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JP4067740B2 - Airbag device for vehicle - Google Patents
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JP4067740B2 - Airbag device for vehicle - Google Patents

Airbag device for vehicle Download PDF

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Publication number
JP4067740B2
JP4067740B2 JP2000147634A JP2000147634A JP4067740B2 JP 4067740 B2 JP4067740 B2 JP 4067740B2 JP 2000147634 A JP2000147634 A JP 2000147634A JP 2000147634 A JP2000147634 A JP 2000147634A JP 4067740 B2 JP4067740 B2 JP 4067740B2
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Japan
Prior art keywords
kgf
line
airbag
barrier layer
cleavage line
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Expired - Fee Related
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JP2000147634A
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Japanese (ja)
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JP2001328502A (en
Inventor
和弘 斉藤
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Marelli Corp
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Calsonic Kansei Corp
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Priority to JP2000147634A priority Critical patent/JP4067740B2/en
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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B60VEHICLES IN GENERAL
    • B60RVEHICLES, VEHICLE FITTINGS, OR VEHICLE PARTS, NOT OTHERWISE PROVIDED FOR
    • B60R21/00Arrangements or fittings on vehicles for protecting or preventing injuries to occupants or pedestrians in case of accidents or other traffic risks
    • B60R21/02Occupant safety arrangements or fittings, e.g. crash pads
    • B60R21/16Inflatable occupant restraints or confinements designed to inflate upon impact or impending impact, e.g. air bags
    • B60R21/20Arrangements for storing inflatable members in their non-use or deflated condition; Arrangement or mounting of air bag modules or components
    • B60R21/215Arrangements for storing inflatable members in their non-use or deflated condition; Arrangement or mounting of air bag modules or components characterised by the covers for the inflatable member
    • B60R21/2165Arrangements for storing inflatable members in their non-use or deflated condition; Arrangement or mounting of air bag modules or components characterised by the covers for the inflatable member characterised by a tear line for defining a deployment opening
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23KSOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K26/00Working by laser beam, e.g. welding, cutting or boring
    • B23K26/36Removing material
    • B23K26/362Laser etching
    • B23K26/364Laser etching for making a groove or trench, e.g. for scribing a break initiation groove
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23KSOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K26/00Working by laser beam, e.g. welding, cutting or boring
    • B23K26/36Removing material
    • B23K26/40Removing material taking account of the properties of the material involved
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23KSOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K2103/00Materials to be soldered, welded or cut
    • B23K2103/16Composite materials
    • B23K2103/166Multilayered materials
    • B23K2103/172Multilayered materials wherein at least one of the layers is non-metallic

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  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Optics & Photonics (AREA)
  • Mechanical Engineering (AREA)
  • Plasma & Fusion (AREA)
  • Laser Beam Processing (AREA)
  • Air Bags (AREA)

Description

【0001】
【発明の属する技術分野】
この発明は、自動車等の車両に取付けられる車両用エアバッグ装置に関するものである。
【0002】
【従来の技術】
自動車等の車両には、緊急時の安全手段としてエアバッグ装置を備えたものがある。上記エアバッグ装置は、車体に所定値以上の衝撃力が加わったときに、インストルメントパネル等の内部に配設されたハウジングに折り畳んで収納されているエアバッグ本体が、インフレータからの圧力気体の圧力によって車室内乗員側へ膨出して、定位置に着座している乗員の頭部等を受け止め、頭部等がインストルメントパネル等に当接しないように保護するものである。
【0003】
そして、上記エアバッグ本体は、膨出時に、インストルメントパネルに形成されたエアバッグリッド部を押圧し、エアバッグリッド部に形成された開裂線を開裂することにより膨出開口を形成し、該膨出開口から車室内乗員側へ膨出されるようになっている。
【0004】
上記エアバッグ装置には、特開平9−156443号公報等のように、表皮層と中間層とバリア層とを備えた多層ラミネートシートの裏面に芯材を溶着してエアバッグリッド部を構成し、このエアバッグリッド部の裏面側からバリア層を越える深さに溝状の開裂線を形成したものがある。
【0005】
【発明が解決しようとする課題】
しかしながら、上記公報のエアバッグ装置では、破断性を確保するため開裂線を、バリア層を越える深さとしているが、芯材と多層ラミネートシートのバリア層とは線膨張係数が異なるため、熱変形時にバリア層が切断された開裂線加工部分に応力が集中し、エアバッグリッド部の表面外観性能を損うことになる。
【0006】
そのため、エアバッグリッド部の開裂線と対応する表面側の位置にキャラクターラインを形成して、エアバッグリッド部の熱変形が目立ちにくくなるようにしている。
【0007】
そこで、本発明の目的は、上記の問題点を解消し、多層ラミネートシートを用いたエアバッグリッド部の熱変形による外観品質の低下を防止することのできる車両用エアバッグ装置を提供することにある。
【0008】
【課題を解決するための手段】
上記課題を解決するために、請求項1に記載された発明では、少なくとも表皮層と発泡体層とバリア層とを備えた多層ラミネートシートの裏面に、前記バリア層とは線熱膨張係数の異なる芯材を溶着してエアバッグリッド部を構成し、溶着された状態の該エアバッグリッド部の裏面側から溝状の開裂線を形成した車両用エアバッグ装置において、前記開裂線は、前記多層ラミネートシートの表面にキャラクターラインがなく、前記芯材の裏面に薄肉部がない、均一肉厚の部分に対し、エアバッグリッド部の裏面側から形成されると共に、前記開裂線は、熱変形時の開裂線加工部分への応力集中が防止されるように、前記芯材を貫通しかつ前記バリア層の一部が残存する深さまで連続して形成され、前記エアバッグリッド部は、開裂線と対応する表面側の位置にキャラクターラインがない、でなだらかな表面形状とされたことを特徴としている。
【0009】
このように構成された請求項1にかかる発明によれば、少なくとも表皮層と発泡体層とバリア層とを備えた多層ラミネートシートの裏面に、前記バリア層とは線熱膨張係数の異なる芯材を溶着してエアバッグリッド部を構成し、溶着された状態の該エアバッグリッド部の裏面側から溝状の開裂線を形成した車両用エアバッグ装置において、前記開裂線は、前記多層ラミネートシートの表面にキャラクターラインがなく、前記芯材の裏面に薄肉部がない、均一肉厚の部分に対し、エアバッグリッド部の裏面側から形成されると共に、前記開裂線は、熱変形時の開裂線加工部分への応力集中が防止されるように、前記芯材を貫通しかつ前記バリア層の一部が残存する深さまで連続して形成され、前記エアバッグリッド部は、開裂線と対応する表面側の位置にキャラクターラインがない、でなだらかな表面形状とされたことにより、以下のような、作用効果を得ることができる。即ち、バリア層が切断されずに残っているので、熱変形時に開裂線加工部分に応力が集中することが防止され、エアバッグリッド部の表面外観性能が低下する(開裂線加工部分にシワやたるみや歪み等の表面外観性能低下部分が生じる)ことが防止される。よって、エアバッグリッド部を、開裂線と対応する表面側の位置に、エアバッグリッド部の熱変形を目立ちにくくするためのキャラクターライン等がない、ほぼ平でなだらかな表面形状とすることができるようになる。
【0010】
また、上記課題を解決するために、請求項2に記載された発明では、請求項1に加え、前記開裂線は、レーザ加工により成形されていることを特徴としている。
【0011】
このように構成された請求項2にかかる発明によれば、レーザ加工による開裂線成形であるため、芯材が多少硬い材質であっても確実に開裂線が形成できる。
【0012】
【発明の実施の形態1】
以下、本発明の具体的な実施の形態1について、図示例と共に説明する。
【0013】
図1〜図5は、この発明の実施の形態1を示すものである。
【0014】
先ず、構成を説明すると、自動車等の車両における車室の前部でかつフロントウインドウガラス1の下部には図1、図2に示すようなインストルメントパネル2が設けられている。このインストルメントパネル2にはエアバッグ膨出用開口3が形成されている。そして、このインストルメントパネル2に対し、エアバッグ膨出用開口3を塞ぐエアバッグリッド部4と、エアバッグモジュール5とからなるエアバッグ装置6が取付けられる。
【0015】
上記インストルメントパネル2は、例えば、芯材7の表面に表皮8を貼着したものである。
【0016】
上記エアバッグリッド部4は、例えば、表皮層10と中間層となる発泡体層11とバリア層12とを有する多層ラミネートシート13を予めエアバッグリッド部4の形状に成形し、この多層ラミネートシート13を射出成形型へ入れて裏面に、バリア層12とは線熱膨張係数の異なる芯材14を射出成形により溶着した構成を備えている。このエアバッグリッド部4の裏面には、溝状の開裂線15が平面視H字状又はU字状等に形成される。
【0017】
表皮層10は厚さを0.05mm〜1.5mm、好ましくは、0.1mm〜1.0mmとする。中間層11としての発泡体層は厚さを1.0mm〜5.0mmとする。バリア層12は厚さを0.1mm〜2.0mmとする。
【0018】
表皮層10に、−40℃での引張強さが250×9.8N/cm2(250Kgf/cm2)〜500×9.8N/cm2(500Kgf/cm2)で、伸び率が50%以上で、引裂強さが10×9.8N/cm2(10Kgf/cm2)以上で、23℃での引張強さが50×9.8N/cm2(50Kgf/cm2)〜100×9.8N/cm2(100Kgf/cm2)で、伸び率が100%以上で、引裂強さが10×9.8N/cm2(10Kgf/cm2)以上で、85℃での引張強さが10×9.8N/cm2(10Kgf/cm2)〜100×9.8N/cm2(100Kgf/cm2)で、伸び率が150%〜500%で、引裂強さが5×9.8N/cm2(5Kgf/cm2)以上の素材を用いる。
【0019】
また、バリア層12に、−40℃での引張強さが130×9.8N/cm2(130Kgf/cm2)〜400×9.8N/cm2(400Kgf/cm2)(好ましくは250Kgf/cm2〜310Kgf/cm2)で、伸び率が65%〜350%(好ましくは100%〜230%)で、引裂強さが65×9.8N/cm2(65Kgf/cm2)〜350×9.8N/cm2(350Kgf/cm2)(好ましくは150Kgf/cm2〜280Kgf/cm2)で、23℃での引張強さが70×9.8N/cm2(70Kgf/cm2)〜250×9.8N/cm2(250Kgf/cm2)(好ましくは130Kgf/cm2〜200Kgf/cm2)で、伸び率が200%〜800%(好ましくは450%〜580%)で、引裂強さが40×9.8N/cm2(40Kgf/cm2)〜150×9.8N/cm2(150Kgf/cm2)(好ましくは40Kgf/cm2〜120Kgf/cm2)で、85℃での引張強さが10×9.8N/cm2(10Kgf/cm2)〜150×9.8N/cm2(150Kgf/cm2)(好ましくは250Kgf/cm2〜350Kgf/cm2)で、伸び率が150%〜450%(好ましくは250%〜350%)で、引裂強さが10×9.8N/cm2(10Kgf/cm2)〜100×9.8N/cm2(100Kgf/cm2)(好ましくは10Kgf/cm2〜50Kgf/cm2)の素材を用いる。
【0020】
また、表皮10に、−20℃での引張強さが200×9.8N/cm2(200Kgf/cm2)〜450×9.8N/cm2(450Kgf/cm2)(好ましくは300Kgf/cm2)で、伸び率が70%以上(好ましくは500%)で、引裂強さが10×9.8N/cm2(10Kgf/cm2)以上(好ましくは10Kgf/cm2)で、23℃での引張強さが50×9.8N/cm2(50Kgf/cm2)〜100×9.8N/cm2(100Kgf/cm2)で、伸び率が100%以上で、引裂強さが10×9.8N/cm2(10Kgf/cm2)以上で、85℃での引張強さが10×9.8N/cm2(10Kgf/cm2)〜100×9.8N/cm2(100Kgf/cm2)で、伸び率が150%〜500%で、引裂強さが5×9.8N/cm2(5Kgf/cm2)以上の素材を用いる。
【0021】
また、バリア層12に、−20℃での引張強さが200×9.8N/cm2(200Kgf/cm2)〜450×9.8N/cm2(450Kgf/cm2)(好ましくは340Kgf/cm2〜310Kgf/cm2)で、伸び率が200%〜800%(好ましくは500%)で、引裂強さが50×9.8N/cm2(50Kgf/cm2)以上(好ましくは50Kgf/cm2)で、23℃での引張強さが70×9.8N/cm2(70Kgf/cm2)〜250×9.8N/cm2(250Kgf/cm2)(好ましくは130Kgf/cm2〜200Kgf/cm2)で、伸び率が200%〜800%(好ましくは450%〜580%)で、引裂強さが40×9.8N/cm2(40Kgf/cm2)〜150×9.8N/cm2(150Kgf/cm2)(好ましくは40Kgf/cm2〜120Kgf/cm2)で、85℃での引張強さが10×9.8N/cm2(10Kgf/cm2)〜150×9.8N/cm2(150Kgf/cm2)(好ましくは250Kgf/cm2〜350Kgf/cm2)で、伸び率が150%〜450%(好ましくは250%〜350%)で、引裂強さが10×9.8N/cm2(10Kgf/cm2)〜100×9.8N/cm2(100Kgf/cm2)(好ましくは10Kgf/cm2〜50Kgf/cm2)の素材を用いてもよい。
【0022】
そのため、バリア層12としては、PPCや、オレフィン系(TEO)TPOエラストマーや、スチレン系(TES)TPSや、ポリエステル系/スチレン系TPE等の素材を用いる。
【0023】
素材の一例として、表皮層10を(TEO)TPO、TPS、PVC、PVC/S・E・B・S系(複合材)、発泡体層11をPPF、PE/PPF、PVCF(塩化ビニール発泡体)、バリア層12を(TEO)TPO、TPS、PPC(複合材)、芯材14をPPC、PPGとする組合せとする。
【0024】
また、素材の他の例として、表皮層10を(TEO)TPO、TPS、PVCPVC/S・E・B・S系(スチレン系)、発泡体層11をEP/PPF、EP/PPF/S・E・B・S系(スチレン系)、バリア層12をPVC/ABS、PPO/S・E・B・S系(スチレン系)、芯材14をPPOG、PC/ABS、ABS、PCとする組合せとする。
【0025】
そして、インストルメントパネル2の芯材14におけるエアバッグ膨出用開口3の部分に、金属製の補強部材16とエアバッグ膨出用開口3を塞ぐドア部材17とがボルト18で固定される。この補強部材16にエアバッグモジュール5がボルト20で接続される。また、エアバッグモジュール5はその下部を図示しないステアリングサポートメンバ等の車体側メンバに固定される。
【0026】
上記エアバッグモジュール5は、圧力気体を噴出するインフレータを収納するインフレータ収納部25と、インフレータからの圧力気体によって展開するエアバッグ本体を収納するエアバッグ本体収納部26とを備えている。
【0027】
この実施の形態1では、上記開裂線15は、上記多層ラミネートシート13の表面にキャラクターライン等がなく、上記芯材14の裏面に薄肉部等がない、ほぼ均一肉厚の部分に対し、エアバッグリッド部4の裏面側から形成される。また、上記開裂線15は、熱変形時の開裂線15の加工部分への応力集中が防止されるように、芯材14を貫通しかつバリア層12の一部が残存する深さまで連続して形成されている(残存部30)。残存部30の肉厚は、例えば、バリア層12の設定肉厚の10%〜90%程度とする。例えば、バリア層12の設定肉厚を1.2mmとした場合、残存部30の肉厚は、0.6±0.5mm、より好ましくは、0.6±0.3mmとする。そして、エアバッグリッド部4は、開裂線15と対応する表面側の位置にキャラクターライン等がない、ほぼ平でなだらかな表面形状とされる。
【0028】
開裂線15は、エアバッグリッド部4を裏返しにして、図4に示すようなレーザー加工機35や、図5に示すような熱刃36又は超音波加工機や、回転カッター刃や、高周波ウェルダー等を用いる。この際、図5に示すように、エアバッグリッド部4を載置する受け台37に真空路38を形成して真空吸引装置39で真空引きするようにしてもよい。また、開裂線加工機として、回転ツール(リュータやエンドミル等)を用いてもよい。この場合も、レーザ加工と略同様に、芯材が多少硬い材質であっても確実に開裂線が形成できる。
【0029】
次に、この実施の形態1の作用について説明する。
【0030】
インフレータが作動すると、このインフレータから圧力気体が噴出され、エアバッグ本体内へと圧力気体が導入される。
【0031】
エアバッグ本体は、この圧力気体の導入に伴って膨張し、この膨張の圧力により先ずドア部材17及びエアバッグリッド部4が開裂線15に沿って開裂されて膨出開口が形成されると同時に、この膨出開口からエアバッグ本体が、車体斜め後方(車室内乗員側)へ向かって膨出する。これによって、エアバッグ本体は定位置に着座している助手席側の乗員の頭部等を受け止め、頭部等がインストルメントパネル2等に当接しないように保護する。
【0032】
そして、この実施の形態1では、開裂線15を、上記多層ラミネートシート13の表面にキャラクターライン等がなく、上記芯材14の裏面に薄肉部等がない、ほぼ均一肉厚の部分に対し、エアバッグリッド部4の裏面側から形成し、開裂線15を、熱変形時の開裂線加工部分への応力集中が防止されるように、芯材14を貫通しかつバリア層12の一部が残存する深さまで連続して形成し、エアバッグリッド部4を、開裂線15と対応する表面側の位置にキャラクターライン等がない、ほぼ平でなだらかな表面形状としたことにより、以下のような、作用効果を得ることができる。即ち、バリア層12が切断されずに残っているので、熱変形時に開裂線15加工部分に応力が集中することが防止され、エアバッグリッド部4の表面外観性能が低下する(開裂線15加工部分にシワやたるみや歪み等の表面外観性能低下部分が生じる)ことが防止される。よって、エアバッグリッド部4を、開裂線15と対応する表面側の位置に、エアバッグリッド部4の熱変形を目立ちにくくするためのキャラクターライン等がない、ほぼ平でなだらかな表面形状とすることができるようになる。
【0033】
また、レーザ加工による開裂線15の成形であるため、芯材が多少硬い材質であっても確実に開裂線15が形成できる。
【0034】
【発明の効果】
以上説明してきたように、請求項1の発明によれば、少なくとも表皮層と発泡体層とバリア層とを備えた多層ラミネートシートの裏面に、前記バリア層とは線熱膨張係数の異なる芯材を溶着してエアバッグリッド部を構成し、溶着された状態の該エアバッグリッド部の裏面側から溝状の開裂線を形成した車両用エアバッグ装置において、前記開裂線は、前記多層ラミネートシートの表面にキャラクターラインがなく、前記芯材の裏面に薄肉部がない、均一肉厚の部分に対し、エアバッグリッド部の裏面側から形成されると共に、前記開裂線は、熱変形時の開裂線加工部分への応力集中が防止されるように、前記芯材を貫通しかつ前記バリア層の一部が残存する深さまで連続して形成され、前記エアバッグリッド部は、開裂線と対応する表面側の位置にキャラクターラインがない、でなだらかな表面形状とされたことにより、以下のような、作用効果を得ることができる。即ち、バリア層が切断されずに残っているので、熱変形時に開裂線加工部分に応力が集中することが防止され、エアバッグリッド部の表面外観性能が低下する(開裂線加工部分にシワやたるみや歪み等の表面外観性能低下部分が生じる)ことが防止される。よって、エアバッグリッド部を、開裂線と対応する表面側の位置に、エアバッグリッド部の熱変形を目立ちにくくするためのキャラクターライン等がない、ほぼ平でなだらかな表面形状とすることができるようになる。また、請求項2の発明によれば、レーザ加工による開裂線成形であるため、芯材が多少硬い材質であっても確実に開裂線が形成できる、という実用上有益な効果を発揮し得る。
【図面の簡単な説明】
【図1】本発明の実施の形態1にかかるインストルメントパネルの斜視図である。
【図2】図1のエアバッグ装置の側方断面図である。
【図3】図2の部分拡大図である。
【図4】開裂線の加工状態を示す図である。
【図5】開裂線の加工状態を示す他の図である。
【符号の説明】
4 エアバッグリッド部
10 表皮層
11 中間層
12 バリア層
13 多層ラミネートシート
14 芯材
15 開裂線
30 残存部
[0001]
BACKGROUND OF THE INVENTION
The present invention relates to a vehicle airbag device attached to a vehicle such as an automobile.
[0002]
[Prior art]
Some vehicles such as automobiles have an airbag device as a safety means in an emergency. In the airbag device, when an impact force of a predetermined value or more is applied to the vehicle body, the airbag main body folded and housed in a housing disposed inside an instrument panel or the like has a pressure gas from the inflator. It bulges out toward the passenger in the passenger compartment due to the pressure, receives the head of an occupant seated at a fixed position, and protects the head from being in contact with the instrument panel or the like.
[0003]
The airbag body presses the airbag grid portion formed on the instrument panel at the time of inflation, and forms an inflation opening by cleaving a tear line formed on the airbag grid portion. It is designed to bulge from the opening toward the passenger in the passenger compartment.
[0004]
In the airbag device, as in JP-A-9-156443, a core material is welded to the back surface of a multilayer laminate sheet having a skin layer, an intermediate layer, and a barrier layer to constitute an airbag grid portion, There is one in which a groove-shaped cleavage line is formed at a depth beyond the barrier layer from the back side of the airbag grid portion.
[0005]
[Problems to be solved by the invention]
However, in the airbag device of the above publication, the cleavage line has a depth exceeding the barrier layer in order to ensure breakability, but the linear expansion coefficient is different between the core material and the barrier layer of the multilayer laminate sheet, so that the thermal deformation Sometimes stress concentrates on the cleavage line processed part where the barrier layer is cut, and the surface appearance performance of the air bag grid part is impaired.
[0006]
For this reason, a character line is formed at a position on the surface side corresponding to the cleavage line of the airbag grid portion so that the thermal deformation of the airbag grid portion is less noticeable.
[0007]
Accordingly, an object of the present invention is to provide a vehicle airbag device that can solve the above-described problems and prevent deterioration in appearance quality due to thermal deformation of an airbag grid portion using a multilayer laminate sheet. .
[0008]
[Means for Solving the Problems]
In order to solve the above-mentioned problems, in the invention described in claim 1, the linear thermal expansion coefficient differs from that of the barrier layer on the back surface of the multilayer laminate sheet including at least the skin layer, the foam layer, and the barrier layer. In a vehicle airbag apparatus in which a core material is welded to form an air bag grid portion, and a grooved tear line is formed from the back side of the welded airbag grid portion, the tear line is the multilayer laminate sheet There is no character line on the surface of the core material, and there is no thin wall portion on the back surface of the core material, and a uniform thickness portion is formed from the back surface side of the airbag grid portion, and the tear line is a tear line at the time of thermal deformation In order to prevent stress concentration on the processed portion, the core is continuously formed to a depth that penetrates the core material and a part of the barrier layer remains, and the air bag grid portion corresponds to the cleavage line. There is no character line in the position of the surface, it is characterized in that it is a smooth surface shape with flat.
[0009]
According to the invention according to claim 1 configured as described above, a core material having a linear thermal expansion coefficient different from that of the barrier layer on the back surface of the multilayer laminate sheet including at least a skin layer, a foam layer, and a barrier layer. In the vehicle airbag apparatus in which a groove-shaped tear line is formed from the back side of the welded airbag grid part, wherein the tear line is a surface of the multilayer laminate sheet There is no character line, and there is no thin wall portion on the back surface of the core material, whereas the uniform wall thickness portion is formed from the back surface side of the airbag grid portion, and the cleavage line is a cleavage line processed portion during thermal deformation. In order to prevent stress concentration on the surface, the air bag grid portion is formed on the surface corresponding to the cleavage line. There is no character line in the position of, by which is a gentle surface shape flat, such as the following, effects can be obtained. That is, since the barrier layer remains without being cut, stress is prevented from concentrating on the cleavage line processed part during thermal deformation, and the surface appearance performance of the air bag grid part is degraded (wrinkles and sagging in the cleavage line processed part). And the occurrence of a surface appearance performance degradation portion such as distortion is prevented. Therefore, the air bag grid part can be formed into a substantially flat and gentle surface shape without a character line or the like for making the thermal deformation of the air bag grid part inconspicuous at the position on the surface side corresponding to the cleavage line. Become.
[0010]
In order to solve the above-mentioned problem, the invention described in claim 2 is characterized in that, in addition to claim 1, the cleavage line is formed by laser processing.
[0011]
According to the invention according to claim 2 configured as described above, since the cleavage line is formed by laser processing, the cleavage line can be surely formed even if the core material is somewhat hard.
[0012]
DESCRIPTION OF THE PREFERRED EMBODIMENTS Embodiment 1
Hereinafter, a specific first exemplary embodiment of the present invention will be described together with illustrated examples.
[0013]
1 to 5 show a first embodiment of the present invention.
[0014]
First, the configuration will be described. An instrument panel 2 as shown in FIGS. 1 and 2 is provided at the front of a passenger compartment in a vehicle such as an automobile and at the lower part of the front window glass 1. An air bag inflation opening 3 is formed in the instrument panel 2. And the airbag apparatus 6 which consists of the airbag grid part 4 and the airbag module 5 which block | close the opening 3 for airbag expansion | swelling with respect to this instrument panel 2 is attached.
[0015]
The instrument panel 2 is obtained by, for example, attaching a skin 8 to the surface of the core material 7.
[0016]
For example, the airbag grid part 4 is formed by previously forming a multilayer laminate sheet 13 having a skin layer 10, a foam layer 11 serving as an intermediate layer, and a barrier layer 12 into the shape of the airbag grid part 4. It is provided with a configuration in which a core material 14 having a different linear thermal expansion coefficient from that of the barrier layer 12 is welded by injection molding on the back surface in an injection mold. A groove-shaped cleavage line 15 is formed on the back surface of the airbag grid part 4 in an H shape or U shape in a plan view.
[0017]
The skin layer 10 has a thickness of 0.05 mm to 1.5 mm, preferably 0.1 mm to 1.0 mm. The foam layer as the intermediate layer 11 has a thickness of 1.0 mm to 5.0 mm. The barrier layer 12 has a thickness of 0.1 mm to 2.0 mm.
[0018]
The skin layer 10 has a tensile strength at −40 ° C. of 250 × 9.8 N / cm 2 (250 Kgf / cm 2 ) to 500 × 9.8 N / cm 2 (500 Kgf / cm 2 ) and an elongation of 50%. The tear strength is 10 × 9.8 N / cm 2 (10 Kgf / cm 2 ) or more, and the tensile strength at 23 ° C. is 50 × 9.8 N / cm 2 (50 Kgf / cm 2 ) to 100 × 9. 0.8 N / cm 2 (100 Kgf / cm 2 ), elongation of 100% or more, tear strength of 10 × 9.8 N / cm 2 (10 Kgf / cm 2 ) or more, and tensile strength at 85 ° C. 10 × 9.8 N / cm 2 (10 Kgf / cm 2 ) to 100 × 9.8 N / cm 2 (100 Kgf / cm 2 ), elongation is 150% to 500%, and tear strength is 5 × 9.8 N / Cm 2 (5 kgf / cm 2 ) or more of material is used.
[0019]
The barrier layer 12 has a tensile strength at −40 ° C. of 130 × 9.8 N / cm 2 (130 kgf / cm 2 ) to 400 × 9.8 N / cm 2 (400 kgf / cm 2 ) (preferably 250 kgf / cm 2 ). cm 2 to 310 Kgf / cm 2 ), the elongation is 65% to 350% (preferably 100% to 230%), and the tear strength is 65 × 9.8 N / cm 2 (65 Kgf / cm 2 ) to 350 ×. 9.8 N / cm 2 (350 Kgf / cm 2 ) (preferably 150 Kgf / cm 2 to 280 Kgf / cm 2 ) and a tensile strength at 23 ° C. of 70 × 9.8 N / cm 2 (70 Kgf / cm 2 ) to 250 × 9.8 N / cm 2 (250 kgf / cm 2 ) (preferably 130 kgf / cm 2 to 200 kgf / cm 2 ), elongation of 200% to 800% (preferably 450% to 580%), tear strength The In 40 × 9.8N / cm 2 (40Kgf / cm 2) ~150 × 9.8N / cm 2 (150Kgf / cm 2) ( preferably 40Kgf / cm 2 ~120Kgf / cm 2 ), tensile strength at 85 ° C. 10 × 9.8 N / cm 2 (10 Kgf / cm 2 ) to 150 × 9.8 N / cm 2 (150 Kgf / cm 2 ) (preferably 250 Kgf / cm 2 to 350 Kgf / cm 2 ), and the elongation is 150. % To 450% (preferably 250% to 350%), and a tear strength of 10 × 9.8 N / cm 2 (10 Kgf / cm 2 ) to 100 × 9.8 N / cm 2 (100 Kgf / cm 2 ) (preferably Is 10 kgf / cm 2 to 50 kgf / cm 2 ).
[0020]
The tensile strength at −20 ° C. of the skin 10 is 200 × 9.8 N / cm 2 (200 Kgf / cm 2 ) to 450 × 9.8 N / cm 2 (450 Kgf / cm 2 ) (preferably 300 Kgf / cm 2 ) with an elongation of 70% or more (preferably 500%) and a tear strength of 10 × 9.8 N / cm 2 (10 Kgf / cm 2 ) or more (preferably 10 Kgf / cm 2 ) at 23 ° C. The tensile strength is 50 × 9.8 N / cm 2 (50 kgf / cm 2 ) to 100 × 9.8 N / cm 2 (100 kgf / cm 2 ), the elongation is 100% or more, and the tear strength is 10 ×. in 9.8N / cm 2 (10Kgf / cm 2) or more, the tensile strength at 85 ℃ 10 × 9.8N / cm 2 (10Kgf / cm 2) ~100 × 9.8N / cm 2 (100Kgf / cm 2 ) with an elongation of 150% to 500% and tear strength A material having a thickness of 5 × 9.8 N / cm 2 (5 kgf / cm 2 ) or more is used.
[0021]
Further, the barrier layer 12 has a tensile strength at −20 ° C. of 200 × 9.8 N / cm 2 (200 Kgf / cm 2 ) to 450 × 9.8 N / cm 2 (450 Kgf / cm 2 ) (preferably 340 Kgf / cm 2 to 310 Kgf / cm 2 ), an elongation of 200% to 800% (preferably 500%), and a tear strength of 50 × 9.8 N / cm 2 (50 Kgf / cm 2 ) or more (preferably 50 Kgf / cm 2 ). cm 2 ) and a tensile strength at 23 ° C. of 70 × 9.8 N / cm 2 (70 Kgf / cm 2 ) to 250 × 9.8 N / cm 2 (250 Kgf / cm 2 ) (preferably 130 Kgf / cm 2 to 200 Kgf / cm 2 ), elongation is 200% to 800% (preferably 450% to 580%), and tear strength is 40 × 9.8 N / cm 2 (40 Kgf / cm 2 ) to 150 × 9.8 N. / cm 2 (15 Kgf / cm 2) (preferably 40Kgf / cm 2 ~120Kgf / in cm 2), tensile strength at 85 ℃ 10 × 9.8N / cm 2 (10Kgf / cm 2) ~150 × 9.8N / cm 2 (150 kgf / cm 2 ) (preferably 250 kgf / cm 2 to 350 kgf / cm 2 ), an elongation of 150% to 450% (preferably 250% to 350%), and a tear strength of 10 × 9.8 N / Cm 2 (10 Kgf / cm 2 ) to 100 × 9.8 N / cm 2 (100 Kgf / cm 2 ) (preferably 10 Kgf / cm 2 to 50 Kgf / cm 2 ) may be used.
[0022]
Therefore, as the barrier layer 12, materials such as PPC, olefin (TEO) TPO elastomer, styrene (TES) TPS, polyester / styrene TPE are used.
[0023]
As an example of the material, the skin layer 10 is (TEO) TPO, TPS, PVC, PVC / S / E / B / S (composite), and the foam layer 11 is PPF, PE / PPF, PVCF (vinyl chloride foam) ), And the barrier layer 12 is a combination of (TEO) TPO, TPS, PPC (composite material), and the core material 14 is PPC, PPG.
[0024]
As another example of the material, the skin layer 10 is (TEO) TPO, TPS, PVCPVC / S · E · B · S (styrene), and the foam layer 11 is EP / PPF, EP / PPF / S · Combination of E / B / S (styrene), barrier layer 12 as PVC / ABS, PPO / S / E / B / S (styrene), and core 14 as PPOG, PC / ABS, ABS, PC And
[0025]
A metal reinforcing member 16 and a door member 17 that closes the airbag inflation opening 3 are fixed to the portion of the airbag inflation opening 3 in the core member 14 of the instrument panel 2 with bolts 18. The airbag module 5 is connected to the reinforcing member 16 with a bolt 20. The lower part of the airbag module 5 is fixed to a vehicle body side member such as a steering support member (not shown).
[0026]
The airbag module 5 includes an inflator accommodating portion 25 that accommodates an inflator that ejects pressure gas, and an airbag main body accommodating portion 26 that accommodates an airbag main body that is deployed by the pressure gas from the inflator.
[0027]
In the first embodiment, the cleavage line 15 has an air bag against a substantially uniform wall portion where there is no character line or the like on the surface of the multilayer laminate sheet 13 and there is no thin portion or the like on the back surface of the core material 14. It is formed from the back side of the grid part 4 . In addition, the cleavage line 15 is continuously penetrated to a depth that penetrates the core material 14 and a part of the barrier layer 12 remains so as to prevent stress concentration on the processed portion of the cleavage line 15 during thermal deformation. It is formed (remaining part 30). The thickness of the remaining portion 30 is, for example, about 10% to 90% of the set thickness of the barrier layer 12. For example, when the set thickness of the barrier layer 12 is 1.2 mm, the thickness of the remaining portion 30 is 0.6 ± 0.5 mm, more preferably 0.6 ± 0.3 mm. The air bag grid 4 has a substantially flat and smooth surface shape without a character line or the like at a position on the surface side corresponding to the cleavage line 15.
[0028]
The tear line 15 is formed by turning the air bag grid portion 4 upside down, a laser processing machine 35 as shown in FIG. 4, a hot blade 36 or an ultrasonic processing machine as shown in FIG. 5, a rotary cutter blade, a high-frequency welder, etc. Is used. At this time, as shown in FIG. 5, a vacuum path 38 may be formed in a cradle 37 on which the air bag grid portion 4 is placed, and vacuum suction may be performed by a vacuum suction device 39. Moreover, you may use a rotary tool (a router, an end mill, etc.) as a cleavage line processing machine. In this case as well, a cleavage line can be reliably formed even if the core material is somewhat hard, as in laser processing.
[0029]
Next, the operation of the first embodiment will be described.
[0030]
When the inflator is activated, the pressure gas is ejected from the inflator, and the pressure gas is introduced into the airbag body.
[0031]
The airbag body is inflated with the introduction of the pressure gas, and at the same time, the door member 17 and the airbag grid part 4 are first cleaved along the cleavage line 15 by the inflation pressure to form an inflated opening. The airbag body bulges from the bulging opening toward the rear of the vehicle body (in the passenger compartment). As a result, the airbag body receives the passenger's head on the passenger seat seated at a fixed position and protects the head from being in contact with the instrument panel 2 or the like.
[0032]
And in this Embodiment 1, the cleavage line 15 has no character line or the like on the surface of the multilayer laminate sheet 13, and there is no thin portion or the like on the back surface of the core material 14 , Formed from the back surface side of the air grid portion 4 , the cleavage line 15 penetrates the core material 14 and a part of the barrier layer 12 remains so that stress concentration on the cleavage line processed portion at the time of thermal deformation is prevented. depth continuously formed to the airbag lid portion 4, tear lines 15 is no character line or the like at a position of a corresponding surface side, by which a smooth surface shape with substantially flat, such as the following, effects An effect can be obtained. That is, since the barrier layer 12 remains without being cut, stress is prevented from concentrating on the processing portion of the cleavage line 15 during thermal deformation, and the surface appearance performance of the air bag grid portion 4 is deteriorated (processing portion of the cleavage line 15). In other words, it is possible to prevent surface appearance performance degradation such as wrinkles, sagging and distortion) . Therefore, the airbag grid part 4 is made to have a substantially flat and gentle surface shape without a character line or the like for making the thermal deformation of the airbag grid part 4 inconspicuous at the position on the surface side corresponding to the cleavage line 15. become able to.
[0033]
Further, since the cleavage line 15 is formed by laser processing, the cleavage line 15 can be reliably formed even if the core material is somewhat hard.
[0034]
【The invention's effect】
As described above, according to the invention of claim 1, the core material having a linear thermal expansion coefficient different from that of the barrier layer on the back surface of the multilayer laminate sheet having at least the skin layer, the foam layer, and the barrier layer. In the vehicle airbag apparatus in which a groove-shaped tear line is formed from the back side of the welded airbag grid part, wherein the tear line is a surface of the multilayer laminate sheet There is no character line, and there is no thin wall portion on the back surface of the core material, whereas the uniform wall thickness portion is formed from the back surface side of the airbag grid portion, and the cleavage line is a cleavage line processed portion during thermal deformation. The air bag grid portion is formed on the surface side corresponding to the cleavage line so as to prevent stress concentration on the core material. Position is not the character line, by which is a gentle surface shape flat, such as the following, effects can be obtained. That is, since the barrier layer remains without being cut, stress is prevented from concentrating on the cleavage line processed part during thermal deformation, and the surface appearance performance of the air bag grid part is degraded (wrinkles and sagging in the cleavage line processed part). And the occurrence of a surface appearance performance degradation portion such as distortion is prevented. Therefore, the air bag grid part can be formed into a substantially flat and gentle surface shape without a character line or the like for making the thermal deformation of the air bag grid part inconspicuous at the position on the surface side corresponding to the cleavage line. Become. In addition, according to the invention of claim 2, since it is cleavage line forming by laser processing, it is possible to exhibit a practically beneficial effect that a cleavage line can be reliably formed even if the core material is somewhat hard.
[Brief description of the drawings]
FIG. 1 is a perspective view of an instrument panel according to a first embodiment of the present invention.
2 is a side sectional view of the airbag device of FIG. 1. FIG.
FIG. 3 is a partially enlarged view of FIG. 2;
FIG. 4 is a diagram showing a processing state of a cleavage line.
FIG. 5 is another view showing a processing state of a cleavage line.
[Explanation of symbols]
4 air bag grid part 10 skin layer 11 intermediate layer 12 barrier layer 13 multilayer laminate sheet 14 core material 15 cleavage line 30 remaining part

Claims (2)

少なくとも表皮層と発泡体層とバリア層とを備えた多層ラミネートシートの裏面に、前記バリア層とは線熱膨張係数の異なる芯材を溶着してエアバッグリッド部を構成し、溶着された状態の該エアバッグリッド部の裏面側から溝状の開裂線を形成した車両用エアバッグ装置において、
前記開裂線は、前記多層ラミネートシートの表面にキャラクターラインがなく、前記芯材の裏面に薄肉部がない、均一肉厚の部分に対し、エアバッグリッド部の裏面側から形成されると共に、
前記開裂線は、熱変形時の開裂線加工部分への応力集中が防止されるように、前記芯材を貫通しかつ前記バリア層の一部が残存する深さまで連続して形成され、
前記エアバッグリッド部は、開裂線と対応する表面側の位置にキャラクターラインがない、でなだらかな表面形状とされたことを特徴とする車両用エアバッグ装置。
At least the core layer having a linear thermal expansion coefficient different from that of the barrier layer is welded to the back surface of the multilayer laminate sheet having at least a skin layer, a foam layer, and a barrier layer to form an air bag grid portion, In the vehicle airbag device in which a groove-shaped tear line is formed from the back side of the airbag grid part,
The cleavage line has no character line on the surface of the multilayer laminate sheet, and there is no thin portion on the back surface of the core material, and is formed from the back side of the air bag grid portion for a uniform thickness portion,
The cleavage line is continuously formed to a depth that penetrates the core material and a part of the barrier layer remains so as to prevent stress concentration on the cleavage line processed part during thermal deformation,
The airbag apparatus according to claim 1, wherein the airbag grid portion has a flat and gentle surface shape without a character line at a position on the surface side corresponding to the cleavage line .
前記開裂線は、レーザ加工により成形されていることを特徴とする請求項1に記載の車両用エアバッグ装置。  The vehicle airbag device according to claim 1, wherein the tear line is formed by laser processing.
JP2000147634A 2000-05-19 2000-05-19 Airbag device for vehicle Expired - Fee Related JP4067740B2 (en)

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