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JP2007118893A - Method and device for forming fracture scheduled part of airbag door - Google Patents

Method and device for forming fracture scheduled part of airbag door Download PDF

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JP2007118893A
JP2007118893A JP2005317337A JP2005317337A JP2007118893A JP 2007118893 A JP2007118893 A JP 2007118893A JP 2005317337 A JP2005317337 A JP 2005317337A JP 2005317337 A JP2005317337 A JP 2005317337A JP 2007118893 A JP2007118893 A JP 2007118893A
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groove
base material
groove forming
forming means
airbag door
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Daisuke Hori
大祐 堀
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Inoac Corp
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Inoue MTP KK
Inoac Corp
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Abstract

<P>PROBLEM TO BE SOLVED: To provide a fracture scheduled part of an airbag door with high accuracy responding to the positional deviation of a base material. <P>SOLUTION: A groove forming means 34 to be movement-controlled by a control means 38 is moved along an outer peripheral contour of an airbag door while performing the cut-in at a predetermined depth from a back surface 12A side of a base material 12 to constitute a vehicular interior member. Before the grooving, the surface position of a part immediately before performing the grooving by the groove forming means 34 in the back surface 12A of the base material 12 is obtained from the back surface 12A side by a measurement means 36, and the position data is output to the control means 38. The control means 38 realizes the predetermined working depth of a groove 18 from the back surface 12A by controlling the working by the groove forming means 34 based on the reference to be successively updated as the position data is input from the measurement means 36. <P>COPYRIGHT: (C)2007,JPO&INPIT

Description

この発明は、車両用内装部材を構成する基材の一方の面に所定深さの溝を加工することで、エアバッグドアの破断予定部を形成する方法およびこの方法を実施するための装置に関するものである。   The present invention relates to a method for forming a predetermined breakage portion of an airbag door by processing a groove having a predetermined depth on one surface of a base material constituting a vehicle interior member, and an apparatus for carrying out the method. Is.

近年生産される殆どの自動車は、衝突事故等による衝撃から乗員を保護するために、運転席用のエアバッグ装置および助手席用のエアバッグ装置が標準装備されている。例えば、助手席用のエアバッグ装置は、乗員室内前方に組付けた車両内装部材としてのインストルメントパネルにおける助手席前方の内部に格納した状態で装備されている。このため図2に例示するように、インストルメントパネル10を構成する合成樹脂製の基材12には、乗員室側へ開放変位するエアバッグドア14,14が、助手席用のエアバッグ装置20に対応した部位に設けられている。   Most automobiles produced in recent years are equipped standardly with an airbag device for a driver's seat and an airbag device for a passenger's seat in order to protect an occupant from an impact caused by a collision accident or the like. For example, an airbag device for a passenger seat is equipped in a state of being stored inside the front of the passenger seat in an instrument panel as a vehicle interior member assembled in front of the passenger compartment. For this reason, as illustrated in FIG. 2, the synthetic resin base material 12 constituting the instrument panel 10 has airbag doors 14 and 14 that are opened and displaced toward the passenger compartment, and the airbag device 20 for the passenger seat. It is provided in the part corresponding to.

前記エアバッグドア14,14は、エアバッグ装置20の作動前では基材12の一部分を構成しており、エアバッグ装置20の作動により膨張を開始したエアバッグ22の押圧力を受けた際に、エアバッグドア14,14の外周輪郭に沿って形成した破断予定部16が破断することで、エアバッグドア14,14は基材12からの分離および開放変位が許容される。そして、エアバッグドア14,14が開放することで、基材12に開口部が画成されて、この開口部を介してエアバッグ22における乗員室側への膨張展開が許容されるようになっている。ここで、エアバッグドア14,14の破断予定部16は、例えば基材12の裏面に所定深さの溝18を連続的に設けたり、或いは複数の有底孔を所要間隔毎に設けることで脆弱化された部分であって、基材12の表面に現われないようになっている。   The airbag doors 14, 14 constitute a part of the base material 12 before the operation of the airbag device 20, and when receiving the pressing force of the airbag 22 that has started to expand due to the operation of the airbag device 20. The airbag doors 14 and 14 are allowed to be separated from the base material 12 and disengaged from each other by breaking the planned break portion 16 formed along the outer peripheral contour of the airbag doors 14 and 14. When the airbag doors 14 and 14 are opened, an opening is defined in the base member 12, and the inflation and deployment of the airbag 22 toward the passenger compartment is allowed through the opening. ing. Here, the fracture | rupture scheduled part 16 of the airbag doors 14 and 14 is providing the groove | channel 18 of the predetermined depth continuously, for example in the back surface of the base material 12, or providing a several bottomed hole for every required space | interval. It is a weakened part and does not appear on the surface of the substrate 12.

ところで、エアバッグドア14,14の破断予定部16は、エアバッグ装置20が作動した際に、迅速かつ確実に破断することが要求される一方、作動前の状態では基材12の一部として意図しない破断や変形等が起きない程度の構造的な強度が必要とされる。すなわち、破断予定部16の破断性および強度は、溝18を所定深さで形成した際に残る基材12の寸法(残留厚さ)により規定され、残留厚さが設計値から外れる場合または破断予定部16の全体に亘って一様でない場合の何れであっても、エアバッグドア14,14の展開性能に悪影響を与える。このように破断予定部16は、その残留厚さが一定になるように形成されることが求められ、±0.1mm程度の厳しい精度が要求されている。   By the way, when the airbag apparatus 20 act | operates, the scheduled break part 16 of the airbag doors 14 and 14 is requested | required to fracture | rupture quickly and reliably, On the other hand, as a part of the base material 12 in the state before an operation | movement. Structural strength is required so that unintended breakage or deformation does not occur. That is, the rupture property and strength of the planned fracture portion 16 are defined by the dimension (residual thickness) of the base material 12 remaining when the groove 18 is formed at a predetermined depth. Any of the cases where the entire scheduled portion 16 is not uniform adversely affects the deployment performance of the airbag doors 14, 14. Thus, it is calculated | required that the fracture | rupture planned part 16 is formed so that the residual thickness may become fixed, and the severe precision of about +/- 0.1mm is requested | required.

前記破断予定部16の形成方法としては、例えばインジェクション成形等の成形技術による基材12の成形工程において、成形型内に画成されるキャビティに進退自在に突出する突片により、基材12の成形と同時に破断予定部16を形成するものがある。この方法は、成形型内において溶融状態にある樹脂原料に突片を所定深さだけ突入した後、樹脂材料がある程度硬化するまで突入状態を保持して、突片の形状を基材12に転写することで破断予定部16をなす溝18を形成するものである。しかしこの方法では、破断予定部16を比較的精度よく形成し得るものの、突片によりキャビティ内の樹脂原料の流動が妨げられたり、硬化速度にばらつき等が生じる影響で、成形された基材12の表面側に模様が浮き出してしまう等の外観の悪化を招く問題がある。   As a method of forming the planned fracture portion 16, for example, in the molding process of the base material 12 by a molding technique such as injection molding, the projecting piece protruding in a cavity defined in the molding die can be used. There is one that forms the planned fracture portion 16 simultaneously with the molding. In this method, after a protrusion is plunged into a resin material in a molten state within a mold by a predetermined depth, the protrusion is held until the resin material is cured to some extent, and the shape of the protrusion is transferred to the substrate 12. By doing so, the groove | channel 18 which makes the fracture | rupture scheduled part 16 is formed. However, in this method, although the planned fracture portion 16 can be formed with relatively high accuracy, the molded base material 12 is affected by the influence of the protrusions that hinder the flow of the resin material in the cavity and the variation in the curing rate. There is a problem that the appearance is deteriorated, such as a pattern protruding on the surface side.

そこで、基材12を所定形状に形成する成形工程の次工程において、レーザーや回転切削工具等を有する形成装置を使用して、基材12を裏面から所定深さだけ切削して溝18を設けることで、エアバッグドア14の破断予定部16を形成する方法が注目されている(例えば、特許文献1参照)。図3に示すように、特許文献1の切削装置は、固定台52に載置固定した基材12を、切削刃54により所定深さで溝18を切削しつつ、切削刃54を所定方向へ移動させることで、所定形状の破断予定部16を形成する構成である。また切削装置は、固定台52における基材12の載置面52aを金属膜で被覆し、切削刃54に金属膜を検知し得る間隔センサ56を設けることで、この間隔センサ56により間隔センサ56から固定台52の載置面での間隔T2を検出している。そして、破断予定部16の残留厚さ(溝18の底面から固定台52の表面までの間隔)Aを、検出した間隔T2から切削刃54の先端と間隔センサ56との間隔T1を減じて計算し、残留厚さAが許容範囲内になるようアクチュエータ(図示せず)により切削刃54の上下位置を制御している。
特開2002−86397号公報
Therefore, in the next step of the forming process for forming the base material 12 into a predetermined shape, the base material 12 is cut by a predetermined depth from the back surface to form the groove 18 using a forming device having a laser, a rotary cutting tool, or the like. Thus, a method of forming the planned break portion 16 of the airbag door 14 has been attracting attention (see, for example, Patent Document 1). As shown in FIG. 3, the cutting apparatus of Patent Document 1 is configured to cut the groove 18 in a predetermined direction while cutting the groove 18 with a predetermined depth by the cutting blade 54 on the base 12 placed and fixed on the fixed base 52. It is the structure which forms the fracture | rupture scheduled part 16 of a predetermined shape by moving. Further, the cutting device covers the mounting surface 52a of the base material 12 on the fixed base 52 with a metal film, and the distance sensor 56 is provided with the distance sensor 56 capable of detecting the metal film on the cutting blade 54. The interval T2 on the mounting surface of the fixed base 52 is detected. Then, the residual thickness A (interval from the bottom surface of the groove 18 to the surface of the fixing base 52) A is calculated by subtracting the interval T1 between the tip of the cutting blade 54 and the interval sensor 56 from the detected interval T2. The vertical position of the cutting blade 54 is controlled by an actuator (not shown) so that the residual thickness A is within the allowable range.
JP 2002-86397 A

ところで基材12は、熱収縮のばらつきや保管時の状態等に起因して変形することがあり、固定台52に載置した際に、載置面52aから基材12が浮き上がって隙間Sが生じる場合がある(図3参照)。すなわち、特許文献1の切削装置は、切削刃54における上下方向の移動を固定台52の載置面52aを基準として制御しているから、基材12が載置面52aから浮き上がった部位では、この浮き上がり分だけ基材12への切込み量が大きくなり、破断予定部16が所定の残留厚さAに形成されない問題が指摘される。このように、固定台52の載置面52aを基準とする構成では、載置面52aに載置した基材12の現実の位置を反映することはできず、要求される精度を有する破断予定部16を常に形成することは難しい。しかも、インストルメントパネル10の構造部分を担う基材12は、比較的剛性が高くて硬質であるので、固定台52に設けた吸引装置による空気吸引や適宜の治具による押え付けにより浮き上がりを完全に防止するのは困難となっており、前述した問題が発現し易くなっている。   By the way, the base material 12 may be deformed due to variations in heat shrinkage, a state at the time of storage, and the like. May occur (see FIG. 3). That is, since the cutting device of Patent Document 1 controls the vertical movement of the cutting blade 54 with reference to the mounting surface 52a of the fixed base 52, at the site where the base material 12 is lifted from the mounting surface 52a, The amount of cut into the base material 12 is increased by this lift, and the problem is that the planned fracture portion 16 is not formed at the predetermined residual thickness A. Thus, in the configuration based on the mounting surface 52a of the fixed base 52, the actual position of the base material 12 mounted on the mounting surface 52a cannot be reflected, and the fracture is scheduled with the required accuracy. It is difficult to always form the portion 16. In addition, since the base material 12 that bears the structural part of the instrument panel 10 is relatively high in rigidity, the base 12 is completely lifted by air suction by a suction device provided on the fixed base 52 and pressing by an appropriate jig. It is difficult to prevent the above problems, and the above-mentioned problems are easily developed.

前述した基材の固定台からの浮き上がりに対応して一定の残留厚さで破断予定部を形成するため、固定台に間隔センサを設け、固定台と基材との隙間に応じて切削刃を進退制御する構成も考えられる。しかし固定台は、あくまでも基材を載置支持する機能が優先されるので、固定台の上方の如く開放された空間に間隔センサを設ける場合と異なり、設置スペースの制約が大きい難点がある。しかも、固定台に間隔センサを設置する構成では、間隔センサを破断予定部の形状に合わせて固定台に複数設置する必要があるから、破断予定部の形状変更に対応できない不都合もある。   In order to form the planned fracture portion with a certain residual thickness in response to the above-described lifting of the base material from the fixed base, an interval sensor is provided on the fixed base, and a cutting blade is provided according to the gap between the fixed base and the base material. A configuration in which advance / retreat is controlled is also possible. However, since the function of placing and supporting the base material is given priority to the fixed base, unlike the case where the distance sensor is provided in an open space such as above the fixed base, there is a problem that the installation space is greatly restricted. In addition, in the configuration in which the interval sensor is installed on the fixed base, it is necessary to install a plurality of interval sensors on the fixed base in accordance with the shape of the planned fracture portion.

すなわち本発明は、従来の技術に係るエアバッグドアの破断予定部形成方法およびその形成装置に内在する前記問題に鑑み、これらを好適に解決するべく提案されたものであって、簡単な構成で、基材の位置ずれに対応して精度良くエアバッグドアの破断予定部を形成し得る方法およびその装置を提供することを目的とする。   That is, the present invention has been proposed in order to suitably solve these problems inherent in the conventional method for forming a fractured portion of an airbag door and the forming apparatus thereof according to the prior art, and has a simple configuration. An object of the present invention is to provide a method and an apparatus for forming a scheduled breakage portion of an airbag door with high accuracy corresponding to a positional shift of a base material.

前記課題を克服し、所期の目的を達成するため、本願の請求項1に係る発明のエアバッグドアの破断予定部形成方法は、
制御手段で移動制御される溝形成手段により、車両用内装部材を構成する基材の一方の面に所定深さの溝を加工することで、エアバッグドアの破断予定部を形成する方法であって、
溝加工に先立ち、前記一方の面における前記溝形成手段により溝加工を行なう直前部位の面位置を、計測手段により該一方の面側から求めて、その位置データを前記制御手段へ出力し、
前記制御手段は、前記計測手段からの位置データの入力に伴って逐次更新される基準に基づき、前記溝形成手段による加工を制御することで、前記一方の面からの溝の加工深さを一定とするようにしたことを特徴とする。
請求項1に係る発明によれば、溝形成手段により溝加工を行なうのに先立って、基材の一方の面における溝形成手段により溝加工が行なわれる直前の面位置を、計測手段により求めることで、当該一方の面における現実の面位置を把握することができる。そして、計測手段から入力された位置データに伴って溝加工を行なう際の基準を逐次更新し、一方の面の現実の面位置が反映された基準に基づき、制御手段により溝形成手段による加工を制御することで、一方の面からの溝の加工深さを一定とすることができる。すなわち、基材の形状の変化や位置ずれに対応して、溝の加工深さを一定とすることができるから、破断予定部の全体に亘って所定の肉厚だけ基材部分を残留して精度良く形成することができる。
In order to overcome the above-mentioned problems and achieve the intended purpose, a method for forming a scheduled breakage portion of an airbag door according to claim 1 of the present application,
This is a method of forming a predetermined breakage portion of an airbag door by processing a groove having a predetermined depth on one surface of a base material constituting a vehicle interior member by a groove forming means whose movement is controlled by a control means. And
Prior to grooving, the surface position of the portion immediately before grooving by the groove forming means on the one surface is obtained from the one surface side by the measuring means, and the position data is output to the control means,
The control means controls the processing by the groove forming means based on a reference that is sequentially updated with the input of position data from the measuring means, so that the processing depth of the groove from the one surface is constant. It is characterized by that.
According to the first aspect of the present invention, prior to performing the groove processing by the groove forming means, the surface position immediately before the groove processing by the groove forming means on one surface of the substrate is obtained by the measuring means. Thus, the actual surface position on the one surface can be grasped. Then, the reference for groove processing is sequentially updated in accordance with the position data input from the measuring means, and the control means performs processing by the groove forming means based on the reference reflecting the actual surface position of one surface. By controlling, the processing depth of the groove from one surface can be made constant. In other words, the processing depth of the groove can be made constant in response to changes in the shape of the base material and positional displacement, so that the base material portion remains by a predetermined thickness over the entire portion to be broken. It can be formed with high accuracy.

請求項2に係る発明は、請求項1記載のエアバッグドアの破断予定部形成方法において、前記制御手段は、更新された基準が前の基準と比較して前記溝形成手段に近接すると判断される場合は、これに応じて前記溝形成手段が基材から退く方向に移動するよう制御され、更新された基準が前の基準と比較して前記溝形成手段から離間すると判断される場合は、これに応じて前記溝形成手段が基材へ向けて進む方向に移動するよう制御される。
請求項2に係る発明によれば、計測手段から入力されて更新された基準と前の基準との比較により溝形成手段を基材に対して進退移動することで、一方の面からの溝の加工深さを一定とすることができる。
According to a second aspect of the present invention, in the method for forming a scheduled breakage portion of the airbag door according to the first aspect, the control means determines that the updated reference is closer to the groove forming means than the previous reference. The groove forming means is controlled to move in a direction away from the base material according to this, and when it is determined that the updated reference is separated from the groove forming means compared to the previous reference, In response to this, the groove forming means is controlled to move in the direction of traveling toward the substrate.
According to the second aspect of the present invention, the groove forming means is moved forward and backward with respect to the base material by comparing the reference inputted by the measuring means and updated with the previous reference, so that the groove from one surface can be moved. The processing depth can be made constant.

請求項3に係る発明は、請求項1または2記載のエアバッグドアの破断予定部形成方法において、前記計測手段は、前記溝形成手段に連動して移動し、該計測手段と前記基材の一方の面との間の距離を測定することで、該一方の面の面位置を求めるようにした。
請求項3に係る発明によれば、基材の一方の面との間の距離を測定する計測手段を、溝形成手段に連動して移動することで、基材の一方の面における溝加工が行なわれる直前の面位置を逐次正確に求めることができる。
According to a third aspect of the present invention, in the method for forming a scheduled breakage portion of the airbag door according to the first or second aspect, the measuring means moves in conjunction with the groove forming means, and the measuring means and the base material The surface position of the one surface was obtained by measuring the distance between the one surface.
According to the invention according to claim 3, the groove processing on the one surface of the substrate can be performed by moving the measuring device that measures the distance between the one surface of the substrate and the groove forming device. The surface position immediately before being performed can be obtained successively and accurately.

前記課題を克服し、所期の目的を達成するため、本願の請求項4に係る発明のエアバッグドアの破断予定部形成装置は、
制御手段で移動制御される溝形成手段により、車両用内装部材を構成する基材の一方の面に所定深さの溝を加工することで、エアバッグドアの破断予定部を形成する装置であって、
前記溝形成手段に連動して移動するように配設され、前記一方の面における前記溝形成手段により溝加工を行なう直前部位の面位置を該一方の面側から求め、その位置データを前記制御手段へ出力する計測手段を備え、
前記制御手段は、前記計測手段からの位置データの入力に伴って逐次更新される基準に基づき前記溝形成手段による加工を制御することで、前記一方の面からの溝の加工深さを一定とするよう構成したことを特徴とする。
請求項4に係る発明によれば、溝形成手段により溝加工を行なうのに先立って、基材の一方の面における溝形成手段により溝加工が行なわれる直前の面位置を、計測手段により求め得るので、当該一方の面における現実の面位置を把握することができる。そして、計測手段から入力された位置データに伴って溝加工を行なう際の基準を逐次更新し、一方の面の現実の面位置が反映された基準に基づき、制御手段により溝形成手段による加工を制御することが可能となり、一方の面からの溝の加工深さを一定とすることができる。すなわち、基材の形状の変化や位置ずれに対応して、溝の加工深さを一定とすることができるから、破断予定部の全体に亘って所定の肉厚だけ基材部分を残留して精度良く形成することができる。
In order to overcome the above-mentioned problems and achieve the intended purpose, an airbag door fracture scheduled part forming device according to claim 4 of the present application is
This is an apparatus for forming a predetermined breakage portion of an airbag door by processing a groove having a predetermined depth on one surface of a base material constituting a vehicle interior member by a groove forming means whose movement is controlled by a control means. And
It is arranged so as to move in conjunction with the groove forming means, the surface position of the portion immediately before the groove forming means on the one surface is subjected to groove processing is obtained from the one surface side, and the position data is controlled by the control Measuring means for outputting to the means,
The control means controls the machining by the groove forming means based on a reference that is sequentially updated with the input of position data from the measuring means, so that the machining depth of the groove from the one surface is constant. It is characterized by having comprised.
According to the fourth aspect of the present invention, prior to performing the groove processing by the groove forming means, the surface position immediately before the groove processing by the groove forming means on one surface of the substrate can be obtained by the measuring means. Therefore, the actual surface position on the one surface can be grasped. Then, the reference for groove processing is sequentially updated in accordance with the position data input from the measuring means, and the control means performs processing by the groove forming means based on the reference reflecting the actual surface position of one surface. It becomes possible to control, and the processing depth of the groove from one surface can be made constant. In other words, the processing depth of the groove can be made constant in response to changes in the shape of the base material and positional displacement, so that the base material portion remains by a predetermined thickness over the entire portion to be broken. It can be formed with high accuracy.

本発明に係るエアバッグドアにおける破断予定部の形成方法によれば、基材の形状や位置ずれに対応して精度良く一定の加工深さで溝を形成することができ、所定の肉厚だけ残留させたエアバッグドアの破断予定部を基材に形成し得る。   According to the method for forming the planned break portion in the airbag door according to the present invention, the groove can be accurately formed at a constant processing depth corresponding to the shape and displacement of the base material, and only a predetermined thickness is provided. The fractured portion of the remaining airbag door can be formed on the base material.

本願の別の発明に係るエアバッグドアの破断予定部形成装置によれば、簡単な構成で、基材の形状や位置ずれに対応して、簡単に精度良く一定の厚さだけ残留させたエアバッグドアの破断予定部を基材に形成し得る。   According to the apparatus for forming a scheduled breakage portion of an airbag door according to another invention of the present application, the air that is easily left in a certain thickness with a simple configuration and corresponding to the shape and displacement of the base material can be easily obtained. The planned break portion of the bag door can be formed on the base material.

次に、本発明に係るエアバッグドアの破断予定部形成方法およびこの形成方法を実施するための形成装置につき、好適な実施例を挙げて、添付図面を参照して以下に説明する。なお、説明の便宜上、図2に示したエアバッグ装置を設けたインストルメントパネルの構成要素と同一の要素については、同一の符号を使用して詳細な説明は省略する。   Next, a preferred embodiment of a method for forming a scheduled breakage portion of an airbag door and a forming apparatus for carrying out this forming method according to the present invention will be described below with reference to the accompanying drawings. For convenience of explanation, the same reference numerals are used for the same elements as those of the instrument panel provided with the airbag device shown in FIG. 2, and detailed description thereof is omitted.

インストルメントパネル(車両内装部材)において、エアバッグドアが一体的に形成される基材は、PPやASG等の合成樹脂材料をインジェクション成形等により所定形状に形成した比較的硬質な部材であり、基材においてエアバッグドアの破断予定部が後述する形成装置により形成される部位は、少なくとも一定の厚さとなっている。エアバッグドアの破断予定部をなす溝は、インストルメントパネルが基材単体で構成される場合は、その多くが基材におけるエアバッグ装置に臨む裏面に設けられ、またインストルメントパネルが基材を表皮材や発泡材等の他の部材で覆った複層で構成される場合は、基材における客室側に臨む表面に設けることもできる。ここで実施例では、エアバッグドアの破断予定部を構成する溝が、基材の裏面に開口するように設けられ、意匠面(表面)となる客室側から破断予定部を識別することができない所謂インビジブルタイプのものについて説明する。すなわち、基材における一方の面とは、破断予定部を構成する溝が開口する面であって、実施例では基材の裏面を指す。   In the instrument panel (vehicle interior member), the base material on which the airbag door is integrally formed is a relatively hard member formed of a synthetic resin material such as PP or ASG into a predetermined shape by injection molding or the like, The portion of the base material where the planned breakage portion of the airbag door is formed by a forming device described later has at least a constant thickness. When the instrument panel is composed of a single base material, most of the grooves forming the planned breakage portion of the airbag door are provided on the back surface of the base material facing the airbag device, and the instrument panel covers the base material. In the case of a multi-layer covered with another member such as a skin material or a foam material, it can also be provided on the surface of the base material facing the cabin. Here, in the embodiment, the groove constituting the planned breakage portion of the airbag door is provided so as to open on the back surface of the base material, and the breakable portion cannot be identified from the cabin side which is the design surface (front surface). A so-called invisible type will be described. In other words, the one surface of the base material is a surface on which a groove constituting the planned fracture portion is opened, and in the examples, refers to the back surface of the base material.

図1に示すように、実施例に係るエアバッグドアの破断予定部形成装置(以下、単に形成装置と云う)は、基材12を保持する固定手段32と、基材12に溝加工を行なう溝形成手段34と、基材12の裏面12Aの面位置を求める計測手段36と、溝形成手段34を移動制御する制御手段38とから基本的に構成される。この形成装置は、基材12に対する溝形成手段34の位置を、制御手段38に予めプログラムした設定情報に基づいて制御するNC加工機であって、制御手段38の制御下に溝形成手段34を所定の軌跡で移動させることで、エアバッグドアの外周輪郭形状の破断予定部16を形成するようになっている。また形成装置は、基材12を固定手段32に保持した際に、溝形成手段34に相対する面である該基材12の裏面(一方の面)12Aから溝形成手段34により溝加工を行なうように設定されており、厚さTの基材12に加工深さFで溝加工して、残留厚さAの破断予定部16を形成するよう構成される。更に形成装置は、溝加工に際して計測手段36により求められた基材12の裏面12Aの面位置を反映して、溝形成手段34による加工が制御され、溝18の加工深さFが裏面12Aから常に一定となるようにすることができる。   As shown in FIG. 1, an airbag door fracture scheduled portion forming apparatus (hereinafter simply referred to as a forming apparatus) according to an embodiment performs a groove process on a base member 12 and a fixing means 32 that holds the base member 12. It basically comprises a groove forming means 34, a measuring means 36 for determining the surface position of the back surface 12A of the substrate 12, and a control means 38 for controlling the movement of the groove forming means 34. This forming apparatus is an NC processing machine that controls the position of the groove forming means 34 with respect to the base material 12 based on setting information pre-programmed in the control means 38, and the groove forming means 34 is controlled under the control of the control means 38. By moving along a predetermined trajectory, the planned fracture portion 16 of the outer peripheral contour shape of the airbag door is formed. Further, when the forming apparatus holds the base material 12 on the fixing means 32, the groove forming means 34 performs groove processing from the back surface (one surface) 12 </ b> A of the base material 12 that is a surface facing the groove forming means 34. In this way, the base material 12 having a thickness T is grooved at a processing depth F to form a planned fracture portion 16 having a residual thickness A. Further, the forming apparatus reflects the surface position of the back surface 12A of the base material 12 obtained by the measuring means 36 at the time of groove processing, the processing by the groove forming means 34 is controlled, and the processing depth F of the groove 18 is changed from the back surface 12A. It can be made constant at all times.

前記固定手段32は、突出するように湾曲する基材12の表面12Bの形状に合わせて形成された固定部32aを備え、この固定部32aは上方に向けて開放するように形成されている。そして基材12は、固定手段32の固定部32aに表面12B側を突合わせた状態で載置されて、湾曲する固定部32aの形状と合致して、固定手段32に動かないように保持される。また固定手段32において、基材12は表面12B側が固定部32aに相対して保持される一方で、溝加工面となる裏面12Aが上方に露出され、上方からの溝加工が許容される。   The fixing means 32 includes a fixing portion 32a formed in accordance with the shape of the surface 12B of the base material 12 that curves so as to protrude, and the fixing portion 32a is formed to open upward. Then, the base material 12 is placed on the fixing portion 32a of the fixing means 32 in a state where the surface 12B side is abutted, and is matched with the shape of the bending fixing portion 32a so as not to move by the fixing means 32. The In the fixing means 32, the base 12 is held with the front surface 12B facing the fixing portion 32a, while the back surface 12A serving as a groove processing surface is exposed upward, and groove processing from above is allowed.

前記溝形成手段34は、固定手段32の固定部32aに対向して該固定手段32の上方に配設され、制御手段38の制御下に固定部32aに保持した基材12に対して三次元的に移動するよう構成される。溝形成手段34としては、エンドミル、フライス、熱刃、超音波カッター、コールドナイフ等の切削工具自体が基材12に切込んで溝18を機械的に形成するものや、レーザーを照射して合成樹脂を材料とする基材12を部分的に融解することで溝18を形成するレーザー照射器等を採用し得る。実施例の溝形成手段34は、外周面および端面に切れ刃があるエンドミル34aを備えたミーリング加工機であって、エンドミル34aを回転させつつ基材12に切込むことで溝18を形成し、溝形成手段34の水平方向への移動に伴ってエンドミル34aが基材12に切込みつつ水平方向へ移動する過程で設けられる条痕が破断予定部16となる。すなわち、実施例の溝形成手段34は、基材12に対して進退する方向へ移動すると共に、基材12の裏面12Aに沿って水平方向へ移動する動作を複合的または個別に行なうよう構成される。   The groove forming means 34 is disposed above the fixing means 32 so as to face the fixing portion 32a of the fixing means 32, and is three-dimensional with respect to the substrate 12 held by the fixing portion 32a under the control of the control means 38. Configured to move. As the groove forming means 34, a cutting tool itself such as an end mill, a milling cutter, a hot blade, an ultrasonic cutter, a cold knife or the like cuts into the substrate 12 to mechanically form the groove 18, or is synthesized by irradiating a laser. A laser irradiator or the like that forms the groove 18 by partially melting the substrate 12 made of resin can be employed. The groove forming means 34 of the embodiment is a milling machine equipped with an end mill 34a having cutting edges on the outer peripheral surface and the end surface, and forms the groove 18 by cutting into the base material 12 while rotating the end mill 34a. As the groove forming means 34 moves in the horizontal direction, the streak provided in the process of moving the end mill 34 a in the horizontal direction while cutting into the base material 12 becomes the planned fracture portion 16. That is, the groove forming means 34 of the embodiment is configured to move in a direction that advances and retreats with respect to the base material 12 and to perform a movement in the horizontal direction along the back surface 12A of the base material 12 in a composite or individual manner. The

前記計測手段36は、固定手段32の固定部32aに対向して該固定手段32の上方に配設され、固定部32aに保持した基材12の裏面12Aの面位置を、該裏面12A側から連続的または所要間隔毎に求めるものである。また、計測手段36は、求めた基材12の裏面12Aの面位置を、位置データとして制御手段38に出力するようになっている。計測手段36としては、レーザー、光や電波等の電磁波や超音波や磁気等その他の非接触式の距離測定装置や、基材12の裏面12Aに接触する従動子の上下方向の変位量を測定する機械的な接触式の距離測定装置が採用可能であって、実施例ではレーザー変位量測定器が採用されている。そして計測手段36では、基材12の裏面12Aにおける測定地点と計測手段36との距離をレーザーにより測定し、当該測定地点の計測手段36との距離の大小から基材12の裏面12Aが占める面位置を特定するようになっている。なお、基材12の裏面12Aの面位置とは、該裏面12Aの占める上下方向(基材12の厚さ方向)の座標である。   The measuring means 36 is disposed above the fixing means 32 so as to face the fixing portion 32a of the fixing means 32, and the surface position of the back surface 12A of the base 12 held by the fixing portion 32a is determined from the back surface 12A side. It is obtained continuously or at every required interval. Further, the measuring means 36 outputs the obtained surface position of the back surface 12A of the base material 12 to the control means 38 as position data. As the measuring means 36, the amount of vertical displacement of the non-contact type distance measuring device such as laser, electromagnetic waves such as light and radio waves, ultrasonic waves, magnetism, etc., or the follower contacting the back surface 12A of the substrate 12 is measured. A mechanical contact type distance measuring device can be employed, and in the embodiment, a laser displacement measuring device is employed. In the measuring means 36, the distance between the measurement point 36 on the back surface 12A of the base material 12 and the measurement means 36 is measured by a laser, and the surface occupied by the back surface 12A of the base material 12 from the magnitude of the distance from the measurement means 36 at the measurement point. The position is specified. The surface position of the back surface 12A of the substrate 12 is a coordinate in the vertical direction (thickness direction of the substrate 12) occupied by the back surface 12A.

前記計測手段36は、制御手段38により水平方向へ所定の軌跡で移動される溝形成手段34の進行方向前側に配設され、溝加工に先立って、基材12の裏面12Aにおいて溝形成手段34により溝加工を行なうべき直前の部位(溝加工直前部位)の面位置を求めるように設定されている。また計測手段36は、溝形成手段34に連動して移動するよう構成され、溝形成手段34が移動しても該溝形成手段34との位置関係が変化せず、相対的な距離が常に一定となっている。なお、基材12の裏面12Aにおける溝加工直前部位とは、溝加工中のエンドミル34aの近傍であって、溝加工につれて水平方向へ移動するエンドミル34aの進行方向前側、進行方向横側および進行方向後側を含み、溝形成手段34で形成した溝18を除く領域を指す。実施例の計測手段36は、溝形成手段34の水平方向への移動における進行方向前側を計測するように設定され、溝加工を行なう予定のラインの全体に亘って基材12の裏面12Aの面位置を求めるようになっている。   The measuring means 36 is disposed on the front side in the traveling direction of the groove forming means 34 that is moved in the horizontal direction by the control means 38, and the groove forming means 34 is formed on the back surface 12A of the substrate 12 prior to the groove processing. Is set so as to obtain the surface position of the part immediately before grooving (the part immediately before grooving). The measuring means 36 is configured to move in conjunction with the groove forming means 34. Even if the groove forming means 34 moves, the positional relationship with the groove forming means 34 does not change, and the relative distance is always constant. It has become. The portion immediately before grooving on the back surface 12A of the substrate 12 is in the vicinity of the end mill 34a during grooving, and the front side in the traveling direction, the lateral side in the traveling direction, and the traveling direction of the end mill 34a moving in the horizontal direction as the grooving is performed. The region including the rear side and excluding the groove 18 formed by the groove forming means 34 is indicated. The measuring means 36 of the embodiment is set so as to measure the front side in the advancing direction in the movement of the groove forming means 34 in the horizontal direction, and the surface of the back surface 12A of the substrate 12 over the entire line scheduled to be grooved. The position is to be calculated.

前記制御手段38は、計測手段36や操作手段等から入力された情報および予めプログラムされた設定情報に基づいて、溝形成手段34やその他の機器を制御するものである。設定情報は、基材12の平面形状やエアバッグドアにおける外周輪郭の形状や溝加工する順序等をプログラムとして予め設定したものであって、制御手段38は設定情報に基づき、溝形成手段34をエアバッグドアの外周輪郭に沿う軌跡で水平方向へ移動するよう制御している。また制御手段38では、溝形成手段34による溝加工の前に操作手段から入力された基材12の厚さTおよび加工深さF等の情報に基づいて、基材12の加工開始点の原点位置データを生成し、加工開始点において制御手段38の原点位置データを基準として、溝形成手段34を当該基準から加工深さFだけ基材12に向けて切込むように制御する。そして制御手段38は、加工開始点において原点位置データに基づく基準から溝形成手段34を加工深さFで切込んだ後、計測手段36からの位置データの入力に伴って逐次更新される基準に基づき、溝形成手段34を制御するよう構成される。   The control means 38 controls the groove forming means 34 and other devices on the basis of information input from the measuring means 36, the operating means, etc. and setting information programmed in advance. The setting information is set in advance as a program such as the planar shape of the base material 12, the shape of the outer peripheral contour of the airbag door, the groove processing order, and the control means 38 determines the groove forming means 34 based on the setting information. It is controlled to move in the horizontal direction along a trajectory along the outer peripheral contour of the airbag door. Further, the control means 38 starts the processing start point of the base material 12 based on information such as the thickness T and processing depth F of the base material 12 input from the operation means before the groove processing by the groove forming means 34. Position data is generated, and the groove forming means 34 is controlled to be cut toward the base material 12 by the machining depth F from the reference, based on the origin position data of the control means 38 at the machining start point. Then, the control means 38 cuts the groove forming means 34 at the machining depth F from the reference based on the origin position data at the machining start point, and then uses it as a reference that is sequentially updated as the position data is input from the measuring means 36. Based on this, the groove forming means 34 is configured to be controlled.

前記形成装置は、更新された基準が、前の基準(または原点位置データに基づく基準)と制御手段38で比較して溝形成手段34(計測手段36)に近接すると判断される場合は、これに応じて溝形成手段34が基材12から退く方向に移動するよう制御される。また形成装置は、更新された基準が、前の基準(または原点位置データに基づく基準)と制御手段38で比較して溝形成手段34(計測手段36)から離間すると判断される場合は、これに応じて溝形成手段34が基材12へ向けて進む方向に移動するよう制御される。この過程で溝形成手段34によりエアバッグドアの外周輪郭に合わせた軌跡で、かつ一定の加工深さFで溝18が切削され、エアバッグドアの破断予定部16が形成されるようになっている。このように形成装置は、溝形成手段34の水平方向への移動につれて形状や位置ずれ等により変化する基材12の裏面12Aの面位置を、溝加工に先立って計測手段36で読取り、この位置データを反映して制御手段38により溝形成手段34を基材12に対して進退移動することで、裏面12Aからの溝18の加工深さFを一定にすることができる。   The forming apparatus determines that the updated reference is close to the groove forming means 34 (measurement means 36) by comparing the previous reference (or the reference based on the origin position data) with the control means 38. Accordingly, the groove forming means 34 is controlled so as to move in the direction of retreating from the substrate 12. Further, the forming apparatus determines that the updated reference is separated from the groove forming means 34 (measurement means 36) by comparing the previous reference (or the reference based on the origin position data) with the control means 38. Accordingly, the groove forming means 34 is controlled to move in the direction of traveling toward the substrate 12. In this process, the groove 18 is cut by the groove forming means 34 with a locus matched to the outer peripheral contour of the airbag door and at a constant processing depth F, so that the scheduled break portion 16 of the airbag door is formed. Yes. In this way, the forming apparatus reads the surface position of the back surface 12A of the base material 12 that changes due to the shape, positional deviation, and the like as the groove forming means 34 moves in the horizontal direction by the measuring means 36 prior to groove processing, and this position. The processing depth F of the groove 18 from the back surface 12A can be made constant by moving the groove forming means 34 forward and backward with respect to the base material 12 by the control means 38 reflecting the data.

〔実施例の作用〕
次に、実施例に係るエアバッグドアの破断予定部形成装置の作用について、この形成装置を用いたエアバッグドアにおける破断予定部形成方法と合わせて説明する。
(Effects of Example)
Next, the operation of the airbag door scheduled break portion forming apparatus according to the embodiment will be described together with the scheduled break portion forming method for the airbag door using the forming apparatus.

先ず基材12を、その表面12Bを固定手段32の固定部32aに突合わせた状態でセットして、溝加工面となる裏面12Aを上方で待機している溝形成手段34に臨ませる。ここで、固定部32aは、基材12の形状に合わせて形成されているから、基材12が形状的に固定部32aに合致して保持される。但し、基材12に、たわみや歪み等の変形がある場合には、基材12の表面12Bと固定部32aとの間に隙間Sができることも有り得る。   First, the base material 12 is set in a state where the front surface 12B is abutted against the fixing portion 32a of the fixing means 32, and the back surface 12A serving as a groove processing surface faces the groove forming means 34 waiting on the upper side. Here, since the fixing | fixed part 32a is formed according to the shape of the base material 12, the base material 12 corresponds to the fixing | fixed part 32a in shape, and is hold | maintained. However, when the base material 12 has deformation such as deflection or distortion, there may be a gap S between the surface 12B of the base material 12 and the fixing portion 32a.

そして、操作手段から基材12の厚さTを制御手段38に入力すると共に、裏面12Aからの溝18の加工深さFを入力する。すなわち形成装置では、固定部32aに載置した基材12の裏面12Aから溝形成手段34が基材12の厚さ方向に進退移動して溝加工するよう構成してあるから、基材12の厚さTと加工深さFとを設定することで、破断予定部16の残留厚さAが決定される。このとき、制御手段38に基材12の厚さTを設定することで、固定手段32の固定部32aに載置した際に、基材12における加工開始点の面位置が固定部32aとの関係より算出され、原点位置データも制御手段38に設定される。なお、基材12の厚さTおよび加工深さFの設定ステップは、必要に応じて実施され、同一厚さTの基材12に同一加工深さFで溝加工するロットでは毎回行なう必要はない。   And while inputting the thickness T of the base material 12 to the control means 38 from an operation means, the process depth F of the groove | channel 18 from the back surface 12A is input. That is, in the forming apparatus, since the groove forming means 34 moves forward and backward in the thickness direction of the base 12 from the back surface 12A of the base 12 placed on the fixing portion 32a, the groove 12 is processed. By setting the thickness T and the processing depth F, the residual thickness A of the planned fracture portion 16 is determined. At this time, by setting the thickness T of the base material 12 in the control means 38, the surface position of the processing start point on the base material 12 is the same as the fixing portion 32 a when the base material 12 is placed on the fixing portion 32 a. Calculated from the relationship, the origin position data is also set in the control means 38. In addition, the setting step of the thickness T and the processing depth F of the base material 12 is performed as necessary, and it is necessary to perform it every time in a lot in which the base material 12 having the same thickness T is grooved at the same processing depth F. Absent.

溝加工工程を開始すると、前記基材12の上方で待機していた溝形成手段34が、裏面12Aの加工開始点に対応する位置に移動すると共に、エンドミル34aが所定の回転速度で回転駆動される。制御手段38に設定した加工開始点の原点位置データに基づき、溝形成手段34が基材12に向けて下降することで、加工開始点における裏面12Aからエンドミル34aが所定の深さに切込まれる。そして、エンドミル34aにより溝加工を行ないつつ、制御手段38の設定情報に基づき、溝形成手段34がエアバッグドアの外周輪郭形状を所定の順序で描くように水平方向へ移動される。   When the groove processing step is started, the groove forming means 34 that has been waiting above the substrate 12 moves to a position corresponding to the processing start point of the back surface 12A, and the end mill 34a is rotationally driven at a predetermined rotational speed. The Based on the origin position data of the machining start point set in the control means 38, the groove forming means 34 descends toward the substrate 12, whereby the end mill 34a is cut to a predetermined depth from the back surface 12A at the machining start point. . Then, while performing groove processing by the end mill 34a, the groove forming means 34 is moved in the horizontal direction so as to draw the outer peripheral contour shape of the airbag door in a predetermined order based on the setting information of the control means 38.

この際に、溝加工工程では、制御手段38の設定情報による溝形成手段34の水平方向への移動につれて変化する基材12の裏面12Aの面位置を、溝加工に先立って計測手段36で読取り、制御手段38に出力する。ここで計測手段36は、基材12の裏面12Aにおける溝形成手段34による溝加工直前部位を読取るよう構成されているから、溝形成手段34の水平方向への移動に伴ってこれから溝加工される部位の現実の面位置を溝加工の前に把握し得る。そして制御手段38では、計測手段36から入力されて更新された基準と前の基準とを比較して、両者の差分だけ溝形成手段34を基材12に対して進退する方向へ移動する。すなわち、基材12の裏面12Aが溝形成手段34側に近接する方向に高くなると判断した場合は、これに応じて基準が高くなり、基材12の裏面12Aが溝形成手段34から離間する方向に低くなると判断した場合は、これに応じて基準が低くなる。従って、溝形成手段34は、裏面12Aにおける面位置の変化を反映した現実に即した基準から加工深さFの溝18を常に切削し得るから、基材12に一定の残留厚さAで破断予定部16が形成されるようになる。形成装置は、エアバッグドアの外周輪郭に沿って溝形成手段34を移動させることで溝加工が終了したら、溝形成手段34を基材12から離間するよう上昇させて待機させると共に、エンドミル34aの回転を停止する。   At this time, in the grooving step, the surface position of the back surface 12A of the substrate 12 that changes as the groove forming means 34 moves in the horizontal direction according to the setting information of the control means 38 is read by the measuring means 36 prior to grooving. To the control means 38. Here, since the measuring means 36 is configured to read the portion immediately before the groove processing by the groove forming means 34 on the back surface 12A of the base material 12, the groove processing is performed from now on as the groove forming means 34 moves in the horizontal direction. The actual surface position of the part can be grasped before grooving. Then, the control means 38 compares the updated reference inputted from the measuring means 36 with the previous reference, and moves the groove forming means 34 in the direction of advancing / retreating with respect to the substrate 12 by the difference between the two. That is, when it is determined that the back surface 12A of the base material 12 increases in the direction approaching the groove forming unit 34, the reference increases accordingly, and the back surface 12A of the base material 12 moves away from the groove forming unit 34. If it is determined that the value will be lower, the reference will be lowered accordingly. Therefore, since the groove forming means 34 can always cut the groove 18 having the processing depth F from the actual reference reflecting the change of the surface position on the back surface 12A, the base material 12 is broken at a constant residual thickness A. The planned portion 16 is formed. When the groove forming process is completed by moving the groove forming means 34 along the outer peripheral contour of the airbag door, the forming apparatus raises the groove forming means 34 away from the base material 12 and waits for the end mill 34a. Stop rotation.

本実施例の破断予定部形成方法によれば、図1(b)に例示するように、基材12が固定部32aから浮き上がって、基材12と固定部32aとの間に隙間Sが空いている場合であっても、計測手段36により得られた位置データが反映されて、浮き上がり分だけ溝形成手段34が上昇変位されるから、この浮き上がった裏面12Aから加工深さFで溝加工が行なわれる。すなわち、固定部32aに対して基材12が位置ずれしていたとしても、計測手段36により反映された基材12の裏面12Aにおける現状の面位置を基準として、溝18を所定深さFで切削することで、破断予定部16を全体として一定の残留厚さAだけ残した状態で精度良く基材12に形成することができる。このように、破断予定部16を全体として一定の残留厚さAで形成し得るから、エアバッグ装置の作動時にエアバッグドアが迅速かつ確実に展開して安定した乗員保護性能を発揮し得る。また、エアバッグ装置の作動前では、基材の一部として適切に構成されるから、車両内装部材について変形等により質感の低下を招くことはない。   According to the method for forming a planned fracture portion of the present embodiment, as illustrated in FIG. 1B, the base material 12 is lifted from the fixing portion 32a, and a gap S is left between the base material 12 and the fixing portion 32a. Even in this case, the position data obtained by the measuring means 36 is reflected, and the groove forming means 34 is lifted and displaced by the lifted amount. Therefore, the groove processing is performed at the processing depth F from the lifted back surface 12A. Done. That is, even if the base material 12 is displaced with respect to the fixed portion 32a, the groove 18 is formed at a predetermined depth F with reference to the current surface position on the back surface 12A of the base material 12 reflected by the measuring means 36. By cutting, it can form in the base material 12 with sufficient precision in the state which left only the fixed residual thickness A as the whole fracture | rupture scheduled part 16. FIG. As described above, since the portion to be broken 16 can be formed with a constant residual thickness A as a whole, the airbag door can be quickly and reliably deployed during the operation of the airbag apparatus, and stable occupant protection performance can be exhibited. In addition, since the air bag apparatus is appropriately configured as a part of the base material before the operation of the airbag apparatus, the vehicle interior member is not deteriorated in texture due to deformation or the like.

また実施例の計測手段36は、溝形成手段34の進行方向前側に配設されると共に、基材12の裏面12Aにおける溝形成手段34の進行方向前側で、該溝形成手段34による溝18の加工を行なう部位を読取っている。すなわち形成装置は、基材12のまさに溝18を加工する部位の位置データに基づいて、基準が設定されて溝形成手段34を進退移動するから、基材12に更に精度良く破断予定部16を形成することができる。   In addition, the measuring means 36 of the embodiment is disposed on the front side in the traveling direction of the groove forming means 34, and on the front side in the traveling direction of the groove forming means 34 on the back surface 12 </ b> A of the base material 12. The part to be processed is read. That is, the forming apparatus moves the groove forming means 34 forward and backward based on the position data of the portion of the base material 12 where the groove 18 is to be processed. Can be formed.

しかも前記計測手段36は、溝加工を行なう側の面である基材12の裏面12Aを計測するものであるから、固定部32aの上方の開放された空間に配設することができ、配設スペースの制約が少ない。すなわち、計測手段36を溝形成手段34の溝加工の進行に伴って移動するように配設可能であり、1つの計測手段36で、破断予定部16を形成する際の全体に亘って基材12の裏面12Aの読取りを行なうことができる。また、破断予定部16の形状の変更や基材12の形状の変更等による基材12の裏面12Aにおける計測位置の段取り替えに対し、スムーズに対応することができる。特に、計測手段36を溝形成手段34に一体的に配設して、溝形成手段34に連動して移動するように構成することで、計測手段36を移動させる手段を省略でき、溝形成手段34に追随して移動するから、計測位置の段取り替えを考える必要がない。   Moreover, since the measuring means 36 measures the back surface 12A of the base material 12, which is the surface on which grooves are processed, it can be disposed in the open space above the fixed portion 32a. There are few space restrictions. That is, the measuring means 36 can be disposed so as to move as the groove forming means 34 proceeds with the groove processing, and the base material is formed over the whole when the planned fracture portion 16 is formed by one measuring means 36. 12 back surface 12A can be read. In addition, it is possible to smoothly cope with the changeover of the measurement position on the back surface 12A of the base 12 due to a change in the shape of the planned fracture portion 16 or a change in the shape of the base 12. In particular, by arranging the measuring means 36 integrally with the groove forming means 34 so as to move in conjunction with the groove forming means 34, the means for moving the measuring means 36 can be omitted, and the groove forming means Since it moves following 34, it is not necessary to consider the changeover of the measurement position.

前記形成装置は、基材12の固定部32aに対する位置ずれに対応し得るので、比較的硬質な基材12であっても治具で固定部32aに押え付ける必要はなく、固定部32aの形状についても基材12の形状に厳密に追随させる高い精度は要求されない。なお、溝形成手段34としてエンドミルを利用したミーリング加工機を採用することで、レーザー加工と比較して設備を簡易にすることができ、コストを低減することができる利点がある。   Since the forming apparatus can cope with a positional shift of the base material 12 with respect to the fixing portion 32a, there is no need to press the fixing portion 32a with a jig even if the base material 12 is relatively hard. In addition, a high accuracy for strictly following the shape of the substrate 12 is not required. By adopting a milling machine using an end mill as the groove forming means 34, there is an advantage that equipment can be simplified and costs can be reduced as compared with laser processing.

(変更例)
(1)実施例では、溝形成手段の基材に対する進退移動制御を、計測手段による基材の裏面の位置データのみに基づいて行なうように構成したが、溝形成手段の基材に対する進退移動制御を、基本的に制御手段の設定情報に基づいて行ない、計測手段により求めた位置データと設定情報との間に差異がある場合に位置データに合わせて溝形成手段を進退して補正することで、位置データによる基準に合わせて溝の加工深さを一定とする構成であってもよい。このような変更例の形成装置では、基材に浮き上がりが生じた場合に、基材の裏面における位置データが設定情報より上方にずれるのに対応して、基材12の浮きの差分だけ基準が変化する。そして制御手段は、溝形成手段を浮きの差分だけ基材に対して進退移動させた後、所定の加工深さで溝を形成することで、破断予定部の残留厚さを常に一定することができる。
(Example of change)
(1) In the embodiment, the forward / backward movement control of the groove forming means with respect to the base material is performed based only on the position data of the back surface of the base material by the measuring means. Is basically performed based on the setting information of the control means, and when there is a difference between the position data obtained by the measurement means and the setting information, the groove forming means is advanced and retracted according to the position data to correct The groove processing depth may be constant according to the reference based on the position data. In such a modified example of the forming apparatus, when the base material is lifted, the reference is based on the difference of the base material 12 in accordance with the position data on the back surface of the base material being shifted upward from the setting information. Change. Then, the control means moves the groove forming means forward and backward with respect to the base material by the difference in floating, and then forms the groove at a predetermined processing depth, so that the residual thickness of the planned fracture portion can be always constant. it can.

(2)実施例では、固定手段に保持した基材に対して、溝形成手段が移動するよう構成したが、固定手段を溝形成手段に対して移動させても、溝形成手段および固定手段を複合的に移動させて、溝形成手段と基材との位置関係を変位させてもよい。
(3)溝形成手段は、水平および垂直方向へ直交変位する3軸の移動態様でけでなく、基材の形状または位置ずれに合わせて三次元的に変位し得る態様であれば、ロボットアームの如く多軸の態様やその他の態様であっても採用し得る。
(4)溝形成手段としてミーリング加工機を採用した態様では、溝形成手段自身を基材に対して進退移動することで、基準の更新に対応して溝加工を行なうよう構成したが、これに変えて溝形成手段としてレーザー照射器を採用した場合は、溝形成手段を基材に対して進退移動することなく、基材に照射するレーザーの出力調節だけで行なうことができる。すなわち、レーザー照射器から照射するレーザーの出力を小さくすることで、基材の裏面における溝形成手段に近接する方向への変位(上昇)に対応して、溝加工を行なうことができる。反対に、レーザー照射器から照射するレーザーの出力を大きくすることで、基材の裏面における溝形成手段から離間する方向への変位(下降)に対応して、溝加工を行なうことができる。なお、レーザーの出力調節だけでなく、溝形成手段を基材に対して進退移動する構成を併用してもよい。
(2) In the embodiment, the groove forming means moves with respect to the base material held by the fixing means. However, even if the fixing means is moved with respect to the groove forming means, the groove forming means and the fixing means are not moved. The positional relationship between the groove forming means and the substrate may be displaced by moving in a complex manner.
(3) The groove forming means is not limited to a three-axis movement mode that is orthogonally displaced in the horizontal and vertical directions, but may be a robot arm as long as it can be displaced three-dimensionally in accordance with the shape or displacement of the substrate. As described above, it is possible to adopt a multiaxial aspect and other aspects.
(4) In the aspect in which the milling machine is adopted as the groove forming means, the groove forming means itself is moved forward and backward with respect to the base material to perform groove processing corresponding to the update of the reference. If a laser irradiator is adopted as the groove forming means, the adjustment can be performed only by adjusting the output of the laser irradiating the substrate without moving the groove forming means forward and backward. That is, by reducing the output of the laser irradiated from the laser irradiator, the groove processing can be performed corresponding to the displacement (rise) in the direction close to the groove forming means on the back surface of the substrate. On the contrary, by increasing the output of the laser irradiated from the laser irradiator, the groove processing can be performed in response to the displacement (lowering) in the direction away from the groove forming means on the back surface of the substrate. In addition to adjusting the output of the laser, a configuration in which the groove forming means moves forward and backward with respect to the substrate may be used in combination.

本発明の好適な実施例に係るエアバッグドアの破断予定部形成装置を示す概略図である。It is the schematic which shows the fracture part formation apparatus of the airbag door which concerns on the preferred Example of this invention. インストルメントパネルを構成する基材に一体成形されたエアバッグドアを例示した断面図である。It is sectional drawing which illustrated the airbag door integrally molded by the base material which comprises an instrument panel. 従来のエアバッグドアにおける破断予定部の切削装置を示す概略図である。It is the schematic which shows the cutting device of the fracture part in the conventional airbag door.

符号の説明Explanation of symbols

12 基材,12A 裏面(一方の面),16 破断予定部,18 溝,
34 溝形成手段,36 計測手段,38 制御手段
12 base material, 12A back surface (one surface), 16 fracture planned part, 18 groove,
34 groove forming means, 36 measuring means, 38 control means

Claims (4)

制御手段(38)で移動制御される溝形成手段(34)により、車両用内装部材を構成する基材(12)の一方の面(12A)に所定深さの溝(18)を加工することで、エアバッグドアの破断予定部(16)を形成する方法であって、
溝加工に先立ち、前記一方の面(12A)における前記溝形成手段(34)により溝加工を行なう直前部位の面位置を、計測手段(36)により該一方の面(12A)側から求めて、その位置データを前記制御手段(38)へ出力し、
前記制御手段(38)は、前記計測手段(36)からの位置データの入力に伴って逐次更新される基準に基づき、前記溝形成手段(34)による加工を制御することで、前記一方の面(12A)からの溝(18)の加工深さを一定とするようにした
ことを特徴とするエアバッグドアの破断予定部形成方法。
A groove (18) having a predetermined depth is formed on one surface (12A) of the base material (12) constituting the vehicle interior member by the groove forming means (34) whose movement is controlled by the control means (38). And a method of forming the expected breakage portion (16) of the airbag door,
Prior to grooving, the surface position of the portion immediately before grooving by the groove forming means (34) on the one surface (12A) is obtained from the one surface (12A) side by the measuring means (36), Output the position data to the control means (38),
The control means (38) controls the processing by the groove forming means (34) based on a reference that is sequentially updated with the input of position data from the measurement means (36), thereby the one surface. A method for forming a scheduled breakage portion of an airbag door, characterized in that the processing depth of the groove (18) from (12A) is made constant.
前記制御手段(38)は、更新された基準が前の基準と比較して前記溝形成手段(34)に近接すると判断される場合は、これに応じて前記溝形成手段(34)が基材(12)から退く方向に移動するよう制御され、更新された基準が前の基準と比較して前記溝形成手段(34)から離間すると判断される場合は、これに応じて前記溝形成手段(34)が基材(12)へ向けて進む方向に移動するよう制御される請求項1記載のエアバッグドアの破断予定部形成方法。   When it is determined that the updated reference is closer to the groove forming means (34) than the previous reference, the control means (38) is configured so that the groove forming means (34) responds accordingly. If it is determined that the updated reference is moved away from the groove forming means (34) compared to the previous reference, the groove forming means ( The method for forming a scheduled breakage portion of an airbag door according to claim 1, wherein 34) is controlled to move in a direction of proceeding toward the base material (12). 前記計測手段(36)は、前記溝形成手段(34)に連動して移動し、該計測手段(36)と前記基材(12)の一方の面(12A)との間の距離を測定することで、該一方の面(12A)の面位置を求めるようにした請求項1または2記載のエアバッグドアの破断予定部形成方法。   The measuring means (36) moves in conjunction with the groove forming means (34), and measures the distance between the measuring means (36) and one surface (12A) of the substrate (12). The method of forming a scheduled breakage portion of the airbag door according to claim 1 or 2, wherein the surface position of the one surface (12A) is obtained. 制御手段(38)で移動制御される溝形成手段(34)により、車両用内装部材を構成する基材(12)の一方の面(12A)に所定深さの溝(18)を加工することで、エアバッグドアの破断予定部(16)を形成する装置であって、
前記溝形成手段(34)に連動して移動するように配設され、前記一方の面(12A)における前記溝形成手段(34)により溝加工を行なう直前部位の面位置を該一方の面(12A)側から求め、その位置データを前記制御手段(38)へ出力する計測手段(36)を備え、
前記制御手段(38)は、前記計測手段(36)からの位置データの入力に伴って逐次更新される基準に基づき前記溝形成手段(34)による加工を制御することで、前記一方の面(12A)からの溝(18)の加工深さを一定とするよう構成した
ことを特徴とするエアバッグドアの破断予定部形成装置。
A groove (18) having a predetermined depth is formed on one surface (12A) of the base material (12) constituting the vehicle interior member by the groove forming means (34) whose movement is controlled by the control means (38). And an apparatus for forming the scheduled breakage portion (16) of the airbag door,
It is arranged to move in conjunction with the groove forming means (34), and the surface position of the one surface (12A) immediately before performing groove processing by the groove forming means (34) on the one surface ( 12A) from the side, comprising the measurement means (36) for outputting the position data to the control means (38),
The control means (38) controls the processing by the groove forming means (34) based on a reference that is sequentially updated with the input of position data from the measurement means (36), thereby the one surface ( An apparatus for forming a scheduled breakage portion of an airbag door, characterized in that the processing depth of the groove (18) from 12A) is constant.
JP2005317337A 2005-10-31 2005-10-31 Method and device for forming fracture scheduled part of airbag door Pending JP2007118893A (en)

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Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2016186467A (en) * 2015-03-27 2016-10-27 カルソニックカンセイ株式会社 Air bag door weak line residual thickness measuring device and measuring method
CN107617771A (en) * 2016-07-15 2018-01-23 首都航天机械公司 A kind of low deformation processing method of large aluminum alloy thin-walled mesh cylinder section

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2016186467A (en) * 2015-03-27 2016-10-27 カルソニックカンセイ株式会社 Air bag door weak line residual thickness measuring device and measuring method
CN107617771A (en) * 2016-07-15 2018-01-23 首都航天机械公司 A kind of low deformation processing method of large aluminum alloy thin-walled mesh cylinder section
CN107617771B (en) * 2016-07-15 2019-07-12 首都航天机械公司 A low-deformation machining method for a large aluminum alloy thin-walled grid cylinder section

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