JPH02184414A - Molding of composite material - Google Patents

Molding of composite material

Info

Publication number
JPH02184414A
JPH02184414A JP1003050A JP305089A JPH02184414A JP H02184414 A JPH02184414 A JP H02184414A JP 1003050 A JP1003050 A JP 1003050A JP 305089 A JP305089 A JP 305089A JP H02184414 A JPH02184414 A JP H02184414A
Authority
JP
Japan
Prior art keywords
edge
face
laminated
side wall
mold
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.)
Granted
Application number
JP1003050A
Other languages
Japanese (ja)
Other versions
JP2730946B2 (en
Inventor
Kazuhiro Oba
大庭 一浩
Takahisa Hasegawa
長谷川 高久
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.)
Subaru Corp
Original Assignee
Fuji Heavy 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 Fuji Heavy Industries Ltd filed Critical Fuji Heavy Industries Ltd
Priority to JP1003050A priority Critical patent/JP2730946B2/en
Publication of JPH02184414A publication Critical patent/JPH02184414A/en
Application granted granted Critical
Publication of JP2730946B2 publication Critical patent/JP2730946B2/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C43/00Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor
    • B29C43/02Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor of articles of definite length, i.e. discrete articles
    • B29C43/20Making multilayered or multicoloured articles
    • B29C43/203Making multilayered articles
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C43/00Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor
    • B29C43/02Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor of articles of definite length, i.e. discrete articles
    • B29C43/10Isostatic pressing, i.e. using non-rigid pressure-exerting members against rigid parts or dies
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C43/00Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor
    • B29C43/02Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor of articles of definite length, i.e. discrete articles
    • B29C43/10Isostatic pressing, i.e. using non-rigid pressure-exerting members against rigid parts or dies
    • B29C43/12Isostatic pressing, i.e. using non-rigid pressure-exerting members against rigid parts or dies using bags surrounding the moulding material or using membranes contacting the moulding material
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/28Shaping operations therefor
    • B29C70/40Shaping or impregnating by compression not applied
    • B29C70/42Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles
    • B29C70/44Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using isostatic pressure, e.g. pressure difference-moulding, vacuum bag-moulding, autoclave-moulding or expanding rubber-moulding
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/28Shaping operations therefor
    • B29C70/54Component parts, details or accessories; Auxiliary operations, e.g. feeding or storage of prepregs or SMC after impregnation or during ageing
    • B29C70/545Perforating, cutting or machining during or after moulding
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C43/00Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor
    • B29C43/02Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor of articles of definite length, i.e. discrete articles
    • B29C43/18Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor of articles of definite length, i.e. discrete articles incorporating preformed parts or layers, e.g. compression moulding around inserts or for coating articles
    • B29C2043/189Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor of articles of definite length, i.e. discrete articles incorporating preformed parts or layers, e.g. compression moulding around inserts or for coating articles the parts being joined
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C43/00Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor
    • B29C43/32Component parts, details or accessories; Auxiliary operations
    • B29C43/36Moulds for making articles of definite length, i.e. discrete articles
    • B29C43/361Moulds for making articles of definite length, i.e. discrete articles with pressing members independently movable of the parts for opening or closing the mould, e.g. movable pistons
    • B29C2043/3615Forming elements, e.g. mandrels or rams or stampers or pistons or plungers or punching devices
    • B29C2043/3621Forming elements, e.g. mandrels or rams or stampers or pistons or plungers or punching devices a plurality of individual elements acting on the material in the same or diferent directions, e.g. making tubular T-joints, profiles
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C43/00Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor
    • B29C43/32Component parts, details or accessories; Auxiliary operations
    • B29C43/36Moulds for making articles of definite length, i.e. discrete articles
    • B29C43/3642Bags, bleeder sheets or cauls for isostatic pressing
    • B29C2043/3644Vacuum bags; Details thereof, e.g. fixing or clamping
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C43/00Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor
    • B29C43/32Component parts, details or accessories; Auxiliary operations
    • B29C43/36Moulds for making articles of definite length, i.e. discrete articles
    • B29C43/40Moulds for making articles of definite length, i.e. discrete articles with means for cutting the article
    • B29C2043/403Moulds for making articles of definite length, i.e. discrete articles with means for cutting the article knife blades
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C43/00Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor
    • B29C43/32Component parts, details or accessories; Auxiliary operations
    • B29C43/52Heating or cooling
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/28Shaping operations therefor
    • B29C70/40Shaping or impregnating by compression not applied
    • B29C70/42Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles
    • B29C70/46Shaping 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
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29LINDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
    • B29L2031/00Other particular articles
    • B29L2031/001Profiled members, e.g. beams, sections
    • B29L2031/003Profiled members, e.g. beams, sections having a profiled transverse cross-section

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Composite Materials (AREA)
  • Moulds For Moulding Plastics Or The Like (AREA)
  • Casting Or Compression Moulding Of Plastics Or The Like (AREA)
  • Moulding By Coating Moulds (AREA)

Abstract

PURPOSE:To enable outline cutting to be easily performed by making specific jigs and tools unnecessary by a method wherein semihardened fiber reinforced plastics are laminated on a mold surface, an excess thickness of the laminated material is cut by moving an edge face of an edge tool along a different level side face, a stiffening plate being in contact with the different level side face and having a contact surface along an outer edge side surface of the laminated material is installed, and said shape is hardened by pressurizing and heating. CONSTITUTION:Laminated materials 16 are piled on upper surfaces, opposed side surfaces, and lower surfaces of opposed mandrels 11, 11. In that case, an edge part of the laminated materials 16 is protruded from a side wall 13 of a groove 12. Tools of a cutter knife 17 or the like are moved along the side wall 13, and the edge part of the laminated materials 16 protruded from the side wall 10 are cut. Then an edge forming parts 14 are fit in the groove part 12. Thereafter, cowl plates 15, 15 are respectively set to the edge surface forming parts 14, 14 on the upper face side and the lower face side. Then, they are vacuum packed, and are hardened by pressurizing and heating with an autoclave to perform molding. In that case, flange edge face forming parts 14 are pushed onto the side wall 13 and a bottom wall by pressurizing, and position is performed by those surfaces.

Description

【発明の詳細な説明】 (産業上の利用分野) 本発明は、繊維強化プラスチックを積層し加圧、加熱し
て硬化する複合材の成形h″法に関するもの−Cある。
DETAILED DESCRIPTION OF THE INVENTION (Industrial Application Field) The present invention relates to a composite material forming method H'' in which fiber-reinforced plastics are laminated and cured by applying pressure and heating.

(従来の技術) 繊維強化プラスチックからなる複合材は軽量で、しかも
高強度を釘するため、航空機なとの構造部材として広く
使用されている。従来、この複合材の成形方法としては
、複?i祠の形状に合わせて形成された型の−Lに未硬
化の複合H料素材を積載し、真空バック成形したまま、
オートクレーブ中で加熱硬化させる方法か知られている
(Prior Art) Composite materials made of fiber-reinforced plastics are lightweight and have high strength, so they are widely used as structural members for aircraft. Conventionally, there have been multiple methods for forming this composite material. The uncured composite H material is loaded into the mold -L formed to match the shape of the i-shrine, and the material is vacuum-back molded.
A method of heat curing in an autoclave is known.

(発明か解決しようとする課題) ところで、−」−記従来の1(合)(の成形方法にあっ
ては、成形後、ルータ−ビット(例えば特開昭57−1
07718)を用いて余肉イ・j形状て硬化された成形
品の外形切断を行なう必要かある。このため、特別なル
ータ−やならい型等の治工具か必要であるとともに、l
′JJ断に宏する工数か増加するという問題点かあった
(Problem to be solved by the invention) By the way, in the conventional molding method 1 (joint) described in "-", after molding, a router bit (for example, JP-A-57-1
07718) to cut the outer shape of the cured molded product with the excess thickness A/J shape. For this reason, special tools such as routers and tracing molds are required, and l
'There was a problem in that the number of man-hours required for JJ increased.

また、人体にf−i害な粉塵が発生するとともに、デラ
ミネーション等の不具合か牛する可能性かあるという問
題点かあった。
In addition, there were problems in that dust harmful to the human body was generated, and there was also the possibility of problems such as delamination.

本発明は、上記問題点を解決し、特別な治工具を必要と
せす容易に外形切断を行なうことができる複合材の成形
方法を提供することを目的とする。
SUMMARY OF THE INVENTION An object of the present invention is to solve the above-mentioned problems and provide a method for forming a composite material, which allows easy cutting of the outer shape without requiring special jigs and tools.

(課題を解決するためのL段) 本発明は、上記課題を解決するためになされたものであ
って、型面に繊維強化プラスチックを積層し加圧、加熱
して硬化する複合十Aの成形方法において、前記型面に
、成形しようとする成形品の外縁側面に沿って型面から
切りドげられた段差側面を有する成形型を準備し、前記
型面に半硬化状態の繊維強化プラスチックを積層し、前
記段差側面に沿って刃物の刃面を移動して、積層体の余
肉を切断し、前記段差側面に!′14妾し、かつ積層体
の外縁側ば1Jに沿う当接IIIJを角°する当板を装
着し、力l圧および加熱し7て硬化するようにしている
(L stage for solving the problem) The present invention has been made to solve the above problem, and the present invention is made by laminating fiber-reinforced plastic on the mold surface and curing it by pressurizing and heating. In the method, a mold having a stepped side surface cut out from the mold surface along the outer edge side of a molded product to be molded is prepared, and a semi-hardened fiber reinforced plastic is applied to the mold surface. Laminate the layers, move the blade surface of the knife along the stepped side surface, cut the excess thickness of the layered product, and then cut the excess thickness on the stepped side surface! A contact plate is attached to the laminate and angles the abutment IIIJ along the outer edge side 1J of the laminate, and is cured by applying pressure and heating 7.

また、前記段差側面は、前記型面に形成された溝の側面
であり、前記当板は、前記溝に係合するようになってい
る。
Further, the stepped side surface is a side surface of a groove formed in the mold surface, and the contact plate is adapted to engage with the groove.

(作 用) 本発明は、型面にi懺維強化プラスチックを積層し加圧
、加熱して硬化する複合材の成形方法において、前記型
面に、成形しようとする成形品の外縁側面に沿って型面
から切り下げられた段差側面をrJ−する成形型を<f
H備し、前記型面に半硬化状態の繊維強化プラスチック
を積層し、前記段差側面に沿って刃物のメJ面を移動し
て、積層体の余肉を切断し、前記段差側面に当接し、か
つ積層体の外縁側面に沿う当接面を何する当板を装着し
、加圧および加熱して硬化するようにし、また、前記段
差側面は、前記型面に形成された溝の側面であるから、
柔軟な積層体をカッターナイフ等の一般的な1−具を使
用して明断することかできる。また、段J2側面によっ
て刃物を案内することができるから、明断作業における
人的影響を(Jl除することかでき、切断粘度を向」−
さぜることができるとともに、作業を容易に行なうこと
かできる。また、当板により端面の成形を行なうので、
成形品の端面品質を向上させることかできる。
(Function) The present invention provides a composite material molding method in which i-fiber-reinforced plastic is laminated on a mold surface and cured by applying pressure and heating. <f>
A semi-hardened fiber-reinforced plastic is laminated on the mold surface, and the J plane of the cutter is moved along the stepped side surface to cut the excess thickness of the laminate and abut against the stepped side surface. , and a contact plate is attached to the abutting surface along the outer edge side of the laminate and cured by applying pressure and heating, and the step side is the side surface of the groove formed on the mold surface. because there is,
The flexible laminate can be cut into pieces using a common tool such as a utility knife. In addition, since the blade can be guided by the side surface of stage J2, the human influence during cutting work can be reduced (Jl), and the cutting viscosity can be improved.
Not only can it be cooled, but it can also be easily worked on. In addition, since the end face is formed using a backing plate,
It is possible to improve the quality of the end face of the molded product.

このようなことから、硬化後の切断作業が不要となり、
したかって、ルータ−1ならい型て9の治工具及び粉塵
処理さ゛の設備を不要とすることができる。
This eliminates the need for cutting after curing.
Therefore, the jigs and tools of the router 1 model 9 and the equipment for dust treatment can be made unnecessary.

(実施例) 以ド、本発明の実施例について、第1図ないし第7図を
参照して説明する。
(Example) Hereinafter, an example of the present invention will be described with reference to FIGS. 1 to 7.

第1図ないし第4図は■断面翼小骨成形型による成形方
法を示すものである。
FIGS. 1 to 4 show a molding method using a ■ cross-section wing ossicle mold.

図中符号11.11は断面略矩形状に形成された一対の
マンドレル(型本体)を示す。このマンドレル11.1
1の上面両端部と下両端部には、それぞれ満12.12
,12.12か形成されており、この溝12の内側の側
壁13は、成形すべき積層体の外縁の位置に形成されて
いる。これらの4つの溝に上面およびド面から突出して
それぞれ嵌合されているのは、フランジ端面成形用部品
14 14 14 1.4である。
Reference numerals 11 and 11 in the figure indicate a pair of mandrels (mold bodies) each having a substantially rectangular cross section. This mandrel 11.1
Each of the upper and lower ends of 1 is filled with 12.12 mm.
, 12.12 are formed, and the inner side wall 13 of this groove 12 is formed at the outer edge of the laminate to be molded. Flange end face forming parts 14 14 14 1.4 are fitted into these four grooves, respectively, protruding from the top and bottom surfaces.

また、マンドレル11の上側および下側のフランジ端面
成形用部品14.14にマンドレルから所定開園離間し
て配設されているのは、フランジ外面成形用カウルプレ
ーti5,1.5である。
Also, disposed on the upper and lower flange end face forming parts 14.14 of the mandrel 11 at a predetermined distance from the mandrel are cowl plates ti5, 1.5 for forming the flange outer surface.

このような成形型で成形を行なうには、まず、第1図に
示すように、対向するマンドレル1]。
In order to perform molding using such a mold, first, as shown in FIG. 1, opposing mandrels 1].

]]の上面、対向する側面、下面に積層体16を積層す
る。この際、積層体]6の端部は溝12の側壁]3から
突出している。
]] Laminated body 16 is laminated on the upper surface, the opposing side surface, and the lower surface. At this time, the end of the laminate [6] protrudes from the side wall [3] of the groove 12.

次に、第2図に示すように、対向する両マンドレル11
.11を所定の間隔にセットし、両マンドレルの上下面
に追加積層を行なう。なお、ここで追加積層のH無は設
π1により異なる。その後、カッターナイフ17等の一
般的な工具を側壁13に沿って移動させ、側壁1Bから
突出している積層体16の端部を切断する。
Next, as shown in FIG.
.. 11 are set at a predetermined interval, and additional lamination is performed on the upper and lower surfaces of both mandrels. It should be noted that here, the number of additional layers to be stacked differs depending on the setting π1. Thereafter, a general tool such as a cutter knife 17 is moved along the side wall 13 to cut the end of the stacked body 16 protruding from the side wall 1B.

次いで、第3図に示すように、溝部12に端面成形用部
品]4を嵌合する。なお、ここで、第2図と第3図に示
す上程は、まず積層体16の4つの端部を切断した後、
4つの端面成形部品]4゜・を溝12.・・に嵌合させ
てもよく、また、積層体]6の1つの端部を切断後その
iF;12に端面成形部品]4を嵌合し、その後他の′
3ケ所について切断と嵌合をくり返してもよい。
Next, as shown in FIG. 3, the end face molding part 4 is fitted into the groove 12. Note that in the steps shown in FIGS. 2 and 3, after cutting the four ends of the laminate 16,
4 end molded parts] 4° groove 12. Alternatively, after cutting one end of the laminate 6, the end face molded part] 4 is fitted to the iF;
Cutting and fitting may be repeated at three locations.

次に、カウルブレー1−15.15をそれぞれ上面側、
下面側の端面成;し部品14.14にセットする。
Next, install cowl brakes 1-15.15 on the top side,
Finish the end face on the bottom side and set it on part 14.14.

その後、真空ハックを行ないオートクレーブにて加圧、
加熱[7て硬化させて成形を行なう。この際、加圧によ
ってフランン端面成形用部品14は溝の側壁]3、底壁
]8に押し付けられ、これらの面によって位置決めされ
る。
After that, perform a vacuum hack and pressurize in an autoclave.
Heat [7] to harden and mold. At this time, the flan end face forming part 14 is pressed against the side wall [3] and bottom wall [8] of the groove by pressure, and is positioned by these surfaces.

このように、上記実施例にあっては、溝12の内側の側
壁]3を成形品の外縁位置に形成し、硬化前にこの側壁
]3に沿って刃物17を移動させることによって積層体
]6を切断するようにしているから、柔軟な積層体]6
を切断することかてき、したかってカッターナイフ17
等の一般的な上置を使用することかできる。また、側壁
ト3によってメJ物を案内することかできるから、切断
作p13における人的影響を()1除することかてぎ、
切断粘度を向」−させることかできるとともに、作業を
容品に行なうことかできる。なお、側壁13に対するカ
ッター17の傾斜による多少の切り残し、切り込み等は
フランン端面成形用部品により規制されるとともに、硬
化時の加熱による樹脂流動等により補丁され、硬化後の
品質・\の影響は殆どない。
In the above embodiment, the inner side wall 3 of the groove 12 is formed at the outer edge of the molded product, and the cutter 17 is moved along the side wall 3 before curing to form the laminate. 6 is cut, so it is a flexible laminate]6
If you want to cut something, use a cutter knife 17
You can use common overrides such as In addition, since the material can be guided by the side wall 3, the human influence in the cutting operation P13 can be reduced by ()1,
It is possible to change the cutting viscosity and also to work on the container. In addition, some uncut edges and cuts caused by the inclination of the cutter 17 with respect to the side wall 13 are regulated by the flan end face molding parts, and are compensated for by resin flow due to heating during curing, and the quality after curing will not be affected. There aren't many.

また、切断形状は、使用する刃物か追従可能な範囲で自
由に設定することかでき、したかって設計の自由を拡大
することかできる。
Further, the cutting shape can be freely set within a range that can be followed by the cutting tool used, thus expanding the freedom of design.

このようなことから、硬化後の切断作業か不要となり、
したかって、ルータ−3ならい型等の治工具および粉塵
処理等の設備を不要とすることかできる。
For this reason, cutting work after curing is no longer necessary.
Therefore, it is possible to eliminate the need for jigs and tools such as a profiling mold for the router 3 and equipment such as dust treatment.

さらに、硬化後の作業を減少させることかできるので、
不具合発生す因を削減することができる。
Furthermore, the work required after curing can be reduced.
The causes of defects can be reduced.

次に、他の実施例について説明する。Next, other embodiments will be described.

第5図は開口部を何する板状部品の外形及び開口部の明
断に適用した例であって、マンドレル21の上面22に
、この上面22からドh°へ1ソノリ込まれた側壁23
を形成し、この側壁23を含む溝24もしくは段差部2
5に端面成形用部品26゜27を係合させたものである
。そして、側壁23に沿ってカッターナイフ28′、1
′Jを移動させて積層体29を切断する。
FIG. 5 shows an example of application to the external shape of a plate-like part and the clear cut of the opening, in which a side wall 23 is cut into the upper surface 22 of the mandrel 21 by 1 inch from the upper surface 22 to the
, and a groove 24 or step portion 2 including this side wall 23
5 and end face molding parts 26° and 27 are engaged with each other. Then, along the side wall 23, a cutter knife 28', 1
'J is moved to cut the laminate 29.

第6図は、C断面を有する部品への適用例であって、切
断形状により゛1′板状の端面成形部品3]を使用する
場合である。この場合にも、マンドレル32のド面に沿
ってカッター33を移動させることによって、積層体3
4の切断を行なう。
FIG. 6 shows an example of application to a part having a C cross section, in which a "1" plate-shaped end face molded part 3 is used depending on the cutting shape. Also in this case, by moving the cutter 33 along the do surface of the mandrel 32, the laminate 3
Make the 4th cut.

第7図は、数状部品の外周に余肉を設ける場合の例であ
り、図11符;:i41はマンドレルを示し、符号42
は端面成形用部品を示す。そして、調整シム43により
切断面としての側壁44を45へ移動させて、カッター
46等−Ctl断する。
FIG. 7 shows an example of providing extra thickness on the outer periphery of a numerical part.
indicates a part for end face molding. Then, the side wall 44 serving as the cutting surface is moved to 45 by the adjustment shim 43, and the cutter 46 etc. -Ctl cut.

〔発明の効果〕〔Effect of the invention〕

以上説明]7たように、本発明においては、柔軟な状態
の積層体を9ノ断することかてき、したがってカッター
ナイフル)−の一般的なI−具を使用することかできる
。また、刃物を案内することができるから、切断オI1
1度を向上させることができる。このようなことから、
硬化後の切断作業を必要としない。したがって、余分な
治工具を必要とせす、また粉塵処理等をイ\要とするこ
とができるという効果か得られる。
As explained above], in the present invention, it is possible to cut the laminate in a flexible state into nine cuts, and therefore a general tool such as a cutter knife can be used. In addition, since the blade can be guided, the cutting tool I1
1 degree can be improved. From such a thing,
No cutting work required after curing. Therefore, the effect that extra jigs and tools and dust treatment etc. can be eliminated can be obtained.

4、図面のIRI ’I’な説明 第1図ないし第4図はI断面翼小骨成形型による成形b
″法を順を追って示す1sji曲図、第5図は板状部品
の外形及び開口部の切断に本発明を適用した例を示す断
面図、第6図はC断面を有する部品・\の適用例を小ず
断面図、第7図は板状部品の外周に余肉を設ける場合の
適用例を示す断面図である。
4. IRI 'I' explanation of drawings Figures 1 to 4 are molding b using an I-section wing ossicle mold.
Fig. 5 is a sectional view showing an example of applying the present invention to cutting the outer shape and opening of a plate-shaped part, and Fig. 6 is an application of a part having a C cross section. An example is a small cross-sectional view, and FIG. 7 is a cross-sectional view showing an application example in which extra thickness is provided on the outer periphery of a plate-shaped component.

]トマントレル、12・ンIη、13・伸j壁、]シ1 14 フランジ端面成形用部品、]5・・カウルプレー
ト、16・積層体、]7・・・カッターナイフ、21・
・・マンドレル 25・・段差部、26.27・・・端面成形用部品、2
8・・カッターナイフ、2つ・積層体、31・・端面成
形用部品、32・マンドレル、3B・・カッタ、34・
・積層体、41・・マンドレル、42・端面成形用部品
、43・J,J整シム、44.45・・側壁、46・・
・カッタ
] Tomantrel, 12. N Iη, 13. Extended wall, ] 1 14 Flange end face forming parts, ] 5. Cowl plate, 16. Laminated body, ] 7. Cutter knife, 21.
・・Mandrel 25・・Step part, 26.27・・Parts for end face forming, 2
8. Cutter knife, 2 laminate, 31. End face forming part, 32. Mandrel, 3B. Cutter, 34.
・Laminated body, 41... Mandrel, 42. End face forming parts, 43. J, J straightening shim, 44. 45... Side wall, 46...
・Cutter

Claims (1)

【特許請求の範囲】 1、型面に繊維強化プラスチックを積層し加圧、加熱し
て硬化する複合材の成形方法において、前記型面に、成
形しようとする成形品の外縁側面に沿って型面から切り
下げられた段差側面を有する成形型を準備し、前記型面
に半硬化状態の繊維強化プラスチックを積層し、前記段
差側面に沿って刃物の刃面を移動して、積層体の余肉を
切断し、前記段差側面に当接し、かつ積層体の外縁側面
に沿う当接面を有する当板を装着し、加圧および加熱し
て硬化することを特徴とする複合材の成形方法。 2、前記段差側面は、前記型面に形成された溝の側面で
あり、前記当板は、前記溝に係合していることを特徴と
する請求項1記載の複合材の成形方法。
[Claims] 1. In a composite material molding method in which fiber-reinforced plastic is laminated on a mold surface and cured by applying pressure and heating, a mold is placed on the mold surface along the outer edge side of the molded product to be molded. A mold having a stepped side surface cut down from the surface is prepared, semi-hardened fiber reinforced plastic is laminated on the mold surface, and the blade surface of the cutter is moved along the stepped side surface to remove the excess thickness of the laminate. A method for forming a composite material, comprising: cutting the composite material, attaching a contact plate having a contact surface that contacts the stepped side surface and along the outer edge side surface of the laminate, and curing by applying pressure and heating. 2. The method for molding a composite material according to claim 1, wherein the stepped side surface is a side surface of a groove formed in the mold surface, and the contact plate is engaged with the groove.
JP1003050A 1989-01-10 1989-01-10 Composite material molding method Expired - Fee Related JP2730946B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP1003050A JP2730946B2 (en) 1989-01-10 1989-01-10 Composite material molding method

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP1003050A JP2730946B2 (en) 1989-01-10 1989-01-10 Composite material molding method

Publications (2)

Publication Number Publication Date
JPH02184414A true JPH02184414A (en) 1990-07-18
JP2730946B2 JP2730946B2 (en) 1998-03-25

Family

ID=11546493

Family Applications (1)

Application Number Title Priority Date Filing Date
JP1003050A Expired - Fee Related JP2730946B2 (en) 1989-01-10 1989-01-10 Composite material molding method

Country Status (1)

Country Link
JP (1) JP2730946B2 (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2008012920A (en) * 2006-06-09 2008-01-24 Honda Motor Co Ltd Manufacturing method for fiber-reinforced composite body
CN106696307A (en) * 2017-01-16 2017-05-24 江苏恒神股份有限公司 Manufacturing mould of H beam of composite materials
CN108381946A (en) * 2013-03-15 2018-08-10 罗尔斯·罗伊斯公共有限公司 Composite material laying equipment

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2008012920A (en) * 2006-06-09 2008-01-24 Honda Motor Co Ltd Manufacturing method for fiber-reinforced composite body
CN108381946A (en) * 2013-03-15 2018-08-10 罗尔斯·罗伊斯公共有限公司 Composite material laying equipment
CN106696307A (en) * 2017-01-16 2017-05-24 江苏恒神股份有限公司 Manufacturing mould of H beam of composite materials
CN106696307B (en) * 2017-01-16 2022-09-13 江苏恒神股份有限公司 Manufacturing die for composite material I-beam

Also Published As

Publication number Publication date
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