JPH0436905Y2 - - Google Patents
Info
- Publication number
- JPH0436905Y2 JPH0436905Y2 JP1987014583U JP1458387U JPH0436905Y2 JP H0436905 Y2 JPH0436905 Y2 JP H0436905Y2 JP 1987014583 U JP1987014583 U JP 1987014583U JP 1458387 U JP1458387 U JP 1458387U JP H0436905 Y2 JPH0436905 Y2 JP H0436905Y2
- Authority
- JP
- Japan
- Prior art keywords
- reinforced composite
- composite material
- resin
- fiber
- joint
- 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
Links
- 239000000463 material Substances 0.000 claims description 25
- 239000003733 fiber-reinforced composite Substances 0.000 claims description 21
- 239000000853 adhesive Substances 0.000 claims description 10
- 230000001070 adhesive effect Effects 0.000 claims description 10
- 239000011347 resin Substances 0.000 claims description 7
- 229920005989 resin Polymers 0.000 claims description 7
- 239000000945 filler Substances 0.000 claims description 6
- 238000010030 laminating Methods 0.000 claims description 3
- HBMJWWWQQXIZIP-UHFFFAOYSA-N silicon carbide Chemical compound [Si+]#[C-] HBMJWWWQQXIZIP-UHFFFAOYSA-N 0.000 claims description 3
- 229910010271 silicon carbide Inorganic materials 0.000 claims description 3
- 239000002184 metal Substances 0.000 description 3
- 238000000465 moulding Methods 0.000 description 3
- 238000010586 diagram Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 239000000835 fiber Substances 0.000 description 1
- 239000012530 fluid Substances 0.000 description 1
- 239000000446 fuel Substances 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 230000002787 reinforcement Effects 0.000 description 1
- 230000003014 reinforcing effect Effects 0.000 description 1
- 238000009958 sewing Methods 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29D—PRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCES IN A PLASTIC STATE
- B29D99/00—Subject matter not provided for in other groups of this subclass
- B29D99/0003—Producing profiled members, e.g. beams
- B29D99/0005—Producing noodles, i.e. composite gap fillers, characterised by their construction
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Lining Or Joining Of Plastics Or The Like (AREA)
- Standing Axle, Rod, Or Tube Structures Coupled By Welding, Adhesion, Or Deposition (AREA)
- Laminated Bodies (AREA)
Description
【考案の詳細な説明】
(産業上の利用分野)
本考案は繊維強化複合材の一体成形構造におけ
る部材間の接合強度の向上を図るようにした継手
に関するものである。[Detailed Description of the Invention] (Industrial Application Field) The present invention relates to a joint designed to improve the bonding strength between members in an integrally molded structure of fiber-reinforced composite material.
(従来の技術)
従来の繊維強化複合材の一体成形接合部構造は
第7図から第10図に示す様に、繊維強化複合材
10のみで形状を工夫する(第7図)、糸11で
縫い合わせる(第8図)、矢尻状の金具12でつ
なぎ合わせる(第9図)、隅部に金属または硬化
した繊維強化複合材13を挿入して接着剤14で
接着(第10図)等であつた。(Prior art) As shown in FIGS. 7 to 10, the conventional integrally molded joint structure of a fiber-reinforced composite material is devised in shape using only the fiber-reinforced composite material 10 (FIG. 7), and a thread 11. They can be sewn together (Fig. 8), joined with arrowhead-shaped fittings 12 (Fig. 9), or inserted into the corners with metal or hardened fiber-reinforced composite material 13 and bonded with adhesive 14 (Fig. 10). Ta.
(考案が解決しようとする問題点)
繊維強化複合材10のみで形状を工夫したもの
(第7図)では、部材間の樹脂のみで負荷に耐え
るため、引き剥がし力が作用する箇所では部材間
の剥がれが生じやすい欠点があつた。また隅部に
金属または硬化した繊維強化複合材を挿入するも
の(第10図)では、樹脂のかわりに接着剤があ
るだけで前記と同じ欠点があつた。更に糸で縫い
合わせる方法(第8図)、矢尻状の金具でつなぎ
合わせる方法(第9図)は、特殊な装置が必要と
なるばかりか、実際の構造に適用することは難し
い等の欠点があつた。(Problem to be solved by the invention) In the case where the shape is devised using only the fiber reinforced composite material 10 (Fig. 7), the load is withstood only by the resin between the members, so the parts where the peeling force is applied are The problem was that it easily peeled off. Further, in the case of inserting a metal or a hardened fiber-reinforced composite material into the corner (FIG. 10), only an adhesive was used instead of the resin, but the same drawbacks as those described above existed. Furthermore, the methods of sewing with thread (Figure 8) and connecting with arrowhead-shaped metal fittings (Figure 9) not only require special equipment, but also have drawbacks such as being difficult to apply to actual structures. Ta.
本考案は前記従来の問題点を解決しようとする
もので、樹脂の部分に炭化珪素等のウイスカを追
加し、ウイスカにより部材間の接合強度を高め、
より軽量で実際の構造に適用しやすい一体成形接
合部構造の継手を提供しようとするものである。 The present invention attempts to solve the above-mentioned conventional problems, by adding whiskers such as silicon carbide to the resin part, and increasing the bonding strength between the parts by the whiskers.
The present invention aims to provide a joint with an integrally molded joint structure that is lighter and easier to apply to actual structures.
(問題点を解決するための手段)
このため本考案は、繊維強化複合材よりなる部
材を積層して作られる継手の境界部に繊維強化複
合材による充填材を配すると共に、同充填材の周
囲又は内部に、炭化珪素等のウイスカを散布した
格子状又は網目状の基材を持つ接着剤、或は樹脂
を含浸させた繊維強化複合材を挿入し、前記部材
及び充填材と同時に成形硬化するようにしてなる
もので、これを問題点解決のための手段とするも
のである。(Means for solving the problem) Therefore, the present invention provides a filler made of fiber reinforced composite material at the boundary of a joint made by laminating members made of fiber reinforced composite material, and An adhesive having a lattice-like or mesh-like base material sprinkled with whiskers such as silicon carbide, or a fiber-reinforced composite material impregnated with resin is inserted around or inside, and molded and hardened at the same time as the above-mentioned member and filler. This is done in such a way that it is used as a means to solve problems.
(作用)
繊維強化複合材を成形硬化する際に余分な樹脂
が除かれるが、この樹脂と共に接着液等とウイス
カを流動させ、部材接合部の繊維とからみ合い、
接合部の強度を向上させる。(Function) When molding and curing the fiber-reinforced composite material, excess resin is removed, but along with this resin, the adhesive fluid and whiskers flow and become entangled with the fibers at the joints of the parts.
Improve the strength of joints.
(実施例)
以下本考案を図面の実施例について説明する
と、第1図〜第6図は本考案の実施例を示す。先
ず第1図及び第2図の第1実施例について説明す
ると、この第1図〜第2図は、航空機の構造等で
一般的に現れる板状の部材1と桁状の部材2,3
から成る構造であり、燃料圧力又は空気圧力等の
引き剥がし力が作用する部分に一体成形構造を適
用する場合、充填材4と部材1、部材2、部材3
との間に第3図及び第4図の如くウイスカ7を散
布した接着剤又は樹脂含浸繊維強化複合材5を挿
入して同時に成形硬化する。(Embodiments) The present invention will be described below with reference to embodiments of the drawings. FIGS. 1 to 6 show embodiments of the present invention. First, the first embodiment shown in Figs. 1 and 2 will be explained. Figs.
When applying an integrally molded structure to a part where peeling force such as fuel pressure or air pressure acts, filler 4 and member 1, member 2, member 3
An adhesive or resin-impregnated fiber-reinforced composite material 5 with whiskers 7 sprinkled thereon is inserted between the two and molded and cured at the same time, as shown in FIGS. 3 and 4.
次に第2実施例を第5図により説明すると、こ
の実施例では第1図の板部材1の部分の巾を短く
してI型ビームとし、ボトル組立の構造要素とし
て使う場合も、第1実施例と同様の箇所にウイス
カを散布した接着剤又は樹脂含浸繊維強化複合材
5を挿入して同時成形硬化し、補強してなるもの
である。 Next, the second embodiment will be explained with reference to FIG. 5. In this embodiment, the width of the plate member 1 in FIG. 1 is shortened to form an I-shaped beam. An adhesive or resin-impregnated fiber-reinforced composite material 5 with whiskers sprinkled thereon is inserted into the same location as in the example, and is simultaneously molded and cured for reinforcement.
次に第3実施例を第6図により説明すると、こ
の実施例では3個以上の腕8を持つ継手を繊維強
化複合材の積層により作る場合、充填材部分6の
繊維強化複合材の間に、ウイスカを散布した接着
剤又は樹脂含浸繊維強化複合材5を挿入し、同時
に成形硬化する。 Next, the third embodiment will be explained with reference to FIG. 6. In this embodiment, when a joint having three or more arms 8 is made by laminating fiber reinforced composite materials, there is Then, the adhesive or resin-impregnated fiber-reinforced composite material 5 sprinkled with whiskers is inserted, and molded and cured at the same time.
(考案の効果)
以上詳細に説明した如く本考案は、ウイスカを
散布した接着剤又は樹脂含浸繊維強化複合材を、
一体成形接合部又は充填材内部に挿入しておき、
同時に成形硬化することにより、ウイスカによる
補強効果が得られるため、実際構造に適用が容易
である。(Effects of the invention) As explained in detail above, the present invention provides an adhesive or resin-impregnated fiber reinforced composite material sprinkled with whiskers.
Insert it into the integrally molded joint or inside the filler,
By molding and curing at the same time, a reinforcing effect by whiskers can be obtained, making it easy to apply to actual structures.
第1図は本考案の実施例を示す継手の、第1実
施例における組付け前の各部材の配置を示す側面
図、第2図は同継手の成形硬化後の側面図、第3
図はウイスカを散布した接着剤又は樹脂含浸繊維
強化複合材の側面図、第4図は同正面図、第5図
及び第6図は夫々本考案の第2,第3実施例を示
す継手の側面図、第7図、第8図、第9図及び第
10図は夫々従来の繊維強化複合材を用いた継手
の側面図である。
図の主要部分の説明、1,2,3……部材、4
……充填材、5……樹脂含浸繊維強化複合材。
Fig. 1 is a side view of a joint showing an embodiment of the present invention, showing the arrangement of each member in the first embodiment before assembly; Fig. 2 is a side view of the joint after molding and hardening;
The figure is a side view of an adhesive or resin-impregnated fiber reinforced composite material with whiskers sprinkled on it, FIG. 4 is a front view of the same, and FIGS. 5 and 6 are joints showing the second and third embodiments of the present invention, respectively. The side view, FIG. 7, FIG. 8, FIG. 9, and FIG. 10 are side views of a joint using a conventional fiber-reinforced composite material, respectively. Explanation of the main parts of the diagram, 1, 2, 3... members, 4
...Filler, 5...Resin-impregnated fiber reinforced composite material.
Claims (1)
る継手の境界部に繊維強化複合材による充填材を
配すると共に、同充填材の周囲又は内部に、炭化
珪素等のウイスカを散布した格子状又は網目状の
基材を持つ接着剤、或は樹脂を含浸させた繊維強
化複合材を挿入し、前記部材及び充填材と同時に
成形硬化することを特徴とする継手。 A filling material made of fiber reinforced composite material is arranged at the boundary of a joint made by laminating members made of fiber reinforced composite material, and whiskers such as silicon carbide are scattered around or inside the filling material in a lattice shape or A joint characterized in that an adhesive having a mesh-like base material or a fiber reinforced composite material impregnated with a resin is inserted and molded and hardened simultaneously with the member and filler.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP1987014583U JPH0436905Y2 (en) | 1987-02-03 | 1987-02-03 |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP1987014583U JPH0436905Y2 (en) | 1987-02-03 | 1987-02-03 |
Publications (2)
Publication Number | Publication Date |
---|---|
JPS63124119U JPS63124119U (en) | 1988-08-12 |
JPH0436905Y2 true JPH0436905Y2 (en) | 1992-08-31 |
Family
ID=30804705
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP1987014583U Expired JPH0436905Y2 (en) | 1987-02-03 | 1987-02-03 |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPH0436905Y2 (en) |
Families Citing this family (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US8540833B2 (en) * | 2008-05-16 | 2013-09-24 | The Boeing Company | Reinforced stiffeners and method for making the same |
US9359060B2 (en) * | 2013-11-07 | 2016-06-07 | The Boeing Company | Laminated composite radius filler with geometric shaped filler element and method of forming the same |
US9440414B2 (en) * | 2014-07-25 | 2016-09-13 | The Boeing Company | Fabric jacketed unidirectional noodle |
JP6502719B2 (en) * | 2015-03-26 | 2019-04-17 | 株式会社Subaru | Aircraft structure, method of manufacturing aircraft structure, and method of creating design information of aircraft structure |
-
1987
- 1987-02-03 JP JP1987014583U patent/JPH0436905Y2/ja not_active Expired
Also Published As
Publication number | Publication date |
---|---|
JPS63124119U (en) | 1988-08-12 |
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