Joining method
10173370 ยท 2019-01-08
Assignee
Inventors
- Yasuhiro Ueno (Miyoshi, JP)
- Takaaki Kiyono (Okazaki, JP)
- Toyokazu Hirota (Okazaki, JP)
- Koichi Inazawa (Miyoshi, JP)
- Tatsuro Nakata (Toyota, JP)
Cpc classification
B29C66/73116
PERFORMING OPERATIONS; TRANSPORTING
B29C65/02
PERFORMING OPERATIONS; TRANSPORTING
B23K2103/42
PERFORMING OPERATIONS; TRANSPORTING
B29K2267/00
PERFORMING OPERATIONS; TRANSPORTING
B29K2033/08
PERFORMING OPERATIONS; TRANSPORTING
B29C66/41
PERFORMING OPERATIONS; TRANSPORTING
B29K2067/003
PERFORMING OPERATIONS; TRANSPORTING
B29K2071/12
PERFORMING OPERATIONS; TRANSPORTING
B29C65/06
PERFORMING OPERATIONS; TRANSPORTING
B29K2277/00
PERFORMING OPERATIONS; TRANSPORTING
B29K2079/00
PERFORMING OPERATIONS; TRANSPORTING
B23K20/1255
PERFORMING OPERATIONS; TRANSPORTING
B29C66/7392
PERFORMING OPERATIONS; TRANSPORTING
B29C66/21
PERFORMING OPERATIONS; TRANSPORTING
B29K2059/00
PERFORMING OPERATIONS; TRANSPORTING
B29K2031/04
PERFORMING OPERATIONS; TRANSPORTING
B29K2071/00
PERFORMING OPERATIONS; TRANSPORTING
B29K2077/00
PERFORMING OPERATIONS; TRANSPORTING
B29C66/7212
PERFORMING OPERATIONS; TRANSPORTING
B29K2025/08
PERFORMING OPERATIONS; TRANSPORTING
B29K2081/04
PERFORMING OPERATIONS; TRANSPORTING
B29C65/7841
PERFORMING OPERATIONS; TRANSPORTING
B29C66/71
PERFORMING OPERATIONS; TRANSPORTING
B29K2267/00
PERFORMING OPERATIONS; TRANSPORTING
B29K2079/085
PERFORMING OPERATIONS; TRANSPORTING
B29K2075/00
PERFORMING OPERATIONS; TRANSPORTING
B21D39/032
PERFORMING OPERATIONS; TRANSPORTING
B29K2069/00
PERFORMING OPERATIONS; TRANSPORTING
B29C66/81431
PERFORMING OPERATIONS; TRANSPORTING
B29K2311/10
PERFORMING OPERATIONS; TRANSPORTING
B29K2031/04
PERFORMING OPERATIONS; TRANSPORTING
B29K2081/06
PERFORMING OPERATIONS; TRANSPORTING
B29C66/45
PERFORMING OPERATIONS; TRANSPORTING
B29K2079/085
PERFORMING OPERATIONS; TRANSPORTING
B29C65/608
PERFORMING OPERATIONS; TRANSPORTING
B29K2033/08
PERFORMING OPERATIONS; TRANSPORTING
B29K2079/00
PERFORMING OPERATIONS; TRANSPORTING
B23K20/22
PERFORMING OPERATIONS; TRANSPORTING
B29K2027/16
PERFORMING OPERATIONS; TRANSPORTING
B29K2067/006
PERFORMING OPERATIONS; TRANSPORTING
B29K2305/00
PERFORMING OPERATIONS; TRANSPORTING
B29K2059/00
PERFORMING OPERATIONS; TRANSPORTING
B29K2071/12
PERFORMING OPERATIONS; TRANSPORTING
B29K2081/04
PERFORMING OPERATIONS; TRANSPORTING
B29K2067/00
PERFORMING OPERATIONS; TRANSPORTING
B23K20/127
PERFORMING OPERATIONS; TRANSPORTING
B21J15/027
PERFORMING OPERATIONS; TRANSPORTING
B29C66/8322
PERFORMING OPERATIONS; TRANSPORTING
B29C65/64
PERFORMING OPERATIONS; TRANSPORTING
B29K2027/16
PERFORMING OPERATIONS; TRANSPORTING
B29C66/7394
PERFORMING OPERATIONS; TRANSPORTING
F16B5/08
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B29K2063/00
PERFORMING OPERATIONS; TRANSPORTING
B29K2067/006
PERFORMING OPERATIONS; TRANSPORTING
B29K2055/02
PERFORMING OPERATIONS; TRANSPORTING
B29K2311/10
PERFORMING OPERATIONS; TRANSPORTING
B29K2067/003
PERFORMING OPERATIONS; TRANSPORTING
B29K2077/00
PERFORMING OPERATIONS; TRANSPORTING
B29K2081/06
PERFORMING OPERATIONS; TRANSPORTING
B29K2277/00
PERFORMING OPERATIONS; TRANSPORTING
B29C66/1122
PERFORMING OPERATIONS; TRANSPORTING
B29K2025/08
PERFORMING OPERATIONS; TRANSPORTING
B29K2033/12
PERFORMING OPERATIONS; TRANSPORTING
B29K2075/00
PERFORMING OPERATIONS; TRANSPORTING
B29K2069/00
PERFORMING OPERATIONS; TRANSPORTING
B29C66/71
PERFORMING OPERATIONS; TRANSPORTING
B29C65/606
PERFORMING OPERATIONS; TRANSPORTING
B29C66/72143
PERFORMING OPERATIONS; TRANSPORTING
B29K2067/00
PERFORMING OPERATIONS; TRANSPORTING
B29C66/7212
PERFORMING OPERATIONS; TRANSPORTING
B29K2071/00
PERFORMING OPERATIONS; TRANSPORTING
F16B5/045
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B29K2305/00
PERFORMING OPERATIONS; TRANSPORTING
B29K2055/02
PERFORMING OPERATIONS; TRANSPORTING
B29K2033/12
PERFORMING OPERATIONS; TRANSPORTING
B29K2063/00
PERFORMING OPERATIONS; TRANSPORTING
International classification
B32B37/00
PERFORMING OPERATIONS; TRANSPORTING
B29C65/02
PERFORMING OPERATIONS; TRANSPORTING
B23K20/12
PERFORMING OPERATIONS; TRANSPORTING
B29C65/06
PERFORMING OPERATIONS; TRANSPORTING
B21D39/03
PERFORMING OPERATIONS; TRANSPORTING
B29C65/64
PERFORMING OPERATIONS; TRANSPORTING
B29C65/78
PERFORMING OPERATIONS; TRANSPORTING
B29C65/00
PERFORMING OPERATIONS; TRANSPORTING
B21K25/00
PERFORMING OPERATIONS; TRANSPORTING
B23K20/22
PERFORMING OPERATIONS; TRANSPORTING
F16B5/08
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16B5/04
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Abstract
A joining method for joining a first member having a hole that is opened on at least one surface, to a second member including a material of which a melting temperature is lower than that of a constituent material of the first member, includes: laminating the second member on the first member so as to cover an opening of the hole; and introducing that material of the second member which is softened or melted into the hole through the opening and curing the material of the second member.
Claims
1. A joining method for joining a first member having a hole that is opened on at least one surface, to a second member made of a fiber reinforced resin member configured such that a fiber material is mixed in resin of which melting temperature is lower than that of a constituent material of the first member, the joining method comprising: laminating the second member on the first member so as to cover a first opening of the hole; orienting the fiber material contained in the second member in a laminating direction while softening or melting of the resin of the second member above the first opening of the hole; introducing the fiber reinforced resin member resin mixed with the resin softened or melted into the hole through the first opening by pushing the fiber reinforced resin member resin; and curing the resin introduced into the hole.
2. The joining method according to claim 1, wherein: the second member includes the fiber material whose length is longer than a diameter of the first opening of the hole.
3. The joining method according to claim 1, wherein: the hole of the first member has a reduced diameter portion reduced in diameter continuously or in a stepped manner toward the first opening.
4. The joining method according to claim 3, wherein: a sectional area of the hole of the first member along a direction perpendicular to the laminating direction is minimized at the first opening.
5. The joining method according to claim 1, wherein: the hole of the first member is formed so as to penetrate from the one surface to the other surface opposite to the one surface.
6. The joining method according to claim 5, wherein: a backing member configured to cover a second opening of the hole which is formed on the other surface is disposed.
7. The joining method according to claim 6, wherein: the backing member includes a depression communicating with the hole via the second opening of the hole which is formed on the other surface and configured such that a sectional area of the depression along the direction perpendicular to the laminating direction is larger than that of the second opening on the other surface; and in the introducing and curing of the resin of the second member, the resin of the second member is introduced into the depression as well as the hole, and then cured.
8. The joining method according to claim 1, wherein: in the introducing and curing of the resin of the second member, the resin of the second member is softened or melted by use of frictional heat.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
(1) Features, advantages, and technical and industrial significance of exemplary embodiments of the invention will be described below with reference to the accompanying drawings, in which like numerals denote like elements, and wherein:
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DETAILED DESCRIPTION OF EMBODIMENTS
(47) With reference to drawings, the following describes embodiments of a joining method of the present invention.
(48) [Embodiment 1]
(49)
(50) <Joining Apparatus Used in Embodiment 1 of Joining Method of Present Invention>
(51) The joining method according to Embodiment 1 of the present invention is performed by use of a joining apparatus including a heater. The joining apparatus 30 mainly includes a heater 31, and a clamping member 34, as illustrated in
(52) The heater 31 and the clamping member 34 configured as such include an abutting surface 31a and an abutting surface 34a, respectively. The abutting surface 34a of the clamping member 34 is moved by a drive mechanism (not shown) in an axis-Xr direction so as to abut with the one surface of the workpiece. The abutting surface 31a of the heater 31 is moved by a drive mechanism (not shown) in the axis-Xr direction to a slightly upper side of the one surface of the workpiece.
(53) <Joining Method Using Joining Apparatus>
(54) Next will be generally described the joining method using the joining apparatus 30 according to Embodiment 1, with reference to
(55) The joining method according to Embodiment 1 mainly includes a laminating step, a softening-melting/introducing step, and a curing step.
(56) First, in the laminating step, the second member 2 is laminated on the first member 1 so as to cover an opening 3a of the hole 3 provided in the first member 1, as illustrated in
(57) Then, in the softening-melting/introducing step, a constituent material of the second member 2, particularly a constituent material of that part of the second member 2 which is placed on the hole 3 of the first member 1 is softened or melted by use of heat of the heater 31, as illustrated in
(58) Further, in the curing step, as illustrated in
(59) Thus, the joining method of Embodiment 1 is performed such that: the second member 2 is laminated on the first member 1 so as to cover the opening 3a of the hole 3 provided in the first member 1; the constituent material of that part of the second member 2 which is placed on the opening 3a of the hole 3 is locally softened or melted by use of heat of the heater 31; the softened or melted constituent material 2c of the second member 2 is introduced into the hole 3 of the first member 1 through the opening 3a of the hole 3; and the constituent material 2c of the second member 2 thus introduced into the hole 3 is cured. This makes it possible to easily join the first member 1 and the second member 2, which are different type of members, at low cost.
(60) [Embodiment 2]
(61)
(62) <Friction Stir Welding Apparatus Used in Embodiment 2 of Joining Method of Present Invention>
(63) The joining method according to Embodiment 2 of the present invention is performed by use of a single acting friction stir welding apparatus as an example of a friction stir welding apparatus. On that account, initially, the following generally describes an example of the single acting friction stir welding (FSW) apparatus used in the joining method according to Embodiment 2, with reference to
(64) As illustrated in
(65) The rotating tool portion 41 has a generally circular column shape. The rotating tool portion 41 is configured to be rotated by the drive mechanism (not shown) around an axis (a rotating axis) Xr and to be slidable relative to the clamping member 44 along a direction of a broken-line arrow Q1, that is, an axis-Xr direction (an up-down direction in
(66) The clamping member 44 is provided outside the rotating tool portion 41 and has a generally cylindrical shape having a hollow. The rotating tool portion 41 is inserted into the hollow. The clamping member 44 is supported by the support member (not shown) via the spring 43, so as to press a workpiece (a second member 2) from one surface (a top face in
(67) The rotating tool portion 41 and the clamping member 44 configured as such include abutting surfaces 41a, 44a, respectively. The abutting surfaces 41a, 44a are moved by the drive mechanism (not shown) in the axis-Xr direction so as to abut with the one surface of the workpiece.
(68) Note that a specific configuration of the single acting friction stir welding (FSW) apparatus 40 in the present embodiment is not limited to the above configuration, and may include other members, which are not described in terms of the FSW apparatus 40.
(69) <Joining Method Using Friction Stir Welding Joining Apparatus>
(70) Next will be generally described the joining method using the FSW apparatus 40 according to Embodiment 2, with reference to
(71) Similarly to the joining method according to Embodiment 1, the joining method according to Embodiment 2 mainly includes a laminating step, a softening-melting/introducing step, and a curing step.
(72) First, in the laminating step, the second member 2 is laminated on the first member 1 so as to cover an opening 3a of a hole 3 provided in the first member 1, as illustrated in
(73) Then, in the softening-melting/introducing step, the rotating tool portion 41 is rotated around the axis Xr, so that a constituent material of the second member 2, particularly a constituent material of that part of the second member 2 which is placed on the hole 3 of the first member 1 is softened or melted by use of frictional heat generated between the abutting surface 41a of the rotating tool portion 41 and the top face 2a of the second member 2, as illustrated in
(74) Further, in the curing step, as illustrated in
(75) Thus, the joining method of Embodiment 2 is performed such that: the second member 2 is laminated on the first member 1 so as to cover the opening 3a of the hole 3 provided in the first member 1; the constituent material of that part of the second member 2 which is placed on the opening 3a of the hole 3 is locally softened or melted by use of frictional heat; the softened or melted constituent material 2c of the second member 2 is introduced into the hole 3 through the opening 3a of the hole 3 of the first member 1; and the constituent material 2c of the second member 2 thus introduced into the hole 3 is cured. This makes it possible to easily join the first member 1 and the second member 2, which are different type of members, at low cost.
(76) Further, in the joining method of Embodiment 2, the constituent material of that part of the second member 2 which is placed on the opening 3a of the hole 3 is softened or melted by use of frictional heat, thereby yielding such an advantage that the constituent material of the second member 2 can be more surely softened and melted.
(77) [Embodiment 3]
(78)
(79) <Friction Stir Welding Apparatus Used in Embodiment 3 of Joining Method of Present Invention>
(80) The joining method according to Embodiment 3 of the present invention is performed by use of a double acting friction stir welding apparatus as a typical example of a friction stir welding apparatus. On that account, initially, the following generally describes a typical example of the double acting friction stir welding (FSW) apparatus used in the joining method according to Embodiment 3, with reference to
(81) As illustrated in
(82) The rotating tool portion 51 is constituted by a pin member 11 and a shoulder member 12. The pin member 11 has a generally circular column shape. The pin member 11 is configured to be rotated by the drive mechanism (not shown) around an axis (a rotating axis) Xr and to be movable relative to the shoulder member 12 along a direction of a broken-line arrow P1, that is, an axis-Xr direction (an up-down direction in
(83) The clamping member 54 is provided outside the shoulder member 12 of the rotating tool portion 51 and has a generally cylindrical shape having a hollow, similarly to the shoulder member 12. The shoulder member 12 is inserted into the hollow. Accordingly, the shoulder member 12 having a generally cylindrical shape is placed on an outer periphery of the pin member 11, and the clamping member 54 having a generally cylindrical shape is placed on an outer periphery of the shoulder member 12. In other words, the clamping member 54, the shoulder member 12, and the pin member 11 have a nested structure in which they are placed coaxially. The clamping member 54 is supported by the support member (not shown) via the spring 53, so as to press a workpiece (a second member 2) from one surface (a top face in
(84) The pin member 11 and the shoulder member 12 constituting the rotating tool portion 51, and the clamping member 54 include an abutting surface 11a, an abutting surface 12a, and an abutting surface 54a, respectively. The abutting surfaces 11a, 12a, and 54a are moved by the drive mechanisms (not shown) in the axis-Xr direction so as to abut with the one surface of the workpiece.
(85) Note that the concrete configuration of the rotating tool portion 51 in the present embodiment is not limited to the configuration described above, and a well-known configuration in the field of FSW can be used appropriately. Further, the friction stir welding apparatus is not limited to the FSW apparatus 50 having the above configuration, and may have a configuration in which the clamping member 54 is provided outside the pin member 11, or may include other members, which are not described in terms of the FSW apparatus 50.
(86) <Joining Method Using Friction Stir Welding Apparatus>
(87) Next will be generally described the joining method using the FSW apparatus 50 according to Embodiment 3, with reference to
(88) The joining method according to Embodiment 3 mainly includes a laminating step, a softening-melting step, an introducing step, and a curing step.
(89) First, in the laminating step, the second member 2 is laminated on the first member 1 so as to cover an opening 3a of a hole 3 provided in the first member 1, as illustrated in
(90) Then, in the softening-melting step, the pin member 11 and the shoulder member 12 are rotated integrally around the axis Xr, so that a constituent material of the second member 2, particularly a constituent material of that part of the second member 2 which is placed on the hole 3 of the first member 1 is softened or melted by use of frictional heat generated between the abutting surfaces 11a, 12a of the pin member 11 and the shoulder member 12 and the top face 2a of the second member 2, as illustrated in
(91) Then, in the introducing step, as illustrated in
(92) Further, in the curing step, as illustrated in
(93) Thus, the joining method of Embodiment 3 is performed such that: the second member 2 is laminated on the first member 1 so as to cover the opening 3a of the hole 3 provided in the first member 1; the constituent material of that part of the second member 2 which is placed on the opening 3a of the hole 3 is locally softened or melted by use of frictional heat; the softened or melted constituent material 2c of the second member 2 is introduced into the hole 3 of the first member 1 through the opening 3a of the hole 3; and the constituent material 2c of the second member 2 thus introduced into the hole 3 is cured. This makes it possible to easily join the first member 1 and the second member 2, which are different type of members, at low cost.
(94) Note that a shape (a longitudinal sectional shape and a cross sectional shape) of the hole provided in the first member can be designed appropriately according to joining strength between the first member and the second member, and so on.
(95) For example, in the above embodiment, in order to obtain an anchor effect, the hole 3 provided in the first member 1 is continuously reduced in diameter toward the opening 3a on the one surface (the top face), so that a sectional area of the hole 3 along a direction perpendicular to a laminating direction (the axis-Xr direction) is minimized at the opening 3a. However, the following fact has been confirmed by the inventor(s): in such a case, a portion cured in the hole 3 of the first member 1 is broken from the second member 2 due to a taper angle or the like of the hole 3, so that the second member 2 may be detached from the first member 1 or a portion cured in the hole 3 of the first member 1 may be slipped off from the hole 3 due to elasticity or the like of the second member 2. In view of this, for example, as illustrated in
(96) Further, the hole provided in the first member may be formed by appropriately combining a reduced diameter portion reduced in diameter continuously or in a stepped manner toward the opening on the one surface (the top face), a linear portion having the same inside diameter in a thickness direction (a laminating direction) of the first member, and an enlarged diameter portion enlarged in diameter continuously or in a stepped manner toward the opening on the one surface (the top face). For example, as illustrated in
(97) Further, needless to say, a shape, in a plan view, of the opening of the hole provided in the first member may be a generally circular shape (see
(98) [Embodiment 4]
(99)
(100) Similarly to the joining method according to Embodiment 3 described above, the joining method according to Embodiment 4 mainly includes a laminating step, a softening-melting step, an introducing step, and a curing step.
(101) First, in the laminating step, the second member 2A is laminated on the first member 1A so as to cover an opening 3aA on a top face 1aA of the hole 3A provided in the first member 1A, as illustrated in
(102) Subsequently, the softening-melting step (see
(103) Thus, the joining method of Embodiment 4 is performed such that: the second member 2A is laminated on the first member 1A so as to cover the opening 3aA on the one surface 1aA of the hole 3A provided in the first member 1A; the constituent material of that part of the second member 2A which is placed on the opening 3aA of the hole 3A is locally softened or melted by use of frictional heat; a softened or melted constituent material 2cA of the second member 2A is introduced into the hole 3A through the opening 3aA of the hole 3A of the first member 1A; and the constituent material 2cA of the second member 2A thus introduced into the hole 3A is cured. This makes it possible to easily join the first member 1A and the second member 2A, which are different type of members, at low cost.
(104) Further, in the joining method of Embodiment 4, the hole 3A of the first member 1A is formed so as to penetrate from the one surface 1aA to the other surface 1bA. Accordingly, in the introducing step, the softened or melted constituent material 2cA of the second member 2A can be introduced into the hole 3A of the first member 1A while gas such as air and the like existing in the hole 3A of the first member 1A is being exhausted through the opening 3bA on the other surface 1bA of the hole 3A. This makes it possible to more tightly and strongly join the first member 1A to the second member 2A, thereby yielding such an advantage that joining strength between the first member 1A and the second member 2A can be increased more effectively.
(105) Note that, similarly to the joining method of Embodiment 3, a shape (a longitudinal sectional shape and a cross sectional shape) of the hole provided in the first member can be designed appropriately according to the joining strength between the first member and the second member, and so on in the joining method of Embodiment 4.
(106) That is, for example, as illustrated in
(107) Further, the hole provided in the first member may be formed by appropriately combining a reduced diameter portion reduced in diameter continuously or in a stepped manner toward the opening on the one surface (the top face), a linear portion having the same inside diameter in the thickness direction (a laminating direction) of the first member, an enlarged diameter portion enlarged in diameter continuously or in a stepped manner toward the opening on the one surface (the top face). For example, as illustrated in
(108) Further, for example, as illustrated in
(109) Further, needless to say, a shape, in a plan view, of the opening of the hole provided in the first member may be a generally circular shape, a generally elliptical shape, a generally elongated hole shape, a polygonal shape such as a square shape, or the like.
(110) [Embodiment 5]
(111)
(112) Similarly to the joining methods according to Embodiments 3, 4, the joining method according to Embodiment 5 mainly includes a laminating step, a softening-melting step, an introducing step, and a curing step.
(113) First, in the laminating step, the second member 2B is laminated on the first member 1B so as to cover an opening 3aB of the hole 3B provided in the first member 1B which opening 3aB is formed on the top face 1aB, as illustrated in
(114) Subsequently, the softening-melting step (see
(115) Further, in the curing step, as illustrated in
(116) Thus, the joining method of Embodiment 5 is performed in such a manner that: the second member 2B is laminated on the first member 1B so as to cover the opening 3aB, on the one surface 1aB, of the linear hole (through hole) 3B provided in the first member 1B; the backing member 55 is disposed on the other surface 1bB of the first member 1B so that the backing member 55 covers the opening 3bB, on the bottom face 1bB, of the hole 3B of the first member 1B and the depression 55a of the backing member 55 communicates with the hole 3B of the first member 1B; the constituent material of that part of the second member 2B which is placed on the opening 3aB of the hole 3B is locally softened or melted by use of frictional heat; the softened or melted constituent material 2cB of the second member 2B is introduced into the hole 3B of the first member 1B and the depression 55a of the backing member 55 through the opening 3aB of the hole 3B; and the constituent material 2cB of the second member 2B thus introduced into the hole 3B and the depression 55a of the backing member 55 is cured. This makes it possible to easily join the first member 1B and the second member 2B, which are different type of members, at low cost.
(117) Further, in the joining method of Embodiment 5, the linear hole (through hole) 3B is formed in advance in the first member 1B. In view of this, in comparison with the joining methods of Embodiments 3, 4, for example, it is possible to restrain a cost required for the machining of the hole 3B of the first member 1B, thereby yielding such an advantage that a remarkable increase in a manufacturing cost of a product manufactured hereby can be restrained.
(118) Further, for example, in the joining method of Embodiment 3, the hole 3 provided in the first member 1 is reduced in diameter continuously toward the opening 3a on the one surface (the top face), so that the sectional area of the hole 3 along the direction perpendicular to the laminating direction (the axis-Xr direction) is minimized at the opening 3a. In this case, if strength of the first member 1 is low or a thickness of the first member 1 is thin, for example, the opening 3a of the hole 3 may be deformed in the introducing step or the like illustrated in
(119) Note that, similarly to the joining methods of Embodiments 3, 4, a shape (a longitudinal sectional shape and a cross sectional shape) of the hole provided in the first member can be designed appropriately according to joining strength between the first member and the second member, and so on in the joining method of Embodiment 5. Further, a shape of the depression formed in the backing member disposed on the bottom face of the first member can be designed appropriately, provided that the backing member can be easily removed from the bottom face of the first member after the curing step, for example.
(120) Further, as illustrated in
(121) [Embodiment 6]
(122) Embodiments 1 to 5 deal with a configuration in which the first member and the second member having a generally flat shape are joined to each other. However, a shape of each of the members as a joining object can be set appropriately. In a case where the flat-shaped second member is used like Embodiments 1 to 5, when part of the second member is introduced into the hole or the like of the first member in the introducing step, a thickness in the part of the second member is decreased at the time of curing the softened or melted constituent material of the second member so as to join the first member to the second member. In view of this, if the second member includes an extra amount of the material corresponding to the part introduced into the hole or the like of the first member in advance, it is considered that the decrease in the thickness of the second member at the time of joining the first member to the second member can be restrained.
(123)
(124) Similarly to the joining methods according to Embodiments 3 to 5, the joining method according to Embodiment 6 mainly includes a laminating step, a softening-melting step, an introducing step, and a curing step.
(125) First, in the laminating step, the second member 2C is laminated on the first member 1C so that the second member 2C covers an opening 3aC, on the top face 1aC, of the hole 3C provided in the first member 1C and the projection 2dC of the second member 2C is placed generally above the hole 3C, as illustrated in
(126) Then, in the softening-melting step, the pin member 11 and the shoulder member 12 are integrally rotated around the axis Xr, so that a constituent material of the second member 2C including the projection 2dC is softened or melted by use of frictional heat generated between the abutting surfaces 11a, 12a of the pin member 11 and the shoulder member 12 and the top face of the projection 2dC of the second member 2C, as illustrated in
(127) Subsequently, the introducing step (see
(128) Thus, the joining method of Embodiment 6 is performed such that: the projection 2dC having generally the same volume as the hole 3C of the first member 1C is formed on the one surface (a surface opposite to the abutting surface with the first member 1C) 2aC of the second member 2C is formed; the constituent material of the second member 2C including the projection 2dC is softened or melted in the softening-melting step; and the constituent material of the second member 2C is introduced into the hole 3C and then cured. This makes it possible to surely restrain a decrease in the thickness of the second member 2C at the time when the first member 1C is joined to the second member 2C and to form the one surface 2aC of the second member 2C in a generally flush manner, so that a design characteristic and the like after the joining between the first member 1C and the second member 2C can be increased markedly.
(129) Note that the joining methods according to Embodiments 1 to 6 do not have a limit in types of the members as the joining object in particular. However, the inventor(s) have confirmed that it is preferable that the second member be made of a fiber reinforced resin member configured such that a fiber material is mixed in resin (matrix resin) of which a melting temperature is lower than the constituent material of the first member.
(130) More specifically, in a case where the second member is made of a fiber reinforced resin member configured such that a fiber material is mixed in resin (matrix resin) of which a melting temperature is lower than the constituent material of the first member, the fiber material included in the second member is oriented in a laminating direction (that is, a direction perpendicular to a lamination plane between the first member and the second member) in the vicinity of the opening of the hole (a region R in
(131) Particularly, in a case where a fiber length of the fiber material contained in the second member is larger than a diameter or the like of the opening of the hole of the first member, the fiber material contained in the second member is oriented surely in the laminating direction in the vicinity of the opening of the hole (that is, the fiber material oriented in the laminating direction is increased), thereby making it possible to more effectively increase the joining strength between the first member and the second member.
(132) Note that in a case where the second member is made of the fiber reinforced resin member, the resin (matrix resin) constituting the second member may be thermo setting resin or thermo plastic resin. Examples of the thermo setting resin include epoxy resin, phenolic resin, melamine resin, and the like. The thermo plastic resin may be, for example, one or more admixtures of polypropylene (PP), polyethylene (PE), polystyrene (PS), AS resin, ABS resin, polyvinylchloride (PVC), methacrylic resin, polyamide (PA), polyester, polyacetal (POM), polycarbonate (PC), polyethylene terephthalate (PET), polybutylene terephthalate (PBT), polymethyl methacrylate (PMMA), polyvinylidene fluoride, polyphenylene oxide, polyphenylene sulfide, poly ether ether ketone, liquid crystal polymer, polyetherimide, polyethersulfone, polyamideimide, thermoplastic epoxy resin, and the like. Further, copolymers mainly containing the thermo plastic resin, and graft resin and blend resin, e.g., an ethylene-vinyl chloride copolymer, a vinyl acetate-ethylene copolymer, a vinyl acetate-vinyl chloride copolymer, an urethane-vinyl chloride copolymer, acrylic acid modified polypropylene, maleic acid modified polyethylene, and the like can be also introduced.
(133) Further, the reinforcement fiber material constituting the second member may be, for example, one or more admixtures of ceramic fibers such as boron, alumina, silicon carbide, silicon nitride, and zirconia, inorganic fibers such as glass fiber and carbon fiber, metal fibers such as copper, steel, aluminum, and stainless, and organic fibers such as polyamide, polyester, and cellulose.
(134) Further, in Embodiments 1 to 6, in order to join the first member having a hole to the second member including the material of which a melting temperature is lower than that of the constituent material of the first member, the joining apparatus including a heater or the friction stir welding apparatus is used. However, any apparatus can be used provided that the constituent material of the second member can be softened or melted and the softened or melted constituent material of the second member can be introduced into the hole of the first member. The constituent material of the second member may be softened or melted by use of heat generation by supersonic vibration or by use of a hot plate heated in advance, or the like, instead of frictional heat. Further, similarly to Embodiments 1, 2, Embodiments 3 to 6 may be performed such that the second member is placed on the first member without using a pushdown force by an apparatus or the like, and the softened or melted constituent material of the second member is introduced into the hole of the first member only by gravity.
(135) Further, Embodiments 1, 2 deal with a configuration in which the first member is joined to the second member through a plurality of steps including the laminating step, the softening-melting/introducing step, and the curing step, and Embodiments 3 to 6 deal with a configuration in which the first member is joined to the second member through a plurality of steps including the laminating step, the softening-melting step, the introducing step, and the curing step. However, needless to say, the constituent material of the second member may be introduced into the hole of the first member through the opening of the hole while the constituent material is being softened or melted, and the constituent material of the second member may be cured in the hole of the first member while the constituent material is being introduced into the hole.
(136) Thus, the embodiments of the present invention have been described with reference to the drawings, but concrete configurations of the present invention are not limited to the above embodiments. Even if there are changes of design or the like within a range that does not deviate from a gist of the present invention, they are included in the present invention.