JP2010217105A - Flying checking contact probe retaining structure and flying inspection apparatus of circuit board - Google Patents

Abstract

<P>PROBLEM TO BE SOLVED: To provide a flying checking contact probe retaining structure, capable of ensuring durability against contact with a number of checking points and a high-reliability flying checking apparatus having the same. <P>SOLUTION: A spring probe 20 constituting a contact probe assembly 10 includes a point-shaped plunger 25 whose front end 25A is brought into contact with a checking point; a barrel 24, in which the other end of the plunger 25 is inserted so as to be advanceable and retractable; and a spring 26 for deviating the plunger 25 to a movement limit in the protruding direction to the barrel 24. The barrel 24 is fixed by using a compound bonding structure 34 onto each of a first fixed surface 32A and a second fixed surface 32B of a stepped portion 32, formed at one end of a substrate part 22 in the longitudinal direction. <P>COPYRIGHT: (C)2010,JPO&INPIT

Description

  The present invention relates to a flying inspection contact probe holding structure and a circuit board flying inspection apparatus.

  As a printed circuit board inspection apparatus, a so-called flying inspection apparatus is known in which a probe is sequentially moved to a plurality of inspection points on the printed circuit board, and a continuity inspection is performed by bringing the probe into contact with a movement destination inspection point (for example, , See Patent Document 1). Further, in such a flying inspection apparatus, one in which a probe is urged toward the printed circuit board by a coil spring coaxially arranged is known (for example, see Patent Document 2).

JP 2003-222649 A Japanese Patent Laid-Open No. 7-92227

  However, in the conventional technique described above, the probe is required to have durability because the probe is sequentially contacted with a large number of inspection points with a small number of probes.

  The present invention can provide a flying inspection contact probe holding structure capable of ensuring durability against contact with a large number of inspection points, and a flying inspection apparatus having the flying inspection contact probe holding structure having high reliability. Is the purpose.

  A flying probe contact probe holding structure according to claim 1 is a needle-like contactor whose one end is in contact with an inspection point, a cylindrical body in which the other end of the contact is inserted so as to be able to advance and retract, A spring probe that includes a biasing member that shifts the contact to the limit of movement in the protruding direction with respect to the cylindrical body, a first fixed surface that faces the thickness direction by having one end in the longitudinal direction being thin, and A step portion having a second fixing surface facing the longitudinal direction is formed along the width direction, and a base plate portion fixed to a moving means for moving the spring probe to an inspection point, and a cylindrical body of the spring probe. And fixing means fixed to each of the first fixing surface and the second fixing surface in the stepped portion of the substrate portion.

  In the flying inspection contact probe holding structure according to the first aspect, the contact of the spring probe is brought into contact with the inspection point while moving forward and backward (extends and contracts) with respect to the cylindrical body fixed to one end portion in the longitudinal direction of the substrate portion. Here, in this flying inspection contact probe holding structure, since the cylindrical body of the spring probe is fixed to the substrate portion, it is not necessary to provide a spring function on the substrate portion, and it is easy to ensure the required strength. In addition, since the spring probe cylinder is fixed to each of the first fixing surface and the second fixing surface in the step portion of the substrate portion, the spring probe cylinder is firmly fixed to the substrate portion. Can do.

  As described above, in the flying inspection contact probe holding structure according to the first aspect, durability against contact with a large number of inspection points can be ensured.

  The flying inspection contact probe holding structure according to claim 2 is the flying inspection contact probe holding structure according to claim 1, wherein the fixing means includes the cylindrical body, the first fixing surface, and the second fixing surface. And an adhesive layer interposed between each of the cylindrical body and the stepped portion, and a covering adhesive layer that covers an adhesion site of the cylindrical body and the stepped portion by the adhesive layer.

  In the flying probe contact probe holding structure according to claim 2, the cylindrical body of the spring probe is bonded (fixed) to each of the first fixed surface and the second fixed surface of the substrate portion via an adhesive layer. The adhesion part by the layer is covered with the covering adhesive layer. For this reason, compared to a configuration in which the spring probe is simply fixed to the substrate portion via an adhesive layer, the strength against repeated loads caused by contact of the contact with a large number of inspection points is high, and durability against repeated contact with the inspection points. Will improve.

  The flying inspection contact probe holding structure according to claim 3 is the flying inspection contact probe holding structure according to claim 1 or 2, wherein the substrate portion includes a first substrate portion, a second substrate portion, and the like. And the step portion is formed by offsetting the position of the one end of the first substrate portion and the second substrate portion in the longitudinal direction.

  In the flying inspection contact probe holding structure according to claim 3, the first fixing surface and the second fixing surface are overlapped so that the first substrate portion and the second substrate portion are overlapped so that the position of one end in the longitudinal direction is offset. The stepped portion is easily and accurately formed. As a result, the flying inspection contact probe holding structure can be constructed with low cost and high accuracy.

  According to a fourth aspect of the present invention, there is provided a flying inspection contact probe holding structure according to the third aspect, wherein the first fixed surface is in a longitudinal direction of the second substrate portion. The thickness direction end surface of the first substrate that protrudes toward one end side in the longitudinal direction by an amount corresponding to the diameter of the cylindrical body, and the second fixing surface has a plate thickness corresponding to the diameter of the cylindrical body. The second substrate portion is an end surface in the longitudinal direction.

  The flying inspection contact probe holding structure according to claim 4, wherein the first fixing surface which is the end surface in the thickness direction of the first substrate portion and the second fixing surface which is the end surface in the longitudinal direction of the second substrate portion are each of the spring probe. It has the same dimensions as the diameter of the cylinder. For this reason, the flying probe contact probe holding structure is configured to be compact (thin) as a whole while ensuring the required strength.

  The contact probe holding structure for flying inspection according to the invention of claim 5 is the contact probe holding structure for flying inspection according to any one of claims 1 to 4, wherein the substrate portion is on the inspection point side. The edge portion has a shape that protrudes most toward the inspection point at one end in the longitudinal direction.

  In the flying inspection contact probe holding structure according to the fifth aspect, one end in the longitudinal direction to which the spring probe in the substrate portion is fixed protrudes toward the inspection point where the contact of the spring probe contacts. For this reason, in this contact probe holding structure for flying inspection, even when a convex portion is located near the inspection point, interference with the convex portion is avoided.

  The flying inspection contact probe holding structure according to the invention of claim 6 is the flying inspection contact probe holding structure according to claim 5, wherein the substrate portion has an arcuate edge on the inspection point side. ing.

  In the flying inspection contact probe holding structure according to claim 6, since the edge on the inspection point side of the substrate portion forms an arc shape, the substrate portion is not formed with a sudden change portion of a cross section (section modulus, etc.) in the longitudinal direction. It is easy to ensure the required strength.

  The contact probe holding structure for flying inspection according to the invention of claim 7 is the contact probe holding structure for flying inspection according to any one of claims 1 to 6, wherein the spring probe is attached to the cylindrical body. A rotation imparting mechanism is provided for rotating the contactor about its own axis as the contact is advanced or retracted.

  In the contact probe holding structure for flying inspection according to the seventh aspect, the contact is rotated about its own axis as the cylinder moves forward and backward. For this reason, even if the inspection point is covered with an insulator, the contact of the spring probe that constitutes the flying inspection contact probe holding structure passes through the insulator and contacts the inspection point.

  A circuit board flying inspection apparatus according to an eighth aspect of the present invention includes a substrate holding portion that holds the substrate to be inspected by suction, and a flying probe contact probe holding structure according to any one of the first to seventh aspects. A probe drive mechanism that is held by the substrate unit and sequentially contacts the contact points of the spring probe with a plurality of inspection points on the substrate to be inspected.

  9. The circuit board flying inspection apparatus according to claim 8, wherein the spring probe of the flying inspection contact probe holding structure driven by the probe driving mechanism is sequentially applied to the plurality of inspection points of the circuit board sucked and held by the board holding portion. The circuit board is inspected by moving and contacting. The flying inspection apparatus includes the flying inspection contact probe holding structure according to any one of claims 1 to 7, which ensures durability against repeated contact with a large number of inspection points. And reliable.

  According to a ninth aspect of the present invention, there is provided a circuit board flying inspection apparatus comprising: a substrate holding portion that holds a substrate to be inspected together with a sheet-like cover material; and a flying inspection contact probe holding structure according to the seventh aspect. And a probe driving mechanism that sequentially contacts the spring probe contacts with a plurality of inspection points on the substrate to be inspected.

  10. The circuit board flying inspection apparatus according to claim 9, wherein the spring of the contact probe holding structure for flying inspection driven by the probe driving mechanism is applied to a plurality of inspection points of the circuit board sucked and held by the board holding portion together with the cover material. The circuit board is inspected as the probe moves and contacts sequentially. In this flying inspection apparatus, by adsorbing the cover material together with the circuit board, partial lifting of the circuit board is prevented or effectively suppressed, and the reliability of the inspection is improved.

  In this flying inspection apparatus, since the contact of the spring probe is rotated in accordance with contact with the probe (advancement / retraction with respect to the cylinder), the contact passes through the cover material and contacts the inspection point of the circuit board. . For this reason, the inspection method which covers a circuit board with a cover material is realizable with a flying inspection device. In addition, it is desirable that the tip of the contactor has a shape in which a plurality of edge portions are formed in the circumferential direction (rotation direction) (for example, a pyramid shape such as a regular triangular pyramid).

  A circuit board flying inspection apparatus according to a tenth aspect of the present invention is the circuit board flying inspection apparatus according to the ninth aspect, wherein the cover material is a sheet material made of unstretched or biaxially stretched polyethylene.

  In the flying inspection apparatus for a circuit board according to claim 10, the circuit board covered with the sheet material is inspected by adsorbing the sheet material made of polyethylene together with the circuit board. Here, since the polyethylene sheet does not tear in one direction when penetrating with the contact of the spring probe, the polyethylene sheet is sucked and held by the board holding part while covering the circuit board to prevent or effect the circuit board. The function to suppress automatically can be maintained. Thereby, in this flying inspection apparatus, the reliability of the inspection of the circuit board is further improved.

  As described above, the flying inspection contact probe holding structure according to the present invention has an excellent effect of ensuring durability against contact with a large number of inspection points.

  In addition, the flying inspection apparatus for a circuit board according to the present invention has an excellent effect of high reliability by applying the above-described flying inspection contact probe holding structure.

It is a perspective view showing the whole contact probe assembly composition concerning the embodiment of the present invention. It is a side view which shows the whole structure of the contact probe assembly which concerns on embodiment of this invention. It is a top view which expands and shows the fixation structure of the spring probe with respect to the board | substrate part of the contact probe assembly which concerns on embodiment of this invention. It is a figure which shows the manufacturing method of the contact probe assembly which concerns on embodiment of this invention, Comprising: (A) is a perspective view which shows a board | substrate part temporary fixing process, (B) is a perspective view which shows a probe adhesion process, (C) is It is a perspective view which shows an adhesion part reinforcement process. It is a longitudinal cross-sectional view of the spring probe which comprises the contact probe assembly which concerns on embodiment of this invention. 1 is a partially broken side view schematically showing a main part of a printed circuit board flying inspection apparatus to which a contact probe assembly according to an embodiment of the present invention is applied. It is a side view which shows the inspection apparatus of the printed circuit board which concerns on the comparative example with embodiment of this invention.

  A contact probe assembly 10 to which a flying inspection contact probe holding structure according to an embodiment of the present invention is applied, and a printed board flying inspection apparatus 11 having the contact probe assembly 10 will be described with reference to FIGS. . First, a schematic overall configuration of the flying inspection apparatus 11 will be described, and then a contact probe assembly 10 which is a main part of the present invention will be described in detail.

(Overall configuration of printed circuit board flying inspection system)
FIG. 6 is a schematic side view in which a main part of the printed board flying inspection apparatus 11 is partially broken. As shown in this figure, the flying inspection apparatus 11 is configured to inspect the continuity of each inspection point of a printed circuit board 12 to be inspected by using a contact probe assembly 10 described in detail later. In this embodiment, the flying inspection apparatus 11 measures the capacitance between the conductor pattern formed on the printed circuit board 12 to be inspected and the reference electrode, and determines the quality of the conductor pattern based on the measured capacitance. Inspected. Hereinafter, a specific description will be given, but a well-known method can be applied to the principle of inspection (good / bad determination), and thus the description thereof is omitted.

  The flying inspection apparatus 11 includes a suction table 14 as a substrate holding unit that sucks and holds the printed circuit board 12 from the side opposite to the inspection surface by evacuation (negative pressure), and a probe driving mechanism that moves the contact probe assembly 10 according to the inspection point. The probe driving unit 16 and a measuring unit (not shown) are mainly configured.

  The suction table 14 has a substrate placement surface 14A that faces horizontally and vertically upward, and is evacuated by a suction device (not shown) from the side opposite to the substrate placement surface 14A (lower surface) through a plurality of suction holes 14B. Thus, the printed circuit board 12 is sucked and held on the substrate placement surface 14A. Further, a partition (projection) 14C for positioning the printed circuit board 12 is provided on the substrate placement surface 14A. In the flying inspection apparatus 11 according to this embodiment, as shown in FIG. 7A, the cover material 18 and the printed circuit board 12 are covered with the suction table so that the sheet-shaped cover material 18 covers the printed circuit board 12 from above. 14 is made to adsorb | suck.

  Thereby, in the contact probe assembly 10, it is set as the structure which can closely_contact | adhere each part of the printed circuit board 12 to the board | substrate mounting surface 14A, without producing a float. The cover material 18 is a non-stretched or biaxially stretched polyethylene sheet having a thickness of 0.1 mm, and is configured not to tear in one direction due to penetration (drilling) by a plunger 25 described later.

  The probe drive unit 16 includes a horizontal drive unit that drives the contact probe assembly 10 in the X and Y directions with respect to the suction table 14 and a vertical drive unit that drives the contact probe assembly 10 in the Z direction. Yes. As a result, in the contact probe assembly 10, the contact probe assembly 10 (the spring probe 20) is moved immediately above the inspection point by the horizontal drive portion of the probe drive unit 16, and then the contact probe assembly 10 is lowered by the vertical drive portion. Thus, the inspection point is inspected by the measuring unit by bringing the spring probe 20 into contact with the inspection point.

  Further, the contact probe assembly 10 lifts the contact probe assembly 10 by the vertical drive unit from the state in which the spring probe 20 is in contact with the inspection point, and then moves the contact probe assembly 10 to another inspection point by the horizontal drive unit. A plurality of inspection points are inspected.

  As shown in FIG. 6, the flying inspection apparatus 11 according to this embodiment includes a pair (two) of contact probe assemblies 10 and a probe driving unit 16.

(Configuration of contact probe assembly)
As shown in FIG. 1, the contact probe assembly 10 includes a spring probe 20 that is brought into contact with an inspection point of a printed circuit board 12 to electrically connect the inspection point and the measurement unit, and a probe of the probe driving unit 16 to which the spring probe 20 is fixed. The board part 22 fixedly attached to the fixing part 16A is configured as a main part.

  As shown in FIG. 5, the spring probe 20 includes a barrel 24 as a cylindrical body, a plunger 25 as a contact having a needle shape and part of the longitudinal direction inserted into the barrel 24, and a plunger A spring 26 as a biasing member that biases 25 toward the protruding side with respect to the barrel 24 is configured as a main part.

  The barrel 24 has an elongated cylindrical shape with a length of about 15 mm and an outer diameter D of about 0.48 mm, and a plunger 25 is inserted into an opening end 24A on one side in the longitudinal direction. In addition, a conductive wire 28 (see FIG. 1) for electrical connection with the measuring unit is connected to the crimped longitudinal other end 24B of the barrel 24 by soldering or the like. Further, a convex portion 24 </ b> C protruding radially inward is formed in the middle portion of the barrel 24 in the longitudinal direction. The barrel 24 functions as a cam that converts the stopper force of the plunger 25 and the stroke force of the plunger 25 into a rotational force. In this embodiment, the material of the barrel 24 is beryllium copper clad with gold.

  The plunger 25 has a tip 25A protruding from the barrel 24 in contact with the inspection point. The distal end portion 25A is formed in a pyramid shape (substantially equilateral triangular pyramid shape in this embodiment), and a plurality of edges 25B are arranged along the circumferential direction. At the other end portion of the plunger 25 located in the barrel 24, a retaining step portion 25C that engages with the convex portion 24C is formed. In this embodiment, the material of the plunger 25 is stainless steel.

  The spring 26 is a compression coil spring, and is arranged in a compressed state between an end 25D of the plunger 25 located in the barrel 24 and the other end 24B in the longitudinal direction of the barrel 24. As a result, the plunger 25 is biased in a direction protruding from the opening end 24A with respect to the barrel 24, and the retaining step portion 25C engages with the convex portion 24C, thereby resisting the biasing force of the spring 26. 24 is prevented from coming off. That is, the position where the retaining step 25C engages with the convex portion 24C is the protrusion limit of the plunger 25 with respect to the barrel 24. In other words, the plunger 25 is biased to the protruding limit by the urging force of the spring 26. The protrusion length of the plunger 25 located at the protrusion limit with respect to the barrel 24 is approximately 2 mm.

  Further, a spiral groove 25E in which the convex portion 24C of the barrel 24 is inserted is formed between the tip portion 25A and the retaining step portion 25C of the plunger 25 (in this embodiment, a portion that is always located in the barrel 24). Has been. Thereby, in the spring probe 20, a part of the force that pushes the plunger 25 into the barrel 24 against the urging force of the spring 26 causes the sliding (cam action) between the groove wall of the spiral groove 25E and the convex portion 24C. Along with this, the plunger 25 is converted into a rotational force around its own axis.

  Due to the cam action of the groove wall of the spiral groove 25E and the convex portion 24C, the plunger 25 is pushed (enters) into the barrel 24 while rotating around its own axis when pressed against the inspection point. . In this embodiment, the rotation angle of the plunger 25 is about 45 ° for the full stroke and about 30 ° for the inspection stroke by the flying inspection device 11. In this embodiment, the groove wall of the spiral groove 25E and the convex portion 24C correspond to the rotation imparting mechanism in the present invention.

  As shown in FIGS. 1 and 5, the substrate portion 22 is formed in a plate shape that is long in the horizontal direction (for example, the X direction of the probe drive unit 16), and the spring probe 20 is fixed to one end portion in the long direction. At the same time, it is fixed to the probe fixing portion 16A of the probe driving unit 16 at a substantially central portion in the longitudinal direction. In this embodiment, the substrate portion 22 is formed by the two screws 30 penetrating the two through holes 22A (see FIG. 4) formed in parallel in the longitudinal direction at a substantially central portion in the longitudinal direction. It is fastened and fixed to the probe fixing portion 16A.

  A step portion 32 is formed at one end in the longitudinal direction of the substrate portion 22, and the barrel 24 of the spring probe 20 is fixed to the step portion 32 by a composite adhesive structure 34 as a fixing means. Specifically, as shown in FIG. 2, the stepped portion 32 has a first fixed surface 32 </ b> A that is an end surface in the thickness direction of the substrate portion 22, and a second fixed surface 32 </ b> B that faces one end side in the longitudinal direction.

  In this embodiment, as shown in FIG. 4A, the substrate portion 22 is configured by overlapping a first substrate portion 36 and a second substrate portion 38 having similar shapes in the thickness direction. . The substrate portion 22 is formed with a step portion 32 by projecting one end portion 36 </ b> A in the longitudinal direction of the first substrate portion 36 in the longitudinal direction with respect to the one end portion 38 </ b> A in the longitudinal direction of the second substrate portion 38.

  In the substrate part 22, the positions of the first substrate part 36 and the second substrate part 38 in the longitudinal direction other ends 36B, 38B are substantially the same. That is, the second substrate portion 38 is formed slightly shorter than the first substrate portion 36. In addition, the first substrate portion 36 and the second substrate portion 38 are formed with through holes 36C and 38C that form the through holes 22A. The through holes 36C and 38C are also used to temporarily hold the first substrate portion 36 and the second substrate portion 38 through the common screw 30 as will be described later. The second substrate portion 38 functions as a positioning reference.

  As described above, the first fixing surface 32A is the end surface in the plate thickness direction of the portion protruding from the longitudinal one end portion 38A of the second substrate portion 38 in the longitudinal one end portion 36A of the first substrate portion 36. The surface 32 </ b> B is a longitudinal end surface (plate thickness portion) of the longitudinal direction one end portion 38 </ b> A of the second substrate portion 38. That is, it can be understood that the stepped portion 32 of the substrate portion 22 forms a space opened on one end side in the longitudinal direction and one side in the plate thickness direction. Further, the width (width along the longitudinal direction of the substrate portion 22) W1 of the first fixed surface 32A is equal to or slightly larger than the outer diameter D of the barrel 24, and the width (substrate portion) of the second fixed surface 32B. The width 22 along the thickness direction 22 is equal to or slightly larger than the outer diameter of the barrel 24.

  Moreover, in this embodiment, it is grasped | ascertained that the step part 32 is formed over the full width of the width direction (vertical direction) of the board | substrate part 22, and forms the space opened on both upper and lower sides. Can do. The spring probe 20 is disposed so as to occupy (penetrate vertically) the space formed by the step portion 32.

  The first substrate portion 36 and the second substrate portion 38 constituting the substrate portion 22 described above are substrates with glass cloth, which is a printed board material, more specifically, FR4 grade (according to National Electric Industry Standard (NEMA)). It is comprised by the heat resistant glass base material epoxy resin laminated board of this.

  The substrate portion 22 has both the first fixed surface 32A and the second fixed surface 32B of the stepped portion 32 bonded via an adhesive layer 34A, and the bonded portion by the adhesive layer 34A is covered as a covering adhesive layer. It is covered with an adhesive layer 34B. That is, in this embodiment, the adhesive layer 34 </ b> A and the covering adhesive layer 34 </ b> B constitute the composite adhesive structure 34.

  More specifically, the adhesive layer 34A is formed by curing an adhesive whose main component is cyanoacrylate (for example, “Aron Alpha Extra 4000” manufactured by Konishi Co., Ltd.). The covering adhesive layer 34B is obtained by curing an adhesive mainly composed of an epoxy resin and a curing agent mainly composed of polythiol (for example, trade name “High Super 30” manufactured by Cemedine Co., Ltd.). . In this embodiment, the cyanoacrylate adhesive forming the adhesive layer 34A penetrates between the first substrate portion 36 and the second substrate portion 38 on one end side in the longitudinal direction of the substrate portion 22, and the first substrate portion 36. This also contributes to fixing the second substrate portion 38 to the second substrate portion 38.

  Further, as shown in FIG. 1, in the contact probe assembly 10, the spring probe 20 is fixed to the substrate portion 22 at a predetermined angle θ with respect to the vertical direction (Z direction driven by the probe drive unit 16). Yes. That is, the step portion 32 of the substrate portion 22 is formed to be inclined by a predetermined angle θ with respect to the vertical direction. The predetermined angle θ does not interfere with each other when the two contact probe assemblies 10 of the flying inspection apparatus 11 come into contact with the adjacent inspection points, and the smooth advance / retreat (stroke) of the plunger 25 with respect to the barrel 24 is ensured. It is set as a value, and is approximately 8 ° in this embodiment.

  The substrate portion 22 constituting the contact probe assembly 10 has one end portion in the longitudinal direction protruding most downward in the vertical direction. In this embodiment, the lower edge 22B of the substrate portion 22 (the first substrate portion 36 and the second substrate portion 38) is formed in an arc shape. The shape of the lower edge 22B is determined so as not to interfere with the screen 14C when the spring probe 20 is brought into contact with the inspection point close to the screen 14C (the plunger 25 is stroked so as to be pushed into the barrel 24). (See FIG. 7B). The barrel 24 of the spring probe 20 has its lower end (opening end 24A) aligned with the lower edge 22B (lower protruding end) of the substrate part 22 or slightly protrudes downward. It is being fixed to the step part 32.

(Manufacturing method of contact probe assembly)
Next, the manufacturing method (procedure) of the contact probe assembly 10 demonstrated above is demonstrated based on FIG. In FIG. 4A, the main part of the contact probe assembly 10 is shown in an exploded perspective view. As shown in this figure, in manufacturing the contact probe assembly 10, first, the first substrate portion 36 and the second substrate portion 38 are temporarily fixed by the screws 30 and the nuts 40 (substrate portion temporary fixing step). . Thereby, the board | substrate part 22 which has the step part 32 in the one end part of a longitudinal direction is temporarily formed.

  Next, as shown in FIG. 4B, the substrate portion 22 is held so that the second fixing surface 32 </ b> B faces the upper side in the vertical direction, and a few drops of cyanoacrylate adhesive are dropped on the step portion 32. Thereafter, the spring probe 20 is set on the step portion 32 so that the adhesive is interposed between the first fixing surface 32A and the second fixing surface 32B (probe bonding step). Then, after the cyanoacrylate adhesive is cured and the adhesive layer 34A is formed, the epoxy resin-polythiol adhesive is covered with the adhesive layer 34A as shown in FIG. 4C. Apply (bonding part reinforcing step).

  When the epoxy resin-polythiol adhesive is cured, the spring probe 20 is fixed to the step portion 32 of the substrate portion 22 by the composite adhesive structure 34. Also, the cyanoacrylate adhesive that has permeated between the first substrate portion 36 and the second substrate portion 38 in the probe bonding step is cured, so that the first substrate portion 36 and the second substrate portion 38 is fixed. As a result, the contact probe assembly 10 can be handled, stored, etc. in a state where the fastening by the screw 30 and the nut 40 is released. In use, the screw 30 is again fastened and fixed to the probe fixing portion 16 </ b> A of the probe driving unit 16.

  Next, the operation of the embodiment will be described.

  In the flying inspection apparatus 11 to which the contact probe assembly 10 having the above configuration is applied, when the printed circuit board 12 is inspected, first, it is positioned on the substrate placement surface 14A of the suction table 14 by the partitioning portion 14C. The printed circuit board 12 is set. Next, the cover material 18 is put on the printed circuit board 12, and the suction table 14 suction device is started. Then, in the flying inspection apparatus 11, the printed circuit board 12 is adsorbed on the substrate mounting surface 14A together with the cover material 18 by evacuation through the plurality of suction holes 14B. The cover material 18 closes the gap on the periphery of the printed circuit board 12, so that the printed circuit board 12 is brought into close contact with the substrate mounting surface 14A without being floated.

  When each probe driving unit 16 is activated from this state, each probe driving unit 16 moves the spring probe 20 above the plurality of inspection points by the horizontal driving unit, and contacts the spring probe 20 to the inspection point by the vertical driving unit (contact). ) Specifically, when the contact probe assembly 10 is moved downward (to the printed circuit board 12 side) by the vertical drive unit of the probe drive unit 16, first, the distal end portion 25A hits the cover member 18, and the contact probe assembly 10 is further moved downward. The plunger 25 is pushed into the barrel 24 while rotating around its own axis.

  Due to the rotation of the plunger 25 and the increase in the pressing force accompanying the increase in the compression amount of the spring 26, the plunger 25 penetrates the cover material 18 and contacts the inspection point of the printed circuit board 12. Thereby, an inspection point and the measurement part of the flying inspection apparatus 11 are conduct | electrically_connected, and the quality of the conductor pattern of the printed circuit board 12 is determined. The flying inspection apparatus 11 repeats the above operation for the number of inspection points.

  Here, since the contact probe assembly 10 constituting the flying inspection apparatus 11 has a structure in which the spring probe 20 is fixed to the step portion 32 of the substrate portion 22, high durability performance can be obtained. For example, as a comparative example having the same size and shape as the contact probe assembly 10, between a portion holding a needle-like probe on a resin plate and a portion fixed to the probe fixing portion 16 </ b> A of the probe driving unit 16. The structure which sets a leaf | plate spring part can be considered. If it demonstrates by comparison with this comparative example, in this comparative example, it is confirmed that durability is low (approximately 20,000 times-30,000 times in a test | inspection point) by the fatigue failure of a leaf | plate spring part.

  On the other hand, in the contact probe assembly 10 that employs the spring probe 20 incorporating the spring 26, the plate spring portion is not set on the substrate portion 22, so there is no fear of fatigue failure of the substrate portion 22. In addition, since the barrel 24 of the spring probe 20 is bonded to each of the first fixing surface 32A and the second fixing surface 32B of the step portion 32 of the substrate portion 22 that is a substrate containing FR4 grade glass cloth, The holding strength of the spring probe 20 is high. In addition, the barrel 24 of the spring probe 20 is fixed to the stepped portion 32 of the substrate portion 22 by the composite adhesive structure 34 including the adhesive layer 34A and the covering adhesive layer 34B. Since the covering adhesive layer 34 </ b> B covers (protects and reinforces), the holding strength of the spring probe 20 with respect to the substrate portion 22 is further increased.

  From the above, it was confirmed that the contact probe assembly 10 showed high durability of 8 million times or more in the number of repeated inspections. In the configuration in which the spring probe 20 is bonded to the substrate portion 22 with the adhesive layer 34A or the covering adhesive layer 34B alone (configuration included in the present invention), it is confirmed that the number of repeated inspections is 1 million times to 2 million times. However, the durability is remarkably improved (synergistically) by employing the composite adhesive structure 34 including the adhesive layer 34A and the covering adhesive layer 34B. I understand that.

  As described above, in the contact probe assembly 10 to which the flying inspection contact probe holding structure according to the present embodiment is applied, durability against repeated contact with a large number of inspection points can be ensured. Further, since the spring probe 20 is fixed to the substrate portion 22 by the composite adhesive structure 34 in a posture inclined with respect to the vertical direction, the composite adhesive structure 34 is not purely sheared due to repeated contact with a large number of inspection points. The peeling load also acts as a component force. This configuration also contributes to securing the holding strength (durability) of the spring probe 20 with respect to the substrate portion 22. It has been confirmed that the durability decreases when the angle θ formed by the spring probe 20 with respect to the vertical direction exceeds 10 °, and the two contact probe assemblies 10 interfere with each other when θ is less than 8 °. There is a risk.

  Further, in the resin plate having the leaf spring portion according to the comparative example, the leaf spring portion may be displaced in the horizontal direction, and the inspection point may be shifted. On the other hand, the contact probe assembly 10 has a configuration in which the spring probe 20 is fixed to the high-rigidity substrate portion 22, so that the spring probe 20 can be reliably brought into contact with a required inspection point.

  Furthermore, since the resin plate having the leaf spring portion according to the comparative example is formed by injection molding, the manufacturing cost is high particularly in the case of small-volume production. On the other hand, the contact probe assembly 10 can form the substrate part 22 (first substrate part 36, second substrate part 38) by machining a glass cloth-containing substrate. It can be manufactured at low cost. In particular, in the contact probe assembly 10, the first substrate portion 36 and the second substrate portion 38 are overlapped to form the substrate portion 22, and therefore, by simple machining and overlapping work (temporary holding with screws 30 and nuts 40). The substrate part 22 having the step part 32 can be obtained. Thereby, the contact probe assembly 10 can be manufactured at a very low cost in the case of small-volume production. Moreover, in the contact probe assembly 10, since the first substrate portion 36 and the second substrate portion 38 are overlapped to form the substrate portion 22, the stepped portion 32 can be formed with high accuracy.

  Furthermore, in the contact probe assembly 10, the first substrate 36 </ b> A is protruded from the second substrate portion 38 having the same thickness as the outer diameter of the barrel 24 by projecting the one end 36 </ b> A in the longitudinal direction by the same amount as the outer diameter of the barrel 24. Since the portion 36 is superposed, the board portion 22 is thin. Thereby, the contact probe assembly 10 can be made compact.

  In the contact probe assembly 10, the formation portion (one end portion in the longitudinal direction) of the step portion 32 to which the spring probe 20 is fixed in the substrate portion 22 protrudes downward with respect to the other portions. Interference between the edge 22B and the partition 14C is avoided. In addition, since the lower edge 22B of the substrate portion 22 has an arc shape, the substrate portion 22 has a cross-section (cross-section) in a configuration in which the formation portion of the stepped portion 32 protrudes downward with respect to other portions as described above. A sudden change part of the coefficient etc. is not formed. Thereby, it is easy to ensure the strength (fatigue strength) of the substrate portion 22 alone, which contributes to ensuring the durability as the contact probe assembly 10.

  Further, since the contact probe assembly 10 employs the spring probe 20 in which the plunger 25 is rotated as the barrel 24 advances and retreats, the plunger 25 penetrates the cover material 18 covering the printed circuit board 12 and serves as an inspection point. The spring probe 20 can be conducted. Moreover, since the distal end portion 25A of the plunger 25 has a substantially equilateral triangular pyramid shape, the ability to penetrate the cover member 18 by the plurality of edges 25B is maintained even if the distal end portion 25A is rounded by repeated contact with the inspection point. . In the contact probe assembly 10, it has been confirmed that the printed circuit board 12 covered with the cover material 18 achieves the above-described number of repeated inspections (durability) of 8 million times or more. In the comparative example in which the probe does not rotate, it has been confirmed that the cover material 18 cannot be penetrated.

  Since the flying inspection apparatus 11 includes the contact probe assembly 10 that can ensure durability against repeated contact with a large number of inspection points, the flying inspection apparatus 11 has high reliability. Moreover, the running cost of the flying inspection apparatus 11 is reduced. Further, since the flying inspection apparatus 11 is configured to adsorb the cover material 18 together with the printed circuit board 12 to the substrate mounting surface 14A of the suction table 14, it is possible to prevent or effectively lift the printed circuit board 12 from the substrate mounting surface 14A. Can be suppressed. Thereby, since the spring probe 20 contacts each inspection point in the printed circuit board 12 accurately, the reliability with respect to inspection (accuracy) is improved. In particular, a configuration (inspection method) using the cover material 18 in the inspection of the flexible substrate is effective.

  Since the plunger 25 of the spring probe 20 rotates with the stroke as described above, the spring probe 20 can be reliably brought into contact with the inspection point of the printed circuit board 12 in the configuration using the cover material 18 (inspection method). . Further, since the cover material 18 is made of a polyethylene sheet that does not have a uniaxially stretched structure, the cover material 18 can be torn in a specific direction with the penetration of the plunger 25 like a cover material made of silicon rubber, for example. In other words, the function of closely contacting the substrate placement surface 14A of the printed circuit board 12 without floating until the inspection is completed is maintained.

  In the above-described embodiment, an example in which the outer diameter D of the barrel 24 is approximately 0.48 mm has been shown. However, the present invention is not limited to this, and the spring probe 20 having a size according to the application can be adopted. Needless to say. Further, for example, in a configuration that does not use the cover material 18 (a flying inspection device, an inspection method), a spring probe in which the plunger does not rotate around its own axis may be used.

  In the above-described embodiment, the example in which the substrate unit 22 is formed by superimposing the first substrate unit 36 and the second substrate unit 38 has been shown. However, the present invention is not limited to this, and for example, a single plate It is good also as a structure which forms the step part 32 in an edge part. However, when the substrate unit 22 is configured with an FR4 grade glass cloth-containing substrate, it is desirable to adopt superposition of the first substrate unit 36 and the second substrate unit 38 in consideration of workability. The substrate portion 22 may be formed by injection molding of resin (including those impregnated with fibers or cloth).

  Furthermore, in the above-described embodiment, the flying inspection apparatus 11 has shown an example of inspecting the quality of the conductor pattern based on the capacitance between the conductor pattern formed on the printed circuit board 12 to be inspected and the reference electrode. The present invention is not limited to this. For example, the present invention may be applied to the flying inspection apparatus 11 that directly contacts the spring probe 20 from the front and back of the printed circuit board 12 to inspect continuity.

10 Contact probe assembly (contact probe holding structure for flying inspection)
11 Flying inspection device 12 Printed circuit board (circuit board)
14 Suction table (substrate holder)
16 Probe drive unit (probe drive mechanism)
18 Cover material 20 Spring probe 22 Substrate part 24 Barrel (cylinder)
25 Plunger (Contact)
26 Spring (biasing member)
32 steps 32A first fixing surface 32B second fixing surface 34 composite adhesive structure (fixing means)
34A Adhesive Layer 34B Cover Adhesive Layer 36 First Substrate Part 38 Second Substrate Part

Claims (10)

A needle-like contact whose one end is in contact with the inspection point, a cylinder inserted at the other end of the contact so as to be able to advance and retreat, and an attachment for shifting the contact to a movement limit in the protruding direction with respect to the cylinder A spring probe including a biasing member;
A step portion having a first fixed surface facing the thickness direction and a second fixed surface facing the longitudinal direction is formed along the width direction by thinning one end in the longitudinal direction, and the spring probe is moved to the inspection point. A substrate portion fixed to a moving means for
Fixing means for fixing the cylindrical body of the spring probe to each of the first fixing surface and the second fixing surface in the step portion of the substrate portion;
A contact probe holding structure for flying inspection.   The fixing means includes an adhesive layer interposed between the cylindrical body and each of the first fixing surface and the second fixing surface, and a covering that covers an adhesive site between the cylindrical body and the stepped portion by the adhesive layer. The contact probe holding structure for flying inspection according to claim 1, comprising an adhesive layer.   The substrate portion is formed by superimposing a first substrate portion and a second substrate portion, and the position of the one end of the first substrate portion and the second substrate portion is offset in the longitudinal direction. The flying probe contact probe holding structure according to claim 1 or 2, wherein the flying probe contact probe holding structure is formed. The first fixing surface is an end surface in the thickness direction of the first substrate protruding toward one end side in the longitudinal direction by an amount corresponding to the diameter of the cylindrical body with respect to the longitudinal end portion of the second substrate portion.
4. The flying inspection contact probe holding structure according to claim 3, wherein the second fixing surface is a longitudinal end surface of the second substrate portion having a thickness corresponding to the diameter of the cylindrical body.   5. The flying inspection according to claim 1, wherein the substrate portion has a shape in which an edge portion on the inspection point side protrudes most toward the inspection point side at one end in the longitudinal direction. Contact probe holding structure.   6. The flying inspection contact probe holding structure according to claim 5, wherein an edge of the substrate portion on the inspection point side has an arc shape.   7. The flying inspection contact according to claim 1, wherein the spring probe has a rotation imparting mechanism that rotates the contact member around its own axis as the contact member advances and retreats with respect to the cylindrical body. Probe holding structure. A substrate holding unit for holding the substrate to be inspected by suction;
A probe for holding the flying inspection contact probe holding structure according to any one of claims 1 to 7 on the substrate portion, and sequentially contacting a contact of the spring probe to a plurality of inspection points on the substrate to be inspected. A drive mechanism;
A circuit board flying inspection apparatus comprising: A substrate holding unit for adsorbing and holding a substrate to be inspected together with a sheet-like cover material;
A probe drive mechanism that holds the flying inspection contact probe holding structure according to claim 7 in the substrate portion, and sequentially contacts a contact of the spring probe with a plurality of inspection points on the substrate to be inspected.
A circuit board flying inspection apparatus comprising:   The circuit board flying inspection apparatus according to claim 9, wherein the cover material is a sheet material made of unstretched or biaxially stretched polyethylene.

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