO 4 on the alloy surface, suppresses the penetration of oxygen into the alloy, and contributes to the improvement of high-temperature atmospheric oxidation resistance. Further, it has the effect of improving the strength of the alloy by being dissolved in the alloy.
【0033】上記したように、Fe含有量の増加によっ
てFe酸化物の生成も活発となるので、Feの高温大気
酸化を抑制するためには強固なSi酸化物層を合金表面
に生成させるのがよい。そのため、Fe含有量の増加に
あわせてSi含有量の下限値も増加させる必要がある。
したがって、Siの耐高温大気酸化性および強度の向上
効果を得るためには、Si含有量を5・e-0.5[Fe]%以
上とする必要がある。一方、Si含有量がある範囲を超
えると合金の延性が低下すると同時に、低融点(110
0℃前後)のFe・Si複合酸化物が生成し、Si酸化
物層が脆弱となるために大気酸化特性が著しく劣化す
る。このSi含有量の上限は、Fe含有量が多くなるに
したがって少なくしなければ延性および耐高温大気酸化
性が劣化する。したがって、Siの上限は、0.01・
e0.5[Fe]%とする必要がある。As described above, since the generation of Fe oxides becomes active due to the increase of the Fe content, it is necessary to form a strong Si oxide layer on the alloy surface in order to suppress the high-temperature atmospheric oxidation of Fe. Good. Therefore, it is necessary to increase the lower limit of the Si content in accordance with the increase in the Fe content.
Therefore, in order to obtain the effect of improving the high-temperature atmospheric oxidation resistance and strength of Si, the Si content needs to be 5 · e −0.5 [Fe] % or more. On the other hand, if the Si content exceeds a certain range, the ductility of the alloy is lowered and, at the same time, the low melting point (110
(Approximately 0 ° C.), an Fe / Si composite oxide is generated, and the Si oxide layer becomes brittle, so that atmospheric oxidation characteristics are significantly deteriorated. If the upper limit of the Si content is not reduced as the Fe content increases, ductility and high-temperature atmospheric oxidation resistance deteriorate. Therefore, the upper limit of Si is 0.01 ·
e 0.5 [Fe] %.
【0034】図2に、本発明で規定するSi含有量の範
囲を示す。FIG. 2 shows the range of the Si content defined in the present invention.
【0035】その他の元素:Fe、OおよびZr以外
に、必要によりAl、Cr、Mn、Ni、CおよびN等
を含有させることができ、これらの作用および好適な含
有量は以下の通りである。Other elements: In addition to Fe, O, and Zr, Al, Cr, Mn, Ni, C, N, and the like can be contained as necessary. The functions and preferable contents of these elements are as follows. .
【0036】Al:Alは、固溶強化によって合金の強
度を向上させる作用があるので、合金の強度をさらに向
上させる必要が場合にAlを含有させるのがよい。Al: Al has the effect of improving the strength of the alloy by solid solution strengthening. Therefore, when it is necessary to further improve the strength of the alloy, it is preferable to contain Al.
【0037】この強度向上効果を得るためには、Al含
有量を0.01%以上とするのが好ましい。ただし、A
l含有量が6.5%を超えると合金の延性が低下する。
したがって、Alを含有させる場合は、0.01〜6.
5%、好ましくは0.01〜5%、さらに好ましくは
0.01〜3.5%とする。In order to obtain this strength improving effect, the Al content is preferably set to 0.01% or more. However, A
If the l content exceeds 6.5%, the ductility of the alloy decreases.
Therefore, when Al is contained, 0.01-6.
5%, preferably 0.01 to 5%, more preferably 0.01 to 3.5%.
【0038】Cr、Mn、Ni、CおよびN:これらの
元素も、いずれも合金に固溶し合金の強度を向上させる
作用がある。上記の効果を発揮させる必要がある場合に
は、Cr、Mn、Ni、CおよびNはいずれも0.01
%以上含有させるのが好ましい。ただし、Cr、Mnお
よびNiの含有量が0.5%、CおよびNの含有量が
0.2%をそれぞれ超えると、これらの元素の固溶量が
過剰になるので、合金の延性が低下する。Cr, Mn, Ni, C and N: All of these elements have a function of improving the strength of the alloy by forming a solid solution in the alloy. When it is necessary to exert the above effects, Cr, Mn, Ni, C and N are all 0.01%.
% Is preferably contained. However, if the contents of Cr, Mn and Ni exceed 0.5% and the contents of C and N exceed 0.2%, the solid solution amounts of these elements become excessive, so that the ductility of the alloy decreases. I do.
【0039】[0039]
【実施例】非消耗電極式アーク溶解法によって、表1お
よび表2に示す化学組成の長さ85mm、幅75mm、
厚さ15mmの鋳塊を溶製した。これら35種の鋳塊を
950℃に加熱した後、熱間圧延して厚さ3mmの板に
した。次いで、熱間圧延した板を850℃に加熱し、3
0分間保持する大気中での焼鈍を施した。鋼板表面を切
削加工してチタン合金板の表面に生成した酸化スケール
を除去して、下記する常温引張試験および耐高温大気酸
化性の評価試験を実施した。EXAMPLE The chemical composition shown in Tables 1 and 2 was 85 mm in length, 75 mm in width,
An ingot having a thickness of 15 mm was produced. After heating these 35 types of ingots to 950 ° C., they were hot-rolled into 3 mm thick plates. Next, the hot-rolled sheet was heated to 850 ° C.
Annealing was performed in the atmosphere for 0 minutes. The steel plate surface was cut to remove the oxide scale formed on the surface of the titanium alloy plate, and the following room temperature tensile test and evaluation test of high-temperature atmospheric oxidation resistance were performed.
【0040】[0040]
【表1】 [Table 1]
【0041】[0041]
【表2】 [Table 2]
【0042】表1に示す符号1〜25は本発明例で、符
号A〜Mは比較例である。表1および表2に示した合金
のFe、Zr含有量との関係は、図1に示す通りであ
る。また、FeとSi含有量との関係は図2に示す通り
である。Reference numerals 1 to 25 shown in Table 1 are examples of the present invention, and reference numerals A to M are comparative examples. The relationship between the Fe and Zr contents of the alloys shown in Tables 1 and 2 is as shown in FIG. The relationship between Fe and Si content is as shown in FIG.
【0043】各試験条件および測定項目は以下の通りと
した。The test conditions and measurement items were as follows.
【0044】(1)常温引張試験 試験法:JIS Z2241の規定による 試験片:板状試験片(JIS Z2201に規定されて
いる13号Bの1/2サイズ、厚さ2mm) 測定 :引張強度、伸び (2)耐高温大気酸化性の評価試験 試験片 :板状試験片(長さ25mm、幅20mm、厚
さ2mm) 加熱条件:900℃、1時間、大気中(アルミナ製容器
に試験片を入れ、発熱体式電気炉内で加熱保持) 測定 :酸化増量(電子天秤による加熱前後の重量変
化の測定) 測定結果を表1および表2にまとめて示す。表中の各評
価の基準は以下の通りとした。(1) Room Temperature Tensile Test Test Method: JIS Z2241 Specimen: Plate-shaped Specimen (1/2 size of No. 13B specified in JIS Z2201, thickness 2 mm) Measurement: Tensile strength, Elongation (2) Evaluation test for high-temperature atmospheric oxidation resistance Test piece: Plate-shaped test piece (length: 25 mm, width: 20 mm, thickness: 2 mm) Heating condition: 900 ° C., 1 hour, in air (test piece in alumina container) And heating and holding in a heating element type electric furnace) Measurement: Increase in oxidation (measurement of weight change before and after heating with an electronic balance) The measurement results are summarized in Tables 1 and 2. The criteria for each evaluation in the table were as follows.
【0045】 引張り強さ ○:800MPa以上 伸び ○:5%以上 ▲:5%未満 耐酸化性 ◎:10g/m2 ○:20gm2以下 ▲:100g
/m2以上 表1より明らかなように、本発明例の符号1〜25につ
いては、酸化増量が16g/m2以下であり、耐高温大
気酸化性に優れている。Tensile strength :: 800 MPa or more Elongation :: 5% or more ▲: Less than 5% Oxidation resistance :: 10 g / m 2 :: 20 gm 2 or less :: 100 g
/ M 2 or more As is clear from Table 1, with respect to the reference numerals 1 to 25 of the examples of the present invention, the increase in oxidation is 16 g / m 2 or less, and they are excellent in high-temperature atmospheric oxidation resistance.
【0046】また、引張試験における引張強度は800
MPa以上、伸びは6%以上で、いずれも実用上十分な
性能である。The tensile strength in the tensile test was 800
At least MPa and an elongation of at least 6%, all of which are practically sufficient performance.
【0047】本発明例のなかで、試料11〜21および
24、25は、ZrとSiを複合して含有させた例であ
る。これらの場合は、本発明例のなかでも酸化増量が比
較的小さく、より耐高温大気酸性が要求される用途に適
している。In the examples of the present invention, samples 11 to 21 and 24 and 25 are examples in which Zr and Si are combined and contained. In these cases, among the examples of the present invention, the oxidation weight gain is relatively small, and thus it is suitable for applications requiring higher-temperature atmospheric acid resistance.
【0048】一方、比較例の試料A〜Jは、酸化増量お
よび伸びのどちらかが劣っている。On the other hand, the samples A to J of the comparative examples are inferior in either the oxidation weight increase or the elongation.
【0049】試料A〜CはZr含有量が低すぎるので、
いずれも酸化増量が100g/m2以上と大きい。ま
た、試料D〜FはZr含有量が多すぎ、試料G〜IはS
i含有量が多すぎるので、伸びが2%以下と低くなって
いる。Samples A to C have too low a Zr content.
In each case, the increase in oxidation is as large as 100 g / m 2 or more. Samples DF have too high a Zr content, and Samples GI have Sr.
Since the i content is too large, the elongation is as low as 2% or less.
【0050】[0050]
【発明の効果】本発明の合金は、酸化し易いFeを含有
しているにもかかわらず、耐高温大気酸化性に優れてお
り、また強度、延性にもにも優れている。したがって、
酸化による歩留まり低下が激減し、加熱中に発生したス
ケールに起因する圧延中の押し込み表面疵の発生もない
ので、品質のよいチタン合金製品を安価に製造すること
ができる。The alloy of the present invention is excellent in high-temperature atmospheric oxidation resistance, and also excellent in strength and ductility, despite containing Fe which is easily oxidized. Therefore,
Since the decrease in yield due to oxidation is drastically reduced and there is no indentation surface flaw during rolling caused by scale generated during heating, a high quality titanium alloy product can be manufactured at low cost.
【図1】本発明で規定するZr含有量の範囲と、実施例
に用いた合金のFeとZr含有関係を示す図である。FIG. 1 is a diagram showing a range of a Zr content specified in the present invention and a relationship between Fe and Zr content of an alloy used in an example.
【図2】本発明で規定するSi含有量の範囲と、実施例
に用いた合金のFeとSi含有関係を示す図である。FIG. 2 is a diagram showing the range of the Si content specified in the present invention and the relationship between the Fe and Si contents of the alloy used in the examples.
Claims (2)
素):0.05〜0.75%を含み、さらにZrを下記
の範囲内で含有していること特徴とする高温の大気中に
おける耐酸化性に優れた高強度、高延性チタン合金。 Zr(質量%):0.01・e0.7[Fe]〜 20・e
-0.2[Fe] ここで、[Fe]は合金中の含有量(質量%)を示し、
eは自然対数の底数を示す(1) In mass%, Fe: 0.2 to 5%, O (oxygen): 0.05 to 0.75%, and Zr in the following range. High-strength, high-ductility titanium alloy with excellent oxidation resistance in high-temperature atmosphere. Zr (% by mass): 0.01 · e 0.7 [Fe] to 20 · e
-0.2 [Fe] where [Fe] indicates the content (% by mass) in the alloy,
e indicates the base of the natural logarithm
素):0.05〜0.75%を含み、さらにZrとSi
とを下記の範囲内で含有していること特徴とする高温の
大気中における耐酸化性に優れた高強度、高延性チタン
合金。 Zr(質量%):0.01・e0.7[Fe]〜 20・e
-0.2[Fe] Si(質量%):0.01・e0.5[Fe]〜5・e
-0.5[Fe] ここで、[Fe]は合金中の含有量(質量%)を示し、
eは自然対数の底数を示す2. The composition contains, by mass%, Fe: 0.2 to 5% and O (oxygen): 0.05 to 0.75%, and further comprises Zr and Si.
A high-strength, high-ductility titanium alloy excellent in oxidation resistance in a high-temperature atmosphere in the following range. Zr (% by mass): 0.01 · e 0.7 [Fe] to 20 · e
-0.2 [Fe] Si (mass%): 0.01 e 0.5 [Fe] to 5 e
-0.5 [Fe] where [Fe] indicates the content (% by mass) in the alloy,
e indicates the base of the natural logarithm
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP14645698A JPH11335757A (en) | 1998-05-28 | 1998-05-28 | High-strength, high-ductility titanium alloy with excellent resistance to high-temperature atmospheric oxidation |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP14645698A JPH11335757A (en) | 1998-05-28 | 1998-05-28 | High-strength, high-ductility titanium alloy with excellent resistance to high-temperature atmospheric oxidation |
Publications (1)
Publication Number | Publication Date |
---|---|
JPH11335757A true JPH11335757A (en) | 1999-12-07 |
Family
ID=15408060
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP14645698A Pending JPH11335757A (en) | 1998-05-28 | 1998-05-28 | High-strength, high-ductility titanium alloy with excellent resistance to high-temperature atmospheric oxidation |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPH11335757A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN106119604A (en) * | 2016-08-18 | 2016-11-16 | 江苏大学 | A Y2O3 alloyed Ti-8Si-1.4Zr alloy and its preparation method |
CN109266907A (en) * | 2018-11-10 | 2019-01-25 | 北京工业大学 | A kind of high strength and low cost Ti-Zr-Fe medical titanium alloy |
US12123065B2 (en) | 2015-12-24 | 2024-10-22 | Posco Co., Ltd | Grain-oriented electrical steel sheet and method for manufacturing same |
-
1998
- 1998-05-28 JP JP14645698A patent/JPH11335757A/en active Pending
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US12123065B2 (en) | 2015-12-24 | 2024-10-22 | Posco Co., Ltd | Grain-oriented electrical steel sheet and method for manufacturing same |
CN106119604A (en) * | 2016-08-18 | 2016-11-16 | 江苏大学 | A Y2O3 alloyed Ti-8Si-1.4Zr alloy and its preparation method |
CN109266907A (en) * | 2018-11-10 | 2019-01-25 | 北京工业大学 | A kind of high strength and low cost Ti-Zr-Fe medical titanium alloy |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
JP4116677B2 (en) | Aluminum-containing iron-based alloys useful as electrical resistance heating elements | |
EP0396338B1 (en) | Oxidation resistant titanium base alloy | |
CA2485122C (en) | Alpha-beta ti-al-v-mo-fe alloy | |
US4711761A (en) | Ductile aluminide alloys for high temperature applications | |
KR101536402B1 (en) | Titanium alloy product having high strength and excellent cold rolling property | |
JP2001089821A (en) | High-strength, high-ductility titanium alloy with excellent resistance to high-temperature atmospheric oxidation | |
EP3844314B1 (en) | Creep resistant titanium alloys | |
Aimone et al. | Niobium alloys for the chemical process industry | |
WO2005118898A1 (en) | Titanium alloy and method of manufacturing titanium alloy material | |
JP2020026568A (en) | Titanium alloy, method for producing the same, and engine component using the same | |
JP2952924B2 (en) | TiAl-based heat-resistant alloy and method for producing the same | |
JP3297011B2 (en) | High strength titanium alloy with excellent cold rollability | |
JPH11335757A (en) | High-strength, high-ductility titanium alloy with excellent resistance to high-temperature atmospheric oxidation | |
JP2936899B2 (en) | Titanium alloy with excellent corrosion resistance and workability to non-oxidizing acids | |
JP2004183079A (en) | Method for producing titanium alloy and titanium alloy material | |
JP2970432B2 (en) | High temperature stainless steel and its manufacturing method | |
JPH083665A (en) | Nickel-base superalloy for die excellent in oxidation resistance and high temperature strength | |
JP3297012B2 (en) | High strength titanium alloy with excellent cold rollability | |
JP3365190B2 (en) | Post heat treatment method for α + β type titanium alloy welded members | |
JPH06228685A (en) | High strength and high ductility tial intermetallic compound and its production | |
JPH04301044A (en) | High toughness titanium alloy capable of cold working | |
JP5533352B2 (en) | β-type titanium alloy | |
JP2009007679A (en) | Titanium alloy and method for producing titanium alloy material | |
JP2001329324A (en) | Titanium alloy | |
JP2915490B2 (en) | High strength aluminum alloy for welded structural materials with excellent resistance to stress corrosion cracking |