Vehicular interior member manufacturing method and airbag rupturing groove manufacturing method

Abstract

Provided are a vehicular interior member manufacturing method and an airbag rupturing groove manufacturing method which can form an airbag rupturing groove excellent in invisibility even in a vehicular interior member having a hard substrate layer, while performing a proper control of the thickness of the remainder of the airbag rupturing groove to be formed. The vehicular interior member manufacturing method is characterized by protruding a metal blade having an edge flattened at least partially against a forming face of the rupturing groove, from a back side of the vehicular interior member and partially into the skin layer wherein a thickness of the skin layer into which the metal blade has not protruded corresponds to a remaining thickness of the skin layer, and confirming whether or not the metal blade is detected at a second detecting position while the metal blade is not detected at a first detecting position.

Claims

1. A manufacturing method of a vehicular interior member having a hard substrate layer at a back side of the vehicular interior member, a skin layer to cover an exterior surface of said hard substrate layer, and an airbag rupturing groove formed in the vehicular interior member and configured to break during deployment of an airbag, wherein said airbag rupturing groove is formed by: providing a metal blade having flattened edge, protruding the edge of the metal blade from the back side of said vehicular interior member through the hard substrate layer and partially into said skin layer to form the rupturing groove, wherein a thickness of said skin layer into which said metal blade has not protruded corresponds to a remaining thickness of said skin layer, using a first eddy-current displacement sensor for confirming whether said metal blade is not detected at a first detecting position that corresponds to a minimum permissible value that is permitted as said remaining thickness of said skin layer, using a second eddy-current displacement sensor for confirming whether or not said metal blade is detected at a second detecting position that corresponds to a maximum permissible value that is permitted as said remaining thickness of said skin layer, wherein the first detecting position and the second detecting position are located at different positions in a thickness direction of said skin layer, and adjusting a height of the metal blade if the metal blade is not detected at both the first and second detecting positions or if the metal blade is detected at both the first and second detecting positions so that the metal blade achieves a specified height to be detected by the second eddy-current displacement sensor at the second detecting position and so as not to be detected by the first eddy-current displacement sensor at the first detecting position.

2. The method of claim 1, wherein the step of adjusting a height of the metal blade is carried out so that a penetration amount of the metal blade into the skin layer is decreased if the first eddy-current displacement sensor detects the metal blade at the first detecting position and if in the second eddy-current displacement sensor detects the metal blade at the second detecting position.

3. The method of claim 1, wherein the step of adjusting a height of the metal blade is carried out so that a penetration amount of the metal blade into the skin layer is increased if the first eddy-current displacement sensor does not detect the metal blade at the first detecting position and if in the second eddy-current displacement sensor does not detect the metal blade at the second detecting position.

4. The manufacturing method of claim 1, wherein the eddy-current displacement sensors are operated to detect the position of the metal blade without stopping protruding operations of the metal blade.

5. The manufacturing method of claim 4, wherein the eddy-current displacement sensors are operated to detect the position of the metal blade while moving the metal blade at a processing speed of at least 300 mm/sec.

6. The manufacturing method of claim 1 further comprising comparing an actual shape of the edge of the metal blade to an ideal shape of the edge of the metal blade after forming the airbag rupturing groove to determine whether the metal blade requires replacement.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

(1) FIG. 1 is a sectional view of the vehicle interior member having the airbag rupturing groove formed using the airbag rupturing groove forming apparatus in the present invention.

(2) FIGS. 2A and 2B are examples showing plane patterns of the formed airbag rupturing groove.

(3) FIG. 3 is a perspective view showing the configuration of the airbag rupturing groove forming apparatus in the first embodiment of the present invention.

(4) FIG. 4 is a top plan view showing structure of the airbag rupturing groove forming apparatus in the first embodiment of the present invention.

(5) FIG. 5 is a figure showing structure of the rupturing groove forming means fixedly mounted in the movement control robot.

(6) FIGS. 6A and 6B are figures showing the first metal blade detecting means and the second metal blade detecting means.

(7) FIGS. 7A and 7B are figures showing dispositions of the first metal blade detecting means and the second metal blade detecting means.

(8) FIGS. 8A and 8B are figures showing other dispositions of the first metal blade detecting means and the second metal blade detecting means.

(9) FIGS. 9A and 9B are figures showing still other dispositions of the first metal blade detecting means and the second metal blade detecting means.

(10) FIG. 10 is a figure showing disposition examples of two or more first metal blade detecting means and the second metal blade detecting means.

(11) FIGS. 11A and 11B are figures showing an airbag rupturing groove forming process in the interior member manufacturing method in the second embodiment of the present invention.

(12) FIGS. 12A and 12B are figures showing an airbag rupturing groove forming process in the interior member manufacturing method in the second embodiment of the present invention.

(13) FIG. 13 is a figure showing a process for inspecting the edge status of the metal blade in the interior member manufacturing method in the second embodiment of the present invention.

(14) FIG. 14 is a perspective view showing the configuration of the airbag rupturing groove forming apparatus in the third embodiment of the present invention.

(15) FIGS. 15A and 15B are figures showing structure of the metal blade provided in the airbag rupturing groove forming apparatus in the third embodiment of the present invention.

DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS

(16) The embodiment of the present invention or the airbag rupturing groove forming apparatus and the method for manufacturing the vehicular interior member will be specifically described in the following, with appropriately referring to figures. However, since the following embodiments just represent one aspect of the present invention, the following description should not limit the present invention, and an embodiment of the present invention is arbitrarily altered within the scope of the present invention.

(17) Note that, among each figure, the same reference number represents the same portion, and description thereof will be appropriately omitted.

(18) A vehicular interior member.

(19) At first, the structure of the vehicular interior member 40 having a formed airbag rupturing groove 49 which is an object of forming an airbag rupturing groove by the airbag rupturing groove forming apparatus of this embodiment will be described, with referring to FIG. 1. FIG. 1 shows a cross-sectional view of the position at which an airbag device 47 is accommodated in the vehicular interior member 40.

(20) In this embodiment, a vehicular interior member 40, which is the object of forming an airbag rupturing groove, is the interior member 40 comprising a hard substrate layer 45, a skin layer 41 to cover the exterior of the hard substrate layer 45, and a foam layer 43 disposed between the hard substrate layer 45 and the skin layer 41. The vehicular interior member 40 constitutes an instrument panel or a door panel which contains an air bag device 47.

(21) This interior member 40 is a molded article made of a resin material. The hard substrate layer 45 has large strength, retains a three-dimensional shape of the interior member 40, and has a mount for installing the air bag device 47. Also, the foam layer 43 is formed between the hard substrate layer 45 and the skin layer 41, and is comparatively soft. The foam layer 43 does not impede an airbag deployment, on one hand, it provides, on the other hand, pleasant touch and three-dimensional decorativeness. Also, the skin layer 41 in the interior member 40 has a decoration of a grain pattern (texture) or the like on its surface, and provides excellent feel of a material to an external appearance of an instrument panel or a door panel or the like.

(22) As for the interior member 40 which is the object of forming the airbag rupturing groove 49 in the present invention, the hard substrate layer 45 takes a role of retaining its three-dimensional shape of the interior member 40, and its strength is enhanced accordingly. Consequently, strength of the hard substrate layer 45 is larger than that of the skin layer 41 or the foam layer 43. Therefore, when an airbag rupturing groove 49 is formed, the hard substrate layer 45 is hard to cut in comparison with the skin layer 41 or the foam layer 43.

(23) Note, although examples of the interior member have three layer structure mentioned above, an interior member comprising only a hard substrate layer and a skin layer, which omitted a foam layer would be possible. Also, on the contrary, an interior member comprising a hard substrate layer, a skin layer and other layers including a foam layer and/or the like is possible.

(24) Also, the airbag rupturing groove 49 is formed from the back side of the interior member 40 as shown in FIG. 1. That is, since there is no airbag rupturing groove 49 on the exterior surface of the skin layer 41, its good invisibility of the interior member 40 is ensured. The airbag rupturing groove 49 is possible to be a solid line as shown in FIG. 2A, or it is possible to be a dotted line or a broken line as shown in FIG. 2B. In the case of an airbag rupturing groove forming apparatus in the first embodiment, the airbag rupturing groove forming apparatus is depicted as to constitute to forming an airbag rupturing groove of a broken line shape.

(25) Also, in case of the interior member 40 having the hard substrate layer 45, it is necessary that the airbag rupturing groove is formed all over the parts ruptured at an airbag deployment time in the hard substrate layer 45. On the contrary, as for the soft skin layer 41, if there is a part to be formed, which became impetus to rupture at an airbag deployment time, it is possible to rupture from that part. Therefore, as for forming the airbag rupturing grooves 49, it could be required that only one part of a rupturing groove reaches to the skin layer 41. However, in case of a flat pattern of the airbag rupturing groove 49 as shown in FIG. 2, it is preferred that the airbag rupturing groove 49 to reach to the skin layer 41 is formed at least one for every span of a line.

(26) Also, in the formed airbag rupturing grooves 49, it is preferred that a remaining thickness T until the external surface of the skin layer 41 is decided considering such as open-and-shut features of an airbag door, balance of invisibility, and mechanical strength or the like. It is preferred that T is a value within the range of 0.3 to 0.8 mm (millimeters). This is because when a remaining thickness of airbag rupturing grooves T is below 0.3 mm, there are cases that invisibility decreases and mechanical strength of the skin layer 41 significantly decreases. On the contrary, this is because when a remaining thickness of airbag rupturing grooves T is over 0.8 mm, there are cases that open-and-shut features significantly decrease.

(27) Therefore, it is more preferred that a remaining thickness of airbag rupturing grooves T is a value within the range of 0.4 to 0.7 mm, and it is much more preferred that a remaining thickness T is a value within the range of 0.45 to 0.6 mm.

(28) An airbag rupturing groove forming apparatus.

(29) Next, an airbag rupturing groove forming apparatus which forms an airbag rupturing groove in a vehicular interior member as the first embodiment of the present invention will be described in detail.

(30) FIG. 3 shows a perspective view of a constitutional example of the airbag rupturing groove forming apparatus 10. Also, FIG. 4 is a plan view from the top of the airbag rupturing groove forming apparatus 10. In FIG. 4, the interior member 40 which is put on a support base is depicted with a broken line.

(31) The airbag rupturing groove forming apparatus 10 mainly comprises the support base 11 on which the interior member 40 is put, the rupturing groove forming means 33 for forming the airbag rupturing groove in the interior member 40 placed on the support base 11, the first metal blade detecting means 67 and the second metal blade detecting means 69 which detect a position of a metal blade 13 constituting the rupturing groove forming means 33, and a controller 16 which controls movement of the airbag rupturing groove forming apparatus 10 and the like.

(32) A support base.

(33) The airbag rupturing groove forming apparatus 10 in this embodiment is provided with the support base 11 on which the interior member is put and fixed when the airbag rupturing groove is formed in the interior member. The interior member mentioned above has the hard substrate layer, and the interior member retains its three-dimensional shape. Therefore, a surface 11a of the support base 11 is structured in three-dimension according to the shape of the interior member to be placed.

(34) Besides, the support base 11 provided in the airbag rupturing groove forming apparatus 10 in this embodiment is composed using nonmetal resin materials in order not to be an obstacle to detecting the metal blade 13 by the first and second metal blade detecting means 67 and 69 as mentioned later.

(35) Further, in the case of the support base 11 in this embodiment being composed using metal material or metal containing nonmetal resin material, so as not to be an obstacle to detecting the metal blade 13 by the first and second metal blade detecting means 67 and 69 as mentioned later, holes penetrating the support base 11 are provided in predetermined places of the support base 11 which corresponds to positions of the first and second metal blade detecting means 67 and 69, and an electric insulation resin material (for example, epoxy resin and silicon resin) is injected in the holes while the first and second metal blade detecting means 67 and 69 are placed at the inside of the holes so that the first and second metal blade detecting means 67 and 69 are fixed and embedded in the holes.

(36) Namely, according to the above constitution, the first and second metal blade detecting means 67 and 69 could detect the metal blade 13 even when the support base 11 is composed of metal material or metal containing nonmetal resin material because a portion composed of metal material or metal containing nonmetal resin material is not present in a surrounding surface of the first and second metal blade detecting means 67 and 69, and a region between the interior member fixed on the support base 11 and the first and second metal blade detecting means 67 and 69.

(37) Also, the surface 11a of the support base 11 is provided with plural suction holes 17 and an aspiration device 18 which aspirates and fixes the interior member placed on the surface 11a through the suction holes 17. As for the aspiration device 18, for example, a vacuum pump could be used. It may be possible that a worker hold down the interior member. However, by providing such aspiration device 18, even an inner interior member having a complicated shape or a large shape could easily be fixed on the support base 11. Thus, the position gap of the interior member and unevenness in a remaining thickness of the airbag rupturing groove could be avoided when the airbag rupturing groove is formed, and it is enabled to form the airbag rupturing groove with high precision. Moreover, unlike a mechanically fixing method, it is enabled to easily change whether or not fixing the interior member by switching on or off operation of the aspiration device 18, and it is enabled to work quickly.

(38) A rupturing groove forming means.

(39) A rupturing groove forming means 33 is provided so that the metal blade 13 is protruded from the hard substrate layer into the vehicular interior member comprising the hard substrate layer, the skin layer and the foam layer, and so that the airbag rupturing groove reaching to the skin layer is to be formed. Since the interior member includes the hard substrate layer which is hard and large in strength, unlike the skin layer or the foam layer, it is required that the rupturing groove forming means 33 could easily cut such hard substrate layer. Also, the means is required that the formed rupturing groove is to be a narrow line width so that its good invisibility from a front surface side of the interior member could keep for a long period of time.

(40) As for the rupturing groove forming means 33, a heat melt blade or an ultrasonic cutter, or the like could appropriately be used. In the airbag rupturing groove forming apparatus 10 in this embodiment, the rupturing groove forming means 33 is provided with the metal blade 13 and an ultrasonic cutter 33a having ultrasonic vibrator (not shown in figures.) which gives ultrasonic vibration to the metal blade 13. This ultrasonic cutter 33a is fixedly mounted to a rupturing groove forming means stationary part 63a within a movement control robot 63.

(41) A magnified perspective view for the vicinity of the rupturing groove forming means stationary part 63a to which the rupturing groove forming means 33 is fixedly mounted, within the movement control robot 63, is shown FIG. 5. A cylinder arm 65 which is controllable in expanding and contracting is installed to the rupturing groove forming means stationary part 63a, and the ultrasonic cutter 33a is fixedly mounted to the cylinder arm 65.

(42) As for the airbag rupturing groove forming apparatus 10 in this embodiment, the metal blade 13 used for the ultrasonic cutter 33a is formed like a plate and its blade edge is flattened against a forming face of the airbag rupturing groove. Therefore, when the metal blade 13 is protrudes into the interior member with supersonic vibration, the airbag rupturing groove could be easily formed at the place where the metal blade 13 is protruded.

(43) The airbag rupturing groove formed using such platelike metal blade 13 basically forms a cutting-plane line having a comparatively narrow line width. Therefore, although the airbag rupturing groove is formed reaching to the back side of the skin layer which is disposed on an exterior surface of the interior member, its existence of the airbag rupturing groove is not recognized from outside, and its good invisibility keeps for a long period of time.

(44) The movement control robot 63 shown in FIG. 3 and FIG. 4 is provided with a rail 64X, 64Y and 64Z, respectively, along X-axis, Y-axis and Z-axis, and is provided with a base plate 62X, 62Y and 62Z, respectively, which moves on the each rail. Each base plate 62X to 62Z moves on the corresponding rail 64X to 64Z by a control signal from a movement controller 16. Of these, a horizontal movement control means relating to flat direction, consists of the rails 64X and 64Y along X-axis and Y-axis, and the base plates 62X and 62Y. Also, a vertical movement control means relating to thickness direction, consists of the rail 64Z along Z-axis and the base plate 62Z. Of these, the rupturing groove forming means stationary part 63a is installed to the base plate 62Z moving on the rail 64Z placed along Z-axis direction, and the rupturing groove forming means stationary part 63a is rotatable with the rotating axis of Z-axis direction as the center.

(45) A movement control of the movement control robot 63, a rotation control of the rupturing groove forming means stationary part 63a and an expanding and contracting control of two cylinder arms 65 are carried out by the movement controller 16 (See FIG. 3). Also, a patterned shape of the airbag rupturing groove to be formed is beforehand memorized in the movement controller 16. Thus, the movement controller 16 outputs a signal so that the rupturing groove forming means stationary part 63a of the movement control robot 63 is allowed to move in the X-axis and Y-axis direction (flat direction). Also, when the airbag rupturing groove is formed, in order to change a direction of the edge of the metal blade 13 along the direction of forming the airbag rupturing groove, a signal to rotate the rupturing groove forming means stationary part 63a is output, and it allows a cylinder arm 65 to expand or contract, and to move in direction of Z-axis (the direction of thickness). As the result, the metal blade 13 having the ultrasonic cutter 33a moves the position along this pattered shape and forms the airbag rupturing groove of a broken line. Besides, the depth of the airbag rupturing groove could be adjusted, by controlling the position in the Z-axis direction of the rupturing groove forming means stationary part 63a within the movement control robot 63.

(46) Note that structure of the movement control robot for the rupturing groove forming means is not limited to the one described in FIG. 3 and FIG. 4, but various structure may be possible. As for another example of structure, an example having an arm robot may be possible.

(47) A metal detecting means.

(48) As shown in FIG. 3 and FIG. 4, in the rupturing groove forming apparatus 10 in this embodiment, the support base 11 is provided with a first metal blade detecting means 67 and a second metal blade detecting means 69, in order to detect a position of the edge of the metal blade 13 constituting the rupturing groove forming means 33.

(49) The first metal blade detecting means 67 and the second metal blade detecting means 69 are disposed inside of the support base 11, and are adapted so that presence or absence of the metal blade 13 is detected in a particular detection position set beforehand. For example, as for the first metal blade detecting means 67 and the second metal blade detecting means 69, a metal detector could be used. It is comprised so that the metal blade 13 is detected when the metal blade arrived at the detection position, but if the metal blade 13 could be detected, a detecting means is not limited in particular.

(50) Since the rupturing groove affects the deployment property of the airbag, management of the thickness of the remaining portion is important. In the rupturing groove forming apparatus 10 in this embodiment, it is structured, considering its invisibility, so that the rupturing groove is formed when the metal blade 13 is protruded into the skin layer disposed on an exterior surface of the interior member. In this embodiment, the thickness of the remaining portion is suitably managed by means of controlling the height position of the edge of the metal blade 13.

(51) A sectional view of the support base 11 cutting along a form-scheduled line of the formed rupturing groove is shown in FIG. 6A, and a situation of forming the airbag rupturing groove 49 in the interior member 40 placed on the support base 11 is shown in FIG. 6B. Note that in FIGS. 6A and 6B, members relating to the suction hole and the aspiration device in the support base 11 are omitted.

(52) As shown in FIGS. 6A and 6B, a first detection position S1 to be detected by the first metal blade detecting means 67 and a second detection position S2 to be detected by the second metal blade detecting means 69 are different in height in the direction of the thickness of the skin layer 41 where the airbag rupturing groove 49 is formed. The second detection position S2 is set to be higher and closer to the hard substrate layer 45. A height h1 of the first detection position S1 over a placing table 11a of the supporting base 11 is set at the minimum height position that is permitted as a remaining thin thickness of the airbag rupturing groove 49. On the contrary, a height h2 of the second detection position S2 over the placing table 11a of the support base 11 is set at the maximum height position that is permitted as a remaining thick thickness of the airbag rupturing groove 49. For example, the height of the first detection position S1 over the placing table 11a of the supporting base 11 is set to be a value within the range of 0.3 to 0.5 millimeter and the height of the second detection position S2 over the placing table 11a of the supporting base 11 is set to be a value within the range of 0.5 to 0.8 millimeter.

(53) In the rupturing groove forming apparatus 10 in this embodiment, a signal detected by the first metal blade detecting means 67 or the second metal blade detecting means 69 is set to be sent to the movement controller 16 mentioned above. The amount of movement to the Z-axis direction of the movement control robot 63 where the metal blade 13 is fixedly mounted is controlled by feedback so that the metal blade 13 is detected by the second metal blade detecting means 69 while the metal blade 13 is not detected by the first metal blade detecting means 67. Hereby, the height position of the metal blade is adjusted so that the remaining thickness of the formed airbag rupturing groove 49 becomes within the desired range. That is, the movement controller 16 carries out functions as a blade edge position deciding unit and a blade edge position adjustment unit, as well.

(54) It is not limitation in particular about the placement position of the first metal blade detecting means 67 or the second metal blade detecting means 69. For example, as shown in FIG. 7A, it may be arranged in the position which overlaps with a form-scheduled line of the airbag rupturing groove L or its extended line, and which is right under each detecting position when the support base 11 is viewed from the upper part. Also, as shown in FIG. 7B, it may also be arranged in the position which overlaps with a form-scheduled line L of the airbag rupturing groove or its extended line, and which is moved from the right under each detecting position when the support base 11 is viewed from the upper part.

(55) Furthermore, as shown in FIGS. 8A and 8B, the position of the first metal blade detecting means 67 and the second metal blade detecting means 69 could be arranged on either side of the form-scheduled line of the airbag rupturing groove L or its extended line, or on both sides of the line.

(56) Also in the example shown in FIGS. 7 and 8, the first detecting position S1 and the second detecting position S2 are located on the form-scheduled line L of the airbag rupturing groove, and are located in different position in a plane. Since the edge of metal blade 13 is flattened, when an edge height of the metal blade retains in an appropriate position, it becomes possible that a metal blade is detected at the second detecting position S2 by the second metal blade detecting means 69 while a metal blade is not detected at the first detecting position S1 by the first metal blade detecting means 67.

(57) Note that in the present invention, as shown in FIGS. 9A and 9B, the first detection position S1 and the second detection position S2 could be arranged in the position on a form-scheduled line L of the airbag rupturing groove, and in the position which overlaps each other in the plane.

(58) As for the first metal blade detecting means 67 or the second metal blade detecting means 69, it may be possible that both or at least either of these comprise two or more means. That is, the rupturing groove forming apparatus 10 in this embodiment, the metal blade 13 having the ultrasonic cutter 33a is protruded multiple times while changing the position to the interior member and forms airbag rupturing grooves of a broken line shape. It could also be configured so that its edge height of the metal blade 13 is judged at plural positions. For example, as mentioned above, when the rupturing groove is formed in such a way as only part of the rupturing groove reaches to the skin layer, it is preferred that the first metal blade detecting means 67 and the second metal blade detecting means 69 are disposed, respectively, at the position where the rupturing groove reaches to the skin layer as shown in FIG. 10. By disposing in this way, since the edge height of the metal blade could be detected at the each position where the rupturing groove reaches to the skin layer, it could be judged whether or not a remaining thickness of the airbag rupturing groove at each position is appropriately formed.

(59) Also, it is preferred that an eddy-current displacement sensor is used as for the first metal blade detecting means 67 and the second metal blade detecting means 69.

(60) The reason is that, in the case of such an eddy-current displacement sensor, there is no need to measure a distance of the edge of the metal blade 13 from the first metal blade detecting means 67 and the second metal blade detecting means 69, since in the present invention, the depth of the airbag rupturing groove could be adjusted by detecting presence or absence of the metal blade 13 in the detection position set beforehand. Thus, in the case of such an eddy-current displacement sensor, the position of the edge of the metal blade could be confirmed even though the eddy current is not stably formed.

(61) Therefore, in the case of such an eddy-current displacement sensor, the position of the edge of the metal blade 13 could be confirmed in a moment (0.1 sec or less) without stopping the metal blade 13, and a working speed of manufacturing the airbag rupturing groove is 300 mm/sec or more.

(62) A metal blade edge status detecting means.

(63) Also, a metal blade edge status detecting means 29 as shown in FIG. 3 and FIG. 4, is a means to detect whether or not there is abrasion or damage in the edge of the metal blade 13. It measure the status of the edge of the metal blade 13, and when status of the damage owing to abrasion or the like is detected, the apparatus could be stopped the operation, and the metal blade could be changed. Consequently, a remaining thickness of the airbag rupturing groove could be adjusted with high precision.

(64) Specifically, the metal blade edge status detecting means 29 is constituted using a laser measuring device or infrared measuring device, or the like. The metal blade edge status detecting means 29 could detect a degree of damage owing to abrasion or the like, by measuring a difference in the edge height between before forming the rupturing groove and after having formed the rupturing groove or by measuring the shade shape of the metal blade, by means of putting the metal blade 13 at the height of a metal blade edge status detecting means 29 position, while keeping a tip of the movement control robot 63 at the height determined beforehand.

(65) By providing such metal blade edge status detecting means 29, it is enabled that a distance between the edge of the metal blade 13 and the placing table 11a in the support base 11 could be maintained in constant state, considering blade status of the metal blade 13. As the result, although a kind, thickness or the like of the skin layer, is changed, the airbag rupturing groove having uniform overall remaining thickness could be quickly formed with high precision.

(66) Next, a manufacturing method of the vehicular interior member in a second embodiment will be described with referring to examples of a manufacturing method of the interior member, which includes the process for forming the airbag rupturing groove in the interior member using the airbag rupturing groove forming apparatus in the first embodiment.

(67) First of all, the vehicular interior member which becomes an object of forming the airbag rupturing groove is prepared. As shown in FIG. 1, the interior member in this embodiment is a three-layer-structured interior member 40, and comprises the hard substrate layer 45, the skin layer 41 which covers the external surface of the hard substrate layer 45 and the foam layer 43 between the hard substrate layer 45 and the skin layer 41.

(68) In the case of such a three-layer-structured interior member 40, comprising for example, the hard substrate layer 45, the foam layer 43 and the skin layer 41, it could be manufactured as follow. First, both a half body of a mold which is in a state of retaining the hard substrate layer 45 formed by injection molding and a half body of a mold which in a state of retaining the skin layer 41 formed by powder slash molding are formed. Then, two half bodies are piled up so that space is formed between the hard substrate layer 45 and the skin layer 41. Lastly, foam material is filled up in the space in order to form the foam layer. In another example, it could be manufactured after forming both a half body of a mold which is in a state of retaining the hard substrate layer 45 formed by injection molding and a half body of another mold, two half bodies are piled up so that space is formed at the front surface side of the hard substrate layer 45. Then, resin material is filled up in the formed space, and on the one hand the skin layer 41 is formed quickly by solidifying the part contacting the molds, and the other hand the foam layer 43 is formed by foaming the other middle part. That is, the skin layer 41 and the foam layer 43 could be formed using different materials in different processes, or the skin layer 41 and the foam layer 43 could be formed from the same material in the same process.

(69) Next, the processed interior member 40 is put down on the placing table 11a in the support base 11, with the skin layer 41 downside, that is, the hard substrate layer 45 upside. Although there is no figure to be shown, after the interior member 40 is placed there, the interior member 40 is fixed by aspirating through the suction hole by operating aspiration means such as a vacuum pump or the like.

(70) Next, as shown in FIG. 11A, the rupturing groove forming means stationary part 63a is moved to the position where the metal blade 13 having the ultrasonic cutter 33a is protruded, by a planar orientation movement means within the movement control robot 63. Then, as shown in FIG. 11B, by allowing the metal blade 13 to go down by a thickness orientation movement means within the movement control robot 63, the metal blade 13 is protruded into the interior member 40 so that a predetermined remaining thickness forms, resulting in forming a rupturing groove 49a which becomes a part of an airbag rupturing groove.

(71) At this situation in this embodiment, in order to form a predetermined remaining thickness in the skin layer 41, the amount of protrusion by the metal blade 13 is controlled by feedback so that the edge of the metal blade 13 retains at a predetermined height, based on detecting signals from the first metal blade detecting means 67 and second metal blade detecting means 69. That is, the airbag rupturing groove 49 is formed adjusting the amount of protrusion by the metal blade 13, so that the metal blade 13 is not detected by the first metal blade detecting means 67 while the metal blade 13 is detected by the second metal blade detecting means 69. Consequently, even when the distance between the rupturing groove forming means stationary part 63a and the edge of the metal blade 13 is changed owing to unevenness in metal blade length or abrasion of the blade edge or the like, it is enabled to appropriately manage the remaining thickness.

(72) The remaining thickness of the airbag rupturing groove is adjusted, for example, to be around 0.5 millimeteres. Specifically, in case both the first metal blade detecting means 67 and the second metal blade detecting means 69 detect the metal blade 13, it is corrected so that an amount of protrusion of the metal blade 13 by the movement control robot 63 becomes small. On the contrary, in case neither the first metal blade detecting means 67 nor the second metal blade detecting means 69 detects the metal blade 13, it is corrected so that an amount of protrusion of the metal blade 13 by the movement control robot 63 becomes large.

(73) Next, after allowing the metal blade 13 to rise and set apart from the interior member 40, by the thickness orientation movement means as shown in FIG. 12A, the rupturing groove forming means stationary part 63a is allowed to move to the location where the next rupturing groove is formed, by the planar orientation movement means, as shown in FIG. 12B. Then the airbag rupturing groove is formed in the same way as described referring to FIG. 11B. Since an airbag rupturing groove of a broken line is set to form in this embodiment, the airbag rupturing groove is formed when repeatedly carrying out upward and downward movement and plane orientation movement by the movement control robot 63.

(74) However, it is not necessary to detect the edge of metal blade 13 in all processes where the metal blade 13 is protruded into the interior member. It is rather preferred to measure at least once for each span when the airbag rupturing groove comprises plural spans.

(75) After all airbag rupturing grooves are formed in such way, the rupturing groove forming means stationary part 63a of the movement control robot 63 is moved and a status of the blade edge 14 of the metal blade 13 is inspected by the metal blade edge status detecting means 29, as shown in FIG. 13. For example, the metal blade 13 is given back to the position of a predetermined height h1, and the degree of damages owing to abrasion or the like is inspected, by comparing shades between an actual blade edge 14 and an ideal blade edge 14 of the metal blade 13, by means of a laser measuring device or an infrared measuring device or the like. Thus, by inspecting the status of the metal blade 13 in this way, it is enabled to more exactly control the metal blade 13 at the next time for forming an airbag rupturing groove. Besides, by inspecting the status of the metal blade 13 after having formed the airbag rupturing groove, when damages is detected in the blade edge, it is possible to stop the apparatus and change the blades.

(76) Note that as for detecting a status of the blade edge of the metal blade, it is also possible to carry out immediately before forming the airbag rupturing groove.

(77) The basic structure in the third embodiment of the present invention is similar to the airbag rupturing groove forming apparatus described in the first embodiment. However, as opposed to being configured so that the airbag rupturing groove forming apparatus 10 described in the first embodiment forms the airbag rupturing groove by carrying out repeatedly in a planar orientation movement and a thickness orientation movement of the metal blade, the airbag rupturing groove forming apparatus 10 in this embodiment is configured so that the metal blade has a blade surface in plane shape similar to the plane pattern of the airbag rupturing groove and the metal blade is protruded only once into the interior member to form the airbag rupturing groove.

(78) The points different from the first embodiment will be mainly described in the following.

(79) A perspective view showing a configuration example in this embodiment for the airbag rupturing groove forming apparatus 110 is shown in FIG. 14. FIG. 15 shows examples of a metal blade 113 provided when an airbag rupturing groove shown in FIG. 2A is formed. Except the metal blade 113 having an ultrasonic cutter 133a, an airbag rupturing groove forming apparatus 110 is basically the same as the airbag rupturing groove forming apparatus 10 as shown in FIGS. 3 and 4, and the same code is used for the same portion of the configuration.

(80) As mentioned above, the metal blade 113 used for the airbag rupturing groove forming apparatus 110 has a blade surface in plane shape similar to the plane pattern of the airbag rupturing groove to be formed. Therefore, in the airbag rupturing groove forming apparatus 110 in this embodiment, after the metal blade 113 is set position by the planar orientation movement means, the airbag rupturing groove is to be formed by only one action, by allowing the metal blade 113 to be protruded with giving ultrasonic into the interior member 40, by the thickness orientation movement means.

(81) The airbag rupturing groove forming apparatus is provided with at least one pair or more of the first metal blade detecting means 67 and the second metal blade detecting means 69, in which the first detection position S1 and the second detection position S2 are set to overlap with a form-scheduled line of the airbag rupturing groove. Thus, the blade edge of the metal blade 113 is detected whether or not it is within a desired range, in the state that the metal blade is kept protruded into the interior member 40. Consequently, the remaining thickness of the formed airbag rupturing groove is appropriately managed whether or not it is within the desired range.