JP3442660B2 - Joining panel structure and panel - Google Patents

Joining panel structure and panel

Info

Publication number
JP3442660B2
JP3442660B2 JP22417398A JP22417398A JP3442660B2 JP 3442660 B2 JP3442660 B2 JP 3442660B2 JP 22417398 A JP22417398 A JP 22417398A JP 22417398 A JP22417398 A JP 22417398A JP 3442660 B2 JP3442660 B2 JP 3442660B2
Authority
JP
Japan
Prior art keywords
thickness
plate
joining
panel
panel structure
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.)
Expired - Fee Related
Application number
JP22417398A
Other languages
Japanese (ja)
Other versions
JP2000052457A (en
Inventor
正樹 熊谷
直 田中
泰永 伊藤
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.)
Sumitomo Light Metal Industries Ltd
Original Assignee
Sumitomo Light Metal Industries Ltd
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 Sumitomo Light Metal Industries Ltd filed Critical Sumitomo Light Metal Industries Ltd
Priority to JP22417398A priority Critical patent/JP3442660B2/en
Publication of JP2000052457A publication Critical patent/JP2000052457A/en
Application granted granted Critical
Publication of JP3442660B2 publication Critical patent/JP3442660B2/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23KSOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K20/00Non-electric welding by applying impact or other pressure, with or without the application of heat, e.g. cladding or plating
    • B23K20/12Non-electric welding by applying impact or other pressure, with or without the application of heat, e.g. cladding or plating the heat being generated by friction; Friction welding
    • B23K20/122Non-electric welding by applying impact or other pressure, with or without the application of heat, e.g. cladding or plating the heat being generated by friction; Friction welding using a non-consumable tool, e.g. friction stir welding
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23KSOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K2101/00Articles made by soldering, welding or cutting
    • B23K2101/02Honeycomb structures
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23KSOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K2101/00Articles made by soldering, welding or cutting
    • B23K2101/04Tubular or hollow articles
    • B23K2101/045Hollow panels

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Standing Axle, Rod, Or Tube Structures Coupled By Welding, Adhesion, Or Deposition (AREA)
  • Furniture Connections (AREA)
  • Pressure Welding/Diffusion-Bonding (AREA)
  • Laminated Bodies (AREA)

Description

【発明の詳細な説明】Detailed Description of the Invention

【0001】[0001]

【発明の属する技術分野】本発明は、各種機材の軽量
化、特に輸送機材における大型の構造体にアルミニウム
及びその合金を使用する際に必要となる接合用パネル構
造体及びパネルに関する。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a lightweight panel structure for various types of equipment, and more particularly to a panel structure for bonding and a panel which are required when aluminum and its alloy are used for a large-scale structure in transportation equipment.

【0002】[0002]

【従来の技術】各種機材の軽量化、特に輸送機材の軽量
化は、燃料の使用量の削減を可能にし、直接環境保護に
つながるため積極的に進められており、各種機材へのア
ルミニウム及びその合金素材の使用が多くなっている。
アルミニウム及びその合金素材は、軽量であると共に最
適な断面形状、例えば、パネル構造体とすることにより
剛性を高くすることができ、平滑性にも優れているた
め、車両、船舶等の輸送機器用部材として適している。
2. Description of the Related Art The weight reduction of various equipment, especially the weight of transportation equipment, has been actively promoted because it enables reduction of fuel consumption and directly leads to environmental protection. The use of alloy materials is increasing.
Aluminum and its alloy materials are lightweight and have an optimum cross-sectional shape, for example, a panel structure that can increase rigidity and is excellent in smoothness, and is therefore suitable for transportation equipment such as vehicles and ships. Suitable as a member.

【0003】パネル構造体には、中空形材やハニカムパ
ネルがある。中空形材は、一定の間隔を有して互いに並
行する2枚の面板の間に複数の柱板を架設してなり、ア
ルミニウム合金の押出成形により作製されているため、
成形できる中空形材の幅が限定される。一方、ハニカム
パネルは、芯材のハニカムコアの周縁部に枠材を配置
し、ハニカムコアの上下面に面板を配設して、この状態
でろう付け炉に入れ、これらをろう付けし一体として作
製されるため、ろう付け炉の大きさにより製作できるハ
ニカムパネルの幅が限定される。
Panel structures include hollow profiles and honeycomb panels. The hollow shape member is formed by extruding an aluminum alloy because a plurality of pillar plates are installed between two face plates that are parallel to each other with a certain distance.
The width of the hollow profile that can be formed is limited. On the other hand, in a honeycomb panel, a frame material is arranged around the periphery of a honeycomb core of a core material, face plates are arranged on the upper and lower surfaces of the honeycomb core, and in this state, they are placed in a brazing furnace and brazed together to form an integral body. As it is manufactured, the size of the brazing furnace limits the width of the honeycomb panel that can be manufactured.

【0004】従って、中空形材やハニカムパネル同士の
接合は必須となり、その接合には強度面からアーク溶接
(TIG、MIG)が適用されているが、アーク溶接に
おいては、溶接時の熱歪みによりアルミニウム合金材料
が変形するという問題点がある。外観を重視する部位で
は、アーク溶接時に形成される余盛りの削除が必要とな
り、更に、溶接時の多大な入熱による溶接部周辺の熱影
響によって強度が低下し、その分パネル構造体を厚肉に
設計しなければならず、折角の軽量効果を減少させてい
る。
Therefore, it is essential to join the hollow shape members and the honeycomb panels together, and arc welding (TIG, MIG) is applied to the joining from the viewpoint of strength. However, in arc welding, due to thermal strain during welding, There is a problem that the aluminum alloy material is deformed. For parts where the appearance is important, it is necessary to remove the surplus that is formed during arc welding, and further, the strength decreases due to the heat effect around the weld due to the large heat input during welding, and the panel structure is thickened accordingly. It must be designed to be meat, which reduces the light weight effect of the corner.

【0005】車両用構造体には、6000系(Al−M
g−Si系)のアルミニウム合金の押出形材が最も多く
使用されているが、通常の6000系アルミニウム合金
では、アーク溶接時に入る熱により溶接熱影響部(HA
Z)が軟化し、本来のアルミニウム合金押出形材の強度
を大きく損ねる。また、アーク溶接特有のブローホール
の発生や凝固割れ等の欠陥が生じることもあり、その手
直しに溶接部をはつり、再溶接を行うため、多大の工数
を要すると共に溶接部の外観も悪くなるという難点もあ
る。
The vehicle structure includes a 6000 series (Al-M
The extruded profile of (g-Si-based) aluminum alloy is most often used. However, in the case of a normal 6000-based aluminum alloy, the heat input during arc welding causes the welding heat-affected zone (HA).
Z) is softened, and the original strength of the extruded aluminum alloy profile is greatly impaired. In addition, there are cases where defects such as blowholes and solidification cracking, which are peculiar to arc welding, may occur, and because the welded part is repaired and re-welded, a lot of man-hours are required and the appearance of the welded part deteriorates. There are difficulties.

【0006】入熱が少なく、軟化や歪みの程度も少ない
接合方式として、アルミニウム及びその合金製の形材の
突き合わせ摩擦接合方法(特開平9−309164号公
報他)がある。この方法によれば、中空形材同士やハニ
カムパネル同士の接合を摩擦接合することで、その接合
部及びその周辺の変形が抑えられ、良好な接合が短時間
で得ることが可能となる。
As a joining method with less heat input and less degree of softening and distortion, there is a butt friction joining method of aluminum and its alloy shape members (Japanese Patent Laid-Open No. 9-309164, etc.). According to this method, the hollow joints and the honeycomb panels are friction-joined to each other, whereby deformation of the joints and the periphery thereof is suppressed, and good joining can be obtained in a short time.

【0007】[0007]

【発明が解決しようとする課題】摩擦接合を適用してア
ルミニウム及びその合金製のパネル構造体同士を接合し
た場合、従来のアーク溶接によって引き起こされる種々
の不都合な点を解消することが可能となるが、アルミニ
ウム及びその合金製のパネル構造体、すなわち、中空形
材やハニカムパネルは、いずれもその軽量化のために面
板や柱板あるいは枠材をできるだけ薄い素材にて作製す
るため、次のような問題点が生じる。
When the friction welding is applied to join the panel structures made of aluminum and its alloy to each other, various disadvantages caused by the conventional arc welding can be eliminated. However, the panel structure made of aluminum and its alloy, that is, the hollow shape and the honeycomb panel, are made as thin as possible of the face plate, the pillar plate or the frame material in order to reduce the weight. Problems arise.

【0008】すなわち、中空形材a同士を摩擦接合する
場合には、図11に示すように、柱板bを隙間のない状
態にして突き合わせ、出来た接合線cに沿って摩擦接合
工具dを移動させるが、摩擦接合中、摩擦接合工具dの
ピンe直下の中空形材aの金属が表面に排出される反作
用のため、接合部fに下向きの力が作用することとな
り、従って、第1次的に柱板bの強度不足による変形や
座屈等が生じ、図12に示すように、第2次的に柱板b
の膨らみgや接合部の金属不足による塑性流動域内の欠
陥、例えば、トンネル状の穴h、亀裂等が生じ易くな
る。
That is, when the hollow shape members a are friction-welded to each other, as shown in FIG. 11, the pillar plates b are abutted with each other without any gap, and the friction welding tool d is attached along the welding line c. Although it is moved, during friction welding, a downward force acts on the joint f due to the reaction that the metal of the hollow shape member a immediately below the pin e of the friction welding tool d is discharged to the surface, and therefore the first portion acts. Next, the pillar plate b is deformed or buckled due to insufficient strength, and as shown in FIG.
Defects in the plastic flow region, such as tunnel-shaped holes h and cracks, are likely to occur due to the bulge g of the metal and the lack of metal in the joint.

【0009】一方、ハニカムパネルの場合においても、
上記中空形材aと同じように、枠材について、第1次的
には枠材の強度不足による変形や座屈等が生じ、第2次
的には枠材の膨らみや接合部の金属不足によるトンネル
状の穴、亀裂等が生ずる。
On the other hand, even in the case of a honeycomb panel,
Similar to the hollow profile a, the frame material is primarily deformed or buckled due to insufficient strength of the frame material, and secondly swelling of the frame material or lack of metal in the joint portion. Due to this, tunnel-shaped holes, cracks, etc. occur.

【0010】本発明は、パネル構造体における上記従来
の問題点を解消するためになされたものであり、その目
的は、軽量というパネル構造体の特性を損なうこと無
く、これら同士の摩擦接合の際に発生する変形や座屈、
膨らみや接合部の欠陥を押さえることの出来る接合用パ
ネル構造体及びパネルを提供することにある。
The present invention has been made in order to solve the above-mentioned conventional problems in the panel structure, and an object thereof is to perform friction bonding between the panel structures without impairing the characteristic of the panel structure that is lightweight. Deformation or buckling that occurs in
An object of the present invention is to provide a joining panel structure and a panel capable of suppressing bulges and defects at joints.

【0011】[0011]

【課題を解決するための手段】本発明は、上記の目的を
達成するために提案されたものであって、下記の構成か
らなることを特徴とするものである。すなわち、請求項
1の発明に係る接合用パネル構造体は、一定の間隔を有
して互いに並行する2枚の面板の間に複数の柱板を架設
してパネル構造体を構成し、該パネル構造体の端部に位
置する前記柱板の両端と2枚の面板との隅角部に厚肉部
を有することを特徴とする。この構成によれば、パネル
構造体の隅角部に設けた厚肉部により、摩擦接合の際の
圧力を吸収し、かつ隅角部が膨らまないから接合部の金
属不足がなく、塑性流動域内の欠陥を生じることがな
い。
The present invention has been proposed to achieve the above object, and is characterized by having the following constitution. That is, in the panel structure for joining according to the invention of claim 1, a plurality of pillar plates are installed between two face plates that are parallel to each other with a constant interval to form a panel structure, and the panel structure is constructed. It is characterized by having thick-walled portions at the corners between the two end plates of the pillar plate located at the end of the structure and the two face plates. According to this configuration, the thick portion provided in the corner portion of the panel structure absorbs the pressure at the time of friction welding, and since the corner portion does not swell, there is no metal shortage in the joint portion, Does not cause defects.

【0012】請求項2の発明は、ハニカムコアの周縁部
に枠材を配置し、該ハニカムコアの上下面に面板を配設
してパネル構造体を構成し、該パネル構造体の前記枠材
の前記面板に対しての平行板と垂直板との隅角部に厚肉
部を有することを特徴とする接合用パネル構造体を提供
するものである。従って、このハニカムコアを有するパ
ネル構造体の隅角部に設けた厚肉部によって、摩擦接合
の際の圧力を吸収し、かつ隅角部が膨らまないから接合
部の金属不足がなく、塑性流動域内の欠陥が生じない。
According to a second aspect of the present invention, a frame material is arranged on the peripheral edge of the honeycomb core, and face plates are provided on the upper and lower surfaces of the honeycomb core to form a panel structure, and the frame material of the panel structure is formed. And a thick plate portion at a corner between a parallel plate and a vertical plate with respect to the face plate. Therefore, the thick portion provided in the corner portion of the panel structure having this honeycomb core absorbs the pressure during friction welding, and the corner portion does not swell, so there is no metal shortage in the joint portion and plastic flow There are no defects in the area.

【0013】また、請求項1〜2の発明においては、面
板の厚さ(t)と柱板または枠材の垂直板の厚さ(γ)
との関係がt/2≦γ<tで、柱板の厚さを0.5mm
以上、面板の厚さを1mm以上としたので、柱板または
枠材の垂直板の厚さが小さく、軽量で且つ摩擦接合の際
に発生する変形や座屈のない接合用パネル構造体が得ら
れる。
Further, in the inventions of claims 1 and 2, the thickness of the face plate (t) and the thickness of the vertical plate of the pillar plate or the frame member (γ).
Is t / 2 ≦ γ <t, and the thickness of the pillar plate is 0.5 mm
As described above, since the thickness of the face plate is set to 1 mm or more, the thickness of the vertical plate of the column plate or the frame member is small, and a joining panel structure which is lightweight and has no deformation or buckling that occurs during friction joining is obtained. To be

【0014】請求項3の発明によれば、厚肉部は摩擦接
合により塑性流動した領域の幅に対して少なくとも2倍
以上であり、且つ摩擦接合により塑性流動した領域が前
記面板の厚みの1〜3倍の範囲にあるから、隅角部が膨
らまず且つ接合部から塑性流動領域にある金属が他に流
出せず、塑性流動域内の欠陥が生じることなく、接合部
強度が充分となり、不必要な入熱と変形がない。
According to the third aspect of the present invention, the thick portion is at least twice the width of the region plastically flowed by friction welding, and the region plastically flowed by friction welding is 1 times the thickness of the face plate. Since it is in the range of up to 3 times, the corners do not swell and the metal in the plastic flow region does not flow out from the joint to the other parts, the defect in the plastic flow region does not occur, the joint strength becomes sufficient, and No required heat input and deformation.

【0015】請求項4の発明は、パネル構造体の端部に
位置する前記柱板の厚さは、面板の厚さの0.5〜3倍
の範囲にあることを特徴とするものであり、摩擦接合時
に座屈しないし、重量もそれほど増加しない。
The invention of claim 4 is characterized in that the thickness of the pillar plate located at the end of the panel structure is in the range of 0.5 to 3 times the thickness of the face plate. , It does not buckle during friction welding and the weight does not increase so much.

【0016】請求項5の発明は、請求項1〜4のいずれ
かに記載の接合用パネル構造体同士を摩擦接合して得ら
れるパネルであり、軽量で接合用パネル構造体同士の摩
擦接合の際に発生する変形や座屈、膨らみや接合部の欠
陥のない大型のパネルを得ることができる。
A fifth aspect of the present invention is a panel obtained by friction-joining the joining panel structures according to any one of the first to fourth aspects, and is lightweight and friction-joined between the joining panel structures. It is possible to obtain a large-sized panel free from deformation, buckling, bulge, and joint defects that occur at the time.

【0017】[0017]

【発明の実施の形態】以下、実施の形態を挙げ、本発明
を図1〜10に基づいて詳述する。図1は本発明の実施
形態を示す接合用パネル構造体の断面図である。図1に
おいて、接合用パネル構造体1は中空形材であり、一定
の間隔を有して互いに並行する2枚の面板2、2の間に
複数の柱板3を架設してパネル構造体4を構成し、該パ
ネル構造体4の端部に位置する柱板3の両端と2枚の面
板2との隅角部5に厚肉部6を形成する。
BEST MODE FOR CARRYING OUT THE INVENTION Hereinafter, the present invention will be described in detail with reference to FIGS. FIG. 1 is a cross-sectional view of a joining panel structure showing an embodiment of the present invention. In FIG. 1, a joining panel structure 1 is a hollow shape member, and a plurality of pillar plates 3 are installed between two face plates 2 and 2 which are parallel to each other with a constant interval, and a panel structure 4 is formed. And a thick wall portion 6 is formed at a corner portion 5 between both ends of the pillar plate 3 located at the end portion of the panel structure 4 and the two face plates 2.

【0018】この接合用パネル構造体1が、アルミニウ
ム(アルミニウム合金を含む、以下同じ)の場合、押出
成形によって一体に作製される。従って、接合用パネル
構造体1は、押し出し方向には理論的にどんな長さのも
のであっても作製可能であるが、幅方向の寸法は、押出
成形機により規制され、余り幅広のものを作製すること
はコスト面から不利となる。
When the joining panel structure 1 is made of aluminum (including aluminum alloy, the same applies hereinafter), it is integrally formed by extrusion molding. Therefore, although the bonding panel structure 1 can be manufactured with theoretically any length in the extrusion direction, the widthwise dimension is regulated by the extruder, and the width is too wide. Manufacturing is disadvantageous in terms of cost.

【0019】そこで、上記接合用パネル構造体1を、そ
の端部に位置する面板2、2及び柱板3を突き合わせ接
合することにより、大型のパネルを作製する。従来、強
度面からアーク溶接が行われていたが、溶接時の多大な
入熱による弊害から摩擦接合が採用するのが好ましい。
一方、接合用パネル構造体1は最大限の軽量化を図るた
め面板2、2及び柱板3は必要最小限の厚みとなってい
る。
Therefore, a large-sized panel is manufactured by butt-joining the above-mentioned joining panel structure 1 with the face plates 2 and 2 and the column plate 3 located at the ends thereof. Conventionally, arc welding has been performed from the viewpoint of strength, but it is preferable to employ friction welding because of the harmful effects of a large amount of heat input during welding.
On the other hand, in the joining panel structure 1, the face plates 2 and 2 and the pillar plate 3 have the necessary minimum thickness in order to maximize the weight reduction.

【0020】このような状況下の接合用パネル構造体1
同士を摩擦接合するには、その接合面10同士を突き合
わせ、治具(不図示)により加圧拘束する。その接合線
に沿い摩擦接合工具11の硬質なピン12を高速回転さ
せ接合面10の一端に刺し込み、その接合線に沿い他端
まで移動させ摩擦接合を行う。その後、接合用パネル構
造体1を裏返し、同じように摩擦接合すると、接合部1
3により接合用パネル構造体1同士を摩擦接合すること
ができ、大型のパネルが得られる。
The joining panel structure 1 under such a condition
In order to frictionally bond the members to each other, the bonding surfaces 10 are butted against each other and pressed and restrained by a jig (not shown). The hard pin 12 of the friction welding tool 11 is rotated at a high speed along the joining line to pierce one end of the joining surface 10 and moved to the other end along the joining line to perform friction joining. Then, the joining panel structure 1 is turned upside down and frictionally joined in the same manner.
The joining panel structures 1 can be frictionally joined to each other by 3, and a large panel can be obtained.

【0021】前記厚肉部6の幅(β+β=2β)は、図
2に示すように、摩擦接合により塑性流動した領域の
幅、すなわち、接合部13の幅(α+α=2α)に対し
て少なくとも2倍以上である(2×2α≦2β─→2α
≦β)。この2倍以上の厚肉部6により、摩擦接合の
際、膨らみや金属不足による空洞が生じないから、面板
2、2及び柱板3を必要最小限の厚みとすることが可能
となっている。但し、この倍率が高すぎる場合は、必要
以上の厚肉部6を有することになり、軽量化の面で不利
となる。2倍に満たない場合は、摩擦接合の際の膨らみ
や金属不足による空洞が生じる恐れがあり、本発明の目
的を達成することが難しくなる。
As shown in FIG. 2, the width of the thick portion 6 (β + β = 2β) is at least the width of the region in which plastic flow is caused by friction welding, that is, the width of the joining portion 13 (α + α = 2α). 2 times or more (2 × 2α ≦ 2β− → 2α
≤ β). The double or more thick portion 6 does not cause cavities due to swelling or lack of metal during friction bonding, so that the face plates 2 and 2 and the column plate 3 can be made to have a necessary minimum thickness. . However, if this magnification is too high, the thick portion 6 is provided more than necessary, which is disadvantageous in terms of weight reduction. If the amount is less than twice, bulging may occur during friction welding or voids may be formed due to lack of metal, making it difficult to achieve the object of the present invention.

【0022】前記接合部13は面板2の厚みに関係す
る。すなわち、図3に示すように、摩擦接合により塑性
流動した領域(α1 )が面板2の厚み(t)の1〜3倍
の範囲にあるのが好ましく(t≦α1 ≦3t)、領域
(α1 )がこの範囲にあると、接合部13の継ぎ手強度
が充分となり、且つ摩擦接合も行い易くなる。この範囲
未満では接合長さが不足し継ぎ手強度が不充分となり、
この範囲を越えると、入熱と変形とを生じ摩擦接合が上
手くいかない結果になる。
The joint portion 13 is related to the thickness of the face plate 2. That is, as shown in FIG. 3, it is preferable that the region (α 1 ) in which plastic flow is caused by friction welding is in the range of 1 to 3 times the thickness (t) of the face plate 2 (t ≦ α 1 ≦ 3t). When (α 1 ) is in this range, the joint strength of the joint portion 13 becomes sufficient, and friction joining becomes easy. If it is less than this range, the joint length will be insufficient and the joint strength will be insufficient,
Exceeding this range causes heat input and deformation, resulting in poor friction welding.

【0023】柱板3の厚みは摩擦接合の作業性に関係す
る。すなわち、図4に示すように、柱板3の厚さ(γ)
は、面板2の厚さ(t)の0.5〜3倍の範囲にあるの
が好ましい(0.5t≦γ≦3t)。柱板3の厚さ
(γ)がこの範囲にあると、摩擦接合時に座屈せず、重
量もそれほど増加しない。この範囲未満では、摩擦接合
時に生じる柱板3に対する下向きの力により座屈する恐
れがあり、この範囲を越えると、いたずらに重量を増す
だけで軽量化の実が上がらない結果になる。面板2の厚
さ(t)と柱板3の厚さ(γ)との関係を図13に示
す。
The thickness of the column plate 3 is related to the workability of friction welding. That is, as shown in FIG. 4, the thickness (γ) of the pillar plate 3
Is preferably in the range of 0.5 to 3 times the thickness (t) of the face plate 2 (0.5t ≦ γ ≦ 3t). When the thickness (γ) of the column plate 3 is within this range, buckling does not occur during friction welding and the weight does not increase so much. Below this range, there is a risk of buckling due to the downward force on the column plate 3 that occurs during friction welding, and above this range, the weight is unnecessarily increased, and the result of weight reduction cannot be achieved. FIG. 13 shows the relationship between the thickness (t) of the face plate 2 and the thickness (γ) of the column plate 3.

【0024】図13に示すように、例えば、本発明の厚
肉部6がある場合には、面板2の厚さが1.5mmの場
合、柱板3の厚さは1.5/2=0.75mmでも摩擦
接合を実施することができる。しかし、厚肉部6がない
と実施できない。また、本発明の面板2の厚さが3mm
の場合には、柱板3の厚さは3/2=1.5mmでも摩
擦接合を実施できる。しかし、厚肉部6がないと、面板
2の厚さが3mmの場合、柱板3の厚さは6/2=3m
mないと実施できない。
As shown in FIG. 13, for example, when there is the thick portion 6 of the present invention, when the thickness of the face plate 2 is 1.5 mm, the thickness of the pillar plate 3 is 1.5 / 2 = Friction welding can be performed even at 0.75 mm. However, it cannot be implemented without the thick portion 6. The thickness of the face plate 2 of the present invention is 3 mm.
In this case, the friction welding can be performed even if the thickness of the pillar plate 3 is 3/2 = 1.5 mm. However, if the thickness of the face plate 2 is 3 mm without the thick portion 6, the thickness of the pillar plate 3 is 6/2 = 3 m.
It cannot be implemented unless m.

【0025】図5は、本発明の他の実施形態である接合
用パネル構造体1aを示す。図1〜4に示す実施形態と
の相違点は、厚肉部6aの形状がアーチ型になっている
点であり、その他の構成、作用については同様であるた
め、図面に符号を付して説明を省略する。
FIG. 5 shows a joining panel structure 1a according to another embodiment of the present invention. The difference from the embodiment shown in FIGS. 1 to 4 is that the shape of the thick-walled portion 6a is arched, and other configurations and operations are the same, and therefore reference numerals are given to the drawings. The description is omitted.

【0026】図6は、本発明の他の実施形態である接合
用パネル構造体1bを示す。図1〜4に示す実施形態と
の相違点は、厚肉部6bの形状が鈍角の膨らみとなっ
て、接合部13の形状(舌片状)に沿う形となっている
点であり、その他の構成、作用については同様であるた
め、図面に符号を付して説明を省略する。
FIG. 6 shows a joining panel structure 1b which is another embodiment of the present invention. The difference from the embodiment shown in FIGS. 1 to 4 is that the shape of the thick portion 6b is an obtuse bulge and follows the shape (tongue shape) of the joint portion 13, and the others. Since the configuration and operation of are the same, the reference numerals are given to the drawings and the description thereof will be omitted.

【0027】図7は、本発明の他の実施形態である接合
用パネル構造体1cを示す。図1〜4に示す実施形態と
の相違点は、厚肉部6cの形状が直角の膨らみとなっ
て、接合部13の形状(舌片状)に沿う形となっている
点である。その他の構成、作用については、図1〜4に
示す実施形態と同様であるため、図面に符号を付して説
明を省略する。
FIG. 7 shows a joining panel structure 1c which is another embodiment of the present invention. The difference from the embodiment shown in FIGS. 1 to 4 is that the shape of the thick portion 6c is a bulge at a right angle, and the shape follows the shape (tongue shape) of the joint portion 13. Other configurations and operations are the same as those of the embodiment shown in FIGS. 1 to 4, and therefore, reference numerals are attached to the drawings and description thereof is omitted.

【0028】図8〜10は本発明の他の実施形態である
接合用パネル構造体、すなわちハニカムパネル1dを示
す。このハニカムパネル1dは、芯材としてのハニカム
コア20の周縁部に枠材21を配置し、ハニカムコア2
0の上下面に面板22、22を配設して、この状態でろ
う付けし一体としてなるものである。
8 to 10 show a joining panel structure, that is, a honeycomb panel 1d, which is another embodiment of the present invention. In this honeycomb panel 1d, a frame material 21 is arranged around the periphery of a honeycomb core 20 as a core material,
The face plates 22 and 22 are arranged on the upper and lower surfaces of No. 0 and brazed in this state to be integrated.

【0029】アルミニウムろう付けのハニカムパネル1
dの場合は、アルミニウムの箔又は薄板から形成される
ハニカムコア20の周縁部にアルミニウムの押出形材か
らなる枠材21を溶接により枠組みし、ハニカムコア2
0の上下面Pには、ハニカムコア20と枠材21に対し
て重なる状態にアルミニウムのブレージングシートから
なる面板22、22を載せ、治具でこれらを一体に固定
してろう付け炉の中に入れ、ハニカムコア20と面板2
2、22との間、枠材21と面板22、22との間をろ
う付け一体とする。なお、ハニカムコア20と枠材21
との間も、ハニカムコア20と面板22、22とから流
動するろうにより部分的にろう付けされる。
Honeycomb panel 1 brazed with aluminum
In the case of d, a frame material 21 made of an extruded aluminum material is framed by welding around the periphery of the honeycomb core 20 formed of an aluminum foil or a thin plate, and the honeycomb core 2
On the upper and lower surfaces P of 0, face plates 22 and 22 made of an aluminum brazing sheet are placed so as to overlap with the honeycomb core 20 and the frame member 21, and they are integrally fixed with a jig into a brazing furnace. Put, honeycomb core 20 and face plate 2
The frame member 21 and the face plates 22 and 22 are integrally brazed. The honeycomb core 20 and the frame member 21
Also, between the two are partially brazed by the brazing fluid flowing from the honeycomb core 20 and the face plates 22, 22.

【0030】このようなハニカムパネル1dの製造に
は、ろう付け炉が使用されるから、ハニカムパネルのサ
イズは、炉のサイズに制約され、大型のものを作製する
には接合作業が必要となる。接合に摩擦接合を採用し、
最大限の軽量化を図るために、面板22、22及び枠材
21を必要最小限の厚みとしている状況は、上記接合用
パネル構造体1、1a〜1cの場合と同様である。
Since a brazing furnace is used to manufacture such a honeycomb panel 1d, the size of the honeycomb panel is limited by the size of the furnace, and a joining operation is required to manufacture a large-sized one. . Adopting friction welding for joining,
The situation in which the face plates 22, 22 and the frame member 21 have the minimum necessary thickness in order to maximize the weight reduction is the same as in the case of the joining panel structures 1, 1a to 1c.

【0031】このため、ハニカムパネル1dは、その枠
材21の面板22、22に対しての平行板23と垂直板
24との隅角部25に厚肉部26を有している。ハニカ
ムパネル1dは、図10に示すように、その接合面27
同士を突き合わせ、治具(不図示)により加圧拘束す
る。その接合線に沿い摩擦接合工具11の硬質なピン1
2を高速回転させ接合面27の一端に刺し込み、その接
合線に沿い他端まで移動させ、摩擦接合を行う。その
後、ハニカムパネル1dを裏返し、同じように摩擦接合
することにより、接合部28によりハニカムパネル1d
同士が摩擦接合され大型のハニカムパネルを作製するこ
とができる。
For this reason, the honeycomb panel 1d has a thick wall portion 26 at a corner portion 25 between the parallel plate 23 and the vertical plate 24 with respect to the face plates 22, 22 of the frame member 21. As shown in FIG. 10, the honeycomb panel 1d has a bonding surface 27.
Butt against each other and pressurize and restrain with a jig (not shown). The hard pin 1 of the friction welding tool 11 along the welding line
2 is rotated at a high speed to be inserted into one end of the joining surface 27, moved along the joining line to the other end, and friction joining is performed. After that, the honeycomb panel 1d is turned over and friction bonded in the same manner, so that the honeycomb panel 1d is bonded by the bonding portion 28.
It is possible to fabricate a large-sized honeycomb panel by friction-bonding each other.

【0032】すなわち、ハニカムパネル1dに設けた厚
肉部26によって、摩擦接合の際の圧力を吸収し、かつ
隅角部25が膨らむことがないから、接合部28の金属
不足がなく、塑性流動域内の欠陥が生じることがない。
この他の構成、作用は、図1〜7に示す実施形態と同様
であるため、図面に符号を付して説明を省略する。
That is, since the thick portion 26 provided in the honeycomb panel 1d absorbs the pressure at the time of friction joining and the corner portion 25 does not swell, there is no metal shortage in the joining portion 28 and plastic flow No defects in the area will occur.
Since other configurations and operations are similar to those of the embodiment shown in FIGS. 1 to 7, the drawings are denoted by reference numerals and the description thereof will be omitted.

【0033】以下、本発明の効果を確認するための実施
例について説明する。 実施例1 図1に示す断面形状を持ち、材質(6N01−T5)、
面板の厚さ3mm、柱板の厚肉部の幅の和が15mm、
厚肉部の角度が45°の接合用パネル構造体を突き合わ
せ、鋼製定盤に固定した。その状態で、ピンが直径5.
0mm、長さが4.5mmで、円盤の直径が10mmの
摩擦接合工具を1000rpmで回転させ、300mm
/分の送り速度で接合線に沿って移動させて摩擦接合を
行った。次いで、裏返しにして反対側を同じように摩擦
接合した。その結果、接合部は、摩擦接合による誤差等
の欠陥が無く、表面にも欠陥が無く、透過X線検査でも
内部に欠陥が無いことが確認出来た。
Examples for confirming the effects of the present invention will be described below. Example 1 Having a cross-sectional shape shown in FIG. 1, a material (6N01-T5),
The thickness of the face plate is 3 mm, the sum of the widths of the thick-walled portions of the pillar plate is 15 mm,
Joining panel structures having an angle of the thick portion of 45 ° were butted and fixed to a steel surface plate. In that state, the pin has a diameter of 5.
A friction welding tool with a diameter of 0 mm and a length of 4.5 mm and a disk diameter of 10 mm is rotated at 1000 rpm to obtain 300 mm.
Friction welding was performed by moving along the joining line at a feed rate of / min. Then, it was turned inside out and the other side was similarly friction-bonded. As a result, it was confirmed that the joint had no defects such as errors due to friction welding, no defects on the surface, and no internal defects by transmission X-ray inspection.

【0034】実施例2 図10に示す断面形状を持ち、材質(6N01−T
5)、枠材の水平板の厚さが3mm、垂直板の厚肉部の
幅の和が15mm、厚肉部の角度が45°のハニカムパ
ネルを面削して平坦とし突き合わせ、鋼製定盤に固定し
た。その状態で実施例1と同じようにして、摩擦接合し
た。その結果、接合部は、摩擦接合による誤差等の欠陥
が無く、表面にも欠陥が無く、透過X線検査でも内部に
欠陥が無いことが確認出来た。
Example 2 It has a sectional shape shown in FIG. 10 and is made of a material (6N01-T).
5), the thickness of the horizontal plate of the frame material is 3 mm, the sum of the widths of the thick parts of the vertical plate is 15 mm, and the honeycomb panel with the angle of the thick part of 45 ° is face-polished to be flat, but the steel plate is fixed. I fixed it to the board. In that state, friction joining was performed in the same manner as in Example 1. As a result, it was confirmed that the joint had no defects such as errors due to friction welding, no defects on the surface, and no internal defects by transmission X-ray inspection.

【0035】比較例1 厚肉部が無いこと以外は、実施例1と全く同様の接合用
パネル構造体同士を同じ条件で、摩擦接合した。その結
果、接合部の裏側に金属が変形してはみ出し、接合部の
金属が不足してトンネル状の欠陥が発生した。
Comparative Example 1 The same joining panel structures as in Example 1 were frictionally joined under the same conditions except that there was no thick portion. As a result, the metal was deformed and squeezed out on the back side of the joint, and the metal at the joint was insufficient, resulting in a tunnel-like defect.

【0036】比較例2 厚肉部が無いこと以外は、実施例2と全く同様のハニカ
ムパネル同士を同じ条件で、摩擦接合した。その結果、
接合部の裏側に金属が変形してはみ出し、接合部の金属
が不足してトンネル状の欠陥が発生した。
Comparative Example 2 The same honeycomb panels as in Example 2 except that there was no thick portion were friction-bonded under the same conditions. as a result,
The metal was deformed and squeezed out on the back side of the joint, and the metal at the joint was insufficient to cause a tunnel-shaped defect.

【0037】[0037]

【発明の効果】以上詳述したように、請求項1の発明に
よれば、パネル構造体の隅角部に設けた厚肉部により、
摩擦接合の際の圧力が吸収され、且つ隅角部が膨らまな
いから接合部の金属不足を生じることがなく、塑性流動
域内の欠陥が生じない。従って、軽量というパネル構造
体の特性を損なうこと無く、これら同士の摩擦接合の際
に発生する変形や座屈、膨らみや接合部の欠陥を押さえ
ることができ、接合品質が良く、しかも良好な仕上がり
の摩擦接合を得ることができ、大型のパネルが少ない工
数で作製でき、低価格化が図れる。
As described above in detail, according to the invention of claim 1, the thick wall portion provided at the corner of the panel structure allows
Since the pressure at the time of friction welding is absorbed and the corners do not swell, metal shortage at the joint does not occur and defects in the plastic flow region do not occur. Therefore, it is possible to suppress deformation, buckling, bulge and defects in the joint portion that occur during frictional joining of these without sacrificing the characteristics of the panel structure that is lightweight, and the joining quality is good and a good finish is obtained. It is possible to obtain the friction bonding of the above, a large-sized panel can be manufactured with a small number of steps, and the cost can be reduced.

【0038】請求項2の発明によれば、このハニカムコ
アを有するパネル構造体の隅角部に設けた厚肉部によ
り、摩擦接合の際の圧力が吸収され、且つ隅角部が膨ら
まないから接合部の金属不足を生じることがなく、塑性
流動域内の欠陥が生じない。従って、上記の効果をハニ
カムパネルにも付与することができる。
According to the second aspect of the present invention, the thick portion provided at the corner portion of the panel structure having the honeycomb core absorbs the pressure at the time of friction bonding and the corner portion does not swell. There will be no metal shortage at the joint, and no defects will occur in the plastic flow region. Therefore, the above effect can be imparted to the honeycomb panel.

【0039】また、請求項1〜2の発明によれば、面板
の厚さ(t)と柱板または枠材の垂直板の厚さ(γ)と
の関係がt/2≦γ<tで、柱板の厚さを0.5mm以
上、面板の厚さを1mm以上としたので、柱板または枠
材の垂直板の厚さが小さく、軽量で且つ摩擦接合の際に
発生する変形や座屈のない接合用パネル構造体が得られ
る。
According to the first and second aspects of the invention, the relationship between the thickness (t) of the face plate and the thickness (γ) of the vertical plate of the column plate or the frame member is t / 2 ≦ γ <t. Since the thickness of the pillar plate is 0.5 mm or more and the thickness of the face plate is 1 mm or more, the thickness of the pillar plate or the vertical plate of the frame material is small, and the deformation and seat that occur during friction bonding are lightweight and seated. A flexible panel structure for joining can be obtained.

【0040】請求項3の発明によれば、厚肉部は摩擦接
合により塑性流動した領域の幅に対して少なくとも2倍
以上であり、且つ摩擦接合により塑性流動した領域が前
記面板の厚みの1〜3倍の範囲にあるから、隅角部が膨
らまず且つ接合部から塑性流動領域にある金属が他に流
出せず、塑性流動域内の欠陥が生じることなく、接合部
強度が充分となり、不必要な入熱と変形がない。従っ
て、接合部の継ぎ手強度が充分あり、且つ良好な摩擦接
合を行うことができる。
According to the invention of claim 3, the thick portion is at least twice the width of the region plastically flowed by friction welding, and the region plastically flowed by friction welding is 1 times the thickness of the face plate. Since it is in the range of up to 3 times, the corners do not swell and the metal in the plastic flow region does not flow out from the joint to the other parts, the defect in the plastic flow region does not occur, the joint strength becomes sufficient, and No required heat input and deformation. Therefore, the joint strength of the joint is sufficient, and good friction joining can be performed.

【0041】請求項4の発明によれば、パネル構造体の
端部に位置する前記柱板の厚さは、面板の厚さの0.5
〜3倍の範囲にあるから、摩擦接合時に座屈せず、重量
を減らすことが可能となる。
According to the invention of claim 4, the thickness of the pillar plate located at the end of the panel structure is 0.5 of the thickness of the face plate.
Since it is in the range of up to 3 times, buckling does not occur during friction welding and the weight can be reduced.

【0042】請求項5の発明によれば、軽量で接合用パ
ネル構造体同士の摩擦接合の際に発生する変形や座屈、
膨らみや接合部の欠陥のない大型のパネルを得ることが
でき、また、大型の軽量パネルの製作を少ない工数で達
成することができ、低価格化が図れる。
According to the fifth aspect of the present invention, deformation and buckling which are lightweight and occur during frictional joining of the joining panel structures,
It is possible to obtain a large-sized panel without bulges and defects in the joint portion, and to manufacture a large-sized lightweight panel with a small number of man-hours, so that the cost can be reduced.

【図面の簡単な説明】[Brief description of drawings]

【図1】本発明の実施形態を示す接合用パネル構造体の
断面図である。
FIG. 1 is a cross-sectional view of a joining panel structure showing an embodiment of the present invention.

【図2】接合用パネル構造体の要部の拡大断面図であ
る。
FIG. 2 is an enlarged cross-sectional view of a main part of a joining panel structure.

【図3】接合用パネル構造体の要部の拡大断面図であ
る。
FIG. 3 is an enlarged cross-sectional view of a main part of the joining panel structure.

【図4】接合用パネル構造体の要部の拡大断面図であ
る。
FIG. 4 is an enlarged cross-sectional view of a main part of the joining panel structure.

【図5】本発明の他の実施形態を示す接合用パネル構造
体の断面図である。
FIG. 5 is a cross-sectional view of a joining panel structure showing another embodiment of the present invention.

【図6】本発明の他の実施形態を示す接合用パネル構造
体の断面図である。
FIG. 6 is a cross-sectional view of a joining panel structure showing another embodiment of the present invention.

【図7】本発明の他の実施形態を示す接合用パネル構造
体の断面図である。
FIG. 7 is a cross-sectional view of a joining panel structure showing another embodiment of the present invention.

【図8】本発明の実施形態であるハニカムパネルの形状
を示す斜視図である。
FIG. 8 is a perspective view showing the shape of a honeycomb panel that is an embodiment of the present invention.

【図9】ハニカムパネルの製作状態を示す断面図であ
る。
FIG. 9 is a cross-sectional view showing a manufactured state of the honeycomb panel.

【図10】本発明の他の実施形態であるハニカムパネル
の摩擦接合状態を示す断面図である。
FIG. 10 is a cross-sectional view showing a friction-bonded state of a honeycomb panel which is another embodiment of the present invention.

【図11】従来例を示す斜視図である。FIG. 11 is a perspective view showing a conventional example.

【図12】従来例を示す断面図である。FIG. 12 is a cross-sectional view showing a conventional example.

【図13】面板の厚さと柱板の厚さとの関係を示すグラ
フである。
FIG. 13 is a graph showing the relationship between the thickness of the face plate and the thickness of the column plate.

【符号の説明】[Explanation of symbols]

1、1a、1b、1c、1d 接合用パネル構造体 2、22 面板 3、b 柱板 4 パネル構造体 5、25 隅角部 6、6a、6b、6c、26 厚肉部 10、27 接合面 11、d 摩擦接合工具 12、e ピン 13、28、f 接合部 20 ハニカムコア 21 枠材 23 平行板 24 垂直板 a 中空形材 c 接合線 g 膨らみ h 穴 1, 1a, 1b, 1c, 1d Panel structure for joining 2.22 face plate 3, b pillar plate 4 panel structure 5, 25 corners 6, 6a, 6b, 6c, 26 Thick part 10, 27 Bonding surface 11, d Friction welding tool 12, e-pin 13, 28, f joint 20 Honeycomb core 21 Frame material 23 parallel plates 24 vertical plate a Hollow frame c joining line g bulge h hole

───────────────────────────────────────────────────── フロントページの続き (56)参考文献 特開 平9−309164(JP,A) 特開 平10−128473(JP,A) 特開 平11−350646(JP,A) 特開 平11−254155(JP,A) 特開 平11−226755(JP,A) 特開2000−681(JP,A) (58)調査した分野(Int.Cl.7,DB名) B23K 20/12 B32B 3/12 E04C 2/36 ─────────────────────────────────────────────────── --- Continuation of the front page (56) Reference JP-A-9-309164 (JP, A) JP-A-10-128473 (JP, A) JP-A-11-350646 (JP, A) JP-A-11- 254155 (JP, A) JP 11-226755 (JP, A) JP 2000-681 (JP, A) (58) Fields investigated (Int.Cl. 7 , DB name) B23K 20/12 B32B 3 / 12 E04C 2/36

Claims (5)

(57)【特許請求の範囲】(57) [Claims] 【請求項1】 一定の間隔を有して互いに並行する2枚
の面板の間に複数の柱板を架設してパネル構造体を構成
し、該パネル構造体の端部に位置する前記柱板の両端と
2枚の面板との隅角部に厚肉部を有し、面板の厚さ
(t)と柱板の厚さ(γ)との関係がt/2≦γ<tで
あり、柱板の厚さが0.5mm以上、面板の厚さが1m
m以上であることを特徴とする接合用パネル構造体。
1. A column structure is constructed by installing a plurality of column plates between two face plates that are parallel to each other with a constant interval, and the column plate is located at an end of the panel structure. The thickness of the face plate has thick parts at the corners between both ends of the face plate and the two face plates.
If the relationship between (t) and the thickness (γ) of the column plate is t / 2 ≦ γ <t,
Yes, pillar plate thickness is 0.5 mm or more, face plate thickness is 1 m
A joining panel structure characterized by having a length of m or more .
【請求項2】 ハニカムコアの周縁部に枠材を配置し、
該ハニカムコアの上下面に面板を配設してパネル構造体
を構成し、該パネル構成体の前記枠材の前記面板に対し
ての平行板と垂直板との隅角部に厚肉部を有し、面板の
厚さ(t)と枠材の垂直板の厚さ(γ)との関係がt/
2≦γ<tであり、枠材の垂直板の厚さが0.5mm以
上、面板の厚さが1mm以上であることを特徴とする接
合用パネル構造体。
2. A frame member is arranged at the peripheral edge of the honeycomb core,
A face plate is arranged on the upper and lower surfaces of the honeycomb core to form a panel structure, and a thick wall portion is formed at a corner between a parallel plate and a vertical plate of the frame member of the panel construct with respect to the face plate. Have and face plate
The relationship between the thickness (t) and the thickness (γ) of the vertical plate of the frame material is t /
2 ≦ γ <t, and the thickness of the vertical plate of the frame material is 0.5 mm or less
A panel structure for bonding, characterized in that the thickness of the upper and the face plates is 1 mm or more .
【請求項3】 前記厚肉部は摩擦接合により塑性流動し
た領域の幅に対して少なくとも2倍以上であり、且つ摩
擦接合により塑性流動した領域が前記面板の厚みの1〜
3倍の範囲にあることを特徴とする請求項1または2記
載の接合用パネル構造体。
3. The thick portion is plastically fluidized by friction welding.
At least twice the width of the open area and
The region in which plastic flow is caused by friction bonding is 1 to 1 of the thickness of the face plate.
It is in the range of 3 times, The statement of claim 1 or 2 characterized by the above-mentioned.
Mounted panel structure for joining.
【請求項4】 前記パネル構造体の端部に位置する前記
柱板の厚さは、面板の厚さの0.5〜3倍の範囲にある
ことを特徴とする請求項1または3記載の接合用パネル
構造体。
4. The thickness of the pillar plate located at the end of the panel structure is in the range of 0.5 to 3 times the thickness of the face plate . Panel structure for joining.
【請求項5】 請求項1〜4のいずれかに記載の接合用
パネル構造体同士を摩擦接合して得られるパネル。
5. A panel obtained by frictionally joining the joining panel structures according to any one of claims 1 to 4 .
JP22417398A 1998-08-07 1998-08-07 Joining panel structure and panel Expired - Fee Related JP3442660B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP22417398A JP3442660B2 (en) 1998-08-07 1998-08-07 Joining panel structure and panel

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP22417398A JP3442660B2 (en) 1998-08-07 1998-08-07 Joining panel structure and panel

Publications (2)

Publication Number Publication Date
JP2000052457A JP2000052457A (en) 2000-02-22
JP3442660B2 true JP3442660B2 (en) 2003-09-02

Family

ID=16809681

Family Applications (1)

Application Number Title Priority Date Filing Date
JP22417398A Expired - Fee Related JP3442660B2 (en) 1998-08-07 1998-08-07 Joining panel structure and panel

Country Status (1)

Country Link
JP (1) JP3442660B2 (en)

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106001866B (en) * 2016-07-11 2019-04-02 上海航天设备制造总厂 A kind of large thick-wall box component welding deformation controlling method
CN112935595A (en) * 2021-02-01 2021-06-11 上海交通大学 Marine I-shaped sandwich plate laser welding tool and using method thereof
JP7473714B2 (en) 2022-08-24 2024-04-23 株式会社神戸製鋼所 Structural member and method for manufacturing the same

Also Published As

Publication number Publication date
JP2000052457A (en) 2000-02-22

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