JPS6143542A - Manufacture of frp parts - Google Patents
Manufacture of frp partsInfo
- Publication number
- JPS6143542A JPS6143542A JP59165368A JP16536884A JPS6143542A JP S6143542 A JPS6143542 A JP S6143542A JP 59165368 A JP59165368 A JP 59165368A JP 16536884 A JP16536884 A JP 16536884A JP S6143542 A JPS6143542 A JP S6143542A
- Authority
- JP
- Japan
- Prior art keywords
- prepreg sheet
- rib
- prepreg
- frp
- molding
- 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.)
- Pending
Links
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
- B29D99/001—Producing wall or panel-like structures, e.g. for hulls, fuselages, or buildings
- B29D99/0014—Producing wall or panel-like structures, e.g. for hulls, fuselages, or buildings provided with ridges or ribs, e.g. joined ribs
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
- B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
- B29C70/28—Shaping operations therefor
- B29C70/40—Shaping or impregnating by compression not applied
- B29C70/42—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles
- B29C70/46—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using matched moulds, e.g. for deforming sheet moulding compounds [SMC] or prepregs
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C2791/00—Shaping characteristics in general
- B29C2791/001—Shaping in several steps
Abstract
Description
【発明の詳細な説明】
[産業上の利用分野]
本発明は、特にリブのあるFRP部品を製造する方法に
関する。DETAILED DESCRIPTION OF THE INVENTION [Field of Industrial Application] The present invention particularly relates to a method for manufacturing ribbed FRP parts.
[従来技術]
従来、長繊維(連続繊維)を配合してなる複数枚のプリ
プレグシートを積層して熱プレス成形することにより、
FRP部品を製造する方法は実用化されている。[Prior art] Conventionally, by laminating and hot press forming multiple prepreg sheets made by blending long fibers (continuous fibers),
Methods for manufacturing FRP parts have been put into practical use.
ところで、軽量化を指向する自動車用部品として、第7
図に示すように、エンジンマウントメンバlをFRPで
製造する場合、高強度・高剛性が要求されることから、
多数のリブ2.・・・、2を形成して補強する必要があ
る。By the way, as an automobile part aiming at weight reduction, the 7th
As shown in the figure, when the engine mount member l is manufactured from FRP, high strength and high rigidity are required.
Many ribs 2. ..., 2 needs to be formed and reinforced.
ところが、リブ2は、第8図に詳細に示すように、長繊
維3の配向方向に対して直角な方向に鋭角で立上がった
突起状であるから、熱プレス成形時に、長繊維3.・・
・、3がリブ2内に入り込み難く、ゲル化した樹脂4の
みが充填されるようになるので(樹脂リッチ)、リブ2
にクラックが発生して高強度・高剛性が得られないとい
う問題があった。However, as shown in detail in FIG. 8, the ribs 2 are protrusions that stand up at an acute angle in a direction perpendicular to the orientation direction of the long fibers 3. Therefore, during hot press molding, the long fibers 3.・・・
・, 3 is difficult to enter into the rib 2, and only the gelled resin 4 is filled (resin rich), so the rib 2
There was a problem in that high strength and high rigidity could not be obtained due to the occurrence of cracks.
なお、FRP成形物の製造方法として、第9図に示すよ
うに、予備成形した浴槽5の底部6と手摺部7どをプリ
プレグシート8で複合一体化するらのが提案されており
(特開昭58−24413号公報参照)、この技術を応
用して、エンジンマウントメンバ1に、繊維が充填され
たリブ2を複合一体化する方法が考えられるが、エンツ
ノマウントメンバlの長繊維とリブ2の繊維とに連続性
かないので、やはり高強度・高剛性が得られないという
問題がある。As a method of manufacturing an FRP molded product, a method has been proposed in which the bottom part 6 and handrail part 7 of a preformed bathtub 5 are compositely integrated with a prepreg sheet 8, as shown in FIG. (Refer to Publication No. 58-24413), it is conceivable to apply this technology to compositely integrate the fiber-filled ribs 2 into the engine mount member 1. Since there is no continuity between the fibers of No. 2, there is still a problem that high strength and high rigidity cannot be obtained.
[発明の目的]
本発明は、上記従来の問題点に鑑みてなされたもので、
リブにも長繊維を充分に充填することを可能としたFR
P部品の製造方法を提供することを目的とするものであ
る。[Object of the invention] The present invention has been made in view of the above-mentioned conventional problems, and
FR that makes it possible to sufficiently fill the ribs with long fibers
The purpose of this invention is to provide a method for manufacturing P parts.
[発明の構成]
このため本発明は、長繊維を配合してなる複数枚のプリ
プレグシートを積層して熱プレス成形し、・リブのある
FRP部品を製造する方法であって、まず、積層成形す
べき複数枚のうちの一部のプリプレグシートを下型上に
載置し、ついで、この一部のプリプレグシートを、下型
に形成されたリブ−成形用171′1部内に、予備成形
型具を用いて圧入充填し、しかる後、残部のプリプレグ
シートをこの予備成形品上に積層載置し、該予備成形品
ともども熱プレス成形するように構成したものである。[Structure of the Invention] Therefore, the present invention is a method for manufacturing an FRP part with ribs by laminating and hot press molding a plurality of prepreg sheets made by blending long fibers. A part of the prepreg sheets out of the plurality of prepreg sheets to be processed is placed on the lower mold, and then this part of the prepreg sheets is placed in the rib-forming part 171' formed in the lower mold and placed in the preforming mold. The structure is such that the prepreg sheet is press-fitted using a tool, and then the remaining prepreg sheet is laminated on top of the preform and hot press molded together with the preform.
[発明の効果]
本発明によれば、柔軟性がある一部のプリプレグシート
にリブを予備成形し、その後に残部のプリプレグシート
ともども熱プレス成形するようにしたから、一部のプリ
プレグシートの長繊維が連続性を保ったままリブ内に十
分に充填されるようになるので、リブの樹脂リッチ化が
防止され、FRP部品に高強度・高剛性を確保できるよ
うになる。[Effects of the Invention] According to the present invention, ribs are preformed on some of the flexible prepreg sheets, and then the remaining prepreg sheets are heat press-molded, so that the length of some of the prepreg sheets can be reduced. Since the fibers are sufficiently filled into the ribs while maintaining continuity, the ribs are prevented from becoming rich in resin, and high strength and high rigidity can be ensured in the FRP parts.
[実施例]
第1図に示すように、成形用下型10にはリブ成形用溝
部10aが形成されていて、この成形用下型10の上に
積層成形すべき複数枚のプリプレグシートIIA、II
Bのうちの一部のプリプレグシートIIAをまず載置す
る。この一部のプリプレグシートIIAは厚みが薄いの
で柔軟性がある。[Example] As shown in FIG. 1, a rib molding groove 10a is formed in the lower molding mold 10, and a plurality of prepreg sheets IIA to be laminated and molded on the lower molding mold 10, II
First, some prepreg sheets IIA of B are placed. This part of the prepreg sheet IIA is thin and has flexibility.
ついで、第2図に示すように、成形用下型lOのリブ成
形用溝部10aに嵌り合う突部12aを打する予備成形
型具I2により、プリプレグシート+1Aを加圧して、
リブ成形用溝部10aにプリプレグシートIIAを圧入
充填する。Next, as shown in FIG. 2, the prepreg sheet +1A is pressurized by a preforming mold tool I2 that hits the protrusion 12a that fits into the rib molding groove 10a of the lower mold lO,
The prepreg sheet IIA is press-fitted into the rib forming groove 10a.
この予備成形工程により、プリプレグシート11Aの長
繊維13が連続性を保ったままりブ成形用iM部り0a
内に十分に充填された予備成形品16゜が成形されるよ
うになる。Through this preforming process, the long fibers 13 of the prepreg sheet 11A maintain their continuity while forming the iM part 0a for molding.
A fully filled preform 16° is now formed.
しかる後、第3図に示すように、残部のプリプレグシー
トllBをこの予備成形品16′ の上に積層載置し、
上型I8を作動させて予備成形品ともども熱プレス成形
する。Thereafter, as shown in FIG. 3, the remaining prepreg sheet LLB is laminated on top of this preform 16'.
The upper mold I8 is operated to perform hot press molding together with the preformed product.
この熟プレス成形工程により、第4図に示すように、両
プリプレグシートIIA、IIBのゲル・化した樹脂1
4が空洞部分15に充填されるとと6に、ゲル化した樹
脂+4により両プリプレグシートlIA、lll3!l
<複合一体化されて、リブ17のあるFRP部品(エン
ノンマウントメンノリ16が完成する。Through this dry press molding process, as shown in Fig. 4, the gelled resin 1 of both prepreg sheets IIA and IIB is
4 is filled into the hollow portion 15, both prepreg sheets lIA, lll3! are formed by the gelled resin +4. l
<The FRP part with ribs 17 (ennon mount menori 16) is completed by being integrated.
この熱プレス成形工程時に、プリプレグシート11Aの
リブ成形用溝部+Oa内に充填された長繊維13が僅か
に復元するが、完成したFRP部品16としては、長繊
維13が連続性を保ったままりブ17内に十分に充填さ
れることになる。During this hot press molding process, the long fibers 13 filled in the rib forming grooves +Oa of the prepreg sheet 11A are slightly restored, but as a completed FRP part 16, the long fibers 13 remain continuous and remain intact. 17 will be fully filled.
第5図は、樹脂リッチのリブが形成されたエンジノマウ
ントメンバ(従来品)lと、本方法により製造されたエ
ンノンマウントメンバ(本案界)16との強度・剛性テ
ストを示すものである。Figure 5 shows the strength and rigidity test of the engine mount member (conventional product) 1 on which resin-rich ribs are formed and the engine mount member 16 manufactured by this method (honankai). .
各メンバ1.16は、長繊維45重量%、知識M115
重量%、樹脂(不飽和ポリエステル)40重量%のプリ
プレグシートで構成した。Each member 1.16 contains long fibers 45% by weight, knowledge M115
It was composed of a prepreg sheet containing 40% by weight of resin (unsaturated polyester).
そして、各メンバ1.16を両端支持して荷重Fを加え
た。その結果を第6図のグラフに示す。Then, each member 1.16 was supported at both ends and a load F was applied. The results are shown in the graph of FIG.
グラフからも明らかなように、従来品lは荷重500〜
550kgで降伏点に達したのに対して、本案界16は
700〜750kgで降伏点に達した。As is clear from the graph, the conventional product 1 has a load of 500~
The yield point was reached at 550 kg, whereas the yield point was reached at 700 to 750 kg for Honkai Kai 16.
従って、従来品1に比べて本案界16は、強度・剛性が
約40%も向上したことがイつかる。Therefore, it can be seen that the strength and rigidity of the present guide 16 are improved by about 40% compared to the conventional product 1.
第1図〜第4図は本発明に係るFRP部品の製造工程を
示す断面図、第5図は強度・剛性試験を示す側面図、第
6図は第5図の試験データを示すグラフ、第7図はFR
P部品(エンジンマウントメノバ)の斜視図、第8図は
従来のリブ部分の断面図、第9図は従来のFRP成形品
の製造方法を示す斜視図である。
lO・・成形用下型、 loa・・・リブ成形用溝部
、+1A、IIB・・ブリプレグンート、 12・・
予備成形型具、 13・・・長繊維、 14・・・
樹脂、16−・FRP部品(エンジンマウントメンノリ
、17・・リブ。1 to 4 are cross-sectional views showing the manufacturing process of FRP parts according to the present invention, FIG. 5 is a side view showing strength and rigidity tests, and FIG. 6 is a graph showing the test data of FIG. Figure 7 is FR
FIG. 8 is a perspective view of a P part (engine mount member), FIG. 8 is a cross-sectional view of a conventional rib portion, and FIG. 9 is a perspective view showing a conventional method of manufacturing an FRP molded product. lO... Lower mold for molding, loa... Groove for rib forming, +1A, IIB... Buri Pregunto, 12...
Preforming tool, 13... long fiber, 14...
Resin, 16-・FRP parts (engine mount menori, 17-・rib.
Claims (1)
を積層して熱プレス成形し、リブのあるFRP部品を製
造する方法であって、 まず、積層成形すべき複数枚のうちの一部のプリプレグ
シートを下型上に載置し、ついで、この一部のプリプレ
グシートを、下型に形成されたリブ成形用溝部内に、予
備成形型具を用いて圧入充填し、しかる後、残部のプリ
プレグシートをこの予備成形品上に積層載置し、該予備
成形品ともども熱プレス成形するようにしたことを特徴
とするFRP部品の製造方法。(1) A method of manufacturing a ribbed FRP part by laminating and hot press molding a plurality of prepreg sheets made by blending long fibers, first, a part of the plurality of sheets to be laminated of the prepreg sheet is placed on the lower mold, then a part of the prepreg sheet is press-fitted into the rib forming groove formed in the lower mold using a preforming tool, and then the remaining part is A method for manufacturing an FRP part, characterized in that a prepreg sheet is laminated and mounted on the preform, and the preform is hot press molded together with the preform.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP59165368A JPS6143542A (en) | 1984-08-06 | 1984-08-06 | Manufacture of frp parts |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP59165368A JPS6143542A (en) | 1984-08-06 | 1984-08-06 | Manufacture of frp parts |
Publications (1)
Publication Number | Publication Date |
---|---|
JPS6143542A true JPS6143542A (en) | 1986-03-03 |
Family
ID=15811040
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP59165368A Pending JPS6143542A (en) | 1984-08-06 | 1984-08-06 | Manufacture of frp parts |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPS6143542A (en) |
Cited By (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5225135A (en) * | 1991-08-30 | 1993-07-06 | General Motors Corporation | Balanced pressure compression molding method |
JP2005307116A (en) * | 2004-04-26 | 2005-11-04 | Shin Dick Kako Kk | Artificial marble waterproof pan |
EP2067615A1 (en) * | 2006-09-28 | 2009-06-10 | Toray Industries, Inc. | Fiber-reinforced plastic and process for production thereof |
EP2133263A3 (en) * | 2008-06-13 | 2011-11-16 | The Boeing Company | Method and apparatus for forming and installing stringers |
US8465613B2 (en) | 2011-08-24 | 2013-06-18 | The Boeing Company | Method and apparatus for fabricating variable gauge, contoured composite stiffeners |
JP2014151648A (en) * | 2013-02-07 | 2014-08-25 | Boeing Co | Method and system of making composite structures having gap fillers with chopped fiber material |
US8974212B2 (en) | 2004-07-26 | 2015-03-10 | The Boeing Company | Systems for manufacturing composite parts with female tools |
US9162380B2 (en) | 2005-04-13 | 2015-10-20 | The Boeing Company | Forming highly contoured composite parts |
US9254619B2 (en) | 2008-05-28 | 2016-02-09 | The Boeing Company | Method and apparatus for fabricating variable gauge, contoured composite stiffeners |
US9387628B2 (en) | 2011-08-24 | 2016-07-12 | The Boeing Company | Method and apparatus for fabricating composite stringers |
JP2017160661A (en) * | 2016-03-09 | 2017-09-14 | 積水化学工業株式会社 | Reinforcement mechanism for long structure |
WO2018088135A1 (en) * | 2016-11-11 | 2018-05-17 | 旭化成株式会社 | Molded article, and compression molding method |
US10369740B2 (en) | 2015-07-09 | 2019-08-06 | The Boeing Company | Method of forming a contoured hat stiffener |
-
1984
- 1984-08-06 JP JP59165368A patent/JPS6143542A/en active Pending
Cited By (18)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5225135A (en) * | 1991-08-30 | 1993-07-06 | General Motors Corporation | Balanced pressure compression molding method |
JP2005307116A (en) * | 2004-04-26 | 2005-11-04 | Shin Dick Kako Kk | Artificial marble waterproof pan |
US8974212B2 (en) | 2004-07-26 | 2015-03-10 | The Boeing Company | Systems for manufacturing composite parts with female tools |
US9561602B2 (en) | 2005-04-13 | 2017-02-07 | The Boeing Company | Forming highly contoured composite parts |
US9162380B2 (en) | 2005-04-13 | 2015-10-20 | The Boeing Company | Forming highly contoured composite parts |
EP2067615A4 (en) * | 2006-09-28 | 2012-04-04 | Toray Industries | Fiber-reinforced plastic and process for production thereof |
JP5315692B2 (en) * | 2006-09-28 | 2013-10-16 | 東レ株式会社 | Manufacturing method of fiber reinforced plastic |
EP2067615A1 (en) * | 2006-09-28 | 2009-06-10 | Toray Industries, Inc. | Fiber-reinforced plastic and process for production thereof |
US9254619B2 (en) | 2008-05-28 | 2016-02-09 | The Boeing Company | Method and apparatus for fabricating variable gauge, contoured composite stiffeners |
EP2133263A3 (en) * | 2008-06-13 | 2011-11-16 | The Boeing Company | Method and apparatus for forming and installing stringers |
US9387627B2 (en) | 2008-06-13 | 2016-07-12 | The Boeing Company | Apparatus for forming and installing stringers |
US8465613B2 (en) | 2011-08-24 | 2013-06-18 | The Boeing Company | Method and apparatus for fabricating variable gauge, contoured composite stiffeners |
US9387628B2 (en) | 2011-08-24 | 2016-07-12 | The Boeing Company | Method and apparatus for fabricating composite stringers |
JP2014151648A (en) * | 2013-02-07 | 2014-08-25 | Boeing Co | Method and system of making composite structures having gap fillers with chopped fiber material |
US10369740B2 (en) | 2015-07-09 | 2019-08-06 | The Boeing Company | Method of forming a contoured hat stiffener |
US11370159B2 (en) | 2015-07-09 | 2022-06-28 | The Boeing Company | Apparatus for forming a contoured hat stiffener |
JP2017160661A (en) * | 2016-03-09 | 2017-09-14 | 積水化学工業株式会社 | Reinforcement mechanism for long structure |
WO2018088135A1 (en) * | 2016-11-11 | 2018-05-17 | 旭化成株式会社 | Molded article, and compression molding method |
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