JPH0368945B2 - - Google Patents
Info
- Publication number
- JPH0368945B2 JPH0368945B2 JP22331882A JP22331882A JPH0368945B2 JP H0368945 B2 JPH0368945 B2 JP H0368945B2 JP 22331882 A JP22331882 A JP 22331882A JP 22331882 A JP22331882 A JP 22331882A JP H0368945 B2 JPH0368945 B2 JP H0368945B2
- Authority
- JP
- Japan
- Prior art keywords
- alloy
- room temperature
- processing
- rate
- temperature
- 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
Links
- 229910045601 alloy Inorganic materials 0.000 claims description 29
- 239000000956 alloy Substances 0.000 claims description 29
- KHYBPSFKEHXSLX-UHFFFAOYSA-N iminotitanium Chemical compound [Ti]=N KHYBPSFKEHXSLX-UHFFFAOYSA-N 0.000 claims description 21
- 229910004337 Ti-Ni Inorganic materials 0.000 claims description 20
- 229910011209 Ti—Ni Inorganic materials 0.000 claims description 20
- 238000005482 strain hardening Methods 0.000 claims description 9
- 238000000034 method Methods 0.000 claims description 7
- 230000009466 transformation Effects 0.000 claims description 6
- 238000010438 heat treatment Methods 0.000 description 11
- 229910000734 martensite Inorganic materials 0.000 description 6
- 239000000463 material Substances 0.000 description 6
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 3
- 238000003754 machining Methods 0.000 description 3
- 230000003446 memory effect Effects 0.000 description 3
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 3
- XKRFYHLGVUSROY-UHFFFAOYSA-N Argon Chemical compound [Ar] XKRFYHLGVUSROY-UHFFFAOYSA-N 0.000 description 2
- 238000007796 conventional method Methods 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 239000007789 gas Substances 0.000 description 2
- 239000011159 matrix material Substances 0.000 description 2
- 238000010791 quenching Methods 0.000 description 2
- 230000000171 quenching effect Effects 0.000 description 2
- 238000005491 wire drawing Methods 0.000 description 2
- CURLTUGMZLYLDI-UHFFFAOYSA-N Carbon dioxide Chemical compound O=C=O CURLTUGMZLYLDI-UHFFFAOYSA-N 0.000 description 1
- 229910000990 Ni alloy Inorganic materials 0.000 description 1
- 229910052786 argon Inorganic materials 0.000 description 1
- 235000011089 carbon dioxide Nutrition 0.000 description 1
- 238000005097 cold rolling Methods 0.000 description 1
- 238000001816 cooling Methods 0.000 description 1
- 230000006866 deterioration Effects 0.000 description 1
- 229910001873 dinitrogen Inorganic materials 0.000 description 1
- 229910000765 intermetallic Inorganic materials 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 229910001000 nickel titanium Inorganic materials 0.000 description 1
- 229910052757 nitrogen Inorganic materials 0.000 description 1
Landscapes
- Heat Treatment Of Nonferrous Metals Or Alloys (AREA)
Description
本発明はTi−Ni合金の加工方法に関するもの
である。
Ti−Niの金属間化合物およびその一部を他の
元素(Cu、Fe)で置換した合金は、顕著な形状
記憶効果を有することが知られている(米国特許
第3174851号、特開昭53−28518号等)。
このような、Ti−Ni合金は、熱間加工性は良
好であるが、冷間加工性は、Ti−Ni合金の変態
特性と機械特性に相関性を有しているので、合金
組成に応じて変化する。Ni過剰側では変態温度
As(℃)が常温以下であり、冷間圧延、伸線加工
はほとんど不可能と言つて良い程の加工性の悪さ
を示す。
表1に、Ni濃度を変化させた場合のTi−Ni合
金を700℃2時間加熱後水焼入れした試験の変態
温度As(℃)と、線径7mmの母材を冷間で伸線し
た場合の最大加工率を示す。
The present invention relates to a method for processing a Ti-Ni alloy. Ti-Ni intermetallic compounds and alloys in which some of them are replaced with other elements (Cu, Fe) are known to have a remarkable shape memory effect (U.S. Pat. No. 3,174,851, JP-A-53 -28518 etc.) Such Ti-Ni alloys have good hot workability, but cold workability depends on the alloy composition, as there is a correlation between the transformation properties and mechanical properties of the Ti-Ni alloy. and change. On the Ni-excess side, the transformation temperature
As (°C) is below room temperature, and the workability is so poor that cold rolling and wire drawing are almost impossible. Table 1 shows the transformation temperature As (℃) of a test in which Ti-Ni alloy was heated at 700℃ for 2 hours and then water quenched when the Ni concentration was varied, and when a base material with a wire diameter of 7 mm was cold drawn. shows the maximum machining rate.
【表】
表1から明らかなように、Ni過剰側ではAs点
は常温より低く加工率が小さいことがわかる。
また第1図に、Ti−Ni合金のNi濃度に対する
室温25℃での降伏応力の変化を示したが、降伏応
力はNi濃度に大きく依存し、Ni過剰側(50.3at
%以上)で大となつている。したがつて、本発明
の目的は、Ni過剰側(50.3at以上)のTi−Ni合
金の冷間加工性を改良することである。
この目的のため、Ti−Ni合金について、母相
状態およびマルテンサイト相状態での引張応力と
伸び率について調べたところ、第2図のとおりで
あつた。即ちNi49.5atのTi−Ni合金(As=80°)
について常温および80℃以上の温度で線引加工し
て、応力と伸び率を調べた。第2図から明らかな
ように、母相状態での材料の変形には加工開始か
ら高い応力を必要とし、マルテンサイト相で加工
する方が加工しやすいことが判明した。
本発明者は、この新たな事実にもとづき、As
点が常温以下となるNi過剰側のTi−Ni合金のAs
点を高くして、常温でマルテンサイト相とする方
法を種々検討したところ、合金を550℃以下の温
度で熱処理することによつてAs点を常温以上に
できることを発見した。
本発明は、このような新規の知見にもとづいて
なされたもので、Niが50.3at%以上でAs点が常
温以下のTi−Ni合金の加工方法において、該合
金の逆変態開始温度Asを常温以上とするために、
該合金を550℃以下で熱処理し、その後常温で冷
間加工することを特徴とするTi−Ni合金の加工
方法である。
なお、熱処理雰囲気は、大気中、窒素ガス中、
アルゴンガス等いずれでも良い。
本発明によれば、Ni過剰側(50.3at%以上)の
Ti−Ni合金でもAs点が常温以上とされ、常温で
マルテンサイト相であるので、冷間加工が容易で
ある。
従来、このようなNi過剰側のTi−Ni合金の冷
間加工の際、冷間加工と700℃加熱後水焼入れす
るという熱処理工程とを交互に繰返すことは、行
なわれていた。この場合の熱処理は機械的な歪の
除去が目的であり、冷間加工率は、通常5%程度
であり、上記の表1に示すように最大でも十数%
であつた。ただし、ドライアイスや液体窒素を用
いてAs点以下に保つて加工した場合、通常30%
程度の加工率が得られるが、加工装置が冷却装置
の併なうので、複雑となるし、作業者の作業効率
も悪く実用的ではない。
しかるに、本発明によれば、高い加工率をもつ
て常温で冷間加工を行なうことができる。
第3図は、合金の熱処理温度とAs点の関係を
種々のNi濃度について測定した結果を示す。同
図において曲線a,b,c,dはNi濃度がそれ
ぞれ51.11at%、50.77at%、50.56at%、50.30at%
の場合である。同図から明かなように、いずれの
合金も、熱処理温度が550℃以下でAs点が25℃以
上となることがわかる。
以下、本発明の実施例について説明する。
Ni51at%のTi−Ni合金について、700℃焼鈍し
たものと、500℃で熱処理したものについて、常
温で引張つた時の伸び率と引張り応力とを測定し
た。その結果を第4図に示す。曲線aが700℃焼
鈍材で、bが500℃熱処理材である。同図から明
らかなように、曲線bで示される本願発明のもの
の方が、引張り応力が加工開始時から特に小さ
く、第2図のマルテンサイト相の曲線と同様の傾
向を示し、加工が容易であることがわかる。
次に、表2に示す種々のNi濃度のTi−Ni合金
について、熱処理として500℃加熱後、水焼入れ
し、線径7mmのものを冷間で伸線加工した場合の
最大加工率を測定した。その結果を、As点とと
もに表2に示した。なお、最大加工率とは破断寸
前における加工率である。[Table] As is clear from Table 1, on the Ni-excess side, the As point is lower than room temperature and the processing rate is small. Figure 1 shows the change in yield stress at room temperature 25°C with respect to the Ni concentration of the Ti-Ni alloy.
% or more). Therefore, an object of the present invention is to improve the cold workability of Ti-Ni alloys on the Ni-excessive side (50.3 at or more). For this purpose, the tensile stress and elongation rate of the Ti-Ni alloy in the parent phase state and martensitic phase state were investigated, and the results were as shown in Figure 2. i.e. Ti-Ni alloy with Ni49.5at (As=80°)
The wire was drawn at room temperature and at a temperature of 80℃ or higher, and the stress and elongation rate were investigated. As is clear from FIG. 2, deformation of the material in the matrix state requires high stress from the start of processing, and it has been found that processing in the martensitic phase is easier. Based on this new fact, the inventor has determined that As
As of the Ti-Ni alloy on the Ni-excessive side where the point is below room temperature
After investigating various methods of raising the As point to form a martensitic phase at room temperature, we discovered that by heat-treating the alloy at a temperature below 550°C, it is possible to raise the As point above room temperature. The present invention was made based on such new findings, and is a method for processing a Ti-Ni alloy in which Ni is 50.3 at% or more and the As point is below room temperature. In order to achieve the above,
This is a method for processing a Ti-Ni alloy, which is characterized in that the alloy is heat treated at 550°C or lower and then cold worked at room temperature. The heat treatment atmosphere is air, nitrogen gas,
Any gas such as argon gas may be used. According to the present invention, on the Ni-excess side (50.3 at% or more)
Ti-Ni alloy also has an As point above room temperature and is in a martensitic phase at room temperature, so cold working is easy. Conventionally, when cold working Ti--Ni alloys on the Ni-excess side, cold working and a heat treatment step of heating to 700° C. and water quenching have been alternately repeated. The purpose of the heat treatment in this case is to remove mechanical strain, and the cold working rate is usually about 5%, and as shown in Table 1 above, the maximum cold working rate is about 10%.
It was hot. However, if processed using dry ice or liquid nitrogen to maintain the temperature below the As point, it is usually 30%
Although a certain processing rate can be obtained, since the processing equipment is also equipped with a cooling device, it becomes complicated and the work efficiency of the operator is poor, making it impractical. However, according to the present invention, cold working can be performed at room temperature with a high working rate. FIG. 3 shows the results of measuring the relationship between the heat treatment temperature of the alloy and the As point for various Ni concentrations. In the same figure, curves a, b, c, and d have Ni concentrations of 51.11 at%, 50.77 at%, 50.56 at%, and 50.30 at%, respectively.
This is the case. As is clear from the figure, for all alloys, the As point is 25°C or higher when the heat treatment temperature is 550°C or lower. Examples of the present invention will be described below. For Ti-Ni alloys containing 51 at% Ni, the elongation and tensile stress when stretched at room temperature were measured for those annealed at 700°C and those heat treated at 500°C. The results are shown in FIG. Curve a is the material annealed at 700°C, and curve b is the material heat-treated at 500°C. As is clear from the figure, the tensile stress of the present invention shown by curve b is particularly small from the start of processing, and it shows the same tendency as the martensitic phase curve in Fig. 2, making it easier to process. I understand that there is something. Next, for Ti-Ni alloys with various Ni concentrations shown in Table 2, after heating to 500 °C as heat treatment, water quenching, and cold wire drawing of wire diameter 7 mm, the maximum processing rate was measured. . The results are shown in Table 2 along with the As points. Note that the maximum machining rate is the machining rate on the verge of fracture.
【表】
いずれも30%以上の加工率を示すことがわか
る。特にNi過剰側の合金については、冷間加工
率が、従来に比して著しく高くなつたばかりでな
く、加工時間も短縮できた。
なお、加工後の各試料に、従来と同様形状記憶
効果を付与する熱処理を施したところ形状記憶効
果においては、従来法によるものと同様で劣化は
見られなかつた。
以上のように、本発明ではNi過剰側のTi−Ni
合金に550℃以下での熱処理を施した後、冷間加
工によつて加工するものであるが、所要の寸法形
状を得るためにこの熱処理と冷間加工の両工程は
一回のみでなく、交互に複数回繰り返しても良
い。[Table] It can be seen that all of them show a processing rate of 30% or more. In particular, for alloys with excessive Ni, not only the cold working rate was significantly higher than before, but also the working time was shortened. In addition, when each sample after processing was subjected to heat treatment to impart a shape memory effect as in the conventional method, the shape memory effect was the same as that obtained by the conventional method and no deterioration was observed. As described above, in the present invention, Ti-Ni on the Ni-excess side
The alloy is heat treated at 550℃ or less and then cold worked, but in order to obtain the required dimensions and shape, both the heat treatment and cold working steps are not only carried out once, but also It may be repeated several times alternately.
第1図は、Ni濃度と降伏応力との関係を示す
図、第2図は、Ti−Ni合金のマルテンサイト相
および母相状態での伸び率と引張り応力との関係
を示す図、第3図は、種々のNi濃度のTi−Ni合
金についての熱処理温度と逆変態温度Asとの関
係を示す図、第4図は、51at%Ni−Ti合金につ
いての700℃焼鈍材と500℃熱処理材についての伸
び率と引張り応力との関係を示す図である。
Figure 1 is a diagram showing the relationship between Ni concentration and yield stress, Figure 2 is a diagram showing the relationship between elongation rate and tensile stress in the martensitic phase and matrix state of Ti-Ni alloy, The figure shows the relationship between heat treatment temperature and reverse transformation temperature As for Ti-Ni alloys with various Ni concentrations. Figure 4 shows the relationship between 700℃ annealed material and 500℃ heat-treated material for 51 at% Ni-Ti alloy. It is a figure showing the relationship between elongation rate and tensile stress about.
Claims (1)
温以下のTi−Ni合金の加工方法において、該合
金の逆変態開始温度を常温以上とするために該合
金を550℃以下で熱処理し、その後常温で冷間加
工することを特徴とするTi−Ni合金の加工方法。1. In a method for processing a Ti-Ni alloy in which Ni is 50.3 at% or more and the reverse transformation start temperature As is below room temperature, the alloy is heat treated at 550 ° C. or below in order to make the reverse transformation start temperature of the alloy above room temperature, A method for processing a Ti-Ni alloy, which is characterized by cold working at room temperature.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP22331882A JPS59113166A (en) | 1982-12-20 | 1982-12-20 | Method for working ti-ni alloy |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP22331882A JPS59113166A (en) | 1982-12-20 | 1982-12-20 | Method for working ti-ni alloy |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS59113166A JPS59113166A (en) | 1984-06-29 |
| JPH0368945B2 true JPH0368945B2 (en) | 1991-10-30 |
Family
ID=16796270
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP22331882A Granted JPS59113166A (en) | 1982-12-20 | 1982-12-20 | Method for working ti-ni alloy |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS59113166A (en) |
-
1982
- 1982-12-20 JP JP22331882A patent/JPS59113166A/en active Granted
Also Published As
| Publication number | Publication date |
|---|---|
| JPS59113166A (en) | 1984-06-29 |
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