JPH0511024B2 - - Google Patents
Info
- Publication number
- JPH0511024B2 JPH0511024B2 JP59189336A JP18933684A JPH0511024B2 JP H0511024 B2 JPH0511024 B2 JP H0511024B2 JP 59189336 A JP59189336 A JP 59189336A JP 18933684 A JP18933684 A JP 18933684A JP H0511024 B2 JPH0511024 B2 JP H0511024B2
- Authority
- JP
- Japan
- Prior art keywords
- plate end
- winding
- support jig
- recesses
- recess
- 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 - Lifetime
Links
- 238000004804 winding Methods 0.000 claims description 14
- 229920005989 resin Polymers 0.000 claims description 10
- 239000011347 resin Substances 0.000 claims description 10
- 239000000835 fiber Substances 0.000 claims description 9
- 238000000034 method Methods 0.000 claims description 9
- 238000004519 manufacturing process Methods 0.000 claims description 7
- 238000005452 bending Methods 0.000 claims description 4
- 238000005192 partition Methods 0.000 claims description 2
- 230000000694 effects Effects 0.000 description 3
- 239000003365 glass fiber Substances 0.000 description 3
- 230000002093 peripheral effect Effects 0.000 description 3
- 229920000049 Carbon (fiber) Polymers 0.000 description 2
- 239000004917 carbon fiber Substances 0.000 description 2
- 239000007788 liquid Substances 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- 239000011324 bead Substances 0.000 description 1
- 239000003054 catalyst Substances 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 239000003822 epoxy resin Substances 0.000 description 1
- LNEPOXFFQSENCJ-UHFFFAOYSA-N haloperidol Chemical compound C1CC(O)(C=2C=CC(Cl)=CC=2)CCN1CCCC(=O)C1=CC=C(F)C=C1 LNEPOXFFQSENCJ-UHFFFAOYSA-N 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 239000005011 phenolic resin Substances 0.000 description 1
- 229920000647 polyepoxide Polymers 0.000 description 1
- 238000011417 postcuring Methods 0.000 description 1
- 229920001187 thermosetting polymer Polymers 0.000 description 1
- 229920006337 unsaturated polyester resin Polymers 0.000 description 1
Landscapes
- Moulding By Coating Moulds (AREA)
Description
【発明の詳細な説明】
〔産業上の利用分野〕
本発明は繊維強化樹脂構造体の製造方法、特に
複雑な空間構造を有する構造体の製造方法に関す
る。DETAILED DESCRIPTION OF THE INVENTION [Field of Industrial Application] The present invention relates to a method for manufacturing a fiber-reinforced resin structure, and particularly to a method for manufacturing a structure having a complicated spatial structure.
繊維強化樹脂構造体とは、あらかじめ樹脂液を
含浸させた糸または紐(ロービング)等の長い糸
状繊維強化材を巻型または治具の周囲に所定の太
さに巻きつけて硬化した後、脱型して得られるも
ので、多彩なデザイン自由度で一次元ないし三次
元の構造体が得られるので、大型構造物としての
開発が進められている。
A fiber-reinforced resin structure is a long filamentous fiber-reinforced material such as thread or string (roving) impregnated with a resin liquid, which is wound around a winding form or jig to a predetermined thickness, cured, and then removed. Since it can be molded into one-dimensional or three-dimensional structures with a wide variety of design freedom, it is being developed as a large-scale structure.
このような構造体の製造方法の一例として、英
国特許公開第2103572A号明細書に記載された方
法がある。この方法においては構造物の外形を形
成する複数個のプレートエンド(仕切板)がその
中央に設けられた孔を挿通する1本のシヤフトに
よつて連結され、かつ、両端部が、マンドレルを
挟んで、該マンドレルによつて支えられたエンド
ビースに連結する構成となつているため、得られ
た空間構造体の形状が直線的になる。 An example of a method for manufacturing such a structure is the method described in British Patent Publication No. 2103572A. In this method, a plurality of plate ends (partition plates) forming the outer shape of the structure are connected by a shaft that passes through a hole provided in the center, and both ends are connected with a mandrel between them. Since the structure is connected to the end bead supported by the mandrel, the shape of the resulting spatial structure becomes linear.
本発明に課せられた問題点はプレートエンドを
自由に位置付けて複雑な形状の繊維強化樹脂構造
体を製造し得る方法を提供することにある。
The problem faced by the present invention is to provide a method in which a fiber-reinforced resin structure having a complex shape can be manufactured by freely positioning the plate ends.
このため本発明者等は所望の形状の軸線の屈折
点に相当する位置に支持治具を配置して相互に固
定した後、周縁部に3個以上の凹部を設けたプレ
ートエンドを上記支持治具の凹部に差込み、しか
る後プレートエンドの凹部に樹脂含浸した連続繊
維の糸または紐をまきつけ、硬化後脱型すること
により所望の形状の空間構造体を得ることにし
た。
For this reason, the present inventors arranged the support jigs at positions corresponding to the bending points of the axes of the desired shape and fixed them to each other, and then attached the plate end with three or more recesses on the peripheral edge to the support jigs. The space structure of the desired shape was obtained by inserting it into the recess of the tool, then winding a resin-impregnated continuous fiber thread or string around the recess of the plate end, and removing it from the mold after hardening.
本発明方法を実施するには1個の凹部を有する
支持治具を所望の形状の軸線上の屈折点に配置
し、該支持治具の凹部に中心孔のあるプレートエ
ンドを差し込み、中心孔にシヤフトを挿通してプ
レートエンド相互を固定してもよいが、実際上は
第1図−○イに示すような構造体の軸線と同一形状
の軸線を有する支持治具を一体成形し、軸線の屈
折点に設けた凹部にプレートエンドを差し込め
ば、プレートエンドが固定してシヤフトを使用す
る必要がない。
To carry out the method of the present invention, a support jig having one recess is placed at a bending point on the axis of the desired shape, and a plate end having a center hole is inserted into the recess of the support jig. Although it is possible to fix the plate ends to each other by inserting a shaft, in practice, a support jig having the same shape as the axis of the structure as shown in Fig. 1-○A is integrally molded, and the axis is fixed. By inserting the plate end into the recess provided at the bending point, the plate end is fixed and there is no need to use a shaft.
一方、構造体の断面形状はプレートエンド周辺
部の凹部の数によつて調整することができる。こ
のようにして支持治具の形状、シヤフトの長さ、
プレートエンドの凹部の数等の調整により空間構
造体の形状を自由に調整することができる。 On the other hand, the cross-sectional shape of the structure can be adjusted by adjusting the number of recesses around the plate end. In this way, the shape of the support jig, the length of the shaft,
The shape of the spatial structure can be freely adjusted by adjusting the number of recesses in the plate end.
本発明に用いる糸状繊維としては炭素繊維、ガ
ラス繊維などが使用でき、例えば炭素繊維として
は太さ約7μmのもの、ガラス繊維としては太さ
13ないし25μmのものが2000ないし30000本から
なる糸(ロービング)またはさらにこれを数本撚
り合わせ、または引揃えた紐(ロービングまたは
ヤーン)が用いられる。またこれらの糸状繊維に
含浸される樹脂としてはエポキシ樹脂、不飽和ポ
リエステル樹脂、フエノール樹脂等の熱硬化性樹
脂が用いられる。これらの樹脂液の組成は、繊維
に含浸させるとき十分繊維の表面にゆきわたるが
流れ落ちない程度の粘度となるように選択し、か
つ特殊の触媒または促進剤を添加するが巻きつけ
終了迄は硬化が始らめものが好ましい。支持治具
は硬化後に取除くがプレートエンド、シヤフト等
は、そのまゝ構造体の中に残してもよい。 Carbon fibers, glass fibers, etc. can be used as the filamentous fibers used in the present invention. For example, carbon fibers have a thickness of about 7 μm, and glass fibers have a thickness of about 7 μm.
A thread (roving) consisting of 2,000 to 30,000 threads of 13 to 25 μm or a string (roving or yarn) made by twisting or aligning several threads thereof is used. Furthermore, thermosetting resins such as epoxy resins, unsaturated polyester resins, and phenol resins are used as the resins impregnated into these filamentous fibers. The composition of these resin liquids is selected so that when impregnating the fibers, the viscosity is such that it sufficiently spreads over the surface of the fibers but does not run off, and special catalysts or accelerators are added, but they do not harden until the end of winding. Preferably from the beginning. The support jig is removed after curing, but the plate end, shaft, etc. may be left in the structure.
以下、本発明の実施例を図面を参照して説明す
る。
Embodiments of the present invention will be described below with reference to the drawings.
第1図−○イは支持治具1にプレートエンド2を
配置した状態を示すもので、前述したように構造
体の軸線に合せて一体成形した支持治具1を用い
ている。上記支持治具1には所定の間隔をもつて
一対の凹部3,3を設け間隙部4a,4b,4c
…にプレートエンド2の1部を差込むことによつ
て該プレートエンド2が固定される。図中のプレ
ートエンド2には中心孔5が設けてあるが、本例
の支持治具1の場合、シヤフトを用いるまでもな
くプレートエンド2の固定がスムースに行はれ、
繊維を巻きつける張力にも十分耐えることができ
る。また第1図−ロに示すように凸部3,3の代
りに溝部6を設けてプレートエンド2を固定して
もよい。 FIG. 1-A shows the state in which the plate end 2 is placed on the support jig 1. As mentioned above, the support jig 1 is integrally molded along the axis of the structure. The support jig 1 is provided with a pair of recesses 3, 3 at a predetermined interval, and gaps 4a, 4b, 4c.
By inserting a portion of the plate end 2 into..., the plate end 2 is fixed. The plate end 2 in the figure is provided with a center hole 5, but in the case of the support jig 1 of this example, the plate end 2 can be fixed smoothly without using a shaft.
It can withstand the tension of wrapping fibers. Further, as shown in FIG. 1B, a groove 6 may be provided in place of the protrusions 3, 3 to fix the plate end 2.
プレートエンド2の周縁部には構造体の断面形
状に応じて凹部7a,7b,7c…が設けられて
あり、これらの凹部7a,7b,7c…に樹脂含
浸繊維を巻きつけてゆくことによりS型ないしル
ープ状の複雑な形状の空間構造体の製作が可能と
なる。 Recesses 7a, 7b, 7c... are provided at the peripheral edge of the plate end 2 according to the cross-sectional shape of the structure, and by winding resin-impregnated fibers around these recesses 7a, 7b, 7c... It becomes possible to manufacture spatial structures with complex shapes such as molds or loops.
第2図イ〜ハはプレートエンド2の各種の形状
を示すもので凹部7a,7b,7c…の数及び形
状は任意に決めることができる。すなわち第2図
−イは断面が四角形の構造体製造に用いられるプ
レートエンド2の標準的なものを示し、第2図−
ロに示すプレートエンドは多角形断面の構造体製
造に用いられ、第2図−ハに示すプレートエンド
2では凹部7a,7b,7c,7dの切り込みを
深くし、巻きとられた繊維が外れないようにして
ある。 FIGS. 2A to 2C show various shapes of the plate end 2, and the number and shape of the recesses 7a, 7b, 7c, . . . can be arbitrarily determined. That is, Fig. 2-A shows a standard plate end 2 used for manufacturing a structure with a rectangular cross section;
The plate end shown in B is used for manufacturing a structure with a polygonal cross section, and in the plate end 2 shown in FIG. It's like this.
第3図は第4図に示す支持治具1及びプレート
エンド2を用いて製造した空間構造体の斜視図を
表わす。すなわち第2図−○イに示すような周縁部
に4個の凹部7a,7b,7c,7dを有し、但
し中心孔5のない厚さ3ないし10mmのガラス繊維
強化樹脂製のプレートエンド2を支持治具1の溝
部6に差込み、各プレートエンド2の対応する凹
部7a,7b…の方向角度が一致するように調整
する。次に第5図に示す巻きつけパターンに従い
座標で表示した凹部(1.0)から出発して樹脂含
浸繊維を係止させてゆく。 FIG. 3 shows a perspective view of a space structure manufactured using the support jig 1 and plate end 2 shown in FIG. 4. That is, a plate end 2 made of glass fiber reinforced resin with a thickness of 3 to 10 mm has four recesses 7a, 7b, 7c, and 7d on the peripheral edge as shown in FIG. 2-A, but does not have a center hole 5. is inserted into the groove 6 of the support jig 1, and adjusted so that the direction angles of the corresponding recesses 7a, 7b, . . . of each plate end 2 match. Next, according to the winding pattern shown in FIG. 5, starting from the recess (1.0) indicated by the coordinates, the resin-impregnated fiber is secured.
巻きつけパターンは矩形波の部分と三角波の部
分とからなり、矩形波の部分は外周部の巻きつけ
順序を示し、三角波の部分は対角線方向の巻きつ
け順序を示している。そして始めの矩形波と三角
波とよりなるシーケンスで一回目の巻きつけを終
り、次に該シーケンスを逆行して二回目の巻きつ
けを行なう。このように2ないし12回巻きつけ
て、第3図に示すような空間構造体が得られる。 The winding pattern consists of a rectangular wave part and a triangular wave part, where the rectangular wave part shows the winding order on the outer periphery, and the triangular wave part shows the winding order in the diagonal direction. Then, the first winding is completed with the sequence consisting of the initial rectangular wave and the triangular wave, and then the sequence is reversed to perform the second winding. By winding the material 2 to 12 times in this manner, a spatial structure as shown in FIG. 3 is obtained.
巻きつけを終つた後支持治具1は取除くがプレ
ートエンド2は取り除かずに室温で数時間硬化
し、さらにオーブン中で後硬化処理し十分な強度
の繊維強化樹脂構造体とする。なおプレートエン
ド2は後硬化処理後も構造体の中に残される。 After winding is completed, the supporting jig 1 is removed, but the plate end 2 is not removed, and is cured at room temperature for several hours, and then post-cured in an oven to obtain a fiber-reinforced resin structure with sufficient strength. Note that the plate end 2 remains in the structure even after the post-curing process.
上記の如く本発明においてはプレートエンドを
所望の軸線に沿つて配置することにより複雑に屈
曲した構造体でも能率的に製造することができ
る。またプレートエンド、シヤフト等は構造体の
中に残しておいてもよく、構造体の強度を高める
効果もある。
As described above, in the present invention, even a complexly curved structure can be efficiently manufactured by arranging the plate ends along a desired axis. Further, the plate end, shaft, etc. may be left in the structure, which has the effect of increasing the strength of the structure.
第1図−○イは支持治具の一例の斜視図を表わ
し、第1図−○ロは他の支持治具の斜視図を表わ
し、第2図−○イは4個の凹部を有するプレートエ
ンドの正面図を表わし、第2図−○ロは8個の凹部
を有するプレートエンドの正面図を表わし、第2
図−○ハは切込みの深い凹部を有するプレートエン
ドの正面図を表わし、第3図は実施例で得た空間
構造体の斜視図を表わし、第4図は実施例で用い
た支持治具及びプレートエンドの斜視図を表わ
し、第5図は第4図に示すプレートエンドへの巻
きつけパターン図を表わす。
図中、1……支持治具、2……プレートエン
ド、3……凸部、4a,4b,4c,4d……間
隙部、5……中心孔、6……溝部、7a,7b,
7c,7d……凹部。
Figure 1-○A represents a perspective view of an example of a support jig, Figure 1-○B represents a perspective view of another support jig, and Figure 2-○A shows a plate having four recesses. Figure 2 - ○ represents a front view of the plate end having eight recesses;
Figure ○C shows a front view of a plate end having a deep recess, Fig. 3 shows a perspective view of the spatial structure obtained in the example, and Fig. 4 shows the support jig and A perspective view of the plate end is shown, and FIG. 5 shows a winding pattern diagram around the plate end shown in FIG. In the figure, 1...Support jig, 2...Plate end, 3...Convex portion, 4a, 4b, 4c, 4d...Gap portion, 5...Center hole, 6...Groove portion, 7a, 7b,
7c, 7d... recessed portions.
Claims (1)
支持治具を配置して相互に固定した後、周縁部に
3個以上の凹部を設けたプレートエンド(仕切
板)を上記の支持治具の凹部に差込み、しかる後
プレートエンドの凹部に樹脂含浸した連続繊維の
糸または紐を巻きつけ、硬化後脱型することを特
徴とする繊維強化樹脂構造体の製造方法。1. After placing the support jigs at positions corresponding to the bending points of the axis of the desired shape and fixing them to each other, place a plate end (partition plate) with three or more recesses on the periphery of the support jig above. A method for manufacturing a fiber-reinforced resin structure, which comprises inserting the structure into the recess of the plate end, then winding a resin-impregnated continuous fiber thread or string around the recess of the plate end, and removing the mold after curing.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP59189336A JPS6166634A (en) | 1984-09-10 | 1984-09-10 | Manufacture of fiber reinforced structural body |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP59189336A JPS6166634A (en) | 1984-09-10 | 1984-09-10 | Manufacture of fiber reinforced structural body |
Publications (2)
Publication Number | Publication Date |
---|---|
JPS6166634A JPS6166634A (en) | 1986-04-05 |
JPH0511024B2 true JPH0511024B2 (en) | 1993-02-12 |
Family
ID=16239632
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP59189336A Granted JPS6166634A (en) | 1984-09-10 | 1984-09-10 | Manufacture of fiber reinforced structural body |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPS6166634A (en) |
-
1984
- 1984-09-10 JP JP59189336A patent/JPS6166634A/en active Granted
Also Published As
Publication number | Publication date |
---|---|
JPS6166634A (en) | 1986-04-05 |
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