JPS622028B2 - - Google Patents

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Publication number
JPS622028B2
JPS622028B2 JP59014663A JP1466384A JPS622028B2 JP S622028 B2 JPS622028 B2 JP S622028B2 JP 59014663 A JP59014663 A JP 59014663A JP 1466384 A JP1466384 A JP 1466384A JP S622028 B2 JPS622028 B2 JP S622028B2
Authority
JP
Japan
Prior art keywords
phase
temperature
treatment
tini
shape memory
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
Application number
JP59014663A
Other languages
Japanese (ja)
Other versions
JPS60169552A (en
Inventor
Hiroki Nakanishi
Tsutomu Inui
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Proterial Ltd
Original Assignee
Hitachi Metals Ltd
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Hitachi Metals Ltd filed Critical Hitachi Metals Ltd
Priority to JP1466384A priority Critical patent/JPS60169552A/en
Publication of JPS60169552A publication Critical patent/JPS60169552A/en
Publication of JPS622028B2 publication Critical patent/JPS622028B2/ja
Granted legal-status Critical Current

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  • Heat Treatment Of Nonferrous Metals Or Alloys (AREA)
  • Springs (AREA)

Description

【発明の詳細な説明】 本発明はTiNi相およびTiNi3相の二相を有する
Ni過剰組成のTi―Ni系形状記憶合金に500〜1100
℃の温度範囲での溶体化処理および200〜700℃の
温度範囲での時効処理を施すことにより高温相→
低温相の変態ヒステリシスが極めて小さい形状記
憶合金を得ることを特徴とするTi―Ni系形状記
憶合金の製造方法に関するものである。
[Detailed description of the invention] The present invention has two phases: a TiNi phase and a TiNi 3 phase.
500 to 1100 for Ti-Ni shape memory alloys with excessive Ni composition
High-temperature phase →
The present invention relates to a method for producing a Ti--Ni shape memory alloy, which is characterized by obtaining a shape memory alloy with extremely small transformation hysteresis in the low-temperature phase.

Ti―Ni系形状記憶合金は顕著な形状記憶効果
を示すことおよび優れた機械的性質、耐食性等を
有することから最も広範囲な実用化の検討がなさ
れているものである。
Ti--Ni shape memory alloys are the ones that are being studied most extensively for practical use because they exhibit a remarkable shape memory effect and have excellent mechanical properties, corrosion resistance, etc.

形状記憶効果は低温でマルテンサイト状態にあ
る材料を変形した後加熱すると元の形状に戻るも
のであり、こうした効果を生ずる温度は通常合金
の逆変態開始温度(As点)、逆変態終了温度(Af
点)、マルテンサイト変態開始温度(As点)およ
びマルテンサイト変態終了温度(Mf点)によつ
て決定され、As点において形状記憶効果が開始
されAf点で終了するものである。この形状記憶
効果を生ずる際の回復力は50〜60Kg/mm2に及ぶも
のであり、この回復力を種々の応用品へ利用する
検討がなされている。その応用の代表例に第1図
に示すような形状記憶効果を繰り返し生じさせる
ことを利用したアクチユエーターがある。このア
クチユエーターはバイアス力としての通常のコイ
ルバネ(バイアスバネ)と形状記憶合金コイルバ
ネとが組み合わされたものであり、低温において
は形状記憶合金がバイアスバネよりも降伏応力の
小さなマルテンサイト相の状態であるためにバイ
アスバネの方が強く、形状記憶合金を変形するよ
うに動作し、逆に高温においては形状記憶合金が
バイアスバネよりも降伏応力の大きなβ相の状態
となり、形状記憶合金がバイアスバネを変形する
ように動作する。この場合高温相→低温相の変態
ヒステリシスが小さい程小さな温度範囲において
アクチユエーターとしての動作が容易に得られ
る。
The shape memory effect occurs when a material that is in a martensitic state at low temperatures is deformed and then returns to its original shape when heated. The temperature at which this effect occurs is usually the reverse transformation start temperature (As point) and the reverse transformation end temperature (A point) of the alloy. Af
The shape memory effect starts at the As point and ends at the Af point. The recovery force when producing this shape memory effect ranges from 50 to 60 kg/mm 2 , and studies are being made to utilize this recovery force in various applied products. A typical example of its application is an actuator that utilizes the repeated generation of a shape memory effect, as shown in Figure 1. This actuator is a combination of a normal coil spring (bias spring) as a bias force and a shape memory alloy coil spring.At low temperatures, the shape memory alloy enters a martensitic phase state with a lower yield stress than the bias spring. Therefore, the bias spring is stronger and acts to deform the shape memory alloy, and conversely, at high temperatures, the shape memory alloy enters the β phase state with a higher yield stress than the bias spring, and the shape memory alloy becomes biased. It works to deform a spring. In this case, the smaller the transformation hysteresis from the high temperature phase to the low temperature phase, the easier it is to operate as an actuator in a small temperature range.

しかし、従来のTi―Ni系合金においては高温
相→低温相の変態ヒステリシスが30℃程度と大き
く、このため低温相、高温相を可逆的に得てアク
チユエーターを動作させる温度範囲が大きくなら
ざるを得ず、動作温度範囲が限定される欠点があ
つた。
However, in conventional Ti-Ni alloys, the transformation hysteresis from high-temperature phase to low-temperature phase is as large as about 30°C, so the temperature range in which the actuator operates by reversibly obtaining the low-temperature phase and the high-temperature phase is difficult. Unavoidably, this had the disadvantage that the operating temperature range was limited.

こうした観点から本発明者らは高温相→低温相
の変態ヒステリシスが小さく、第1図に示すよう
なアクチユエーターの動作を容易にする合金を得
るためにTiNi相およびTiNi3相の二相を有するNi
過剰組成のTi―Ni系形状記憶合金に特許請求の
範囲に記載の処理を施したところ有益な効果をも
たらすことを発見したものである。すなわち、溶
体化処理および時効処理により過飽和NiがTiNi3
粒子となつてマトリツクス中に析出し、これに伴
なつて中間相変態が導入され、変態が2段階的に
起こるようになり、高温相→低温相(中間相)の
変態が非常に小さくなる。
From this point of view, the present inventors developed a two-phase TiNi phase and a TiNi 3 phase in order to obtain an alloy that has a small transformation hysteresis from high temperature phase to low temperature phase and facilitates the operation of the actuator as shown in Figure 1. with Ni
It has been discovered that beneficial effects can be brought about when the treatment described in the claims is applied to a Ti--Ni type shape memory alloy with an excessive composition. In other words, supersaturated Ni becomes TiNi 3 through solution treatment and aging treatment.
It becomes particles and precipitates in the matrix, and along with this, an intermediate phase transformation is introduced, and the transformation occurs in two stages, and the transformation from high temperature phase to low temperature phase (intermediate phase) becomes extremely small.

次に本発明における処理条件の限定理由につい
て述べる。
Next, the reasons for limiting the processing conditions in the present invention will be described.

溶体化処理温度についは500℃未満においては
TiNiマトリツクス中へTiNi3の十分な固溶度が得
られないものと考えられ、その効果が十分認めら
れない。また1100℃をこえると酸化によるTi元
素の滅失が問題となる。以上の観点から500〜
1100℃の温度範囲に限定した。
Regarding solution treatment temperature below 500℃
It is thought that sufficient solid solubility of TiNi 3 in the TiNi matrix cannot be obtained, and its effect is not sufficiently recognized. Furthermore, when the temperature exceeds 1100°C, loss of Ti element due to oxidation becomes a problem. 500~ from the above point of view
The temperature range was limited to 1100℃.

時効処理温度については200℃未満においては
十分なTiNi3粒子の析出が起こらず、また700℃を
こえると中間相変態が導入できなくなり、高温相
→低温相(中間相)変態による小ヒステリシスが
得られなくなる。以上の観点から200〜700℃の温
度範囲に限定した。
Regarding the aging treatment temperature, sufficient precipitation of TiNi 3 particles does not occur at temperatures below 200°C, and when it exceeds 700°C, intermediate phase transformation cannot be introduced, resulting in a small hysteresis due to the transformation from high temperature phase to low temperature phase (intermediate phase). I won't be able to do it. From the above point of view, the temperature range was limited to 200 to 700°C.

記憶処理温度については700℃を越える温度に
おいては形状記憶特性が劣化し、また中間相変態
が消失し高温相→低温相(中間相)変態による小
ヒステリシスが得られなくなる。以上の観点から
700℃以下の温度範囲に限定した。
Regarding the memory treatment temperature, at temperatures exceeding 700°C, the shape memory properties deteriorate, and the mesophase transformation disappears, making it impossible to obtain a small hysteresis due to the transformation from high temperature phase to low temperature phase (intermediate phase). From the above point of view
The temperature range was limited to 700℃ or less.

なお、溶体化処理前および時効処理前に記憶す
べき所定の形状に拘束する場合には時効処理によ
り形状を記憶させることが可能であるので記憶処
理を必要としないが、時効処理後に拘束する場合
には記憶処理が必要となる。また記憶すべき所定
の形状への拘束の時期については特許請求の範囲
に記載のいずれかにおいても良好な結果が得られ
る。
Note that when constraining to a predetermined shape to be memorized before solution treatment and aging treatment, the shape can be memorized by aging treatment, so memory treatment is not required; however, when constraining after aging treatment requires memory processing. Furthermore, as for the timing of constraint to a predetermined shape to be memorized, good results can also be obtained with any of the claims.

以下本発明を実施例に基づき説明する。 The present invention will be explained below based on examples.

実施例 1 TiNi相およびTiNi3相の二相を有するNi過剰組
成のTi―50.7at%Ni合金を高周波誘導溶解した後
1000℃にて2時間真空焼鈍を行なつて均一化処理
を施し、その後900℃にて鍛造を行なつてφ12
棒とした。この棒を更に熱間加工および冷間加工
を施しφの線とした。次にこの線を第1図に示
すようなコイルバネに成形し拘束した後800℃に
て2時間溶体化処理も行ない、更に400℃にて5
時間時効処理を施した後変位―温度曲線の測定お
よび示差走査熱量計(DSC)を用いた変態点の
測定を行ない高温相→低温相(中間相)の変態ヒ
ステリシスを確認した。
Example 1 After high-frequency induction melting of a Ti-50.7at%Ni alloy with Ni-excessive composition having two phases of TiNi phase and TiNi three phases
Vacuum annealing was performed at 1000°C for 2 hours to homogenize the material, followed by forging at 900°C to obtain a φ12 bar. This rod was further hot-worked and cold-worked into a wire of φ1 . Next, this wire was formed into a coil spring as shown in Fig. 1, and after being restrained, it was subjected to solution treatment at 800℃ for 2 hours, and then at 400℃ for 5 hours.
After time aging, the displacement-temperature curve was measured and the transformation point was measured using a differential scanning calorimeter (DSC) to confirm the transformation hysteresis from high temperature phase to low temperature phase (intermediate phase).

第2図に実施例1における時効処理後のDSC
による変態点の測定結果を示す。従来の合金にお
いては低温相高温相の変態に起因するDSCピ
ークが加熱時および冷却時に1つづつ認められる
のに対し、本発明方法による合金は中間相変態が
導入され、加熱、冷却時に各々2つづつのピーク
を有する。これに伴なつて冷却時のピークは加熱
時の変態終了温度とほとんど同じ温度で開始する
ようになり、高温相→低温相(中間相)の変態ヒ
ステリシスがほとんど0℃となる。また第3図に
実施例1のコイルバネにおもりにより一定荷重を
付加した場合の変位―温度曲線を示すが、従来材
に比べ極めてヒステリシスが小さくなつているこ
とが明らかである。なお、比較のために従来材の
DSCによる変態点測定結果および変位―温度曲
線を第4図および第5図に示した。
Figure 2 shows DSC after aging treatment in Example 1.
The measurement results of the transformation point are shown. In conventional alloys, one DSC peak due to the transformation of the low-temperature phase to the high-temperature phase is observed during heating and one during cooling, whereas in the alloy produced by the method of the present invention, an intermediate phase transformation is introduced, and two peaks are observed during heating and cooling, respectively. It has one peak after another. Along with this, the peak during cooling starts at almost the same temperature as the transformation end temperature during heating, and the transformation hysteresis from the high temperature phase to the low temperature phase (intermediate phase) becomes almost 0°C. Further, FIG. 3 shows a displacement-temperature curve when a constant load is applied to the coil spring of Example 1 by a weight, and it is clear that the hysteresis is extremely small compared to the conventional material. For comparison, the conventional material
The transformation point measurement results and displacement-temperature curves by DSC are shown in FIGS. 4 and 5.

実施例 2 Ti―51.0at%Ni合金を実施例1の場合と同様な
方法によりφの線とした後800℃にて2時間溶
体化処理を行なつた。次に実施例1の場合と同様
な方法によりコイルバネに成形し拘束した後500
℃にて2時間時効処理を施した。第6図に実施例
2における時効処理後のDSCによる変態点の測
定結果を示す。図から明らかなように中間相変態
が認められ、これに伴なつて高温相→低温相(中
間相)の変態ヒステリシスは2℃程度の非常に小
さい値が得られている。なお、この場合には、時
効処理温度の影響により加熱時の2つのピークが
ほぼ同じ温度に重なつている。また第7図に実施
例2のコイルバネにおもりにより一定荷重を付加
した場合の変位―温度曲線を示すが、従来材に比
べ極めて良好なヒステリシスが得られていること
が明らかである。
Example 2 A Ti-51.0at%Ni alloy was formed into a φ1 wire in the same manner as in Example 1 , and then solution treatment was performed at 800° C. for 2 hours. Next, after forming into a coil spring and restraining it by the same method as in Example 1,
Aging treatment was performed at ℃ for 2 hours. FIG. 6 shows the measurement results of the transformation point by DSC after the aging treatment in Example 2. As is clear from the figure, an intermediate phase transformation is observed, and along with this, the transformation hysteresis from the high temperature phase to the low temperature phase (intermediate phase) has a very small value of about 2°C. In this case, the two peaks during heating overlap at approximately the same temperature due to the influence of the aging treatment temperature. Further, FIG. 7 shows a displacement-temperature curve when a constant load is applied to the coil spring of Example 2 by a weight, and it is clear that extremely good hysteresis is obtained compared to the conventional material.

実施例 3 Ti―51.2at%Ni合金を実施例1の場合と同様な
方法によりφの線とした後900℃にて2時間溶
体化処理を行なつた。次に400℃にて10時間時効
処理を施した後実施例1と同様な方法によりコイ
ルバネに成形し拘束し、更に400℃にて30分間記
憶処理を行なつた。この時の高温相→低温相(中
間相)の変態ヒステリシスは1℃であり、またコ
イルバネの変位―温度曲線においても良好なヒス
テリシスが確認された。
Example 3 A Ti-51.2at%Ni alloy was formed into a φ1 wire in the same manner as in Example 1 , and then solution treatment was performed at 900° C. for 2 hours. Next, it was aged at 400°C for 10 hours, then molded into a coil spring and restrained in the same manner as in Example 1, and further subjected to memory treatment at 400°C for 30 minutes. The transformation hysteresis from the high temperature phase to the low temperature phase (intermediate phase) at this time was 1°C, and good hysteresis was also confirmed in the displacement-temperature curve of the coil spring.

以上実施例で述べたように本発明による合金は
従来の合金に比べ高温相→低温相(中間相)の変
態ヒステリシスが極めて小さく、アクチユエータ
ー等に使用される場合の動作温度範囲の制限を著
しく緩和すると同時に熱応答性を高めるものであ
り極めて有益である。
As described in the examples above, the alloy according to the present invention has an extremely small transformation hysteresis from high temperature phase to low temperature phase (intermediate phase) compared to conventional alloys, and can limit the operating temperature range when used in actuators etc. It is extremely beneficial as it significantly relaxes and at the same time increases thermal responsiveness.

【図面の簡単な説明】[Brief explanation of the drawing]

第1図は形状記憶合金を用いたアクチユエータ
ーを示す図、第2図は実施例1の合金のDSCに
よる変態点測定結果を、第3図は実施例1のコイ
ルバネの変位―温度曲線を示す図、第4図は従来
の合金のDSCによる変態点測定結果を、第5図
は従来の合金の変位―温度曲線を示す図、第6図
は実施例2の合金のDSCによる変態点測定結果
を、第7図は実施例2のコイルバネの変位―温度
曲線を示す図である。 1:コイルバネ、2:形状記憶合金コイルバ
ネ。
Figure 1 shows an actuator using a shape memory alloy, Figure 2 shows the transformation point measurement results of the alloy of Example 1 by DSC, and Figure 3 shows the displacement-temperature curve of the coil spring of Example 1. Figure 4 shows the transformation point measurement result of the conventional alloy by DSC, Figure 5 shows the displacement-temperature curve of the conventional alloy, and Figure 6 shows the transformation point measurement result of the alloy of Example 2 by DSC. The results are shown in FIG. 7, which shows the displacement-temperature curve of the coil spring of Example 2. 1: Coil spring, 2: Shape memory alloy coil spring.

Claims (1)

【特許請求の範囲】 1 TiNi相およびTiNi3相の二相を有するNi過剰
組成のTi―Ni系形状記憶合金において、加工後
記憶させるべき所定の形状に拘束し、次に500〜
1100℃の温度範囲において溶体化処理した後急冷
処理を施し、その後更に200〜700℃の温度範囲に
おいて時効処理を施すことを特徴とする形状記憶
合金の製造方法。 2 TiNi相およびTiNi3相の二相を有するNi過剰
組成のTi―Ni系形状記憶合金において、加工後
500〜1100℃の温度範囲において溶体化処理した
後急冷処理を施し、次に記憶させるべき所定の形
状に拘束し、その後更に200〜700℃の温度範囲に
おいて時効処理を施すことを特徴とする形状記憶
合金の製造方法。 3 TiNi相およびTiNi3相の二相を有するNi過剰
組成のTi―Ni系形状記憶合金において加工後500
〜1100℃の温度範囲において溶体化処理した後急
冷処理を施し、次に200〜700℃の温度範囲におい
て時効処理を施した後記憶すべき所定の形状に拘
束し、その後更に700℃以下の温度範囲において
記憶処理を行なうことを特徴とする形状記憶合金
の製造方法。
[Claims] 1. In a Ti--Ni shape memory alloy with a Ni-excess composition having two phases, a TiNi phase and a TiNi 3 phase, it is constrained to a predetermined shape to be memorized after processing, and then
A method for manufacturing a shape memory alloy, which comprises performing solution treatment in a temperature range of 1100°C, followed by rapid cooling treatment, and then further performing aging treatment in a temperature range of 200 to 700°C. 2 In a Ti-Ni shape memory alloy with a Ni-excessive composition that has two phases, a TiNi phase and a TiNi 3 phase, after processing
A shape characterized by being subjected to solution treatment in a temperature range of 500 to 1100°C, followed by rapid cooling treatment, then constrained to a predetermined shape to be memorized, and then further subjected to aging treatment in a temperature range of 200 to 700°C. A method for manufacturing memory alloys. 3 After processing in a Ti-Ni shape memory alloy with Ni-excessive composition that has two phases: TiNi phase and TiNi 3 phase,
After solution treatment in the temperature range of ~1100℃, quenching treatment is performed, then aging treatment is performed in the temperature range of 200 to 700℃, and then restrained to a predetermined shape to be memorized, and then further at a temperature of 700℃ or less. 1. A method for producing a shape memory alloy, the method comprising performing a memory treatment within a range.
JP1466384A 1984-01-30 1984-01-30 Manufacture of shape memory alloy Granted JPS60169552A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP1466384A JPS60169552A (en) 1984-01-30 1984-01-30 Manufacture of shape memory alloy

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP1466384A JPS60169552A (en) 1984-01-30 1984-01-30 Manufacture of shape memory alloy

Publications (2)

Publication Number Publication Date
JPS60169552A JPS60169552A (en) 1985-09-03
JPS622028B2 true JPS622028B2 (en) 1987-01-17

Family

ID=11867450

Family Applications (1)

Application Number Title Priority Date Filing Date
JP1466384A Granted JPS60169552A (en) 1984-01-30 1984-01-30 Manufacture of shape memory alloy

Country Status (1)

Country Link
JP (1) JPS60169552A (en)

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS58151445A (en) * 1982-02-27 1983-09-08 Tohoku Metal Ind Ltd Titanium-nickel alloy having reversible shape storage effect and its manufacture
JPS5928548A (en) * 1982-08-06 1984-02-15 Kazuhiro Otsuka Superelastic shape-memory ni-ti base alloy and manufacture thereof

Also Published As

Publication number Publication date
JPS60169552A (en) 1985-09-03

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