METHOD FOR MAKING TITANIUM-NICKEL ALLOYS

Abstract: A method of making TiNi-alloys having Ni 45 to 60 at % comprises the steps of forming a composite of Ti and Ni mat­ erial, dimention-reducing and diffusing. The method ables to make the setting and changing of each of the composition ratio very easily and certainly. Further, it can repress the scattering of the composition in the interior of the alloy and the variations of the properties of the product.

Description: BACKGROUND OF THE INVENTION 1. Field of the Invention: The present invention relates to the method of making TiNi-alloys, compound material used therein and TiNi-alloys and in particular to the method of making TiNi-alloys having homogeneous composition, which are usable in the capacity of, for example, shape-memorizing alloys or superelastic alloys. 2. Description of the prior art: The TiNi-alloys have various functions such as the shape-memorizing effect, the superelastic behavior, or the oscillation-proof effect. Therefore, they are credited with having the ability of lending themselves to the wide range of many purposes. Heretofore, however, in order to acquire such kinds of TiNi alloys, alike to general alloys, they have been manufactured through many number of processes such as hot working, cold working and heat treatment on ingot obtained by melting titanium together with nickel until they become wire rods of desired size, and further conducting on them after-treatment (for example, heat treatment) with the object of imparting the shape-memorizing effect or others on them. But in the case of such manufacturing methods, it is difficult not only to controll the composition of titanium with nickel at the time of melting but also hard to obtain the product of the homogeneous distribution of the composition because of employing the Ti material being apt to oxidize, and further there occurs a defect of being liable to mix the impurities of oxygen, carbon or the other gases thereinto at the time of melting, too. Consequently, as shown in Fig. 30 (illustrated hereinafter), there are scattered in the product obtained by conventional melting process many number of impurities such as oxide presenting an appearance of black spots, which exert a bad influence upon the performance of the TiNi-alloys. By way of example, in the shape-memorizing alloy, even when modifying Ni-composition only by 0.1 at percentage, its transformation point varies sharply, in company with which its working temperature also is displaced, therefore the change of the composition rate due to the above-mentioned oxidation becomes a big problem. Further, in the diameter-reducing step, it is impossible to require the high diameter-reducing rate per one treatment of a work because the TiNi-alloy is hard to work, as a result of which many number of processes are required for obtaining a wire smaller than 1mm diameter, thereby incurring some defects such as being poor in productivity, becoming expensive, or others. The powder metallurgy method has been known as another method for making the TiNi-alloy wherein Ti powder and Ni powder being mixed at suitable range are sintered by the heat treating diffusion. However, in the method, since the powder has the large surface area and the oxide layer formed at the surface of Ti powder being apt to oxidize is turned to oxide of Ti₄Ni₂O, there occurs the troubles such as the displacement of the transformation point and the diminution of strength and life owing to the voids formed in the TiNi-alloys. Furthermore, in order to solve a part of the above-mentioned controversial points, there is proposed in the Japanese Patent Application Disclosure No.116340 of 1984, a method for obtaining the TiNi phase (Nitinol) by making Ti and Ni adhere closely through pressure or metal plating and therewith making them diffuse through heating. In this method, however, the diffusing velocity is tardy, whereas a lot of time are required reversely for producing a large-diametral article. For instance, even in order to obtain a wire of about 0.5 to 1mm in diameter which is much in demand, it is necessary to take a long time exceeding 100 hours of the diffusive heat treatment. In the result, this method also is not so available in practical use. Such being the case, the exhaustive utilization of the TiNi-alloy has not been contemplated in the past for all its many functions and excellent properties. By the way, although the TiNi-alloys surpass other high-performance material such as CuZn-alloy, CuAlZn-alloy there has developed a need for higher property. Under these circumstances, the present invention has been completed by finding out that the controversial point immanent in the selected method should be soluble on the basis of conducting the diameter-reducing working and the diffusing process after the plurality of compound wire assembled by making the Ti wire rods to contact with the Ni material inserted into a sheathing container. SUMMARY OF THE INVENTION Accordingly, it is an object of this invention to provide such a method as referred-to above having the ability to produce the TiNi-alloys excellent in homogeneous property, by which method the productivity is to be elevated and the cost is also to be lowered. This object is achieved with the method as claimed in claim 1. BRIEF DESCRIPTION OF THE DRAWINGA Fig. 1 is a perspective view schematically showing a Ti-lineal wire being used in the method according to the invention: Fig. 2 is a perspective view illustrating by example a compound wire; Fig. 3 is a perspective view showing a pre-drawn and diameter-reduced one of the compound wire seen in Fig. 2; Fig. 4 is a perspective view illustrating by example a composite; Fig. 5 is a perspective view illustrating by example the composite being through the diameter-reducing working and having a compound material therein; Fig. 6 is a perspective view exemplifing a diffusion step; Fig. 7 is a perspective view showing a secondary composite wherein the compound materials shown in Fig. 5 are installed in a secondary sheathing container; Fig. 8 is a perspective view showing a diameter-reduced secondary composite by the drawn working; Fig. 9 is a perspective view eximplifing a diffusion step; Fig. 10 is a perspective view showing another example of the compound wire; Figs. 11 through 13 are perspective views showing still another examples of the compound wire; Fig. 14 is a perspective view showing by example a compound material; Fig. 15 is a transverse cross-section of the compound material shown in Fig. 14; Figs. 16 through 17 are perspective views showing another compound material; Fig. 18 is a transverse cross-section of the compound material shown in Fig. 16; Fig. 19 is a perspective view showing by example a diffused compound material; Fig. 20 is a microphotograph showing the metal tissue of the compound wire body which is formed of the Ti lineal wire being Ni metal-plated, Figs. 21 and 22 are microphotographs showing the respective metal tissues of each compound material; Figs. 23(a) and 23(b) are microphotographs illustrating by example the respective metal tissues after the diffusing working; Fig. 24 is a microphotograph showing the metal tissue of a compound material which is through the secondary diameter-reducing working: Fig. 25 is a microphotograph showing a metal tissue of the compound material shown in Fig. 24 which is diffused imperfectly; Fig. 26 is a microphotograph showing a metal tissue in cross-section of the compound material shown in Fig. 24 which is diffused; Fig. 27 is a microphotograph showing a longitudinal metal tissue of the compound material of Fig. 26; Fig. 28 is a graphical representation showing a relation between the strength and the strain of NiTi-alloy obtained in the method of the invention; Fig. 29 is a microphotograph showing a metal tissue of a product being obtained by the method of the invention; and Fig. 30 is microphotograph showing a metal tissue of the product being obtained by conventional manufacturing methods. DETAILED DESCRIPTION The manufacturing method of the TiNi-alloy in accordance with the invention is characterized in that there is formed a composite 9 in which a plurality of compound wire 6 are disposed in a sheathing container 7, the compound wire 6 consisting of Ti lineal wire 2 and Ni material 3 that is made to touch at least with a part of the surface of the Ti lineal wire 2, while the composite 9 being conducted on diameter-reducing process and the diffusing process in the container 11, providing a TiNi phase. The sheathing container 7 is removed from the composite 9 during the diffusion step or after the diffusion step and thereafter the compound material is cold-worked to form the TiNi-alloy. Although, in general, the Ti-lineal wire 2 is a small-diametral wire rod being made up of pure titanium, it may be possible to utilize as substitute for the pure Ti-lineal wire such Ti-alloys as containing or being covered with Cu,V,Mo,Al,Fe,Cr,Co and the other materials with the view of improving divers properties such as the transformation point at the final product, the mechanical properties, the workability, and others. Further, it is also good that the lineal wire 2 may be enhanced in its touchability with the Ni-material 3 by forming its own cross-section not only circular but also non-circular. On the other hand, there is used for the Ni-material in addition to the pure Ni, the Ni-alloys containing or being covered with various kinds of another material as mentioned above. Fig. 2 shows an example of the compound wire in which the Ni material 3 is made to contact with the whole surface of the Ti-lineal wire 2 by employing as the covering 4 covering the Ti lineal wire 2. Fig. 10 shows another compound wire 6 in which the Ni material being formed in a shape of the wire is made to contact with a part of the surface of the Ti lineal wire 2 by twisting together with the Ti lineal wire 2. The NiTi composition ratio of the compound wire 6 is put within the limit of Ni 45 to 60 at % and Ti 55 to 40 at % or less. If desired, one or more from the third elements discribed above may be inclusive. As for the compound wire 6 shown in Fig. 2, in which the Ni material is used as a covering 4, it is indeed possible to form the covering 4 surrounding the Ti lineal wire 2, for example, by the cladding process by which the Ni material 3 such as a pipe material or a tape material is laid on the surface of the Ti lineal wire 2, or by the melt-jetting process, the evaporating process, or the plating process, but in particular the coating 4 as being formed by means of the galvanoplasty is preferable from the viewpoint of the equipment, the productivity, and the covering precision. In such a case, it is possible to use for the Ti lineal wire 2 ordinarily the one having the diameter of about 0.05 to 5mm, however, in the case of forming the covering 4 by using the galvanoplasty, the one of about 0.2 to 2mm in diameter can be preferably used for the purpose of above all enhancing the workability and the productivity. The reason for saying, this is that if the linear diameter of the Ti-lineal wire 2 is too big, the amount of the plating of the Ni also naturally grows bigger, and it requires long hours for the plating work, while if being too small, it becomes inferior in the workability , because, in the manufacturing method of the TiNi-alloys according to this invention, it is necessary to regulate in advance the composition rate of the Ti material to the Ni material in the compound wire. Incidentally, the products having the above-mentioned value are available on the market easily in composition. At the time of the plating treatment, it is desired especially that the scales or the impurities on the surface of the Ti-lineal wire 2 are removed beforehand, and, if necessary, it is also good to elevate the degree of the close adhesion of the Ti-lineal wire 2 to the Ni-material 3 after the above- mentioned covering treatment, and further to conduct the preparatory wire-stretching treatment (shown in Fig. 3) to a slight degree in order to crush such as voids is seen in Fig. 20. In this case, the above-mentioned Ni material 3 functions also as a lubricant to elevates its natural workability, and further is able to repress the oxidation of the internal Ti lineal wire 2. Still more, it is possible by the method of this invention to form compound wire in the shape of tape by laminating the tape-shapedly made Ni material 3 on the likewise tape-shaped Ti lineal wire successively on one surface or on both surfaces thereof. In the case of the compound wire in which the Ni material is utilized is a Ni lineal wire as shown in Fig. 10, the Ti lineal wire 2 being twisted together with the Ni lineal element 5, the ones having the smaller diameter, for example, the ones of 0.1 to 1mm in diameter can be used conveniently on the same ground. When the linear diameter of the Ti lineal wire 2 is too big, the state of twisting together with Ni lineal element 5 is not good, as a result of which the number of the working steps is increased at the time of the diameter-reducing working, wherefore the productivity is impeded so much. Inversely, when being too small, there is likely to occur the breaking of the wire rod against the twisting work, and not only that, the wire of such a small diameter is inferior in the productivity by comparison, thereby entailing an increase in cost. On the other hand, as the Ni lineal element 5 being used in intertwisting, the one of the linear diameter being the same size as the above Ti lineal wire 2 can be used. When twisting together the Ti lineal wire 2 and the Ni lineal element 5, the respective thickness or diameter and number of pieces of them are set preparatorily so as to be able to obtain a preferable tissue rate of titanium to nickel. For example, in the case the TiNi alloy of 50 at % is to be obtained by Ni as a stoichiometric composition, when the diameter of the Ti lineal wire 2 is 0.187mm and the diameter of the Ni lineal element 5 is 0.2mm, then the ratio of their number of pieces each to other is set at 2:1, and when they are of the nearly same dimeter, their ratio of 3:2 or the like is set. Of course, the above-mentioned composition ratio is allowable to be set as one likes, depending upon the equilibrium of required shape-memorizing property and others, but in general it is put into practice almost within the limits of Ni 45 to 60 at % and Ti 55 to 40 at % or less where the TiNi phase is able to be produced. In the method according to this invention, it is able to obtain easily and accurately the alloy of a desired composition ratio by regulating the composition ratio and the combination of titanium to and with nickel in the compound wire 6. Incidentally, as the number of the inserted piece is increased and their lineal diameter is decreased, the homogeneity is enhanced so more. By the way, it is preferable that the number of times of the twisting work is confined to the extent of about 0.2 to 2 times per cm for reasons of prevention of the breaking of wires at the time of the succeeding diameter-reducing working and from the viewpoint of the convenience of the inserting working into the sheathing container 7. Furthermore, the number of Ti lineal wire and Ni lineal wire as well as the twisting are suitably selected. As above described, the compound wire in which the Ni material are made to contact with at least a part of the surface of the Ti lineal wire 2, by covering or twisting as shown in Figs. 2 and 10. Further, when inserting a plurality of of such compound wires 6 into, for example, the cylinder-shaped sheathing container 7, then there is formed one composite 9. As for the sheathing container 7, it is possible to apply, for example, some cylindrical body such as a pipe material or a hoop wound material which is made up of various kinds of metals, easy to be plastically deformed, for example, such as the Monel metal, copper, soft steel, nickel, or the like. It is also preferable to conduct the Ni plating beforehand on the inner face thereof, thereby preventing the diffusion from the sheathing container 7 to the compound wire 6 at time of the diffusing process, and vice versa. Further, such as the cross-sectional form and size of the sheathihg container 7 is selected by preferance, however, those things are decided in consideration of the productivity and the quality of the product in the course of the diameter-reducing working and the diffusing process on the basis of the initial lineal diameter, the number of pieces and the diameter of the final product of the compound wire 6 to be inserted into the sheathing container 7. Next, the composite 9 is then drawn by conducting the cold drawing, the swaging working, the rolling working, the extruding working, or others on the composite 9 so as to draw the final size and form, wherein the Ti lineal wire have the desired final fibrous diameter such as less than 0.1 mm, as shown in Fig.5. According to the diameter reduction of the composite 9 through the drawing steps, the compound wires 6 being also drawn down to preselected diameter and being mechanically bonded each other at the sufaces thereof, there is formed the compound material 10 as shown in Figs. 14, 16 and 17. The compound material 10 in the condition is banded together in such a degree as being able to maintain a unit after the removal of the sheathing container 7. Besides, fine unevenness is formed on the surface of Ti lineal wire 2 and Ni material 3, which may increase the mechanical bonding strength. Also, the compound material 10 formed of compound wires 6 has a homogeneous composition ratio through the full length and is able to drawn down to approximately final shape and dimension owing to its facility of deformation. Figs. 14, 15 and 21 shows the compound material 10 formed by plating and Figs. 16, 17 and 22 shows the same one formed by twisting, respectively, while being based on the working process as mentioned above. As shown in Fig. 21 and Fig. 22, it proves that the Ti lineal wire 2 and the Ni material 3 both becomes small diametral and adhere closely each to other in full, thus preventing the residue of the contact gap. Such a diameter-reducing working is conducted at the working rate of more than 50 %, and, if necessary, in the course of the above-mentioned diameter-reducing working is inserted the annealing process at low temperature or in a short space of time. Especially, by conducting the diameter-reducing working on the both (the Ti lineal wire 2 and the Ni material 3) so as to become fibriform, it becomes possible to shorten the heating time of the subsequent diffusing process by a large margine and to flatten the surface of the product, thereby heightening the value thereof, too. Following the diameter-reducing working, the diffusing process is conducted on the diameter-reduced composite 9 while heating within the limites of, for example, 700 to 1100°C, whereby the compound wire 6 having Ti Ni is made to change into the TiNi phase as the chemical compound. The diffusion is a mutual phenomenon which occurs on the basis of the fact that the Ti atoms shift to the Ni side, on the one hand, and on the other, the Ni atoms shift to the Ti side respectively. Therefore, in order to make this reaction complete in a short time, it is preferable to shorten the shifting distance as such as possible, whereby the thus diameter-reduced Ti lineal wire 2 and Ni material 3 can be made to diffuse in a short time, while the diffused compound material 13 shown in Fig. 19 having homogeneous TiNi phase is produced inside the sheathing 7 by the compound material 10. The diffused compound material 13 is easily removed from the sheathing container 7 and the diffused material 13 being diffused perfectly turned to the TiNi alloy 1. In this connection, when the diffusing reaction is insufficient on account of the heating time being too short, then not only the TiNi phase A but also the TiNi₃ phase C, Ti₂Ni phase B, Ni phase B, and Ti phase D sometimes remain behind as they are, as showing in Fig. 23(a), in the case where the compound wire was formed, for example, by plating. In such a case, the present invention is also to select the conditions for treating them depending on the object. On the other hand, Fig. 23(b) shows the state where the diffusing treatment at 900°C for 1 hour has been conducted after the diameter-reducing working on the composite 9 which is made up by bundling a plurality Ni-plated TiNi wire bodies 6, but here is proven that the diffusion is not yet done completely. The diffused compound material 13 has an undiffused Ti base material 8 inwhich the Ti material 2 is surrounded by the diffused layer D( A, B and C) and is separated each other by the Ni material 3. And the Ti base materials 8 are disposed uniformly and are one body with the Ni material 3. The diffused layer D is increased in thickness according to the degree of the diffusion treatment. Also, the thickness of the layer D is small less than some µmm, in the early diffusing stage. It is good that the heating treatment is done at the same temperature, but also it does not matter that the treatment is conducted while varying the temperature in stages. According to the experiment of the invention, it was found that there are formed at the heating temperature of 900°C, the TiNi phase of 40 µm in thickness through the 2 hours treatment, but the TiNi phase of 70 µm in thickness through the 10 hours treatment, from the above, if the Ti lineal wire 2 is made minutely, for example, up to 70 µm, it is possible theoretically that 5 hours of the heating time will suffice to make the Ti lineal wire 2 diffuse. In this case, it goes without saying that there happens some difference among the diffusing hours required depending on the temperatures. Practically, though in this state, the surface of the diffused compound material 13 is covered with the sheathing container 7 and is insufficient in its function. Therefore, it in desired that the sheathing container 7 is removed therefrom by using the chemical method or the mechanical method for example, such as, cutting method, in the course of the diffusing process or after the same process. After removing the sheating container a cold working step is effected. This cold working step results in an improvement of the surface properties as well as in a promotion of the homogeneity of the tissue. Finally, for example, when intending to use the shape-memorization, it becomes possible to obtain the product desired first by forming it into the prescribed form (for example, the spring-shape) and then by heat-treating it at about 400 to 500 °C. Or again, in the case of the super-elastic alloy, the working is enabled by changing, for example, the Ni composition ratio and by lowering the transformation point near to a degree of the sub-zero temperature, which will be made possible on the basis of the utilization of this invention. Into the bargain, the TiNi-alloys which are ought to be obtained if having recourse to the method of this invention are not limited only to the circular form in section, but also have the ability to correspond to the non-circular forms for example, such as the elliptic shape, the square shape, the plate and the other deformed shape, and further they have the applicability to all descriptions of the sizes which are freely set covering a wide range from the minute up to the large. Description will be now directed to the method making the TiNi alloy having one or more third element selected from the group consisting essentially of Cu, V, Mo, Cr, Al, Fe, Co and so on. Fig. 11 shows an example wherein the Ti lineal wire 2 intertwisted by the third element lineal wire 12 is wrapped by the covering 4 formed of Ni material 3. Figs. 12 and 13 are a schematic drawings to explain embodiments where, as is seen in the figures, the compound wire 6 substantially, surrounding the Ti lineal wire 2 is obtained by intertwisting the Ni lineal element 5 made of the Ni materials 3 and the third element lineal wires 12 around the Ti lineal wire 2 being arranged in the center. Applied to the Ti lineal wire 2 and the Ni lineal elements 5 being using in this case are respectively lineal wires being made of pure metals thereof, while there are used the third element lineal wires 12 which have been regulated so as to be substituted with less than 5 at % of the final TiNi alloy product are selected from the group of the third elements. As for the diameter of the above-mentioned third element lineal wire 12, it is desirable to use many pieces of minute one of, for example, about 0.05 to 0.8 mm in diameter. In using, they are to be arranged so as to be scattered in the TiNi wire body 6 as well as the compound material 10 as uniformly as possible. Although the above-mentioned third elements are selected in consideration of the regulation of the transformation point and the improvement of its mechanical properties, and in accordance with the other desired objects, yet their composition ratios exceeding 5 at % is not preferable because of lowering the workability. As shown in Figs. 7 through 9, the compound material 10 obtained by the process illustrated in Figs. 1 through 6 is available to use as the wire 6A corresponding to the compound wire 6 shown in Figs. 1, 10, 11 and 12. The compound material 10 is released from the sheathing container 7 of the composite 9 by the suitable means such as selective chemical attack of the sheathing container 7. The sheathing 7 may be removed by another means, for example, mechanical, removal, electrochemical dissolution. The compound material 10 thus obtained has a diameter of e.g. about 0.64 mm and is as one body owing to the mechanical bonding between the compound wires 6. Further, when the sheathing container 7 is removed by the acid such as a hot nitric acid fluid, the Ni material 3 is apt to be solved away from the surface of the compound material 10, thereby the surplus layer 15 wherein the Ti element being more rich than internal tissue is formed. The compound material 10 being released from the sheathing container 7 by the mechanical means may be provided with the surplus layer 15 of Ni, by plating the Ni material therearound as the lubricant. Besides, the TiNi alloy per se is also available as a material 6A, and the Ni coating is generally adopted as for the lubricant. One hundred twenty (120) of the compound material 10 are disposed in the secondary sheathing container 7A, thereby the secondary composite 9A is formed. The composite 9A is drawn down to the final small dimention as shown in Fig. 8. As a result, the material 6A is allowed to grow small diameter and the void therein is eliminated. Such a diameter-reducing process is conducted at the working rate of about 50 %. In Fig. 24 is shown the microphotograph of the cross section of the secondary compound material manufactured as described above and corroded by a suitable corrosive agent. It is seen that the Ti material and the Ni material are dispersed uniformly, since the boundary between them is quite obscure. The diffusing process is conducted on the secondary composite 9A. Fig. 25 is a microphotograph in two centuples showing the transverse section of the secondary compound material which is not well diffused. It is seen that the intermittent reinforcing layer 17 is extending in netlike configuration through the base 16 comprising the Ti material and the Ni material which are partially diffused. Fig. 26 is a microphotograph in two centuples showing the tissue in cross section of the secondary compound material which is enough diffused. And Fig. 27 is that of the tissue thereof in longitudinal section. As illustrated in Fig. 26, the reinforcing layer 17 decreases the thickness thereof and almost continuously extends in hexagonal-netlike through the base 16 where the Ti material and the Ni material are diffused. The reinforcing layer 17 also extends longitudinally. The reinforcing layer 17 is supposed to be formed from the Ti₂Ni in case of the surplus layer 15 being rich in Ti and TiNi₃ in case of the surplus layer 15 being rich in Ni as mentioned before. Also, the concentration is presumed to change gradually in the layer 17. Although TiNi₃ and Ni₂Ti are metal compounds made from Ni and Ti similar to the base 16, the TiNi₃ and Ti₂Ni are harder and more difficult to work than the base 16. For example, the hardness of the TiNi₃ comprising 73 through 78 Ni at % is of Hv400 through 500. Consequently, it is quite important to control the volume ratio of the reinforcing layer 17 in order to avoid deterioration thereof, and the ratio should be selected in accordance with the desired objects and properties. Additionally, another material, for example, the ceramic powder or metalic oxide such as TiO₂, Al₂O₃, Cr₂O₃ which may not affect chemically the TiNi phase is also available to form the reinforcing layer 17. The powder may be applied on the body comprising the compound wire 6, compound material 10 or the wire of TiNi alloys by spraying, painting with a brush or other means. The reinforcing layer 17 similar to that made from Ti and Ni is formed by reducing the diameter of the composite in which a plurarity of the body is disposed in the sheathing container. Besides, the reinforcing layer 17 extends in netlike may be formed in case that the powder is applied throughout the circumference of the body, and also the layer 17 extends in longitudinal direction intermittently or continuously. When the powder is applied only longitudinally passing through a portion of circumference of the body, the layer 17 running in longitudinal direction may be obtained. Owing to the secondary diameter-reducing process, the Ti lineal wire 2 is reduced in diameter down to less than 5 µm, thereby enabling to shorten the hours for diffusing step. The elongated body turnes to the TiNi alloy through the diffusing step and removing step. The heating treatment for diffusion may be done it the same temperature, but also it does not matter that the temperature may vary in stages. As described above, the method of this invention enables to make the setting and changing of each of the composition ratio very easily and certainly by using the composite inserting into the sheathing container a plurality of compound wire, where the Ti lineal wire and the Ni material of the required quantity are made to contact with each other by making the both contact through covering or intertwisting. And not only that, it can repress the scattering of the composition in the interior of the alloy and the variations of the properties of the product. Furthermore, since each of the above-mentioned lineal wires may be made into the minute line up to the fibrous shape by the diameter- reducing working, it becomes possible not only to shorten the dispersing time very much, but also to set freely the form and size of the alloy to be obtained in the wide range. On the other hand, the Ti material has the defect liable to let the oxide film usually generate on the surface while working, however, it is possible for this invention to restrain the oxidation and to make the heat treatment in the atmosphere, because of the working being practicable under the cover of the sheathing container. Further, in manufacturing the Ti wire, there is no necessity to provide any large-scale equipment, because of being able to prevent the mixture of any impure gas and to manufacture irrespective of the turnout, the manufacture by the use of the method of this invention comes to have many effect such as the good yield rate, the lowering of the production cost, the enhancement of the homogeneity of the product, and so on. Incidentally, the TiNi alloy obtained on the basis of the method of this invention his also the pure and clean tissue free of such as oxide as understood from Fig. 29, wherefore it was possible to obtain the one of the very small hysteresis. The TiNi alloys conducted through the secondary diameter-reducing process shown in Figs. 7 through 9 has better properties, such as the mechanical strength, life time and so on. As the features for the super-elastic alloy, δM, δR and hysteresis as well as the rate of the energy loss are improved. Further, the shape-memorizing property and the recovery stress in addition to the speed of responce are also improved. Additionally, thermal fatigue life property becomes stable. Consequently, small sized ones may be available, thereby the seat of the material being shortened. This invention will be now explained more circumstantially basing on some examples, (Example 1) On the surface of the pure Ti lineal wire 2 of 0.47mm in diameter was conducted the Ni plating of about 65µm in thickness, and then 70 pieces of the compound wire 6 constituting the Ni composition ratio of 50 at % were inserted into the sheathing container 7 being made of the soft steel pipe of 8 mm in outer diameter, 6 mm in inner diameter, and 1000 mm in length. In this way, there was obtained the composite 9. On this compound body 2 was conducted the reducing working in the working ratio of 10 to 20 % per die, amounting to 99,7 % in total by means of a cold wire-stretching machine. At this time, the above-mentioned Ti core material holds 2.5 µm, and the thickness of the surface Ni plating preserves 17 to 19 µm, both in the nearly same composition ratio at the state of their own raw materials, while each covering stuff 4 adheres closely without gap and with certainty. On the thus worked composite 9 was conducted the heating treatment at 900°C for 10 hours in the atmosphere, and the internal Ni and Ti materials were made to diffuse, whereby the alloy having the TiNi phase was obtained. Incidentally, the above-mentioned sheathing container 7 was removed by scans of chemical method after the above heating treatment. This straight TiNi alloy is of the thickness having the diameter of 0.3 mm. After bending this by hand up to an angle of about 90°, when applying heat to it, than it recovered to the original straight-line form. (Example 2) Immediately after conducting the cold working in the working ratio of 25 % on the TiNi alloy obtained in Example 1 to mold it into a sticky spring of the outer diameter of 4 mm, that TiNi alloy was made to memory the shape of a spring through the heat treatment at 450°C for 10 minutes. After stretching this spring while giving the load of 8 %, when putting it into the hot water of 60°C, then it recovered to its original form in a moment. The result obtained by comparing this specimen where the temperature of the transformation point was measured by the DSC thermometer with the shape-memorizing alloy of Ni50 at % abtained by the dissolution method as a conventional method is listed in Table 4 as follows; This invention comparative case Ni composition ratio 50 at % 50 at % As point 56 °C 78 °C Ms point 50 °C 60 °C hysteresis As-Ms 6 °C 18 °C

Claims: A method of making TiNi-alloys comprising the steps of: forming a composite by providing in a sheathing container plural sections of a compound wire comprising Ti lineal wire made of Ti material and Ni material made to contact at least a portion of the surface of said Ti lineal wire, wherein said compound wire has a Ni content of 45 to 60% by weight; reducing the dimension of said composite so as to reduce said compound wire therein; effecting a diffusion process on said composite to cause a TiNi phase to be produced by a diffusion reaction; removing said sheathing container from said composite during said diffusion step or after said diffusion step; and thereafter cold-working said compound material to form a TiNi alloy. The method of claim 1, wherein said compound wire comprises one or more elements selected from the group consisting of Cu, V, Mo, Cr, Al, Co and Fe. The method of claim 1, wherein said Ni material is in a form of an elongated Ni lineal element. The method of claim 3, wherein said Ni lineal element contacts the surface of said Ti lineal wire by twisting with each other. The method of claim 4, wherein the number of twists is 0.2 to 2 per cm. The method of claim 1, wherein said diffusion is effected by heating at a temperature of 700 o to 1100⁰ C. The method of claim 6, wherein said temperature is varied in stages. The method of claim 1, wherein said Ti lineal wire has a diameter of about 0.05 to 5 mm. The method of claim 1, wherein said Ni material contacts the surface of said Ti lineal wire by being plated thereon. The method of claim 1, wherein said Ni material contacts the surface of said Ti lineal wire by means of cladding of pipe material or hoop material made of Ni.

Inventors: ISHIBE, HIDEOMI C/O NIPPON SEISEN CO.,LTD.
Applicants: NIPPON SEISEN CO., LTD.
Application year: 1986
Main classification: C22C1
IPC codes: C22C1