JP2009094080A - Method for manufacturing contact and method for manufacturing connection device using the contact - Google Patents

Abstract

<P>PROBLEM TO BE SOLVED: To provide a contact formed in an amorphous state having better spring properties as compared to conventional one, a method for manufacturing the contact, a connection device using the contact, and a method for manufacturing the connection device. <P>SOLUTION: The present invention provides a contact comprising an elastic deforming portion that includes at least one amorphous part. The elastic deforming portion includes an auxiliary elastic member 41 made of, for example, NiP (a P content of 15 atomic percentage). In this case, an amorphous phase 50 is predominant in the auxiliary elastic member 41. This enhances spring properties such as a yield stress more than conventionally. <P>COPYRIGHT: (C)2009,JPO&INPIT

Description

  The present invention relates to a connection device (for example, an IC socket) having a contact to which, for example, an IC (integrated circuit) or the like is mounted. In particular, the contact is formed in an amorphous state to improve spring characteristics. And a method of manufacturing a connecting device using the contact.

  The semiconductor inspection apparatus described in Patent Document 1 electrically temporarily connects a semiconductor to an external circuit board or the like. A large number of spherical contacts arranged in a lattice shape or a matrix shape are provided on the back side of the semiconductor, and a large number of recesses are provided on an insulating substrate facing the contact, and spiral contacts are provided in the recesses. Opposed.

When the back side of the semiconductor is pressed toward the insulating substrate, the spiral contact comes into contact with the outer surface of the spherical contact so that the spiral contact is spirally wound. The electrical connection between the two is ensured.
JP 2002-175859 A

  For example, in the said patent document 1, the said spiral contactor is formed including copper foil and nickel plating. Although not specifically described in Patent Document 1, the spiral contact is performed while heat-treating the spiral contact in order to ensure contact between the semiconductor spherical contact and the spiral contact. Is three-dimensionally molded.

  However, due to the heat treatment during the three-dimensional molding, the spiral contact is crystallized, yield stress is reduced, and the spring characteristics are deteriorated, so that there is a problem that the elastic contact does not function properly.

  In patent document 1, nickel plating is provided in a part of spiral contactor. It is expected that not only copper foil but also nickel plating will form a spiral contact so that the spiral contact will be easily elastically deformed appropriately, but the nickel will rapidly crystallize due to heat treatment and other causes. Since it becomes brittle when promoted, damage such as breaking of the spiral contact tends to occur frequently.

  Even when the spiral contact is not particularly subjected to heat treatment for three-dimensional molding, when the spiral contact is used in a burn-in test apparatus or the like, the spiral contact is necessarily placed under heating. Therefore, it is necessary to improve the spring characteristics of the spiral contactor under the heating environment.

  Therefore, the present invention is for solving the above-described conventional problems, and in particular, a method for manufacturing a contact in which the contact is formed in an amorphous state, and the spring characteristics can be improved as compared with the prior art, and the contact An object of the present invention is to provide a method of manufacturing a connection device using the above.

The present invention relates to a method of manufacturing a contact having an elastically deformable portion,
Forming the elastic deformation portion with Ni-P or Ni-B Ni alloy;
Heating the elastically deformed portion in a three-dimensionally formed state;
The heating temperature is within a range of 200 ° C. to 300 ° C., and the amorphous state of the Ni alloy is maintained.
In the present invention, the composition ratio of P is preferably 15 atomic% or more and 30 atomic% or less.

Further, the present invention provides a method for manufacturing a contact having an elastically deformable portion,
Forming the elastically deformable portion with a Ni-W Ni alloy;
Heating the elastically deformed portion in a three-dimensionally formed state;
The heating temperature is in the range of 200 ° C. to 700 ° C., and the amorphous state of the Ni alloy is maintained.

  In the present invention, the W composition ratio is preferably 14.5 atomic% or more and 36 atomic% or less. More preferably, the W composition ratio is 20 atomic% or more.

  The Ni alloy (Ni-X (X = P, B, W)) has a higher crystallization temperature than Ni, and the Ni alloy can maintain an amorphous state even when heated under the same conditions as in the prior art. In the present invention, the Ni alloy constituting the elastically deformable portion can be made into an amorphous state, and the contact having excellent spring characteristics can be formed easily and appropriately.

  In the present invention, the heating step is preferably performed at a temperature lower than the crystallization temperature of the Ni alloy. Thereby, the Ni alloy can be appropriately brought into an amorphous state.

  Moreover, in this invention, it is preferable to apply the stress in the plastic region of the said Ni alloy to the said elastic deformation part, and to heat the said elastic deformation part in the state shape | molded three-dimensionally. Thereby, especially shortening of heating time can be aimed at.

The heating time is preferably between 36 minutes and 1 hour.
In the present invention, the elastically deformable portion can be formed only of the Ni alloy.

  In the present invention, an elastic region made of the Ni alloy can be formed in a part of the cross section of the elastically deforming portion cut from the film thickness direction. For example, the elastic deformation part is formed to include a conductive member and an auxiliary elastic member. At this time, the conductive member is formed of a material having a specific resistance lower than that of the auxiliary elastic member, and the auxiliary elastic member is formed. The member can be formed of the Ni alloy having a higher yield point and elastic modulus than the conductive member.

Furthermore, the present invention includes a base and a contact provided on the base, wherein the external connection portion of the electronic component contacts the elastically deforming portion of the contact.
The elastic deformation portion of the contact is formed by any one of the manufacturing methods described above. As a result, the elastically deformable portion can be formed in an amorphous state, and it becomes possible to appropriately and easily manufacture a connection device having the contact that has better spring characteristics than the conventional one.

  According to the present invention, according to the method for manufacturing a contact having an elastically deformable portion, Ni-X constituting the elastically deformable portion can be in an amorphous state, and the contactor having excellent spring characteristics can be formed easily and appropriately. I can do it.

  1 is a perspective view showing an inspection apparatus used in a test for confirming the operation of an electronic component, and FIG. 2 is a sectional view taken along line 2-2 of FIG. is there.

  As shown in FIG. 1, the inspection apparatus 10 includes a base 11 and a lid 12 that is rotatably supported via a hinge 13 provided on one edge of the base 11. ing. The base 11 and the lid body 12 are formed of an insulating resin material or the like, and a loading region 11A that is concave in the Z2 direction is formed at the center of the base 11. An electronic component 1 such as a semiconductor can be mounted in the loading area 11A. A locked portion 14 is formed on the other edge of the base 11.

  As shown in FIG. 2, in this inspection apparatus 10, a large number of connection terminals (for example, spherical connection terminals shown in FIG. 2) 1 a are arranged on the lower surface of the electronic component 1 in a matrix (lattice or grid). This is intended for inspection.

  As shown in FIG. 2, the base 11 has a predetermined diameter, and a plurality of through holes (through holes) 11 a penetrating from the front surface of the loading area 11 </ b> A to the back surface of the base 11 are formed on the electronic component 1. It is provided corresponding to the connection terminal 1a.

  On the upper surface of the through hole 11a (the surface of the loading region 11A), a plurality of spiral contacts 20 in which the contacts are formed in a spiral shape are provided.

  FIG. 3 is a perspective view of the spiral contact 20. As shown in FIG. 3, a plurality of the spiral contacts 20 are formed on the base 11 with predetermined intervals in the X direction and the Y direction shown in the figure.

  Each spiral contact 20 has a base portion 21 fixed to the edge of the upper open end of the through hole 11a like the spiral contact 20 shown in the upper left in FIG. The winding start end 22 is provided on the base 21 side. And it extends in a spiral shape from the winding start end 22, and the winding end 23 is positioned substantially at the center of the through hole 11a. In the spiral contact 20, a spiral portion at a position facing the through hole 11 a in the height direction functions as an elastic deformation portion 20 a.

  A conductive portion (not shown) is formed on the inner wall surface of the through hole 11a, and the upper end of the conductive portion and the base portion 21 of the spiral contactor 20 are connected by a conductive adhesive or the like. The opening end below the through hole 11a is closed by a connection terminal 18 connected to the conducting portion.

  As shown in FIG. 2, a printed board 30 having a plurality of wiring patterns and other circuit components is provided below the base 11, and the base 11 is fixed on the printed board 30. . The surface of the printed circuit board 30 is provided with a counter electrode 31 facing the connection terminal 18 provided on the bottom surface of the base 11, and the connection terminals 18 are in contact with the counter electrodes 31, respectively. The electronic component 1 and the printed circuit board 30 are electrically connected via the inspection apparatus 10.

  On the other hand, at the center position of the inner surface of the lid 12 of the inspection apparatus 10, a convex pressing portion 12a that presses the electronic component 1 downward in the figure is provided so as to face the loading area 11A. Further, a lock portion 15 is formed at a position on the opposite side to the hinge portion 13.

  Between the inner surface of the lid body 12 and the pressing portion 12a, a biasing member made of a coil spring or the like that biases the pressing portion 12a away from the inner surface of the lid body 12 is provided (not shown). . Therefore, when the electronic component 1 is mounted in the through hole 11a and the lid 12 is closed and locked, the electronic component 1 can be elastically pressed in the direction approaching the surface of the loading region 11A (Z2 direction). It has become.

  The size of the loading area 11A of the base 11 is substantially the same as the outer shape of the electronic component 1, and when the electronic component 1 is mounted on the loading area 11A and the lid 12 is locked, the electronic component 1 side Each of the connection terminals 1a and each of the spiral contacts 20 on the inspection apparatus 10 side can be accurately positioned correspondingly.

  When the lock portion 15 of the lid 12 is locked to the locked portion 14 of the base 11, the electronic component 1 is pressed downward in the figure by the pressing portion 12a, so that each connection terminal 1a holds each spiral contact 20. Push down in the through hole 11a (downward in the figure). At the same time, the elastic deformation portion 20a of the spiral contactor 20 is deformed so as to be expanded from the winding end 23 toward the winding start end 22 (outward from the center of the spiral) and embraces the outer surface of the connection terminal 1a. Thus, the connection terminals 1a and the spiral contacts 20 are connected.

  When the elastically deforming portion 20a of the spiral contactor 20 is cut in the film thickness direction from the line 4 which is parallel to the width direction, and the cut surface is viewed from the direction of the arrow, the cut surface is as shown in FIG. ing.

  In FIG. 4A, the auxiliary elastic member 41 is formed on the conductive member 40 in an overlapping manner. The conductive member 40 is made of a material having a specific resistance lower than that of the auxiliary elastic member 41, and the auxiliary elastic member 41 is made of a material having a yield point and an elastic coefficient higher than those of the conductive member 40.

  As shown in FIG. 4A, by forming the conductive member 40 and the auxiliary elastic member 41 so as to overlap each other, good conductivity of the spiral contactor 20 is secured by the conductive member 40, and the spiral contactor is good. The spring property is secured by the auxiliary elastic member 41.

  In FIG. 4A, the conductive member 40 may be formed on the auxiliary elastic member 41 in an overlapping manner.

  4A, both the conductive member 40 and the auxiliary elastic member 41 may be formed by plating, or the conductive member 40 may be formed of a metal foil, and the auxiliary elastic member 41 may be It may be plated.

  In FIG. 4B, the conductive member 40, the auxiliary elastic member 41, and the coating member 42 are laminated in this order from the bottom. Here, the coating member 42 is provided to improve hardness and wear resistance. The coating member 42 is preferably formed of a material having a specific resistance lower than that of the elastic member 41 and has a function of reducing contact resistance with a contact of an electronic component.

  4C, the upper surface, the lower surface, and both side surfaces of the conductive member 40 are completely surrounded by the auxiliary elastic member 41. Thus, it is preferable that the conductive member 40 be completely surrounded by the auxiliary elastic member 41 because the spring property of the spiral contact 20 can be improved more appropriately.

  FIG. 4D is an application example of FIG. 4C. For example, the auxiliary elastic member 41 completely surrounds the upper surface, the lower surface, and both side surfaces of the conductive member 40, and the surface of the auxiliary elastic member 41 is covered with the coating member 42. It is the composition which covers.

  The conductive member 40 is made of Cu or Cu alloy. For example, a Corson alloy containing Cu, Si, and Ni is selected as the Cu alloy forming the conductive member 40. The auxiliary elastic member 41 is preferably formed of Ni-X (where X is one or more of P, W, and B). When the conductive member 40 is formed of Cu or Cu alloy (excluding Corson alloy), the spiral contact 20 can be formed at low cost and good conductivity can be ensured. However, since the spring property can hardly be expected, it is necessary to select Ni-X having excellent spring property for the auxiliary elastic member 41 and appropriately improve the spring characteristic of the elastic deformation portion 20a. That is, for example, when Ni is selected as the auxiliary elastic member 41, an effective improvement in spring characteristics cannot be expected, and the sag rate or the like becomes large. Specifically, for example, the combination of Cu / Ni cannot be expected to have good spring characteristics compared to Cu / Ni-X. Therefore, in this embodiment, the auxiliary elastic member 41 is preferably formed of Ni-X (where X is one or more of P, W, and B). The coating member 42 is selected from Au, Ag, Pd, and Sn.

  The auxiliary elastic member 41 is formed by plating as described above. The plating may be either electrolytic plating or electroless plating. For example, when the auxiliary elastic member 41 is formed so as to cover the periphery of the conductive member 40 as shown in FIGS. 4C and 4D, the auxiliary elastic member 41 is formed by an electroless plating method.

  The characteristic part in the present embodiment is that the auxiliary elastic member 41 is formed in an amorphous state. The auxiliary elastic member 41 is made of a Ni-X alloy as described above. The Ni-X alloy has a higher crystallization temperature than Ni, and the Ni-X alloy does not crystallize and maintains an amorphous state even at the temperature at which the Ni crystallizes. The auxiliary elastic member 41 is, for example, formed by plating with a NiP alloy, and the composition ratio of P is preferably 15 atomic% or more. When the composition ratio of P is 15 atomic% or more, the precipitation of Ni crystals can be appropriately suppressed as compared with the case where the composition ratio of P is smaller than 15 atomic%. The auxiliary elastic member 41 becomes brittle due to the precipitation of Ni crystals, which causes a significant decrease in spring characteristics represented by the yield point and the like. The composition ratio of P is preferably 30 atomic% or less. This is because if it exceeds 30 atomic%, brittle intermetallic compounds such as NiP, Ni5P2, and Ni2P5 are generated. When W is selected as the element X, the composition ratio of W is preferably in the range of 14.5 atomic% to 36 atomic%. More preferably, the composition ratio of W is 20 atomic% or more. Thereby, NiW can be formed in an amorphous state. When B is selected as the element X, the composition ratio of B is preferably in the range of 15 atomic% to 30 atomic%. Thereby, NiB can be formed in an amorphous state.

  The auxiliary elastic member 41 is most preferably completely amorphous (amorphous phase) as a whole. For example, ultrafine precipitates (emprio) having a diameter of 1 nm or less may be precipitated. The composition of the ultrafine precipitate may be Ni, for example, or may be the element X or Ni-X. Note that the ultrafine precipitate is only a few particles in size and is not a crystal. For this reason, even if the ultrafine precipitates are deposited, the properties as amorphous are appropriately maintained. Further, in the present embodiment, the state where crystals are partially precipitated is not excluded. For example, in the material state shown in FIG. 5, the amorphous 50 is dominant, but the emprio 51 and the crystal 52 are partially seen. The diameter (maximum diameter) of the crystal 52 is about 3 nm to 15 nm. At this time, the crystal 52 is preferably an intermetallic compound crystal formed of Ni—X instead of Ni. For example, when the auxiliary elastic member 41 is formed of a NiP alloy, the composition of the crystal 52 is Ni3P. Ni crystals change the film into a very brittle material, but even if the intermetallic compound crystals are precipitated, the deterioration of the spring characteristics can be suppressed as compared with the precipitation of Ni crystals. As shown in FIG. 5, even if the intermetallic compound crystal 52 is deposited, the periphery thereof is covered with the amorphous 50, and the amorphous 50 is in a dominant state. The amorphous 50 preferably occupies 60% by volume to 100% by volume in the auxiliary elastic member 41. That is, in this embodiment, the elastic auxiliary member 41 is entirely formed in an amorphous state, a state in which amorphous and ultrafine precipitates are mixed, a crystal other than amorphous (preferably an intermetallic compound crystal), Although it has ultrafine precipitates, it includes all the states in which the amorphous occupies 60% by volume or more in the film. The amorphous content is more preferably 80% by volume or more, and still more preferably 90% by volume or more. In the present specification, all of these states are collectively referred to as an “amorphous state”. Of the above three states, the most preferable is a state in which the whole is amorphous, and the next preferable is a state in which the amorphous and ultrafine precipitates are mixed.

  By including the auxiliary elastic member 41 in the elastic deformation portion 20a of the spiral contactor 20 and forming the auxiliary elastic member 41 in an amorphous state, the yield point of the elastic deformation portion 20a can be improved as compared with the conventional case. Specifically, it can have a yield point where the load is 19.6 mN or more and the displacement is 0.1 mm or more. Further, by forming the auxiliary elastic member 41 in an amorphous state, crack resistance (hardness to break) can be improved, and the spiral contact 20 can be appropriately formed into a three-dimensional shape with a predetermined height, Even when the connecting device 10 is repeatedly used, the sag rate of the spiral contact 20 can be appropriately reduced as compared with the conventional case.

  As shown in FIG. 3, the elastic deformation portion 20a of the spiral contact 20 is three-dimensionally formed in a spiral shape upward. The three-dimensional molding is performed under heating. Conventionally, in the case where Ni is used as the auxiliary elastic member 41 of the elastically deforming portion 20, there is a problem that the spring characteristics are deteriorated due to crystallization of Ni under heating during three-dimensional molding. By using a Ni-X alloy as the elastic member 41, the auxiliary elastic member 41 can be maintained in an amorphous state, and the spring characteristics represented by the above-described yield point can be improved as compared with the conventional case.

  Further, the cross-sectional area ratio {(the cross-sectional area of the auxiliary elastic member 41 / the overall cross-sectional area of the auxiliary elastic member 41) × 100 (%)} of the auxiliary elastic member 41 in the cross section shown in FIG. 4 is preferably 30% or more. 50% or more is more preferable. Thereby, a spring constant can be improved and a sag rate can be reduced appropriately.

  In the present embodiment, the elastic deformation portion 20a is three-dimensionally shaped (substantially conical) upward. Solid molding is performed under heating. Thereby, the elastic deformation part 20a can maintain a predetermined three-dimensional state even by repeated use and the like, and can make good contact with the connection terminal 1a. In the present embodiment, the elastic deformation portion 20a is appropriately maintained in an amorphous state also by heat treatment when the elastic deformation portion 20a is formed, heat treatment performed in a burn-in test, or the like.

  The conductive member 40 may not be in an amorphous state like the auxiliary elastic member 41, that is, a crystal may be dominant. Rather, the conductive member 40 is preferably a crystal in order to ensure good conductivity.

  A method for manufacturing the spiral contact 20 will be described. 6 to 8 show a method of manufacturing the spiral contact 20 until the spiral contact 20 is mounted on the base 11 and the elastic deformation portion 20a of the spiral contact 20 is three-dimensionally formed upward. FIG.

  As shown in FIG. 6, a through hole 11a is formed in the base 11, and a conductive portion 60 made of a conductive material is formed around the through hole 11a by sputtering or the like. As described above, the spiral contact 20 includes the base portion 21 and the elastically deformable portion 20a formed to extend from the base portion 21. The spiral contactor 20 has a configuration in which an auxiliary elastic member 41 made of a NiP alloy is formed by electroless plating around a conductive member 40 made of, for example, copper foil (FIG. 4C). The elastic deformation portion 20a is formed in a spiral shape. The base portion 21 of the spiral contact 20 is held by a resin sheet 71 such as a polyimide resin for holding the spiral contacts 20 so as not to be separated. Similarly to the base 11, the resin sheet 71 has a through hole at a position facing the elastic deformation portion 20 a in the height direction.

  The spiral contact 20 held by the resin sheet 71 is placed on the base 11, and at this time, the elastic deformation portion 20 a of the spiral contact 20 is exactly in the height direction with the through hole 11 a of the base 11. The elastic deformable portion 20a and the through hole 11a are aligned so that the conductive adhesive 61 is placed around the base hole 21 of the base 11 on the through hole 11a. Paste using At this time, the base portion 21 is electrically connected to the conductive portion 60 via the conductive adhesive 61.

  As shown in FIG. 6, the protrusion adjusting member 70 is inserted into the through hole 11 a from below the spiral contact 20, and the protrusion adjusting member 70 is pushed upward.

  As shown in FIG. 7, the elastic deformation portion 20 a of the spiral contact 20 is pushed upward by pushing up the protrusion adjusting member 70. At this time, the protrusion adjusting member 70 is pushed up while performing heat treatment, and after the predetermined time has elapsed, the protrusion adjusting member 70 is removed (FIG. 8).

  As described above, the three-dimensional molding of the elastic deformation portion 20a is performed while performing heat treatment, so that the elastic deformation portion 20a is maintained in a state of protruding upward even when the protrusion adjusting member 70 is removed.

  As shown in FIG. 7, the protrusion adjusting member 70 is moved upward until the height dimension from the upper surface 21a of the base portion 21 of the spiral contactor 20 to the apex A at the highest position of the elastic deformation portion 20a becomes H1. Push up and keep the state of FIG. 7 under heating. As shown in FIG. 8, when the protrusion adjusting member 70 is removed, the height of the elastically deforming portion 20a when viewed from the upper surface 21a of the base portion 21 of the spiral contactor 20 as a reference due to a slight springback is from H1. Slightly lower to H2. For this reason, the height dimension H1 of the elastic deformation part 20a at the stage where the protrusion adjusting member 70 is pushed upward in anticipation of the spring back is larger than the actually required height dimension H2 of the elastic deformation part 20a. It is necessary to set it high.

  As described above, the three-dimensional molding process of the elastic deformation portion 20a is performed under heating. In the present embodiment, the auxiliary elastic member 41 is formed of a Ni-X alloy as the auxiliary elastic member 41 of the elastic deformation portion 20a. The crystallization temperature is higher than that of Ni, and the auxiliary elastic member 41 is crystallized under the heating temperature of about 200 ° C. to 300 ° C., which is the heating temperature in the conventional three-dimensional molding. Without maintaining the amorphous state properly.

  In the present embodiment, the auxiliary elastic member 41 can be appropriately maintained in an amorphous state even by the above-described three-dimensional molding under heating. Therefore, the stress in the plastic region of the auxiliary elastic member 41 is three-dimensionally formed. The elastic deformation portion 20a can be three-dimensionally deformed by applying to the elastic deformation portion 20a. By deforming in the plastic region of the auxiliary elastic member 41, the auxiliary elastic member 41 can be fixedly dislocated, and the energy required for it is changed from the movable dislocation to the fixed dislocation when deforming in the elastic region of the auxiliary elastic member 41. It is smaller than the energy required to do it. Therefore, in this embodiment, the heating time can be shortened. Conventionally, for example, the heating time required for about 1 hour can be shortened from several minutes to several tens of minutes. Thus, even when the heating time is shortened as compared with the prior art, the spiral contact 20 having a small sag rate can be manufactured. I can do it. When the auxiliary elastic member 41 is formed of Ni as in the prior art, the Ni crystallizes under heating. Therefore, when three-dimensional molding is performed by applying stress in the plastic region, only the elastic deformation portion 20a having very poor spring properties is obtained. Therefore, it was necessary to perform the above three-dimensional molding while applying stress in the elastic region. In such a case, it is necessary to set the heating time longer because the energy required from the movable dislocation to the fixed dislocation is very large. On the other hand, in the present embodiment, the heating time can be shortened as described above, so that the manufacturing process is facilitated.

  Further, even when the spiral contact 20 is used in a planar shape (state shown in FIG. 6) without three-dimensionally forming the elastic deformation portion 20a of the spiral contact 20 as described above, for example, in a burn-in test apparatus or the like. When the connecting device 10 shown in FIG. 1 is used, the spiral contact 20 is inevitably placed under heating. However, in this embodiment, since the auxiliary elastic member 41 constituting the elastic deformation portion 20a of the spiral contactor 20 can be appropriately maintained in an amorphous state, the spring characteristics of the elastic deformation portion 20a can be maintained well, and the durability can be improved. An excellent connection device 10 can be provided.

  The elastic deformation portion 20a of the spiral contact 20 may have a shape other than the spiral shape. However, if the elastic deformation portion 20a has a spiral shape, the elastic deformation portion 20a is deformed so as to surround the connection terminal 1a regardless of the shape of the connection terminal 1a of the electronic component 1. This is preferable because the contact area between the elastic deformation portion 20a and the connection terminal 1a is widened and the contact property with the connection terminal 1a can be ensured.

  In the present embodiment, the auxiliary elastic member 41 is preferably formed of Ni-X (where X is any one or more of P, W, and B). When the element X is formed of P, the composition ratio of P is preferably 15 atomic% or more and 30 atomic% or less. When the element X is formed of W, the W composition ratio is preferably 14.5 at% or more and 36 at% or less, more preferably 20 at% or more. Further, when the element X is formed of B, it is preferable to form the B within a composition ratio of 15 atomic% to 30 atomic%.

  As described above, the crystallization temperature of the auxiliary elastic member 41 can be made higher than when Ni is used as the auxiliary elastic member 41, and the heating temperature of about 200 ° C. to 300 ° C. during three-dimensional molding is higher than the crystallization temperature. Therefore, even if the auxiliary elastic member 41 is heated and three-dimensionally molded, the auxiliary elastic member 41 can be appropriately maintained in an amorphous state. In particular, when the auxiliary elastic member 41 is formed of NiW, even if the heating temperature is increased to about 700 ° C., the heating temperature falls below the crystallization temperature, and the auxiliary elastic member 41 can be appropriately maintained in an amorphous state. Since the allowable range of the heating temperature can be expanded in this way, the three-dimensional molding process can be performed appropriately and easily.

  Further, as a method of three-dimensional molding, a spiral elastic deformation portion 20a is formed on a conical base, for example, without depending on a method of heat treatment in a state where the elastic deformation portion 20a is pushed upward by the protrusion adjusting member 70 shown in FIG. After the formation and removal of the base, the elastic deformation portion 20a may be three-dimensionally formed by the heat treatment described above or after the heat treatment, and then removing the base.

  Further, in the present embodiment, the elastic deformation portion 20a of the spiral contactor 20 does not have the laminated structure shown in FIG. 4. For example, the elastic deformation portion 20a may be composed of only the auxiliary elastic member 41. In such a case, it is preferable that the entire elastic deformation portion 20a is in an amorphous state.

  The Ni—X alloy mentioned as the material of the auxiliary elastic member 41 is an example, and other materials may be used.

  FIG. 9 (comparative example) and FIG. 10 (comparative example) are TEM photographs of a NiP alloy containing 12.5 atomic% of P. FIG. 9 is a TEM photograph in which NiP alloy is formed by plating and no heating is performed. FIG. 10 is a TEM photograph of the NiP alloy after the NiP alloy is plated and heated at 250 ° C. for 1 hour. It is.

  When the material state was analyzed from the TEM photograph shown in FIG. 9, it was confirmed that Ni3P intermetallic compound crystals accounted for the majority, and that Ni microcrystals existed between the intermetallic compound crystals. .

  Further, when the material state was analyzed from the TEM photograph shown in FIG. 10, most of the Ni3P intermetallic compound crystals occupy and there were Ni microcrystals and single crystals between the intermetallic compound crystals. I was able to confirm that.

  FIG. 11 (Example), FIG. 12 (Example) and FIG. 13 (Example) are TEM photographs of a NiP alloy containing 19 atomic% P. FIG. 11 shows a TEM photograph in a state where the NiP alloy is plated and no particular heating is performed. FIG. 12 shows a TEM photograph of the NiP alloy after the NiP alloy is plated and heated at 250 ° C. for 36 minutes. FIG. 13 is a TEM photograph of the NiP alloy after the NiP alloy is plated and heated at 250 ° C. for 1 hour.

  When the substance state was analyzed from the TEM photograph shown in FIG. 11, it was found that crystals were not seen and were amorphous.

  Next, when the material state was analyzed from the TEM photograph shown in FIG. 12, it was confirmed that ultrafine precipitates (emprio) of 1 nm or less existed although there was not much change from the state of FIG.

  Next, when the substance state was analyzed from the TEM photograph shown in FIG. 13, precipitation of intermetallic compounds was observed in part. The intermetallic compound was Ni3P, and no Ni crystal was observed. Further, as shown in FIG. 13, it was found that the periphery of the intermetallic compound was surrounded by an amorphous state and maintained in an amorphous state.

  FIG. 14 (Example) shows that the NiP alloy containing 15 atomic% of P was plated on a copper substrate by an electroless plating method, and this composite member was heat treated at 250 ° C. for 1 hour. It is a TEM photograph of a composite member. As shown in FIG. 14, although the copper substrate was crystallized, the NiP alloy part was not found to have a lump when it was crystallized, and the NiP alloy part was confirmed to be amorphous. .

  FIG. 15 shows a case where a plurality of Cu substrates are prepared, NiPs having different P composition ratios are plated on each Cu substrate, and a plurality of composite members (a) to (j) each made of a Cu substrate and a NiP alloy are formed. It is an X-ray diffraction diagram after heating at 250 ° C. for 1 hour.

  As shown in FIG. 15, a crystal peak of the Ni {111} plane is observed in the composite members (a) to (d) in which the composition ratio of P is changed from 7.9 atomic% to 14.7 atomic%. I was able to confirm. On the other hand, even when the composition ratio of P is 16.1 atomic%, a slight crystal peak of the Ni {111} plane is observed, which is considered to be a 1 nm ultrafine crystal precipitate (emprio). There is no crystallization. As described above, the experimental results shown in FIGS. 9 to 15 show that the P concentration should be 15 atomic% or more in order to maintain the NiP alloy in an amorphous state.

  Next, a NiP alloy was plated around the spiral contact copper foil by electroless plating. At this time, the composition ratio of P was 19 atomic%. Stress was applied to the spirally formed elastic deformation portion of the spiral contactor, and the elastic deformation portion 20a was deformed upward using the protrusion adjusting member 70 in the same manner as in the step of FIG. Solid molding). The heating conditions were a temperature of 250 ° C. and a time of 1 hour.

  In the experiment, as shown in FIG. 16, the stress applied to the elastically deforming portion of the spiral contactor was changed variously, and the height dimension of the elastically deforming portion was changed. The “height of the protrusion adjustment member” on the graph of FIG. 16 refers to the height H3 from the upper surface 21a of the base 21 of the spiral contactor 20 shown in FIG. 1 to the tip of the protrusion adjustment member 70. As the height dimension H3 increases, the stress applied to the elastically deformable portion increases. The “post-forming height” on the graph of FIG. 16 is the elastic deformation from the upper surface 21a of the base 21 of the spiral contactor 20 after the protrusion adjusting member 70 is removed, as shown in the process diagram of FIG. It means the height H2 up to the vertex A protruding to the uppermost part of the portion 20a.

  After the forming (after the three-dimensional molding), the elastic deformation portion 20a is spiraled as shown in FIG. 6 while applying stress downward (that is, the direction returning from the state of FIG. 8 to the state of FIG. 6). The upper surface of the elastically deforming portion 20a of the contact 20 becomes the same height as the upper surface 21a of the base 21 (until the spiral contact 20 has a planar shape), and the state is returned to the state shown in FIG. And maintained under heating at 150 ° C. (burn-in; BI). Thereafter, when the stress applied to the elastic deformation portion 20a is removed, the elastic deformation portion 20a is deformed again upward. The height dimension of the elastic deformation portion 20a at that time is shown as "post-BI height" on the graph of FIG. Similarly to the “forming height”, “post-BI height” means a height from the upper surface 21a of the base 21 of the spiral contactor 20 to the apex A protruding to the uppermost side of the elastic deformation portion 20a.

  When {(“post-forming height” − “post-BI height”) / “post-forming height”} × 100 is defined as a sag ratio (%), as shown in FIG. It has been found that the sag rate can be suppressed to 30% or less even if the stress applied during molding changes variously. The increase in the sag rate is a proof that the elastically deforming portion 20a is gradually plastically deformed, so it is desirable to keep the sag rate as low as possible.

  Incidentally, as shown in FIG. 16, when a stress higher than 1440 MPa is applied at about 1440 MPa as a boundary, the NiP alloy is three-dimensionally formed in the plastic region, while a stress lower than 1440 MPa is applied. In this case, the NiP alloy is three-dimensionally formed in the elastic region. Considering the sag, it is considered that the sag is performed via a movable dislocation. For this reason, in order to form the elastically deformable portion 20a having a small amount of slack, it is considered that it is necessary to perform a process for reducing the movable dislocations and forming the fixed dislocations during three-dimensional molding.

  When the NiP alloy is three-dimensionally formed in the elastic region, a large amount of energy is required to change the movable dislocation to the fixed dislocation. For this reason, in order to form the elastically deformable portion 20a by applying a stress of 1440 MPa or less, it is necessary to lengthen the heating time in order to form a fixed dislocation. On the other hand, when the NiP alloy is three-dimensionally formed in the plastic region, since the elastic deformation portion 20a is plastically deformed, the internal dislocations can be fixed and displaced with low energy. Therefore, it is possible to form the elastically deformable portion 20a having a small sag in a heating time when the NiP alloy is three-dimensionally formed in the plastic region and in a shorter time than when three-dimensionally forming the elastic region.

  FIG. 16 is a characteristic diagram when an amorphous NiP alloy is used for the elastically deformable portion 20a. By using an amorphous NiP alloy, the heating time can be shortened as compared with the prior art.

  Next, the spiral contact having the same structure as that used in the experiment of FIG. 16 (that is, the electroless plating of NiP containing 15 atomic% of P around the copper foil) is used. In the experiment of FIG. 18, the three-dimensional molding shown in FIGS. 7 and 8 is performed for 72 hours under heating at 200 ° C. while applying a stress of 2500 MPa to the deformed portion, and in the experiment of FIG. 19, FIGS. 20 is performed for 36 minutes under heating at 250 ° C., and in the experiment of FIG. 20, the solid molding shown in FIGS. 7 and 8 is performed for 9 minutes under heating at 250 ° C., and then the elasticity of each spiral contactor is performed. The “height after forming” (height after three-dimensional molding) of the deformed portion was measured, and in all the experiments of FIGS. 18 to 20, while applying the stress to return the elastic deformable portion 20 a to the state of FIG. 24 hours under heating When heated (burn-in 1), the height of the elastic deformation part 20a deformed again as shown in FIG. 8 after removing the stress is measured as “post-BI height 1”, and the elastic deformation part 20a is again measured as shown in FIG. Heating at 150 ° C. for 48 hours while applying stress to return to the state (burn-in 2), removing the stress and deforming again as shown in FIG. 2 ". The “post-forming height”, “post-BI height 1”, and “post-BI height 2” all extend from the upper surface 21a of the base 21 of the spiral contactor 20 to the apex A protruding to the uppermost side of the elastic deformation portion 20a. Measured at height.

  Further, the sag rate was determined as {(“post-forming height” − “post-BI height 1 or post-BI height 2”) / “post-forming height”} × 100. The experimental results are shown in FIGS.

  As shown in FIGS. 18 to 20, in all experiments, the sag rate could be suppressed to 30% or less. In addition, in the experiment of FIG. 20, the heating time at the time of three-dimensional molding is only 9 minutes, but the sag rate is 30% or less, and the heating time that is performed for about 1 hour as in the conventional case is several minutes to several tens. It was confirmed that a spiral contact with a sag rate of 30% or less could be produced even when shortened to a minute.

  Next, in the experiments shown in FIGS. 21 and 22, the NiP alloy is formed around the copper foil by electroless plating, the composition ratio of P is 12.5 atomic% in the comparative example, and the composition ratio of P in the examples. 19 atomic%, a plated spiral contact is formed, and in both the comparative example and the example, after three-dimensional molding is performed at 250 ° C. for 1 hour, the elastic contact portion of the spiral contact is formed. A load was applied and the amount of displacement until the spiral contact was broken was measured. The “displacement amount” is the elastic deformation portion that descends by applying the load downward from the vertex A of the elastic deformation portion of the spiral contact in the state of FIG. 8 (the state in which the load is not applied). Is a descending amount H4 to the vertex A ′ (see FIG. 8).

  FIG. 21 is a comparative example, and FIG. 22 is an example. Since the NiP alloy used in the experiment of FIG. 21 has a P composition ratio of 12.5 atomic%, it is crystallized by three-dimensional molding under heating. On the other hand, the NiP alloy used in the experiment of FIG. Since the ratio is 15 atomic%, the amorphous state is maintained even by three-dimensional molding under heating. In the comparative example of FIG. 21, the elastically deformed portion of the spiral contactor broke with a displacement of about 250 μm. However, in the embodiment of FIG. 22, the elastically deformable portion of the spiral contactor does not break even when displaced by 500 μm or more. I understood it.

  FIG. 23 shows the formation of a large number of spiral contacts in which a NiP alloy is plated around the copper foil by electroless plating and the composition ratio of P is 12.5 atomic%. Each spiral contact is formed at 250 ° C. After three-dimensional molding under heating for 1 hour, a test projection member is made to oppose the elastic deformation portion of each spiral contact, and the projection member is lowered to 1000 MPa to 1500 MPa with respect to the elastic deformation portion. Pushing until stress within the range is applied, then raising the protruding member to the original position, raising and lowering the protruding member 3000 times, and bending the elastic deformation part of the spiral contact (life test) Was examined both when the protrusions were raised and lowered 1000 times. As shown in FIG. 23, when the stress applied to the elastically deformed portion of the spiral contactor is small, the rate at which the elastically deformed portion of the spiral contactor is broken is reduced, but when the stress of about 1500 MPa is applied 3000 times, 80% It was found that the elastic deformation part of a nearby spiral contact breaks. Further, even when the protrusion member is moved up and down 1000 times, the elastic deformation portion of the spiral contactor is bent, and the elastic deformation portion cannot be broken to 0%. It was found that the spiral contactor having excellent durability could not be produced with an elastically deformable portion having the above.

  On the other hand, an amorphous NiP alloy (P is 15 atomic%) is formed by electroless plating around the spiral contact of the embodiment formed by applying the stress shown in FIGS. In the spiral contact formed by plating, there was no spiral contact that could be broken even when a stress of 2000 MPa was applied up to 4000 times using the same method as the experiment of FIG. From this, it was found that the durability is greatly improved when an amorphous NiP alloy is used for the elastically deformable portion.

  Next, a spiral contact having an auxiliary elastic member made of a NiP alloy having a P composition ratio of 15 atomic% used in the experiment of FIG. 18 (three-dimensional molding was performed for 72 hours under heating at 200 ° C., Example 1) A spiral contact having an auxiliary elastic member made of a NiP alloy having a composition ratio of P of 15 atomic% used in the experiment of FIG. 19 (three-dimensional molding was performed for 36 minutes under heating at 250 ° C., implementation Example 2), a spiral contact (Example 3) formed by performing three-dimensional molding at 250 ° C. for 18 minutes having an auxiliary elastic member made of a NiP alloy having a P composition ratio of 15 atomic%, experiment of FIG. Each of the spiral contacts having auxiliary elastic members made of a NiP alloy having a P composition ratio of 15 atomic% (three-dimensional molding performed under heating at 250 ° C. for 9 minutes, Example 4) Use each It was examined the yield point of Iraru contacts.

  In the experiment, the elastic deformation part of each three-dimensionally shaped spiral contactor is pressed downward, the load when reaching the yield point, and the descending amount H4 (displacement amount) of the vertex A of the elastic deformation part at that time (See FIG. 8). The experimental results are shown in Table 1 below.

  It was found that the load and the amount of displacement at the yield point did not change much in the spiral contact of each example. As shown in Table 1, it was found that a yield point with a load of 2 gf (19 mN) or more and a displacement of 0.1 mm or more can be obtained in each spiral contact. Preferably, it was found that a yield point with a load of 4 gf (38 mN) or more and a displacement of 0.2 mm or more can be obtained.

  In FIG. 24, a plurality of Cu substrates are prepared, NiWs having different W composition ratios are plated on each Cu substrate, and a plurality of composite members (k) to (p) each made of a Cu substrate and a NiW alloy are formed. It is an X-ray diffraction diagram after heating at 250 ° C. for 1 hour.

  As shown in FIG. 24, it was confirmed that when the W composition ratio was 12.5 atomic%, a crystal peak of the Ni {111} plane was observed. On the other hand, even when the composition ratio of W is 14.9 atomic% and 19.7 atomic%, a crystal peak of the Ni {111} plane is slightly observed. However, according to a TEM photograph described later, amorphous is dominant. It was the target. When the W composition ratio was 24.4 atomic%, 27.7 atomic%, or 35.1 atomic%, no crystal peak of the Ni {111} plane was observed.

  FIG. 25 shows a TEM photograph and a transmission electron diffraction image after heating an NiW alloy containing 12.5 atomic% of W at 250 ° C. for 1 hour. FIG. 26 shows an NiW alloy containing 14.9 atomic% of W at 250 ° C. FIG. 27 shows a TEM photograph and a transmission electron diffraction image after heating a NiW alloy containing 19.7 atomic% of W at 250 ° C. for 1 hour. 28 is a TEM photograph and a transmission electron diffraction image after heating an NiW alloy containing 24.4 atomic% of W at 250 ° C. for 1 hour. The transmission electron beam diffraction image was obtained by cutting the NiW alloy from a direction parallel to the film thickness and allowing the electron beam to enter from a direction perpendicular to the cut surface.

  As shown in the TEM photograph of FIG. 25, the amorphous portion is not seen, the lattice stripes facing in the same direction are clearly seen, and diffraction diffraction spots on the reciprocal lattice plane appear in the transmission electron beam diffraction image. I found out. Further, as a result of indexing the reciprocal lattice plane, it was found that the crystal was predominantly Ni crystal.

  Next, it was found that lattice stripes of about 5 to 10 nm appeared in the TEM photograph shown in FIG. The direction of the lattice fringes is in a random direction, which is considered to be because crystals (or ultrafine crystal precipitates) are precipitated from amorphous. Further, in the transmission electron beam diffraction image, halo ring indicating the presence of amorphous appeared, and thus it was found that the NiW in FIG. 26 is predominantly amorphous.

  Next, it was found that lattice stripes of about 4 to 6 nm appeared in the TEM photograph shown in FIG. The direction of the lattice fringes is in a random direction, which is considered to be because crystals (or ultrafine crystal precipitates) are precipitated from amorphous. Further, halo ring indicating the presence of amorphous appears in the transmission electron beam diffraction image. The halo ring appears more clearly in FIG. 27 than in FIG. Therefore, it was found that the NiW in FIG. 27 is more amorphous than the NiW in FIG.

  Next, in the TEM photograph shown in FIG. 28, lattice fringes of 5 nm or less can be seen in some places, but the presence of the lattice fringes is smaller than in the case of FIGS. 26 and 27, and the transmission electron beam diffraction image is very clear. Since halo ringing appeared, it was found that the NiW in FIG. 28 is more amorphous than the NiW in FIG. 26 and the NiW in FIG.

  As described above, the experimental results of FIGS. 24 to 28 show that the W composition ratio of NiW is preferably in the range of 14.5 atomic% to 36 atomic%, more preferably 20 atomic% or more. It was. More preferably, it is 24.4 atomic% or more. Thereby, NiW can be appropriately made into an amorphous state.

  Next, FIG. 29 shows X-ray diffraction after preparing a plurality of composite members obtained by plating NiP having 19.7 atomic% W on a Cu substrate, and subjecting each composite member to heat treatment at different temperatures. FIG.

  FIG. 30 is an X-ray diffraction pattern after preparing a plurality of composite members obtained by plating NiP having 27.7 atomic% W on a Cu substrate and heat-treating each composite member at different temperatures. is there.

  As shown in FIG. 29, when W was 19.7 atomic%, it was confirmed that when the heat treatment temperature was about 600 ° C., a crystal peak of the Ni {111} plane was observed. Further, as shown in FIG. 30, when W was 27.7 atomic%, it was confirmed that when the heat treatment temperature was about 700 ° C., a crystal peak of the Ni {111} plane was observed.

  Thus, it was found that crystallization can be suppressed even when the heat treatment temperature is increased as the W composition ratio is increased. In particular, in the case of NiW, depending on the W composition ratio, crystallization can be suppressed even if the heat treatment temperature is increased to about 700 ° C. Therefore, it was found that the allowable range of the heat treatment temperature can be greatly widened and the amorphous state can be effectively maintained. .

The perspective view which shows the test | inspection apparatus used for the test for confirming operation | movement of an electronic component, 1 is a cross-sectional view taken along line 2-2 of FIG. An enlarged perspective view showing the shape of the spiral contact in this embodiment, 4A, FIG. 4B, FIG. 4C, and FIG. 4D are cross-sectional views when the contact pieces for each turn constituting the spiral contact in this embodiment are cut in the film thickness direction from the direction parallel to the width direction, The schematic diagram which shows the substance state of the auxiliary | assistant elastic member in this embodiment, 1 process drawing (partial sectional view) showing the manufacturing method of the spiral contact until the spiral contact is mounted on the base 11 and the elastically deforming portion of the spiral contact is directed upward. One process diagram (partial cross-sectional view) performed next to FIG. One process diagram (partial cross-sectional view) performed after FIG. TEM photograph of NiP alloy containing 12.5 atomic% of P without any particular heating, A TEM photograph of the NiP alloy after heating at 250 ° C. for 1 hour with respect to a NiP alloy containing 12.5 atomic% of P, TEM photograph of NiP alloy containing 19 atomic% of P without any heating, A TEM photograph of the NiP alloy after heating at 250 ° C. for 36 minutes against a NiP alloy containing 19 atomic% of P, TEM photograph of NiP alloy after heating at 250 ° C. for 1 hour against NiP alloy containing 19 atomic% of P, A NiP alloy containing 15 atomic% of P on a copper substrate is formed by electroless plating, and this composite member is heat-treated at 250 ° C. for 1 hour. A plurality of Cu substrates are prepared, NiPs having different P composition ratios are formed on each Cu substrate by plating, and a plurality of composite members (a) to (j) made of a Cu substrate and a NiP alloy are each set to 1 at 250 ° C. X-ray diffraction diagram after heating for a while, A NiP alloy (P is plated by 19 atomic% by electroless plating around the copper foil in the shape of a spiral contact, and three-dimensionally molded under predetermined conditions by applying different stresses to the elastically deformed portion of the spiral contact. Then, when the height dimension (post-forming height) of the elastic deformation part is measured, and then the heat dimension is measured under a predetermined condition to measure the height dimension (post-BI height) of the elastic deformation part. A graph showing the relationship between the stress applied to the elastically deformed portion of the spiral contactor and the height after forming and the height after BI; The graph which shows the relationship between the stress applied to the elastic deformation part of the spiral contact and the sag rate when the sag rate is obtained based on the experimental result of FIG. Using the spiral contact having the same configuration as the spiral contact used in the experiment of FIG. 16, three-dimensional molding is performed under a predetermined condition to measure the height dimension (post-forming height) of the elastic deformation portion, and then The spiral contact is heated under a predetermined condition to measure the height dimension (post-BI height 1) of the elastic deformation portion, and the spiral contact is heated under a predetermined condition to measure the elasticity. A graph showing the relationship between the post-forming height, the post-BI height 1, the post-BI height 2 value, and the sag rate when the height dimension of the deformed portion (post-BI height 2) is measured; Using the spiral contact having the same configuration as the spiral contact used in the experiment of FIG. 16, three-dimensional molding is performed under a predetermined condition to measure the height dimension (post-forming height) of the elastic deformation portion, and then The spiral contact is heated under a predetermined condition to measure the height dimension (post-BI height 1) of the elastic deformation portion, and the spiral contact is heated under a predetermined condition to measure the elasticity. A graph showing the relationship between the post-forming height, the post-BI height 1, the post-BI height 2 value, and the sag rate when the height dimension of the deformed portion (post-BI height 2) is measured; Using the spiral contact having the same configuration as the spiral contact used in the experiment of FIG. 16, three-dimensional molding is performed under a predetermined condition to measure the height dimension (post-forming height) of the elastic deformation portion, and then The spiral contact is heated under a predetermined condition to measure the height dimension (post-BI height 1) of the elastic deformation portion, and the spiral contact is heated under a predetermined condition to measure the elasticity. A graph showing the relationship between the post-forming height, the post-BI height 1, the post-BI height 2 value, and the sag rate when the height dimension of the deformed portion (post-BI height 2) is measured; A spiral contact is formed by plating a NiP alloy around the copper foil by electroless plating, setting the P composition ratio to 12.5 atomic%, and performing three-dimensional molding under predetermined conditions. A graph showing a relationship between the displacement and the load when a load is applied to the elastic deformation portion of the child and the displacement until the spiral contact is broken is measured; After forming a NiP alloy around the copper foil by electroless plating, plating a spiral contact with a P composition ratio of 19 atomic%, and performing three-dimensional molding under predetermined conditions, the spiral contact A graph showing a relationship between the displacement amount and the load when a load is applied to the elastically deformed portion and the displacement amount until the spiral contactor breaks is measured; After forming a large number of spiral contacts formed by plating an NiP alloy around the copper foil by electroless plating with a P composition ratio of 12.5 atomic%, each spiral contact is three-dimensionally molded under predetermined conditions Then, the test projection member is pushed into the elastic deformation portion of the spiral contact with a predetermined stress, and then the projection member is separated from the elastic deformation portion, and the elevation operation of the projection member is performed up to 3000 times. The relationship between the stress applied to the elastically deforming portion when the protruding member is pushed and the rate at which the elastically deforming portion of the spiral contactor breaks (life test) is raised and lowered 1000 times and 3000 times. Graphs obtained in each case, A plurality of Cu substrates are prepared, NiWs having different W composition ratios are formed on the respective Cu substrates by plating, and a plurality of composite members (k) to (p) made of a Cu substrate and a NiW alloy are each set at 250 ° C. X-ray diffraction diagram after heating for a while, TEM photograph and transmission electron diffraction image after heating NiW alloy containing 12.5 atomic% W at 250 ° C. for 1 hour, A TEM photograph and a transmission electron diffraction image after heating a NiW alloy containing 14.9 atomic% of W at 250 ° C. for 1 hour, A TEM photograph and a transmission electron diffraction image after heating a NiW alloy containing 19.7 atomic% of W at 250 ° C. for 1 hour, A TEM photograph and a transmission electron diffraction image after heating an NiW alloy containing 24.4 atomic% of W at 250 ° C. for 1 hour, X-ray diffraction patterns after preparing a plurality of composite members obtained by plating NiP having 19.7 atomic% W on a Cu substrate, and heat-treating each composite member at different temperatures; X-ray diffractograms after preparing a plurality of composite members formed by plating NiP having 27.7 atomic% W on a Cu substrate and heat-treating each composite member at different temperatures;

Explanation of symbols

1 Electronic component 1a Spherical contact (connection terminal)
DESCRIPTION OF SYMBOLS 10 Connection apparatus 11 Base 20 Spiral contact 20a Elastic deformation part 21 Base 40 Conductive member 41 Auxiliary elastic member 42 Coating member 50 Amorphous 51 Ultra fine precipitate (Emprio)
52 Intermetallic Compound Crystal 70 Projection Adjustment Member

Claims (12)

In the method of manufacturing a contact having an elastically deformable portion,
Forming the elastic deformation portion with Ni-P or Ni-B Ni alloy;
Heating the elastically deformed portion in a three-dimensionally formed state;
And a heating temperature within a range of 200 ° C. to 300 ° C., and maintaining the amorphous state of the Ni alloy.   The method for producing a contact according to claim 1, wherein the composition ratio of P is 15 atomic% or more and 30 atomic% or less. In the method of manufacturing a contact having an elastically deformable portion,
Forming the elastically deformable portion with a Ni-W Ni alloy;
Heating the elastically deformed portion in a three-dimensionally formed state;
And a heating temperature within a range of 200 ° C. to 700 ° C. to maintain the amorphous state of the Ni alloy.   The method for producing a contact according to claim 3, wherein the W composition ratio is 14.5 at% or more and 36 at% or less.   The method for producing a contact according to claim 4, wherein the composition ratio of W is 20 atomic% or more.   The method for manufacturing a contact according to claim 1, wherein the heating step is performed at a temperature lower than a crystallization temperature of the Ni alloy.   The manufacturing method of the contactor of any one of Claim 1 thru | or 6 which applies the stress in the plastic area of the said Ni alloy to the said elastic deformation part, and heats the said elastic deformation part in the state shape | molded three-dimensionally.   The method for manufacturing a contact according to any one of claims 1 to 7, wherein the heating time is between 36 minutes and 1 hour.   The method for manufacturing a contact according to any one of claims 1 to 8, wherein the elastically deforming portion is formed of only the Ni alloy.   The method for manufacturing a contact according to any one of claims 1 to 8, wherein an elastic region made of the Ni alloy is formed in a part of a cross section of the elastic deformation portion cut from a film thickness direction.   The elastic deformation portion is formed to include a conductive member and an auxiliary elastic member. At this time, the conductive member is formed of a material having a specific resistance lower than that of the auxiliary elastic member, and the auxiliary elastic member is formed. The method for manufacturing a contact according to claim 10, wherein the contact point is formed of the Ni alloy having a higher yield point and elastic modulus than the conductive member. In a manufacturing method of a connection device having a base and a contact provided on the base, wherein an external connection portion of an electronic component contacts an elastic deformation portion of the contact,
The method for manufacturing a connection device, wherein the elastic deformation portion of the contact is formed by the manufacturing method according to claim 1.

Images