[go: up one dir, main page]

JP2012193751A - Method for mounting hollow member and fastening member, and mounting structure - Google Patents

Method for mounting hollow member and fastening member, and mounting structure Download PDF

Info

Publication number
JP2012193751A
JP2012193751A JP2011056043A JP2011056043A JP2012193751A JP 2012193751 A JP2012193751 A JP 2012193751A JP 2011056043 A JP2011056043 A JP 2011056043A JP 2011056043 A JP2011056043 A JP 2011056043A JP 2012193751 A JP2012193751 A JP 2012193751A
Authority
JP
Japan
Prior art keywords
hollow member
fastening member
hollow
fastening
insertion portion
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Withdrawn
Application number
JP2011056043A
Other languages
Japanese (ja)
Inventor
Kotaro Nakamichi
昂太郎 中道
Toshio Watanabe
敏雄 渡邉
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Toyota Motor Corp
Original Assignee
Toyota Motor Corp
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Toyota Motor Corp filed Critical Toyota Motor Corp
Priority to JP2011056043A priority Critical patent/JP2012193751A/en
Publication of JP2012193751A publication Critical patent/JP2012193751A/en
Withdrawn legal-status Critical Current

Links

Images

Landscapes

  • Standing Axle, Rod, Or Tube Structures Coupled By Welding, Adhesion, Or Deposition (AREA)

Abstract

【課題】部品点数や組み付け工数の増加を抑制しながら、容易な方法で、しかも確実に、締結部材を中空部材に取り付けることのできる中空部材と締結部材の取付方法を提供する。
【解決手段】挿入孔5を有し、レーザ光を透過する透過性材料から構成される中空部材10と、挿入孔5に挿入可能な挿入部12を有し、レーザ光を吸収する吸収性材料であって熱可塑性材料から構成される締結部材20を準備する第1の工程と、挿入孔5を介して中空部材10の内部に締結部材20の挿入部12を挿入する第2の工程と、中空部材10の内部に挿入された挿入部12の端部13に中空部材10の外部からレーザ光Rを照射して溶融させ、挿入部12を中空部材10の内周面4に押圧して挿入孔5よりも相対的に大きなフランジ部14を挿入部12に形成する第3の工程からなる。
【選択図】 図1
To provide a hollow member and a fastening member mounting method capable of securely and securely mounting a fastening member to a hollow member in an easy manner while suppressing an increase in the number of parts and the number of assembly steps.
An absorptive material that has an insertion hole and has a hollow member made of a transparent material that transmits laser light, and an insertion portion that can be inserted into the insertion hole, and absorbs laser light. A first step of preparing a fastening member 20 made of a thermoplastic material, a second step of inserting the insertion portion 12 of the fastening member 20 into the hollow member 10 through the insertion hole 5, The end portion 13 of the insertion portion 12 inserted inside the hollow member 10 is melted by irradiating the laser beam R from the outside of the hollow member 10 and the insertion portion 12 is pressed against the inner peripheral surface 4 of the hollow member 10 for insertion. This is a third step of forming a flange portion 14 relatively larger than the hole 5 in the insertion portion 12.
[Selection] Figure 1

Description

本発明は、中空部材と締結部材の取付方法および取付構造体に関するものである。   The present invention relates to a mounting method and a mounting structure for a hollow member and a fastening member.

従来から、車両の内装部品や外装部品の裏面には、当該部品の剛性を高め、熱による変形を抑制する目的で、補強材としてのリブやボックス構造等が設けられている。特に、閉空間を有するボックス構造(中空構造)は、リブ等に対して多方向からの荷重に耐え得る構造を有していることで、当該部品の剛性を効果的に高めることができる。   2. Description of the Related Art Conventionally, ribs, box structures, and the like as reinforcing materials have been provided on the back surfaces of interior parts and exterior parts of vehicles in order to increase the rigidity of the parts and suppress deformation due to heat. In particular, a box structure (hollow structure) having a closed space has a structure that can withstand a load from multiple directions with respect to a rib or the like, thereby effectively increasing the rigidity of the component.

また、それらの部品の裏面にはクリップ等の締結部材が取り付けられており、この締結部材によって内装部品や外装部品がボディを構成するインナパネルやドアパネル、バンパビーム等に取り付けられる。たとえば、上記部品の裏面に設けられた閉空間を有するボックス構造(中空構造)に締結部材を取り付ける方法としては、タッピングスクリューやボルト等の別途の締結部材を用いて締結部材をボルト締めする方法や、締結部材の台座(クリップ台座)を溶着する方法、両面テープ等の接着剤を用いて締結部材の台座を接着する方法などを挙げることができる。   Further, a fastening member such as a clip is attached to the back surface of these parts, and the interior part and the exterior part are attached to an inner panel, a door panel, a bumper beam and the like constituting the body by the fastening member. For example, as a method of attaching a fastening member to a box structure (hollow structure) having a closed space provided on the back surface of the component, a method of bolting the fastening member using a separate fastening member such as a tapping screw or a bolt, And a method of welding a base (clip base) of a fastening member, a method of adhering a base of a fastening member using an adhesive such as a double-sided tape, and the like.

ここで、図7を参照して、従来の中空部材と締結部材の取付方法、特にタッピングビスを用いて中空部材にクリップ等の締結部材を取り付ける方法を説明する。まず、図7(a)で示すように、例えばハニカム構造を有する中空部材Aと、台座Dと頭部Eを備えた締結部材(クリップ)Cを準備し、中空部材Aの一方の側壁に貫通孔Bを形成する。ここで、貫通孔Bの位置は、後述するビスGの取り付け位置に対応している。なお、締結部材Cの台座DにもビスGが貫通可能な貫通孔Fが設けられている。次いで、図7(b)で示すように、締結部材Cを中空部材Aの取付位置に配置する。そして、図7(c)で示すように、締結部材Cの台座Dの貫通孔Fと中空部材Aの貫通孔BにビスGを貫通させ、ビスGの頭部Hと中空部材Aで締結部材Cの台座Dを挟持する。   Here, with reference to FIG. 7, a conventional method of attaching a hollow member and a fastening member, particularly a method of attaching a fastening member such as a clip to the hollow member using a tapping screw will be described. First, as shown in FIG. 7A, for example, a hollow member A having a honeycomb structure and a fastening member (clip) C having a pedestal D and a head E are prepared and penetrated into one side wall of the hollow member A. Hole B is formed. Here, the position of the through hole B corresponds to a mounting position of a screw G described later. A through hole F through which the screw G can penetrate is also provided in the base D of the fastening member C. Next, as shown in FIG. 7B, the fastening member C is disposed at the attachment position of the hollow member A. Then, as shown in FIG. 7C, the screw G is passed through the through hole F of the base D of the fastening member C and the through hole B of the hollow member A, and the fastening member is connected with the head H of the screw G and the hollow member A. C pedestal D is clamped.

図7で示すビスやボルト等による従来の取付方法によれば、中空部材Aや締結部材Cに加えて、ビスG等の別途の締結部材が必要となり、部品点数が増加して車両の軽量化を図ることができない。また、締結部材CのビスGによる組み付け工数が増加することで、製造コストが高騰してしまう可能性がある。また、締結部材Cが内装部品や外装部品の表面側(意匠面)に取り付けられる場合には、ビスGがこれらの部品の表面側に露出することから、その外観が損なわれる可能性がある。さらに、車両走行時等に発生する車両振動に伴って中空部材Aが振動すると、ビスG等の別途の締結部材が徐々に緩み、締結力が低下して、部品の損傷や異音の発生の要因となるといった問題もある。このような緩みを抑制する手段としては、たとえば、ねじロック剤を用いる方法や緩み防止のワッシャを用いる方法、ねじ山の一部を変形させたノンロックねじを用いる方法などを適用することができる。しかしながら、それらの方法はいずれも、追加の部材が必要となったり、ねじに特殊な加工が必要となるために、車両重量の増加と製造コストの更なる高騰に繋がる。   According to the conventional mounting method using screws, bolts and the like shown in FIG. 7, in addition to the hollow member A and the fastening member C, a separate fastening member such as a screw G is required, and the number of parts is increased and the weight of the vehicle is reduced. I can't plan. Moreover, there is a possibility that the manufacturing cost will increase due to an increase in the number of assembling steps by the screw G of the fastening member C. Further, when the fastening member C is attached to the surface side (design surface) of the interior part or the exterior part, the screw G is exposed to the surface side of these parts, so that the appearance may be impaired. Further, when the hollow member A vibrates with the vibration of the vehicle that occurs when the vehicle travels, a separate fastening member such as a screw G is gradually loosened, and the fastening force is reduced, causing damage to parts and generation of abnormal noise. There is also a problem that becomes a factor. As a means for suppressing such loosening, for example, a method using a screw locking agent, a method using a washer for preventing loosening, a method using a non-locking screw in which a part of a thread is deformed can be applied. . However, all of these methods require additional members or special processing of the screws, leading to an increase in vehicle weight and a further increase in manufacturing costs.

また、締結部材の台座を中空部材に溶着する方法によれば、車両振動等に起因して溶着部に応力が発生した際に、台座の溶着が剥離して締結部材が中空部材から脱落する可能性がある。溶着面積を大きくすることで溶着部に発生する応力を低減できるものの、この手法では締結部材の重量が増加し、ひいては車両全体の軽量化を阻害してしまう。また、接着剤によって締結部材の台座を中空部材に接着する方法では、様々な環境下で使用される車両等において、経年劣化によって接着剤の接着強度が急激に低下することがあり、車両の耐久年数が経過する前に接着剤による接着が剥離して締結部材が中空部材から脱落してしまう可能性がある。   Further, according to the method of welding the base of the fastening member to the hollow member, when stress is generated in the welded portion due to vehicle vibration or the like, the welding of the base is peeled off and the fastening member can be detached from the hollow member. There is sex. Although the stress generated in the welded portion can be reduced by increasing the welded area, this method increases the weight of the fastening member and thus inhibits the weight reduction of the entire vehicle. Further, in the method of bonding the base of the fastening member to the hollow member with an adhesive, the adhesive strength of the adhesive may be drastically reduced due to deterioration over time in a vehicle or the like used in various environments. There is a possibility that the bonding by the adhesive peels off before the years elapse and the fastening member falls off the hollow member.

上記方法に対して、緩みの発生し得る別途の締結部材を使用することなく、部品点数や組み付け工数を低減して樹脂や金属からなる部材を他の部材に取り付ける方法が特許文献1,2に開示されている。   In contrast to the above method, Patent Documents 1 and 2 disclose a method of attaching a member made of resin or metal to another member by reducing the number of parts or the number of assembly steps without using a separate fastening member that may be loosened. It is disclosed.

特許文献1には、鉄系材料からなる端子キャップの穴にアルミニウム系材料からなるピン状突起を嵌め込み、ピン状突起の先端部を押しつぶしてピン状突起と穴をリベット固定するリベット固定部を形成し、このリベット固定部近傍の端子キャップの穴の壁面にレーザ光を照射してリベット固定部を溶接する方法が開示されている。   In Patent Document 1, a pin-shaped protrusion made of an aluminum-based material is fitted into a hole of a terminal cap made of an iron-based material, and a tip portion of the pin-shaped protrusion is crushed to form a rivet fixing portion that fixes the pin-shaped protrusion and the hole to a rivet. And the method of welding a rivet fixing part by irradiating a laser beam to the wall surface of the hole of the terminal cap near this rivet fixing part is disclosed.

また、特許文献2には、レーザ光に対する透過性樹脂部材に形成された凹部に、レーザ光に対する非透過性樹脂部材に形成された凸部を嵌合し、透過性樹脂部材側から凸部にレーザ光を照射して凸部を溶融させることで、双方の部材同士を溶着固定する方法が開示されている。   Further, in Patent Document 2, a convex portion formed on a non-transparent resin member for laser light is fitted into a concave portion formed on a resin member transparent to laser light, and the convex portion is formed from the transparent resin member side. A method is disclosed in which both members are welded and fixed by irradiating a laser beam to melt the convex portion.

特開2010−086782号公報JP 2010-087882 A 特開2005−007759号公報JP-A-2005-007759

特許文献1に開示されている取付方法においては、端子キャップの穴よりも相対的に大きなリベット固定部をピン状突起に形成できるものの、リベット固定具を用いてピン状突起の先端部をつぶす必要があり、ハムカム等の閉空間からなる中空部材への締結部材の取付には適用することができない。また、レーザ光を照射する前に先端部をつぶすために大きな押圧荷重が必要となり、端子キャップが変形してしまう可能性もある。   In the mounting method disclosed in Patent Document 1, a rivet fixing portion that is relatively larger than the hole of the terminal cap can be formed on the pin-like protrusion, but the tip portion of the pin-like protrusion needs to be crushed using a rivet fixing tool. And cannot be applied to attachment of a fastening member to a hollow member made of a closed space such as a ham cam. In addition, a large pressing load is required to crush the tip before irradiating the laser beam, and the terminal cap may be deformed.

また、特許文献2に開示されている方法においては、閉空間においても樹脂部材同士を溶着することができるものの、凹部と凸部とは面接着により接着されており、十分な取付強度を保証することができない。特許文献2には、気密性及び接着強度を高めるために、透過性樹脂部材の凹部に窪みを設け、非透過性樹脂部材の凸部にビード状の突起を設けることが開示されているものの、このようなビード状の突起を備えた凸部を凹部内に配置する際には突起が凹部の側壁と接触して、突起を所定の位置に配置するまでの間に大きな押圧荷重が必要となる。   Further, in the method disclosed in Patent Document 2, although the resin members can be welded even in a closed space, the concave portion and the convex portion are bonded by surface bonding, and sufficient mounting strength is guaranteed. I can't. Patent Document 2 discloses that in order to improve airtightness and adhesive strength, a recess is provided in the concave portion of the permeable resin member, and a bead-shaped protrusion is provided in the convex portion of the non-permeable resin member. When a convex portion having such a bead-shaped projection is arranged in the concave portion, a large pressing load is required until the projection comes into contact with the side wall of the concave portion and the projection is arranged at a predetermined position. .

本発明は上記する課題に鑑みてなされたものであり、部品点数や組み付け工数の増加を抑制しながら、容易な方法で、しかも確実に締結部材を中空部材に取り付けることのできる中空部材と締結部材の取付方法と、軽量かつ高い締結強度で締結部材が取り付けられた中空部材と締結部材の取付構造体を提供することを目的とする。   SUMMARY OF THE INVENTION The present invention has been made in view of the above-described problems, and a hollow member and a fastening member that can attach a fastening member to a hollow member with an easy method while suppressing an increase in the number of parts and assembly steps. It is an object of the present invention to provide a mounting structure for a fastening member and a hollow member to which a fastening member is attached with a light weight and high fastening strength.

前記目的を達成すべく、本発明の中空部材と締結部材の取付方法は、挿入孔を有し、レーザ光を透過する透過性材料から構成される中空部材と、該挿入孔に挿入可能な挿入部を有し、少なくとも該挿入部がレーザ光を吸収する吸収性材料であって熱可塑性材料から構成される締結部材を準備する第1の工程と、前記挿入孔を介して前記中空部材の内部に前記締結部材の挿入部を挿入する第2の工程と、前記中空部材の内部に挿入された前記挿入部の端部に該中空部材の外部からレーザ光を照射して溶融させ、該挿入部を該中空部材の内周面の一部に押圧して該挿入部に前記挿入孔よりも相対的に大きなフランジ部を形成する第3の工程からなるものである。   In order to achieve the above object, the hollow member and fastening member mounting method according to the present invention includes a hollow member having an insertion hole and made of a transparent material that transmits laser light, and an insert that can be inserted into the insertion hole. A first step of preparing a fastening member having a portion, and at least the insertion portion is an absorptive material that absorbs laser light and is made of a thermoplastic material, and the inside of the hollow member through the insertion hole A second step of inserting the insertion portion of the fastening member into the hollow member, and melting the end portion of the insertion portion inserted into the hollow member by irradiating a laser beam from the outside of the hollow member. This is composed of a third step of pressing a part of the inner peripheral surface of the hollow member to form a flange portion relatively larger than the insertion hole in the insertion portion.

ここで、中空部材の形成素材としては、たとえばポリプロピレン(PP)、ポリアセタール(POM)、ポリエチレンテレフタレート(PET)、ポリブチレンテレフタレート(PBT)、ポリカーボネート(PC)、液晶ポリマー等を挙げることができる。なお、中空部材の形成素材は、熱可塑性樹脂であっても良いし、熱硬化性樹脂であっても良い。   Here, examples of the material for forming the hollow member include polypropylene (PP), polyacetal (POM), polyethylene terephthalate (PET), polybutylene terephthalate (PBT), polycarbonate (PC), and liquid crystal polymer. The material for forming the hollow member may be a thermoplastic resin or a thermosetting resin.

また、締結部材の形成素材としては、たとえばポリブチレンテレフタレート(PBT)、ポリカーボネート(PC)、ポリアミド6(PA6)、ポリフェニレンスルフィド(PPS)等を挙げることができる。なお、レーザ光を吸収して発熱を促進するために、これらの樹脂にカーボンブラックや難燃剤等の無機または有機添加剤等が添加された素材から形成されてもよい。   Examples of the material for forming the fastening member include polybutylene terephthalate (PBT), polycarbonate (PC), polyamide 6 (PA6), polyphenylene sulfide (PPS), and the like. In addition, in order to absorb laser light and promote heat generation, these resins may be formed from a material in which an inorganic or organic additive such as carbon black or a flame retardant is added.

上記する取付方法によれば、ビス等の別途の締結部材が不要となり、部品点数や組み付け工数を低減することができる。また、中空部材の内部に挿入された挿入部の端部に中空部材の外部からレーザ光を照射して溶融させ、この溶融された挿入部を中空部材の内周面の一部に押圧することで、中空部材の内周面に対する押圧荷重を抑制することができ、中空部材の変形を抑制しながら容易に挿入部の端部にフランジ部を形成することができる。また、その溶融部を押圧して挿入孔よりも相対的に大きなフランジ部を形成することで、挿入部を押圧するための別途の工具が不要となり、中空部材のような閉空間であってもフランジ部を容易に形成することができる。さらに、挿入孔よりも大きなフランジ部が挿入部に形成されることで、中空部材から締結部材が脱落することを確実に防止することができ、中空部材に対する締結部材の固定信頼性を高めることができる。   According to the mounting method described above, a separate fastening member such as a screw is not required, and the number of parts and assembly man-hours can be reduced. Further, the end of the insertion portion inserted into the hollow member is melted by irradiating laser light from the outside of the hollow member, and the molten insertion portion is pressed against a part of the inner peripheral surface of the hollow member. Thus, the pressing load on the inner peripheral surface of the hollow member can be suppressed, and the flange portion can be easily formed at the end of the insertion portion while suppressing deformation of the hollow member. In addition, by pressing the melted portion to form a flange portion that is relatively larger than the insertion hole, a separate tool for pressing the insertion portion becomes unnecessary, and even in a closed space such as a hollow member The flange portion can be easily formed. Furthermore, since the flange portion larger than the insertion hole is formed in the insertion portion, it is possible to reliably prevent the fastening member from dropping from the hollow member, and to improve the fixing reliability of the fastening member to the hollow member. it can.

また、前記第3の工程においては、前記挿入部の前記端部を前記中空部材の前記内周面の一部に当接させた後に、該端部にレーザ光を照射する実施の形態が好ましい。この形態によれば、レーザ光の照射時間を短縮して、締結部材の取付工程に要するコストを抑制することができる。   Further, in the third step, an embodiment in which the end portion of the insertion portion is brought into contact with a part of the inner peripheral surface of the hollow member and then the end portion is irradiated with laser light is preferable. . According to this aspect, the laser light irradiation time can be shortened, and the cost required for the fastening member attaching step can be suppressed.

また、前記第3の工程において、前記挿入部の前記端部を前記中空部材の前記内周面に押圧しながら該端部にレーザ光を照射することで、押圧時の挿入部の硬化を抑制することができ、取付工程における押圧荷重の増加を抑制して、容易に挿入部の端部に均一なフランジ部を形成することができる。   Further, in the third step, the end portion of the insertion portion is pressed against the inner peripheral surface of the hollow member while irradiating the end portion with laser light, thereby suppressing the hardening of the insertion portion during pressing. It is possible to suppress the increase of the pressing load in the attachment process, and it is possible to easily form a uniform flange portion at the end portion of the insertion portion.

また、上記する取付方法においては、前記締結部材の前記フランジ部と前記中空部材の前記内周面の一部を分離して該フランジ部を固化させる第4の工程をさらに含む実施の形態が好ましい。たとえば、フランジ部が中空部材に当接された状態で当該フランジ部を冷却固化させると、フランジ部と当接している中空部材の表面には、そのフランジ部の熱収縮に起因してひけが発生する可能性が高い。そこで、前記第4の工程によって、フランジ部を中空部材の内周面から分離して固化させることで、締結部材の挿入部が押圧される中空部材の表面のひけの発生を抑制することができ、中空部材の優れた外観(意匠面)を保証することができる。   Moreover, in the mounting method described above, an embodiment that further includes a fourth step of separating the flange portion of the fastening member and a part of the inner peripheral surface of the hollow member to solidify the flange portion is preferable. . For example, if the flange portion is cooled and solidified in a state where the flange portion is in contact with the hollow member, sink marks are generated on the surface of the hollow member in contact with the flange portion due to thermal contraction of the flange portion. There is a high possibility of doing. Therefore, by the fourth step, the flange portion is separated from the inner peripheral surface of the hollow member and solidified, thereby suppressing the occurrence of sink marks on the surface of the hollow member where the insertion portion of the fastening member is pressed. The excellent appearance (design surface) of the hollow member can be guaranteed.

また、上記する取付方法においては、固化された前記フランジ部を該中空部材の内周面の他部と係合させる第5の工程をさらに含む実施の形態が好ましい。この第5の工程によれば、締結部材を中空部材に係合させて固定することができ、たとえば、この締結部材を用いて中空部材を車両のボディパネル等の他の部材に取り付ける際にも、中空部材に対する締結部材の動きを抑制して、容易かつ確実に中空部材を他の部材に取り付けることができる。   Moreover, in the mounting method described above, an embodiment further including a fifth step of engaging the solidified flange portion with the other portion of the inner peripheral surface of the hollow member is preferable. According to the fifth step, the fastening member can be engaged with and fixed to the hollow member. For example, when the hollow member is attached to another member such as a vehicle body panel using the fastening member. The movement of the fastening member relative to the hollow member can be suppressed, and the hollow member can be attached to another member easily and reliably.

ここで、前記中空部材は少なくとも1つの隔壁によって複数のセルに分割されており、該セルの少なくとも1つに前記挿入孔が設けられている形態とすることができる。このようなセルの断面形状としては、たとえばハニカム形状や三角形、四角形等の多角形状や、円形状、楕円形状等を挙げることができる。   Here, the hollow member may be divided into a plurality of cells by at least one partition wall, and the insertion hole may be provided in at least one of the cells. Examples of the cross-sectional shape of the cell include a honeycomb shape, a polygonal shape such as a triangle and a quadrangle, a circular shape, and an elliptical shape.

さらに、前記中空部材と前記締結部材の前記挿入部の溶解パラメータの差が1.0以上である実施の形態が好ましい。   Furthermore, an embodiment in which a difference in solubility parameter between the hollow member and the insertion portion of the fastening member is 1.0 or more is preferable.

ここで、「溶解パラメータ(Solubility Parameter、SP値)」とは、二成分系溶液の溶解度、たとえば溶質と溶媒の混ざり易さを判断する目安となるものであり、溶解パラメータが近い物質は混ざり易い性質を備えていることが知られている。たとえば、正則溶液理論においては、溶媒−溶質間に作用する力は分子間力のみとモデル化されるため、液体分子を凝集させる相互作用は分子間力のみであると考えることができる。そして、液体の凝集エネルギー△Eと蒸発エンタルピー(モル蒸発熱)△Hは、△H=△E+P△Vの関係にあることから、溶解パラメータδは、蒸発エンタルピー△Hとモル体積Vから以下の式(1)で定義される。   Here, the “solubility parameter (SP value)” is a measure for determining the solubility of the binary solution, for example, the ease of mixing the solute and the solvent, and substances having similar solubility parameters are likely to be mixed. It is known to have properties. For example, in the regular solution theory, the force acting between the solvent and the solute is modeled as only the intermolecular force, and therefore, the interaction causing the liquid molecules to aggregate can be considered to be only the intermolecular force. Since the liquid cohesive energy ΔE and the evaporation enthalpy (molar evaporation heat) ΔH are in a relationship of ΔH = ΔE + PΔV, the solubility parameter δ is calculated from the evaporation enthalpy ΔH and the molar volume V as follows: It is defined by equation (1).

Figure 2012193751
Figure 2012193751

ここで、Rは気体定数=8.31447J/K・mol、Tは液体温度であり、SP値は、1cmの液体が蒸発するために必要な蒸発熱の平方根(cal/cm0.5から計算されるものである。 Here, R is a gas constant = 8.331447 J / K · mol, T is the liquid temperature, and the SP value is the square root of the heat of vaporization (cal / cm 3 ) required for evaporation of 1 cm 3 of liquid . It is calculated from 5 .

たとえば、中空部材と締結部材の挿入部が非相溶であれば、双方の部材が混ざり合うことがなく、前記第4の工程において締結部材のフランジ部と中空部材の内周面を分離する際に、容易に双方を分離することができる。しかし、中空部材と締結部材の挿入部が相溶であっても、それらの相溶性が低く、中空部材と締結部材の挿入部の溶解パラメータの差が1.0以上であれば、第4の工程において中空部材と締結部材の挿入部を界面剥離により分離することができ、分離時の中空部材や締結部材の母材破壊を確実に防止することができる。   For example, if the insertion portion of the hollow member and the fastening member is incompatible, the two members do not mix, and the flange portion of the fastening member and the inner peripheral surface of the hollow member are separated in the fourth step. In addition, both can be easily separated. However, even if the insertion part of the hollow member and the fastening member is compatible, the compatibility thereof is low, and if the difference in the solubility parameter between the hollow member and the insertion part of the fastening member is 1.0 or more, the fourth In the process, the insertion portion of the hollow member and the fastening member can be separated by interfacial peeling, and the base material destruction of the hollow member and the fastening member during separation can be reliably prevented.

また、本発明は、締結部材が中空部材に取り付けられた中空部材と締結部材の取付構造体にも及ぶものである。前記中空部材は挿入孔を有し、かつレーザ光を透過する透過性材料から構成され、前記締結部材は挿入部を有し、少なくとも該挿入部がレーザ光を吸収する吸収性材料であって熱可塑性材料から構成されており、前記締結部材の前記挿入部の少なくとも一部が前記中空部材の挿入孔を介して前記中空部材の内部に収容されており、前記中空部材の内部に収容された前記挿入部の端部が、前記中空部材の外部からのレーザ光照射によって溶融され、該中空部材の内周面の一部に対する押圧によって形成された前記挿入孔よりも相対的に大きなフランジ部を備えているものである。   Further, the present invention extends to a mounting structure for a fastening member and a hollow member in which the fastening member is attached to the hollow member. The hollow member has an insertion hole and is made of a transmissive material that transmits laser light, and the fastening member has an insertion portion, and at least the insertion portion is an absorptive material that absorbs laser light and is heated. It is made of a plastic material, and at least a part of the insertion portion of the fastening member is accommodated in the hollow member through an insertion hole of the hollow member, and the accommodating portion is accommodated in the hollow member. An end portion of the insertion portion includes a flange portion that is melted by laser light irradiation from the outside of the hollow member and is relatively larger than the insertion hole formed by pressing against a part of the inner peripheral surface of the hollow member. It is what.

本実施の形態の中空部材と締結部材の取付構造体によれば、締結部材を中空部材に取り付けるための別途の締結部材が不要となり、部品点数の増加が抑制され、車両等の軽量化を図ることができる。また、挿入部の端部に形成されるフランジ部によって、高い締結強度を保証することができ、中空部材に対する締結部材の固定信頼性を高めることができる。さらに、ビス等の別途の締結部材が表面に露出することがなく、優れた外観(意匠面)を保証することができる。   According to the mounting structure of the hollow member and the fastening member of the present embodiment, a separate fastening member for attaching the fastening member to the hollow member becomes unnecessary, an increase in the number of parts is suppressed, and the weight of the vehicle or the like is reduced. be able to. Moreover, high fastening strength can be ensured by the flange part formed in the edge part of an insertion part, and the fixation reliability of the fastening member with respect to a hollow member can be improved. Furthermore, a separate fastening member such as a screw is not exposed on the surface, and an excellent appearance (design surface) can be guaranteed.

以上の説明から理解できるように、本発明の中空部材と締結部材の取付方法とその取付構造体によれば、部品点数の増加を抑制することで軽量化と製造工程の簡素化を図ることができ、さらに挿入部にフランジ部を形成することで中空部材と締結部材の締結強度を高めることができる。   As can be understood from the above description, according to the mounting method and the mounting structure of the hollow member and the fastening member of the present invention, it is possible to reduce the weight and simplify the manufacturing process by suppressing the increase in the number of parts. Furthermore, the fastening strength of the hollow member and the fastening member can be increased by forming the flange portion in the insertion portion.

本発明の中空部材と締結部材の取付方法を説明する図であり、(a)は中空部材と締結部材を準備する第1の工程を示した図であり、(b)は、第1の工程に続いて、挿入孔を介して挿入部を挿入する第2の工程を示した図であり、(c)は、第2の工程に続いて、挿入部の端部にレーザ光を照射して溶融させ、挿入部を中空部材の内周面に押圧してフランジ部を形成する第3の工程を示した図である。It is a figure explaining the attachment method of the hollow member and fastening member of this invention, (a) is the figure which showed the 1st process of preparing a hollow member and a fastening member, (b) is the 1st process. FIG. 9C is a diagram showing a second step of inserting the insertion portion through the insertion hole, and (c) is a step of irradiating the end of the insertion portion with laser light following the second step. It is the figure which showed the 3rd process which melts and presses an insertion part on the internal peripheral surface of a hollow member, and forms a flange part. 図1(a)で示す中空部材のA−A矢視図である。It is an AA arrow directional view of the hollow member shown to Fig.1 (a). 図1(c)で示す第3の工程に続いて、締結部材のフランジ部と中空部材を分離してフランジ部を固化させる第4の工程を示した図である。It is the figure which showed the 4th process of separating the flange part and hollow member of a fastening member, and solidifying a flange part following the 3rd process shown in FIG.1 (c). 図3で示す第4の工程に続いて、固化されたフランジ部を中空部材の内周面の他部と係合させる第5の工程を示した図である。FIG. 10 is a view showing a fifth step of engaging the solidified flange portion with the other portion of the inner peripheral surface of the hollow member following the fourth step shown in FIG. 3. 中空部材と締結部材を想定した試験片を示した斜視図である。It is the perspective view which showed the test piece supposing the hollow member and the fastening member. 中空部材と締結部材のSP値の差と溶着強度の関係を示した図である。It is the figure which showed the relationship between the difference of SP value of a hollow member and a fastening member, and welding strength. 従来の中空部材と締結部材の取付方法を説明する図であり、(a)は中空部材と締結部材を準備する工程を説明する図であり、(b)は締結部材を中空部材の取付位置に配置する工程を説明する図であり、(c)はビスで締結部材を中空部材へ取り付ける工程を説明する図である。It is a figure explaining the attachment method of the conventional hollow member and a fastening member, (a) is a figure explaining the process of preparing a hollow member and a fastening member, (b) is a fastening member in the attachment position of a hollow member. It is a figure explaining the process of arrange | positioning, (c) is a figure explaining the process of attaching a fastening member to a hollow member with a screw.

以下、図面を参照して本発明の実施の形態を説明する。   Embodiments of the present invention will be described below with reference to the drawings.

図1は、本発明の中空部材と締結部材の取付方法を説明する図であり、図1(a)は中空部材と締結部材を準備する第1の工程を示した図であり、図1(b)は、第1の工程に続いて、挿入孔を介して挿入部を挿入する第2の工程を示した図であり、図1(c)は、第2の工程に続いて、挿入部の端部にレーザ光を照射して溶融させ、挿入部を中空部材の内周面に押圧してフランジ部を形成する第3の工程を示した図である。また、図2は、図1(a)で示す中空部材のA−A矢視図である。   FIG. 1 is a diagram illustrating a method for attaching a hollow member and a fastening member according to the present invention, and FIG. 1 (a) is a diagram illustrating a first step of preparing the hollow member and the fastening member. b) is a diagram showing a second step of inserting the insertion portion through the insertion hole following the first step, and FIG. 1C is a drawing of the insertion portion following the second step. It is the figure which showed the 3rd process of irradiating a laser beam to the edge part of this, melt | dissolving, and pressing an insertion part on the internal peripheral surface of a hollow member, and forming a flange part. Moreover, FIG. 2 is an AA arrow view of the hollow member shown in FIG.

まず、図1(a)で示すように、レーザ光を透過する透過性材料からなる中空部材10と、レーザ光を吸収する吸収性材料であって熱可塑性材料からなる締結部材(たとえば、クリップ)20を準備する(第1の工程)。   First, as shown in FIG. 1A, a hollow member 10 made of a transparent material that transmits laser light, and a fastening member made of a thermoplastic material that absorbs laser light and is made of a thermoplastic material (for example, a clip). 20 is prepared (first step).

図示するように、中空部材10は、その一方側の側壁1と、側壁1とは反対側の他方側の側壁2を有し、側壁1と側壁2は中空部材10の内部空間を分割する隔壁3によって接続され、中空部材10の内部空間に1つのセル9が形成されている。また、一方側の側壁1の略中央部には挿入孔5が設けられている。なお、中空部材10の挿入孔5については、第1の工程よりも先に、予めドリル等の切削工具を用いて閉空間を備えた中空部材10の側壁1に穿設することができる。   As shown in the figure, the hollow member 10 has a side wall 1 on one side and a side wall 2 on the other side opposite to the side wall 1, and the side wall 1 and the side wall 2 partition the internal space of the hollow member 10. 3, one cell 9 is formed in the internal space of the hollow member 10. Further, an insertion hole 5 is provided in a substantially central portion of the side wall 1 on one side. In addition, about the insertion hole 5 of the hollow member 10, it can pierce in the side wall 1 of the hollow member 10 provided with closed space beforehand using cutting tools, such as a drill, prior to a 1st process.

締結部材20は頭部11と挿入部12を有していて、頭部11は、たとえばボディ構成部材であるボディパネル等の他の部材に取付けられる際に使用される。また、挿入部12は、中空部材10の挿入孔5に挿入可能な大きさや形状を備えている。なお、この挿入部12の長さL2(締結部材20の頭部11を除いた長さ)は、少なくとも中空部材10の挿入方向の深さL1よりも長い。   The fastening member 20 has a head portion 11 and an insertion portion 12, and the head portion 11 is used when attached to another member such as a body panel which is a body constituting member. The insertion portion 12 has a size and a shape that can be inserted into the insertion hole 5 of the hollow member 10. The length L2 of the insertion portion 12 (the length excluding the head 11 of the fastening member 20) is at least longer than the depth L1 of the hollow member 10 in the insertion direction.

なお、図1(a)で示す中空部材10は、図2で示すようにセル9の断面形状が六角形を呈するハニカム構造を備えている。   The hollow member 10 shown in FIG. 1A has a honeycomb structure in which the cross-sectional shape of the cells 9 is hexagonal as shown in FIG.

上記する第1の工程に続いて、図1(b)で示すように、たとえば不図示の保持手段によって締結部材20の頭部11を保持しながら、締結部材20の挿入部12を挿入孔5を貫通して中空部材10の内部へ(矢印X1方向へ)挿入する(第2の工程)。   Subsequent to the first step described above, as shown in FIG. 1B, the insertion portion 12 of the fastening member 20 is inserted into the insertion hole 5 while holding the head portion 11 of the fastening member 20 by, for example, a holding means (not shown). Is inserted into the hollow member 10 (in the direction of the arrow X1) (second step).

挿入部12の端部13を中空部材10の側壁2の内周面4と当接させた後、図1(c)で示すように、中空部材10の他方側の側壁2の外部に配置したレーザ発振機50から、中空部材10の側壁2を透過して、中空部材10の内部に挿入された挿入部12の端部13に赤外線レーザ光Rを照射する。そして、レーザ光Rを吸収して溶融した挿入部12を、たとえば不図示の保持手段により中空部材10の側壁2の内周面4に押圧し、挿入孔5よりも相対的に外径の大きなフランジ部14を形成する(第3の工程)。なお、挿入部12の一部を中空部材10の内部に挿入した後、挿入部12の端部13を中空部材10の側壁2の内周面4と当接させる前に、中空部材10のセル9内に挿入された挿入部12の端部13にレーザ光を照射して挿入部12を溶融させることもできる。   After the end portion 13 of the insertion portion 12 is brought into contact with the inner peripheral surface 4 of the side wall 2 of the hollow member 10, it is disposed outside the side wall 2 on the other side of the hollow member 10 as shown in FIG. From the laser oscillator 50, the infrared laser light R is irradiated to the end portion 13 of the insertion portion 12 that is transmitted through the side wall 2 of the hollow member 10 and inserted into the hollow member 10. Then, the insertion portion 12 that has absorbed and melted the laser light R is pressed against the inner peripheral surface 4 of the side wall 2 of the hollow member 10 by, for example, a holding means (not shown), and has a relatively larger outer diameter than the insertion hole 5. The flange portion 14 is formed (third step). In addition, after inserting a part of insertion part 12 into the inside of the hollow member 10, before making the edge part 13 of the insertion part 12 contact | abut with the internal peripheral surface 4 of the side wall 2 of the hollow member 10, the cell of the hollow member 10 is used. It is also possible to melt the insertion portion 12 by irradiating the end portion 13 of the insertion portion 12 inserted into the laser beam 9 with a laser beam.

第3の工程においては、挿入部12を中空部材10の側壁2に押圧する際にレーザ発振機50を停止し、溶融された挿入部12の残留熱を利用して挿入部12を熱変形させてフランジ部14を形成することができる。また、溶融した挿入部12を中空部材10の側壁2に押圧する際にもレーザ発振機50からレーザ光Rを照射することで、溶融した挿入部12を高温状態に保持することができ、より均一なフランジ部14を形成することができる。   In the third step, the laser oscillator 50 is stopped when the insertion portion 12 is pressed against the side wall 2 of the hollow member 10, and the insertion portion 12 is thermally deformed using the residual heat of the molten insertion portion 12. Thus, the flange portion 14 can be formed. In addition, when the molten insert portion 12 is pressed against the side wall 2 of the hollow member 10, the laser insert 50 can irradiate the laser beam R to hold the melted insert portion 12 in a high temperature state. A uniform flange portion 14 can be formed.

このように、溶融した挿入部12を中空部材10の内周面4に押圧してフランジ部14を形成することで、中空部材10の内周面4に対する押圧荷重を抑制しながら挿入部12の端部13に容易にフランジ部14を形成することができる。また、挿入孔5よりも相対的に大きなフランジ部14が挿入部12に形成されることで、締結部材20が中空部材10から脱落することを確実に防止することができ、中空部材10に対する締結部材20の固定信頼性を高めることができる。   In this way, by pressing the melted insertion portion 12 against the inner peripheral surface 4 of the hollow member 10 to form the flange portion 14, the pressing load on the inner peripheral surface 4 of the hollow member 10 can be suppressed while suppressing the pressing load of the insertion portion 12. The flange portion 14 can be easily formed on the end portion 13. In addition, since the flange portion 14 that is relatively larger than the insertion hole 5 is formed in the insertion portion 12, it is possible to reliably prevent the fastening member 20 from falling off the hollow member 10, and to fasten the hollow member 10. The fixing reliability of the member 20 can be improved.

なお、レーザ発振機50により挿入部12の端部13に垂直にレーザ光Rを照射することで、効率的に挿入部12の端部13を溶融させることができる。また、レーザ発振機50を走査し、挿入部12の多方面からレーザ光Rを照射することで、より均一に挿入部12を溶融させて均一なフランジ部14を形成することができる。さらに、レーザ発振機50を複数配置し、挿入部12の様々な角度から同時にレーザ光Rを照射してもよい。   Note that the end portion 13 of the insertion portion 12 can be efficiently melted by irradiating the laser beam R perpendicularly to the end portion 13 of the insertion portion 12 by the laser oscillator 50. Further, by scanning the laser oscillator 50 and irradiating the laser beam R from many directions of the insertion portion 12, the insertion portion 12 can be melted more uniformly and the uniform flange portion 14 can be formed. Further, a plurality of laser oscillators 50 may be arranged, and the laser beam R may be irradiated simultaneously from various angles of the insertion portion 12.

次に、図3は、図1(c)で示す第3の工程に続いて、締結部材のフランジ部と中空部材を分離してフランジ部を固化させる第4の工程を示した図である。   Next, FIG. 3 is a view showing a fourth step of solidifying the flange portion by separating the flange portion and the hollow member of the fastening member following the third step shown in FIG.

たとえば、図1(c)で示すように、締結部材20の挿入部12が中空部材10の側壁2と当接した姿勢で溶融した挿入部12が冷却固化すると、中空部材10の側壁2の表面には、溶融した挿入部12が固化する際の熱収縮によってひけが発生する可能性がある。そこで、第3の工程でフランジ部14を形成した後、レーザ発信機50を停止し、図3で示すように、締結部材20のフランジ部14が溶融した状態で締結部材20を矢印X2方向へ移動させ、中空部材10の側壁2の内周面4からフランジ部14を分離して、フランジ部14を冷却固化させる(第4の工程)。なお、フランジ部14の冷却方法としては、たとえば自然放熱による冷却や冷却器による冷却等を適用することができる。   For example, as shown in FIG. 1C, when the inserted portion 12 melted in a posture in which the insertion portion 12 of the fastening member 20 is in contact with the side wall 2 of the hollow member 10 is cooled and solidified, the surface of the side wall 2 of the hollow member 10. In some cases, sinks may occur due to thermal contraction when the molten insertion portion 12 is solidified. Therefore, after forming the flange portion 14 in the third step, the laser transmitter 50 is stopped, and as shown in FIG. 3, the fastening member 20 is moved in the arrow X2 direction in a state where the flange portion 14 of the fastening member 20 is melted. The flange portion 14 is separated from the inner peripheral surface 4 of the side wall 2 of the hollow member 10 to cool and solidify the flange portion 14 (fourth step). In addition, as a cooling method of the flange part 14, cooling by natural heat dissipation, cooling by a cooler, etc. are applicable, for example.

ここで、締結部材20の挿入部12と中空部材10の溶解パラメータ(SP値)の差が大きければ、中空部材10や締結部材20を母材破壊させることなく、締結部材20のフランジ部14を中空部材10の側壁2の内周面4から界面剥離させることができる。   Here, if the difference in the solubility parameter (SP value) between the insertion portion 12 of the fastening member 20 and the hollow member 10 is large, the flange portion 14 of the fastening member 20 can be removed without destroying the hollow member 10 or the fastening member 20. Interfacial peeling can be performed from the inner peripheral surface 4 of the side wall 2 of the hollow member 10.

このように、中空部材10の側壁2の内周面4とフランジ部14を分離した後、フランジ部14を冷却固化させることで、中空部材10と締結部材20が冷却速度の異なる樹脂材料から構成されている場合であっても、中空部材10の側壁2の表面のひけの発生を確実に防止することができる。また、締結部材20の挿入部12と中空部材10のSP値の差を大きくすることで、分離時の中空部材10の変形や破損を確実に防止することができ、中空部材10の優れた外観(意匠面)を保証することができる。   Thus, after separating the inner peripheral surface 4 and the flange portion 14 of the side wall 2 of the hollow member 10, the hollow portion 10 and the fastening member 20 are made of resin materials having different cooling rates by cooling and solidifying the flange portion 14. Even if it is the case where it is done, generation | occurrence | production of the sink of the surface of the side wall 2 of the hollow member 10 can be prevented reliably. Further, by increasing the difference in SP value between the insertion portion 12 of the fastening member 20 and the hollow member 10, deformation and breakage of the hollow member 10 during separation can be reliably prevented, and the excellent appearance of the hollow member 10 (Design surface) can be guaranteed.

なお、中空部材10の側壁2の表面のひけの発生をより確実に防止するために、分離後のフランジ部14と側壁2の内周面4との間隔D1は、0.1mm以上であるのが好ましい。   In order to prevent the sink of the surface of the side wall 2 of the hollow member 10 more reliably, the distance D1 between the flange portion 14 after separation and the inner peripheral surface 4 of the side wall 2 is 0.1 mm or more. Is preferred.

また、レーザ光を照射しながら中空部材10の側壁2の内周面4からフランジ部14を分離させることで、分離時のフランジ部14の固化を確実に防止することができ、中空部材10の側壁2の表面のひけの発生を効果的に抑制することもできる。   Further, by separating the flange portion 14 from the inner peripheral surface 4 of the side wall 2 of the hollow member 10 while irradiating the laser beam, solidification of the flange portion 14 at the time of separation can be surely prevented. The occurrence of sink marks on the surface of the side wall 2 can also be effectively suppressed.

このように、レーザ光照射によって溶融された挿入部12の端部13が冷却固化されて、締結部材20が中空部材10に取り付けられた中空部材10と締結部材20の取付構造体が形成され、この取付構造体が今度はたとえばボディを構成するインナパネルやドアパネル、バンパビーム等に取り付けられることとなる。   Thus, the end portion 13 of the insertion portion 12 melted by the laser light irradiation is cooled and solidified, and the attachment structure of the hollow member 10 and the fastening member 20 in which the fastening member 20 is attached to the hollow member 10 is formed. This attachment structure is now attached to, for example, an inner panel, a door panel, a bumper beam, or the like constituting the body.

図4は、上記第4の工程により冷却固化されたフランジ部14を中空部材10の側壁1の挿入孔5周りの周辺部6と係合させる工程を説明したものである。   FIG. 4 illustrates a step of engaging the flange portion 14 cooled and solidified in the fourth step with the peripheral portion 6 around the insertion hole 5 of the side wall 1 of the hollow member 10.

図3で示す第3の工程によって中空部材10に取り付けられた締結部材20の挿入部12(フランジ部14)は、中空部材10のセル9内で自由に動くことができる。そこで、図4で示すように、弾性を有する係合部7を中空部材10の側壁1に予め形成しておき、締結部材20を矢印X3方向へさらに移動させて、締結部材20のフランジ部14を中空部材10の側壁1と係合部7によって挟持し、締結部材20のフランジ部14を中空部材10の側壁1の挿入孔5周りの周辺部6と係合させて固定する(第5の工程)。   The insertion portion 12 (flange portion 14) of the fastening member 20 attached to the hollow member 10 by the third step shown in FIG. 3 can freely move within the cell 9 of the hollow member 10. Therefore, as shown in FIG. 4, the engaging portion 7 having elasticity is formed in advance on the side wall 1 of the hollow member 10, and the fastening member 20 is further moved in the direction of the arrow X <b> 3, so that the flange portion 14 of the fastening member 20. Is sandwiched between the side wall 1 of the hollow member 10 and the engaging portion 7, and the flange portion 14 of the fastening member 20 is engaged with and fixed to the peripheral portion 6 around the insertion hole 5 of the side wall 1 of the hollow member 10 (fifth). Process).

この第5の工程によれば、締結部材20を中空部材10に対して固定して取り付けることができ、中空部材10に対する締結部材20の動きを抑制することができる。よって、たとえば車両の組立工程において、中空部材10に取り付けられた締結部材11の頭部11を、例えばインナパネルやドアパネル、バンパビーム等に設けられた貫通孔に容易かつ確実に取り付けることができ、この中空部材10と締結部材20の取付構成体の車両に対する取り付け作業を簡素化することができる。   According to the fifth step, the fastening member 20 can be fixed and attached to the hollow member 10, and the movement of the fastening member 20 with respect to the hollow member 10 can be suppressed. Therefore, for example, in the vehicle assembly process, the head 11 of the fastening member 11 attached to the hollow member 10 can be easily and reliably attached to, for example, a through-hole provided in an inner panel, a door panel, a bumper beam, etc. It is possible to simplify the work of attaching the mounting structure of the hollow member 10 and the fastening member 20 to the vehicle.

なお、中空部材10の側壁2の内周面4と締結部材20のフランジ部14の間隔D2を0.1〜0.2mm程度とすることで、係合部7等の別途の係合手段を用いることなく、車両に対する取り付け作業に支障の無い範囲内で、上記取付構成体の締結部材20の動き(がたつき)を抑制することもできる。   In addition, by setting the distance D2 between the inner peripheral surface 4 of the side wall 2 of the hollow member 10 and the flange portion 14 of the fastening member 20 to about 0.1 to 0.2 mm, additional engagement means such as the engagement portion 7 can be provided. Without using it, the movement (rattle) of the fastening member 20 of the mounting structure can be suppressed within a range that does not hinder the mounting operation on the vehicle.

なお、図1,3,4で示す中空部材10の側壁1,2と隔壁3の断面形状については上記形態に限定されず、それらのうち少なくともいずれかを曲面形状で形成することができる。たとえば側壁1,2と隔壁3のすべてを連続的に曲面形状で形成して、中空部材10のセル9の断面形状を略円形状とすることもできる。   In addition, about the cross-sectional shape of the side walls 1 and 2 and the partition 3 of the hollow member 10 shown by FIG.1, 3,4, it is not limited to the said form, At least any one can be formed in a curved-surface shape. For example, all of the side walls 1 and 2 and the partition wall 3 can be continuously formed in a curved shape, and the cross-sectional shape of the cell 9 of the hollow member 10 can be made substantially circular.

[中空部材と締結部材の溶着強度に関する実験とその結果]
本発明者等は、上記中空部材と締結部材に適した樹脂材料を特定するために、以下の手順により作製した比較例1,2と実施例1〜3について引張試験を実施し、その溶着強度(引張強度)と破壊形態を測定した。
[Experiment and result on welding strength of hollow member and fastening member]
In order to identify the resin material suitable for the hollow member and the fastening member, the present inventors conducted a tensile test on Comparative Examples 1 and 2 and Examples 1 to 3 prepared by the following procedure, and the welding strength thereof. (Tensile strength) and fracture mode were measured.

まず、表1で示す4種の樹脂材料を用いて、中空部材と締結部材を想定した双方の試験片を用意した。ここで、中空部材の形成素材としては、比較的SP値の小さいポリプロピレン(PP)とポリブチレンテレフタレート(PBT)を使用した。そして、中空部材の前記他方側の側壁を想定して1mm厚の試験片31を用意した。また、締結部材の形成素材としては、表1で示す4種の材料(ポリプロピレン(PP)、ポリブチレンテレフタレート(PBT)、ポリカーボネート(PC)、ポリアミド(PA6))を使用した。そして、締結部材の前記挿入部を想定して3mm厚の試験片32を用意した(図5(a)参照)。   First, using the four types of resin materials shown in Table 1, both test pieces assuming a hollow member and a fastening member were prepared. Here, as a material for forming the hollow member, polypropylene (PP) and polybutylene terephthalate (PBT) having a relatively small SP value were used. A 1 mm thick test piece 31 was prepared assuming the other side wall of the hollow member. Moreover, as a forming material of a fastening member, four types of materials shown in Table 1 (polypropylene (PP), polybutylene terephthalate (PBT), polycarbonate (PC), and polyamide (PA6)) were used. A test piece 32 having a thickness of 3 mm was prepared assuming the insertion portion of the fastening member (see FIG. 5A).

Figure 2012193751
Figure 2012193751

そして、上記で用意した中空部材と締結部材双方の試験片のうち、SP値が同じ若しくはSP値の差が小さい試験片を選択して比較例1,2を作製した。表2で示すように、比較例1は、中空部材と締結部材双方の試験片の形成素材がPPである。比較例2は、中空部材の試験片の形成素材がPBT、締結部材の試験片の形成素材がPCである。   Then, out of the test pieces of both the hollow member and the fastening member prepared above, the test pieces having the same SP value or a small difference in SP value were selected to produce Comparative Examples 1 and 2. As shown in Table 2, in Comparative Example 1, the material for forming the test pieces of both the hollow member and the fastening member is PP. In Comparative Example 2, the material for forming the test piece for the hollow member is PBT, and the material for forming the test piece for the fastening member is PC.

また、上記で用意した中空部材と締結部材双方の試験片のうち、SP値の差が相対的に大きい試験片を選択して実施例1〜3を作製した。実施例1〜3すべてにおいて、中空部材の試験片の形成素材はPPである。また、締結部材の試験片の形成素材はそれぞれ、実施例1がPBT、実施例2がPC、実施例3がPA6である。   Moreover, Examples 1-3 were produced by selecting a test piece having a relatively large difference in SP value from the test pieces of both the hollow member and the fastening member prepared above. In all of Examples 1 to 3, the material for forming the test piece of the hollow member is PP. In addition, the forming material of the test piece of the fastening member is PBT in Example 1, PC in Example 2, and PA6 in Example 3.

比較例1,2の中空部材の試験片と締結部材の試験片のSP値の差は、それぞれ0.0,0.1である。また、実施例1,2,3の中空部材の試験片と締結部材の試験片のSP値の差は、それぞれ1.0,1.1,4.5である。   The difference in SP value between the test piece of the hollow member and the test piece of the fastening member in Comparative Examples 1 and 2 is 0.0 and 0.1, respectively. Moreover, the difference of SP value of the test piece of the hollow member of Examples 1, 2, and 3 and the test piece of a fastening member is 1.0, 1.1, and 4.5, respectively.

なお、比較例1,2と実施例1〜3を作製するに当たり、中空部材の他方側の側壁を想定した1mm厚の試験片31に、締結部材の挿入部を想定した3mm厚の試験片32を当接させた後、中空部材の試験片31に対して締結部材の試験片32を1.1MPaで押圧しながら、試験片31の反対側に配置されたロフィン社製半導体レーザ発振機から焦点径がφ5mmとなるように試験片32の端部33にレーザ光を照射して、溶融した試験片32の端部33に約5〜6mmの幅を有するフランジ部34を形成した(図5(b)参照)。   In preparing Comparative Examples 1 and 2 and Examples 1 to 3, a 1 mm thick test piece 31 assuming the other side wall of the hollow member and a 3 mm thickness test piece 32 assuming an insertion portion of a fastening member. After pressing the test piece 32 of the fastening member against the test piece 31 of the hollow member at 1.1 MPa, the focal point is taken from the semiconductor laser oscillator manufactured by Roffin Corporation disposed on the opposite side of the test piece 31. The end portion 33 of the test piece 32 was irradiated with laser light so that the diameter was 5 mm, and a flange portion 34 having a width of about 5 to 6 mm was formed on the end portion 33 of the melted test piece 32 (FIG. 5 ( b)).

上記手順により作製した比較例1,2と実施例1〜3について、図5(b)で示す矢印Y方向へ引張試験を実施し、その溶着強度(引張強度)と破壊形態を測定した。その結果を表2に示す。   About the comparative examples 1 and 2 and Examples 1-3 produced by the said procedure, the tension test was implemented to the arrow Y direction shown in FIG.5 (b), and the welding strength (tensile strength) and the fracture | rupture form were measured. The results are shown in Table 2.

Figure 2012193751
Figure 2012193751

表2で示すように、比較例1,2においては、中空部材と締結部材の試験片同士のSP値が同じ若しくは双方のSP値の差が小さいため、双方の試験片同士が溶着され、引張試験後の中空部材側の試験片が母材破壊していることが確認された。また、その際の溶着強度(引張強度)は、それぞれ30MPa,40MPaであった。   As shown in Table 2, in Comparative Examples 1 and 2, the SP values of the test pieces of the hollow member and the fastening member are the same or the difference between the SP values of the two members is small. It was confirmed that the test piece on the hollow member side after the test was broken. Further, the welding strength (tensile strength) at that time was 30 MPa and 40 MPa, respectively.

実施例1〜3においては、中空部材と締結部材の試験片同士のSP値の差が大きいため、レーザ光照射後においても双方の試験片同士が溶着しておらず、引張試験において双方の試験片が界面剥離していることが確認された。なお、引張試験においてはほとんど引張力を作用させることなく双方の試験片同士を分離することができたため、溶着強度は確認されなかった。   In Examples 1 to 3, since the difference in SP value between the test pieces of the hollow member and the fastening member is large, both the test pieces are not welded even after laser beam irradiation, and both tests are performed in the tensile test. It was confirmed that the pieces were peeled at the interface. In addition, in the tensile test, since both test pieces were able to isolate | separate almost without applying a tensile force, the welding strength was not confirmed.

図6は、中空部材と締結部材の試験片同士のSP値の差と溶着強度の関係を示した図である。図示するように、中空部材と締結部材の試験片同士のSP値の差が1.0以上であれば、双方の試験片同士が溶着されないため、溶着強度が発生せず、界面剥離によって双方の試験片同士を分離することができることが実証された。すなわち、中空部材と締結部材のSP値の差が1.0以上であれば、図3で示す第4の工程において、締結部材のフランジ部を中空部材の側壁の内周面から分離させる際にも、中空部材や締結部材を変形若しくは破損させることなく、双方の部材同士を分離できることが実証された。   FIG. 6 is a diagram showing the relationship between the SP value difference between the test pieces of the hollow member and the fastening member and the welding strength. As shown in the figure, if the difference in SP value between the test pieces of the hollow member and the fastening member is 1.0 or more, both test pieces are not welded to each other. It has been demonstrated that the specimens can be separated from each other. That is, when the difference in SP value between the hollow member and the fastening member is 1.0 or more, in the fourth step shown in FIG. 3, when the flange portion of the fastening member is separated from the inner peripheral surface of the side wall of the hollow member. It has also been demonstrated that both members can be separated without deforming or damaging the hollow member or the fastening member.

以上、本発明の実施の形態を図面を用いて詳述してきたが、具体的な構成はこの実施形態に限定されるものではなく、本発明の要旨を逸脱しない範囲における設計変更等があっても、それらは本発明に含まれるものである。   The embodiment of the present invention has been described in detail with reference to the drawings. However, the specific configuration is not limited to this embodiment, and there are design changes and the like without departing from the gist of the present invention. They are also included in the present invention.

1,2…側壁、3…隔壁、4…内周面、5…挿入孔、9…セル、10…中空部材、11…頭部、12…挿入部、13…端部、14…フランジ部、20…締結部材、31…中空部材の試験片、32…締結部材の試験片、50…レーザ発振機、R…レーザ DESCRIPTION OF SYMBOLS 1, 2 ... Side wall, 3 ... Partition, 4 ... Inner peripheral surface, 5 ... Insertion hole, 9 ... Cell, 10 ... Hollow member, 11 ... Head, 12 ... Insertion part, 13 ... End part, 14 ... Flange part, DESCRIPTION OF SYMBOLS 20 ... Fastening member, 31 ... Test piece of hollow member, 32 ... Test piece of fastening member, 50 ... Laser oscillator, R ... Laser

Claims (8)

中空部材と締結部材の取付方法であって、
挿入孔を有し、レーザ光を透過する透過性材料から構成される中空部材と、該挿入孔に挿入可能な挿入部を有し、少なくとも該挿入部がレーザ光を吸収する吸収性材料であって熱可塑性材料から構成される締結部材を準備する第1の工程と、
前記挿入孔を介して前記中空部材の内部に前記締結部材の挿入部を挿入する第2の工程と、
前記中空部材の内部に挿入された前記挿入部の端部に該中空部材の外部からレーザ光を照射して溶融させ、該挿入部を該中空部材の内周面の一部に押圧して前記挿入孔よりも相対的に大きなフランジ部を該挿入部に形成する第3の工程からなる中空部材と締結部材の取付方法。
A mounting method for a hollow member and a fastening member,
A hollow member having an insertion hole and made of a transparent material that transmits laser light and an insertion part that can be inserted into the insertion hole, and at least the insertion part is an absorbing material that absorbs laser light. A first step of preparing a fastening member made of a thermoplastic material;
A second step of inserting the insertion portion of the fastening member into the hollow member through the insertion hole;
The end portion of the insertion portion inserted into the hollow member is irradiated with a laser beam from the outside of the hollow member to be melted, and the insertion portion is pressed against a part of the inner peripheral surface of the hollow member. A method for attaching a hollow member and a fastening member, comprising a third step of forming a flange portion relatively larger than the insertion hole in the insertion portion.
前記第3の工程において、前記挿入部の前記端部を前記中空部材の前記内周面の一部に当接させた後に、該端部にレーザ光を照射する請求項1に記載の中空部材と締結部材の取付方法。   The hollow member according to claim 1, wherein, in the third step, the end portion of the insertion portion is brought into contact with a part of the inner peripheral surface of the hollow member, and then the end portion is irradiated with laser light. And attachment method of the fastening member. 前記第3の工程において、前記挿入部の前記端部を前記中空部材の前記内周面に押圧しながら該端部にレーザ光を照射して前記フランジ部を形成する請求項1または2に記載の中空部材と締結部材の取付方法。   The said 3rd process WHEREIN: While pressing the said edge part of the said insertion part to the said internal peripheral surface of the said hollow member, a laser beam is irradiated to this edge part, and the said flange part is formed. Mounting method of hollow member and fastening member. 前記締結部材の前記フランジ部と前記中空部材の前記内周面の一部を分離して該フランジ部を固化させる第4の工程をさらに含む請求項1〜3のいずれかに記載の中空部材と締結部材の取付方法。   The hollow member according to any one of claims 1 to 3, further comprising a fourth step of separating the flange portion of the fastening member and a part of the inner peripheral surface of the hollow member to solidify the flange portion. Attachment method of a fastening member. 固化された前記フランジ部を該中空部材の内周面の他部と係合させる第5の工程をさらに含む請求項4に記載の中空部材と締結部材の取付方法。   The method for attaching the hollow member and the fastening member according to claim 4, further comprising a fifth step of engaging the solidified flange portion with the other portion of the inner peripheral surface of the hollow member. 前記中空部材が少なくとも1つの隔壁によって複数のセルに分割されており、該セルの少なくとも1つに前記挿入孔が設けられている請求項1〜5のいずれかに記載の中空部材と締結部材の取付方法。   The hollow member and the fastening member according to any one of claims 1 to 5, wherein the hollow member is divided into a plurality of cells by at least one partition wall, and the insertion hole is provided in at least one of the cells. Mounting method. 前記中空部材と前記締結部材の前記挿入部の溶解パラメータの差が1.0以上である請求項1〜6のいずれかに記載の中空部材と締結部材の取付方法。   The method for attaching the hollow member and the fastening member according to any one of claims 1 to 6, wherein a difference in solubility parameter between the insertion portion of the hollow member and the fastening member is 1.0 or more. 中空部材と締結部材の取付構造体であって、
前記中空部材は挿入孔を有し、かつレーザ光を透過する透過性材料から構成され、前記締結部材は挿入部を有し、少なくとも該挿入部がレーザ光を吸収する吸収性材料であって熱可塑性材料から構成されており、
前記締結部材の前記挿入部の少なくとも一部が前記中空部材の挿入孔を介して前記中空部材の内部に収容されており、
前記中空部材の内部に収容された前記挿入部の端部が、前記中空部材の外部からのレーザ光照射によって溶融され、該中空部材の内周面の一部に対する押圧によって形成された前記挿入孔よりも相対的に大きなフランジ部を備えている中空部材と締結部材の取付構造体。


A mounting structure of a hollow member and a fastening member,
The hollow member has an insertion hole and is made of a transmissive material that transmits laser light, and the fastening member has an insertion portion, and at least the insertion portion is an absorptive material that absorbs laser light and is heated. Composed of plastic material,
At least a part of the insertion portion of the fastening member is accommodated in the hollow member through an insertion hole of the hollow member;
The insertion hole formed by pressing the end of the insertion part accommodated in the hollow member by laser light irradiation from the outside of the hollow member and pressing a part of the inner peripheral surface of the hollow member A mounting structure of a hollow member and a fastening member having a relatively larger flange portion.


JP2011056043A 2011-03-15 2011-03-15 Method for mounting hollow member and fastening member, and mounting structure Withdrawn JP2012193751A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP2011056043A JP2012193751A (en) 2011-03-15 2011-03-15 Method for mounting hollow member and fastening member, and mounting structure

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP2011056043A JP2012193751A (en) 2011-03-15 2011-03-15 Method for mounting hollow member and fastening member, and mounting structure

Publications (1)

Publication Number Publication Date
JP2012193751A true JP2012193751A (en) 2012-10-11

Family

ID=47085841

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2011056043A Withdrawn JP2012193751A (en) 2011-03-15 2011-03-15 Method for mounting hollow member and fastening member, and mounting structure

Country Status (1)

Country Link
JP (1) JP2012193751A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR20180017007A (en) * 2015-06-11 2018-02-20 부트벨딩 아게 Fixed to lightweight building elements

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR20180017007A (en) * 2015-06-11 2018-02-20 부트벨딩 아게 Fixed to lightweight building elements
KR102685535B1 (en) * 2015-06-11 2024-07-17 부트벨딩 에스아 Fastening to lightweight building elements

Similar Documents

Publication Publication Date Title
US9030835B2 (en) Method for welding a plastic housing
JP6876605B2 (en) How to interconnect objects
JP6578372B2 (en) Electronic control device and method of manufacturing electronic control device
JP2005315424A (en) Fastener
EP3205480B1 (en) Laser bonded structure, electronic control device, and method for producing laser bonded structure
BR112018006466B1 (en) METHOD FOR MECHANICALLY ATTACHING A FASTENER TO A FIRST OBJECT, FASTENER AND ASSEMBLY COMPRISING THAT FASTENER
JP2008128422A (en) Hole plug
BR112019019563A2 (en) joining objects
KR101893073B1 (en) Production method for bonded structure, and bonded structure
TWI704994B (en) Method for manufacturing joint structure and joint structure
US11117331B2 (en) Vehicular interior member
JP2016046243A (en) Lighting device, electronic equipment, frame structure and process of manufacture of frame structure
JP6341156B2 (en) Resin bonded body, resin bonded body manufacturing method, and vehicle structure
BR112017022155B1 (en) METHOD OF MECHANICALLY CONNECTING A CONNECTOR TO A FIRST OBJECT AND CONNECTOR DEVICE TO BE CONNECTED TO AN OPENING OF A FIRST OBJECT
WO2016125594A1 (en) Manufacturing method for joined structural body and joined structural body
JP2012193751A (en) Method for mounting hollow member and fastening member, and mounting structure
JP2016141078A (en) Weld structure
JP6941705B1 (en) Mounting part, in-vehicle device, mounting method
JP2014027835A (en) Protector and manufacturing method of the same
JP6198493B2 (en) Composite molded product
CN110446594A (en) Accessories for attaching to components
US20130219687A1 (en) Fastening method
KR101917768B1 (en) Heterojunction body
JP5280219B2 (en) Spoiler
JP5352431B2 (en) Hole seal structure

Legal Events

Date Code Title Description
A300 Withdrawal of application because of no request for examination

Free format text: JAPANESE INTERMEDIATE CODE: A300

Effective date: 20140603