JP2006256325A - Method for arranging ejection channel on airbag covering loaded with target breaking line and assembly component manufactured by the method - Google Patents

Method for arranging ejection channel on airbag covering loaded with target breaking line and assembly component manufactured by the method Download PDF

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JP2006256325A
JP2006256325A JP2006057942A JP2006057942A JP2006256325A JP 2006256325 A JP2006256325 A JP 2006256325A JP 2006057942 A JP2006057942 A JP 2006057942A JP 2006057942 A JP2006057942 A JP 2006057942A JP 2006256325 A JP2006256325 A JP 2006256325A
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Prior art keywords
airbag cover
coupling
engagement
break line
airbag
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JP2006057942A
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Japanese (ja)
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Norbert Preuss
プロイス ノルベルト
Michael Krug
クルーク ミヒャエル
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Jenoptik Automatisierungstechnik GmbH
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Jenoptik Automatisierungstechnik GmbH
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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
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C65/00Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
    • B29C65/02Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure
    • B29C65/14Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using wave energy, i.e. electromagnetic radiation, or particle radiation
    • B29C65/16Laser beams
    • B29C65/1629Laser beams characterised by the way of heating the interface
    • B29C65/1635Laser beams characterised by the way of heating the interface at least passing through one of the parts to be joined, i.e. laser transmission welding
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C65/00Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
    • B29C65/56Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using mechanical means or mechanical connections, e.g. form-fits
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C65/00Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
    • B29C65/56Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using mechanical means or mechanical connections, e.g. form-fits
    • B29C65/58Snap connection
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C65/00Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
    • B29C65/72Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by combined operations or combined techniques, e.g. welding and stitching
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C65/00Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
    • B29C65/02Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure
    • B29C65/06Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using friction, e.g. spin welding
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C65/00Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
    • B29C65/02Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure
    • B29C65/08Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using ultrasonic vibrations
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/70General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
    • B29C66/73General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset
    • B29C66/739General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the material of the parts to be joined being a thermoplastic or a thermoset
    • B29C66/7392General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the material of at least one of the parts being a thermoplastic
    • B29C66/73921General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the material of at least one of the parts being a thermoplastic characterised by the materials of both parts being thermoplastics
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29LINDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
    • B29L2022/00Hollow articles
    • B29L2022/02Inflatable articles
    • B29L2022/027Air bags
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29LINDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
    • B29L2031/00Other particular articles
    • B29L2031/30Vehicles, e.g. ships or aircraft, or body parts thereof
    • B29L2031/3005Body finishings
    • B29L2031/3038Air bag covers

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Optics & Photonics (AREA)
  • Health & Medical Sciences (AREA)
  • Electromagnetism (AREA)
  • Toxicology (AREA)
  • Air Bags (AREA)
  • Lining Or Joining Of Plastics Or The Like (AREA)

Abstract

<P>PROBLEM TO BE SOLVED: To provide a method for integrating an ejection channel onto an airbag covering by melting, without mechanical force applied on the airbag covering. <P>SOLUTION: A material engagement is performed by laser transmission welding, to avoid a mechanical load on a target breaking line integrated in an airbag covering (1) in arranging the ejection channel (2) by material engagement. A pressing force required for this purpose is applied by a frictional engagement or a positive engagement encompassing joint surfaces (3) to be welded. <P>COPYRIGHT: (C)2006,JPO&NCIPI

Description

組み込まれたエアバッグ開口を備えたエアバッグカバーでは、その作動のためにエアバッグの通路のために作られた開口の大きさ及び形状は目標破断線の形状で決まる。エアバッグカバーは、エアバッグが収容される乗用車の内部パネル又はカバーの全てを表す。   In an airbag cover with an integrated airbag opening, the size and shape of the opening created for the airbag passage for its operation is determined by the shape of the target break line. The airbag cover represents all the inner panels or covers of the passenger car in which the airbag is accommodated.

目標破断線はしばしば閉じた長方形、台形、楕円形又は自由な形状の表面を表す。この表面はヒンジ領域でのみ遮断され、目標破断線が裂けたときに同じ形状及び大きさの開口を開け放つ。ヒンジ領域は横長さ全体にわたって延び、それで目標破断線は例えばU形になる。   The target break line often represents a closed rectangular, trapezoidal, elliptical or free-form surface. This surface is blocked only in the hinge region, leaving an opening of the same shape and size when the target break line is torn. The hinge region extends over the entire lateral length, so that the target break line is, for example, U-shaped.

意図した開口輪郭の外周線上に向かい合って位置した点の連結線として目標破断線を形成することも知られている。例えば、H形又はX形目標破断線である。   It is also known to form a target break line as a connecting line between points located on the outer peripheral line of the intended opening contour. For example, an H-shaped or X-shaped target break line.

目標破断線がエアバッグカバーに加えられる方法にかかわらず、一般的に、この目標破断線に沿ってエアバッグカバーの機械的弱まりが生じる。   Regardless of the manner in which the target break line is applied to the airbag cover, a mechanical weakening of the airbag cover generally occurs along the target break line.

エアバッグカバーがこの弱まった線に沿って再製可能な非常に僅な裂け耐性を有し、それでエアバッグの通路のための開口を解放するためにそこに作用する所定の押圧の結果エアバッグが作動するときに、目標破断線が確かに裂けるように、機械的弱まりの程度は選択されなければならない。   The airbag cover has a very slight tear resistance that can be remanufactured along this weakened line, so that the airbag acts as a result of a predetermined pressure acting on it to open the opening for the airbag passage. The degree of mechanical weakening must be selected to ensure that the target break line will tear when activated.

しかし、ドライバー室側から作用する任意の機械力が例えば乗客又は乗用車の乗客室に運ばれた荷物のために目標破断線の一部の裂けをもたらさないように、裂け耐性は十分に高くなければならない。   However, the tear resistance must be sufficiently high so that any mechanical force acting from the driver's compartment side will not cause part of the target break line to tear, for example, for luggage carried to passengers or passenger cabins. Don't be.

自然環境の影響による任意の力及び長期間の応力にかかわらず、目標破断線は美的理由のために乗客室から永久的に見えるべきでない。   Regardless of any forces and long-term stresses due to the effects of the natural environment, the target break line should not be permanently visible from the passenger compartment for aesthetic reasons.

例えば、後に発射通路を配置するためにエアバッグカバーに作業をする際、目標破断線を損傷しないように注意しなければならない。   For example, care must be taken not to damage the target break line when working on the airbag cover later to place the firing passage.

発射通路は基本的に管状であり、異なる断面形状を有する。それは開口エアバッグの横膨張を制限し、エアバッグの膨張方向を乗客室の方へ案内する働きをする。発射通路はその内周に関して実質的に開口の形状に適合している。発射通路の外形は様々に考えられる。しばしば、空気チャネル、固定要素、ケーブルホルダーなどの様々な他の機能部品が実際の機能領域の外側の発射通路に形成される。この場合、発射通路はエアバッグカバーのより広範な下部構造の室部分である。   The firing passage is essentially tubular and has a different cross-sectional shape. It limits the lateral inflation of the opening airbag and serves to guide the direction of inflation of the airbag toward the passenger compartment. The firing passage is substantially adapted to the shape of the opening with respect to its inner circumference. Various external shapes of the launch passage are possible. Often, various other functional components such as air channels, securing elements, cable holders, etc. are formed in the firing passage outside the actual functional area. In this case, the firing passage is the chamber portion of the wider substructure of the airbag cover.

理想的には、一方で目標破断線に沿ってエアバッグカバーを保持し、他方で作動したときに乗客室において最大限のボリュームでエアバッグを広げるために、エアバッグカバーに隣接する発射通路の内周は目標破断線で定められた開口より幾らか小さくなければならない。   Ideally, in order to hold the airbag cover along the target break line on the one hand and spread the airbag at full volume in the passenger compartment when actuated on the other hand, the launch passage adjacent to the airbag cover The inner circumference must be somewhat smaller than the opening defined by the target break line.

全ての場合で、発射通路の内周線は目標破断線に近くなければならない。しかしながら、これは、エアバッグカバーに発射通路を設けるための従来技術から知られた方法ではすぐに可能ではない。   In all cases, the inner circumference of the launch passage must be close to the target break line. However, this is not immediately possible with the methods known from the prior art for providing a firing passage in the airbag cover.

発射通路、エアバッグカバー又は多層エアバッグカバーの場合の発射通路に面する内側層はプラスチックでできている。   In the case of a launch passage, airbag cover or multilayer airbag cover, the inner layer facing the launch passage is made of plastic.

超音波溶着又は摩擦溶着は自動大量生産に適しており、永久的に固定した2つのプラスチック部品の結合を作り出す。   Ultrasonic welding or friction welding is suitable for automated mass production and creates a bond between two permanently fixed plastic parts.

よく知られているように、溶着連結は結合すべき部品の振動により超音波溶着で生じる。すなわち、溶着連結が作られる時間を通して動的機械的力が作用し、目標破断線に伝わる。   As is well known, welded connections occur by ultrasonic welding due to the vibration of the parts to be joined. That is, the dynamic mechanical force acts through the time when the welded connection is made and is transmitted to the target break line.

摩擦溶着では、全工程において作用する動的機械的力に加えて静的機械的力も生じ、結合すべき2つの部品を共に圧縮する。   In friction welding, in addition to the dynamic mechanical forces acting in the entire process, static mechanical forces are also generated, compressing the two parts to be joined together.

なるべく機械的力が目標破断線に負荷を与えるのを防ぐために、選択された結合領域は目標破断線のすぐ近く又は隣接してはならない。   In order to prevent mechanical forces from loading the target break line as much as possible, the selected coupling region should not be close to or adjacent to the target break line.

ゆえに、発射通路の選択された外周は意図されたエアバッグ開口の外周より大きくなければならず、あるいは特別なステップが構造の点においてとられなければならない。   Therefore, the selected perimeter of the firing passage must be larger than the perimeter of the intended airbag opening, or special steps must be taken in terms of construction.

エアバッグカバーと発射通路が担持され、溶着の際互いに抗して保持される高価な保持装置の必要も不都合である。   The need for an expensive holding device that carries the air bag cover and firing passage and is held against each other during welding is also disadvantageous.

当業者にはレーザ透過溶着によりプラスチックを溶着することも知られている。この場合、当業者は溶着連結を作るために溶着の際に溶着圧力が生じなければならないことを知っている。ゆえに、この方法は別な方法では適さないようである。   It is also known to those skilled in the art to weld plastics by laser transmission welding. In this case, the person skilled in the art knows that a welding pressure must be generated during welding in order to make a welded connection. Therefore, this method seems not suitable for another method.

本発明の目的は、エアバッグカバーに作用する機械的力なしで溶着により発射通路をエアバッグカバーに結合させる方法を開発することである。   It is an object of the present invention to develop a method for joining a firing passage to an airbag cover by welding without mechanical forces acting on the airbag cover.

また、本発明の目的は、溶着の際にエアバッグカバーに作用する機械的力のない溶着方法により互いに結合されるエアバッグカバーと発射通路を有する組立部品を提供することである。   It is another object of the present invention to provide an assembly part having an airbag cover and a firing passage which are coupled to each other by a welding method without mechanical force acting on the airbag cover during welding.

この目的は、請求項1の本発明に従う方法及び請求項5の本発明に従う組立部品により達成される。   This object is achieved by the method according to the invention of claim 1 and the assembly according to the invention of claim 5.

有利な構造は従属請求項に示されている。   Advantageous structures are indicated in the dependent claims.

本発明の本質は、結合すべき2つの部品(発射通路とエアバッグカバー)の間に溶着に必要な機械的押圧力が加えられ、溶着工程自体よりも先に蓄えられることである。これは、結合すべき部品が摩擦係合又は確動係合により互いに固定される点で実現される。目標破断線に負荷がかからない、エアバッグ開口の外側に静的な力を一度加えることで手動又は自動で結合が実行される。   The essence of the invention is that the mechanical pressing force required for welding is applied between the two parts to be joined (firing passage and airbag cover) and stored prior to the welding process itself. This is achieved in that the parts to be joined are fixed together by frictional engagement or positive engagement. Coupling is performed manually or automatically by applying a static force once outside the airbag opening where no load is applied to the target break line.

本発明を実施例に則して図を用いて以下により完全に説明する。   The invention will be described more fully below with the aid of examples and using the figures.

エアバッグカバーと発射通路を本発明に従って互いに結合するために、特別な構造ステップがエアバッグカバーと発射通路にとられる。すなわち、摩擦係合又は確動係合が作り出されるように結合領域の幾何学的形状が適合しなければならない。   In order to connect the airbag cover and the firing passage to each other according to the present invention, special structural steps are taken in the airbag cover and the firing passage. That is, the geometry of the coupling area must be adapted so that a frictional or positive engagement is created.

エアバッグカバーは、発射通路に面する側面に、エアバッグ開口の外側の目標破断線の所与の形状を取り囲む輪状カラーを有しなければならず、発射通路は、目標破断線にちょうど重なるようにカラーで囲まれた領域に延びるようにこの輪状カラー上に位置する。   The airbag cover must have on the side facing the firing passage a ring collar surrounding the given shape of the target breaking line outside the airbag opening, so that the firing passage just overlaps the target breaking line. It is located on this ring-shaped collar so as to extend to the area surrounded by the collar.

カラー(つば)の異なる断面形状の例が図1〜3に示されている。カラーと結合した発射通路がそれぞれの場合に概略的に示されている。   Examples of cross-sectional shapes with different collars are shown in FIGS. The firing passage combined with the collar is shown schematically in each case.

例えば、図1はエアバッグカバー1に形成されたカラーの台形又は円錐形断面を示す。発射通路2の対応する形状により、2つの部品が結合すると、摩擦係合によって結合すべき2つの部品を共に保持する円錐形結合が生じる。カラーに形成された外側コーンと発射通路2に形成された内側コーンの外面の間で力が作用する。これらの2つの外面は2つの部品が共に溶着されるべき結合表面3をも表す。   For example, FIG. 1 shows a trapezoidal or conical cross section of a collar formed in an airbag cover 1. Due to the corresponding shape of the firing channel 2, when the two parts are joined, a conical joint is created that holds the two parts together to be joined by frictional engagement. A force acts between the outer cone formed in the collar and the outer surface of the inner cone formed in the firing passage 2. These two outer surfaces also represent the bonding surface 3 where the two parts are to be welded together.

図2では、カラー断面は長方形である。発射通路2と結合する際、別な摩擦係合がプレスフィット(圧入)により生じる。この場合でも、互いに圧縮される円筒形表面は溶着連結のための結合表面3である。   In FIG. 2, the color cross section is rectangular. When coupled with the firing passage 2, another frictional engagement occurs by press-fit. Even in this case, the cylindrical surfaces that are compressed together are the bonding surfaces 3 for the welded connection.

図3では、結合すべき2つの部品はスナップイン連結により連結している。   In FIG. 3, two parts to be joined are connected by snap-in connection.

予備的結合状態において2つの部品に張力がない限り、すなわち、連結が単に確動係合に依存する限り、生じた材料の溶解が広がろうとするときにのみ2つの部品の結合表面の間で力が先ず作用する。   As long as there is no tension between the two parts in the pre-bonded state, i.e. as long as the connection only relies on positive engagement, the resulting material dissolution will only be between the bonding surfaces of the two parts. Force acts first.

例えば、直接のねじ連結も可能であるが、確かに確動係合ほど適切でない。   For example, a direct screw connection is possible, but certainly not as good as positive engagement.

レーザ溶着連結の強度は一般的に材料強度より劣ることはないので、エアバッグカバーにおける結合表面の空間的位置は原則的に強度に関連する理由のため重要でない。理想的には、結合スペースは、エアバッグが広がるときにせん断応力のみが作用するように配置される。当業者により、溶着に必要なレーザビームが最適に連結するように結合すべき部品の幾何学的形状及び結合表面の位置が設計される。   Since the strength of the laser weld connection is generally not inferior to the material strength, the spatial position of the bonding surface in the airbag cover is in principle not important for reasons related to strength. Ideally, the coupling space is arranged so that only shear stress acts when the airbag is spread. The person skilled in the art designs the geometry of the parts to be joined and the position of the joining surface so that the laser beam required for welding is optimally coupled.

目標破断線の導入を邪魔しないように、エアバッグカバーに形成されるカラーの高さはできるだけ低いが、前記のように発射通路との予備的な結合連結を作るために十分である。このようにして生じる摩擦係合又は確動係合は、レーザ透過溶着で作られる実際の連結と明確に区別するために以下では予備的結合連結と称する。予備的結合連結は結合すべき部品を互いに位置決め・固定し、表面(以下では、結合表面という)が互いに押圧される押圧力を蓄える。   The height of the collar formed on the airbag cover is as low as possible so as not to interfere with the introduction of the target break line, but is sufficient to make a preliminary coupling connection with the firing passage as described above. The frictional or positive engagement thus produced is hereinafter referred to as a preliminary coupling connection in order to clearly distinguish it from an actual connection made by laser transmission welding. Preliminary joint connection positions and fixes the parts to be joined together and stores a pressing force with which surfaces (hereinafter referred to as joining surfaces) are pressed together.

次に、連結に永続的な機械的安定性を与えるレーザ透過溶着による材料係合を作る際、この押圧力は必要な溶着圧力を生じさせる。予備的結合連結が単に確動係合であるとき、結合領域に形成した材料溶解が広がろうとするとこの押圧力が先ず逆の力として生じる。   This pressing force then creates the necessary welding pressure when creating material engagement by laser transmission welding that provides permanent mechanical stability to the connection. When the preliminary coupling connection is simply positive engagement, this pressing force is first generated as an opposite force when the material dissolution formed in the coupling region is about to spread.

レーザ透過溶着法と、レーザ透過材料とレーザ吸収材料の適切な組み合わせの必要は当業者に知られており、ここではこれ以上説明する必要はない。原則として、発射通路が固定されるエアバッグカバーの後部から、また照射領域の結合表面の前部に位置した材料だけがレーザビームのために透明である限り前部から、結合表面の照射が可能である。   The need for a laser transmission welding method and an appropriate combination of laser transmission material and laser absorption material is known to those skilled in the art and need not be described further here. In principle, it is possible to irradiate the coupling surface from the rear of the airbag cover to which the launch passage is fixed and from the front as long as only the material located in front of the coupling surface in the irradiation area is transparent for the laser beam It is.

結合すべき部品の予備的結合は、レーザ透過溶着の際、必要な溶着圧力の影響下で溶着位置の発射通路とエアバッグカバーを保持するために高価な装置が必要でないという決定的な利点を有する。   Preliminary joining of the parts to be joined has the decisive advantage that, during laser transmission welding, no expensive equipment is required to hold the firing path and airbag cover in the welding position under the influence of the required welding pressure. Have.

エアバッグカバーは、目標破断線を導入する際に保持された同じ保持装置に保持される。溶着工程の際、機械的力はエアバッグカバーに作用せず、ゆえに目標破断線に作用しない。   The airbag cover is held by the same holding device that is held when the target break line is introduced. During the welding process, the mechanical force does not act on the airbag cover and therefore does not act on the target break line.

本発明の分野に知識のある者は、本発明が明細書の例で提供された実施形態の細部に限定されず、付属の請求項に説明されるように本発明の範囲を逸脱することなく他の特別な形態でも実施できることを理解できる。   Those skilled in the art of the present invention are not limited to the details of the embodiments provided by way of example in the specification, and do not depart from the scope of the invention as set forth in the appended claims. It can be understood that other special forms can be implemented.

予備的連結としてプレスフィットによる組立部品を示す図である。It is a figure which shows the assembly component by press fitting as preliminary connection. 予備的連結として円錐形連結による組立部品を示す図である。FIG. 5 shows an assembly part with a conical connection as a preliminary connection. 予備的連結としてスナップイン連結による組立部品を示す図である。It is a figure which shows the assembly component by a snap-in connection as a preliminary connection.

符号の説明Explanation of symbols

1 エアバッグカバー
2 発射通路
3 結合表面
1 Airbag cover 2 Launch passage 3 Binding surface

Claims (8)

組み込まれた目標破断線を備えたエアバッグカバーに発射通路を取り付ける方法であって、
発射通路(2)をエアバッグカバー(1)に対して位置決め・固定する予備的連結を作り、予備的連結の摩擦係合又は確動係合により目標破断線を囲むリング形結合領域内の結合表面(3)に沿って発射通路(2)とエアバッグカバー(1)が互いに平らに接触し、
レーザ透過溶着によって予備的連結の結合表面の間の材料係合を作る方法ステップを有し、
予備的連結によって必要な溶着圧力が与えられる方法。
A method of attaching a firing passage to an airbag cover with an incorporated target break line,
Making a preliminary connection for positioning and fixing the firing passage (2) with respect to the airbag cover (1), and coupling in a ring-shaped coupling area surrounding the target break line by frictional engagement or positive engagement of the preliminary coupling The launch passage (2) and the airbag cover (1) are in flat contact with each other along the surface (3),
Having a method step of creating material engagement between the coupling surfaces of the preliminary connection by laser transmission welding;
A method in which the necessary welding pressure is provided by the preliminary connection.
摩擦係合がプレスフィットにより実現されることを特徴とする請求項1に記載の方法。   The method according to claim 1, wherein the frictional engagement is realized by press-fit. 摩擦係合が円錐形連結により実現されることを特徴とする請求項1に記載の方法。   The method according to claim 1, wherein the frictional engagement is realized by a conical connection. 確動係合がスナップイン連結により実現されることを特徴とする請求項1に記載の方法。   The method according to claim 1, wherein positive engagement is achieved by a snap-in connection. 組み込まれた目標破断線を備えたエアバッグカバー(1)と発射通路(2)を有する組立部品であって、
目標破断線を取り囲むカラーがエアバッグカバー(1)に設けられ、
リング形結合表面(3)がカラーに形成され、摩擦係合又は確動係合及びレーザ透過溶着による材料係合によって、発射通路に形成された結合表面(3)に連結される組立部品。
An assembly part having an airbag cover (1) with a built-in target break line and a firing passage (2),
A collar surrounding the target break line is provided on the airbag cover (1),
An assembly in which a ring-shaped coupling surface (3) is formed in the collar and connected to the coupling surface (3) formed in the firing path by frictional engagement or positive engagement and material engagement by laser transmission welding.
結合表面(3)がコーンの外面であることを特徴とする請求項5に記載の組立部品。   6. Assembly according to claim 5, characterized in that the coupling surface (3) is the outer surface of a cone. 結合表面(3)が円筒の外面であることを特徴とする請求項5に記載の組立部品。   6. Assembly part according to claim 5, characterized in that the coupling surface (3) is the outer surface of a cylinder. 結合表面(3)が円形表面であることを特徴とする請求項5に記載の組立部品。   6. Assembly part according to claim 5, characterized in that the coupling surface (3) is a circular surface.
JP2006057942A 2005-03-18 2006-03-03 Method for arranging ejection channel on airbag covering loaded with target breaking line and assembly component manufactured by the method Pending JP2006256325A (en)

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DE200510013262 DE102005013262A1 (en) 2005-03-18 2005-03-18 Firing channel fixation method for air bag cover, involves forming firmly bonded connection between joint surfaces of pre-joint by laser welding, where welding pressure is provided by joint, which positions and fixes channel at cover

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JP2012176662A (en) * 2011-02-25 2012-09-13 Toyoda Gosei Co Ltd Positioning structure of air bag door
JP2013173322A (en) * 2012-02-27 2013-09-05 Hayakawa Rubber Co Ltd Intermediate member for laser bonding and bonding method using laser beam
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DE29816568U1 (en) * 1998-09-15 1998-11-05 TRW Automotive Safety Systems GmbH, 63743 Aschaffenburg Airbag module for motor vehicle steering wheels
DE20220612U1 (en) * 2002-06-26 2003-12-04 Autoliv Development Ab Air bag module, comprising front cover permanently attached to rim of housing by gluing or welding
DE10318962A1 (en) * 2003-04-26 2004-11-11 Adam Opel Ag Lining for an airbag housing of a motor vehicle, especially a knee airbag housing has a multiple shell structure, is fixed to the chassis and extends over an outlet opening of an airbag housing

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JP2012176662A (en) * 2011-02-25 2012-09-13 Toyoda Gosei Co Ltd Positioning structure of air bag door
JP2013173322A (en) * 2012-02-27 2013-09-05 Hayakawa Rubber Co Ltd Intermediate member for laser bonding and bonding method using laser beam
JP2014162174A (en) * 2013-02-27 2014-09-08 Calsonic Kansei Corp Vibrating welding part structure
CN108367505A (en) * 2015-10-22 2018-08-03 詹诺普蒂克自动化技术有限公司 Melting welding component and method for manufacturing melting welding component
CN108367505B (en) * 2015-10-22 2020-06-19 詹诺普蒂克自动化技术有限公司 Fusion welding component and method for manufacturing a fusion welding component
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