JPS6212581A - Manufacture of fiber composition material-wound body skin - Google Patents

Manufacture of fiber composition material-wound body skin

Info

Publication number
JPS6212581A
JPS6212581A JP15427686A JP15427686A JPS6212581A JP S6212581 A JPS6212581 A JP S6212581A JP 15427686 A JP15427686 A JP 15427686A JP 15427686 A JP15427686 A JP 15427686A JP S6212581 A JPS6212581 A JP S6212581A
Authority
JP
Japan
Prior art keywords
fiber
winding
thread
wound
backward
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
JP15427686A
Other languages
Japanese (ja)
Other versions
JPH0749351B2 (en
Inventor
レネ・モイレル
フランツ・ドラッヒエンベルク
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.)
Airbus Defence and Space GmbH
Original Assignee
Messerschmitt Bolkow Blohm AG
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 Messerschmitt Bolkow Blohm AG filed Critical Messerschmitt Bolkow Blohm AG
Publication of JPS6212581A publication Critical patent/JPS6212581A/en
Publication of JPH0749351B2 publication Critical patent/JPH0749351B2/en
Anticipated expiration legal-status Critical
Expired - Lifetime 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
    • B29C69/00Combinations of shaping techniques not provided for in a single one of main groups B29C39/00 - B29C67/00, e.g. associations of moulding and joining techniques; Apparatus therefore
    • B29C69/001Combinations of shaping techniques not provided for in a single one of main groups B29C39/00 - B29C67/00, e.g. associations of moulding and joining techniques; Apparatus therefore a shaping technique combined with cutting, e.g. in parts or slices combined with rearranging and joining the cut parts
    • B29C69/002Winding
    • 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
    • B29C53/00Shaping by bending, folding, twisting, straightening or flattening; Apparatus therefor
    • B29C53/56Winding and joining, e.g. winding spirally
    • B29C53/58Winding and joining, e.g. winding spirally helically
    • B29C53/60Winding and joining, e.g. winding spirally helically using internal forming surfaces, e.g. mandrels
    • B29C53/602Winding and joining, e.g. winding spirally helically using internal forming surfaces, e.g. mandrels for tubular articles having closed or nearly closed ends, e.g. vessels, tanks, containers
    • 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
    • B29C53/00Shaping by bending, folding, twisting, straightening or flattening; Apparatus therefor
    • B29C53/56Winding and joining, e.g. winding spirally
    • B29C53/58Winding and joining, e.g. winding spirally helically
    • B29C53/60Winding and joining, e.g. winding spirally helically using internal forming surfaces, e.g. mandrels
    • B29C53/62Winding and joining, e.g. winding spirally helically using internal forming surfaces, e.g. mandrels rotatable about the winding axis
    • B29C53/66Winding and joining, e.g. winding spirally helically using internal forming surfaces, e.g. mandrels rotatable about the winding axis with axially movable winding feed member, e.g. lathe type winding
    • B29C53/665Coordinating the movements of the winding feed member and the mandrel

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Reinforced Plastic Materials (AREA)
  • Processing And Handling Of Plastics And Other Materials For Molding In General (AREA)
  • Nonwoven Fabrics (AREA)
  • Moulding By Coating Moulds (AREA)

Abstract

(57)【要約】本公報は電子出願前の出願データであるた
め要約のデータは記録されません。
(57) [Summary] This bulletin contains application data before electronic filing, so abstract data is not recorded.

Description

【発明の詳細な説明】 本発明は、特許請求の範囲第1項の上位概念に記載の繊
維組成材料−巻体外皮を造るための方法に関する。
DETAILED DESCRIPTION OF THE INVENTION The present invention relates to a method for producing a fibrous composition-wound shell according to the preamble of claim 1.

繊維組成外皮、例えば繊維組成−サンドウィッチ構造体
を、スレッドアイを回転する巻心に対して相対的に往復
運動させて行う連続的な巻付は成形方法により、補強糸
を等しい多いさの度数或いは最高一つだけ異なる度数で
スレッドアイを前進および前進運動させて巻心上に載置
して造ることが知られている。このようにして形成され
た繊維組成外皮は二つの互いに交差して編組みされた糸
組織から成り、これらの糸組織の交差角度は巻付は工程
において選択された補強糸のリード角の二倍はど大きく
、かつ両糸組織の方向では同じ強度の繊維補強関与、即
ち同じ強度挙動と剛性挙動を有している。
Continuous winding of the fiber composition shell, e.g. the fiber composition sandwich structure, by reciprocating the thread eye relative to the rotating core, is carried out using reinforcing threads of equal or greater frequency or It is known to make a thread eye resting on the winding core with forward and forward movements of up to one different degree. The fiber composition skin thus formed consists of two intersectingly braided thread structures, the crossing angle of these thread structures being twice the lead angle of the reinforcing threads selected in the winding process. The fiber reinforcement is large and has the same strength of fiber reinforcement in both thread weave directions, ie the same strength and stiffness behavior.

これに対して、糸結び位置を介して互いに交差されかつ
それぞれ異なる糸密度を有する多数の糸組織から組成さ
れていてかつ主応力方向或いは変形方向を伴う繊維組成
構造体に形成する際荷重に適応しかつ重量が好都合な繊
維分布を達するのに必要とされる繊維組成外皮はたて糸
補強した繊維組成−織物よりも著しく高い機械上のおよ
び経費上の出費をもって、例えば織成方法によって造ら
なければならない。この場合これに加えて、このような
織物が僅かな面積重量の段階でしか、および僅かなたて
糸−よこ柔化率でしか使用し得す、なかんずく高度の軽
量構造様式にまさに必要な網状化されていない、しかし
破断の危険のある特別な繊維種類、即ち特に超モジュー
ルの炭素繊維はこのような繊維に加工できないと言うこ
とが事実が加わる。
On the other hand, when forming a fiber composition structure with a principal stress direction or a deformation direction, the structure is composed of a large number of yarn structures that intersect with each other through the yarn knotting position and have different yarn densities, and has a principal stress direction or a deformation direction. And the fiber composition required to achieve a favorable fiber distribution by weight has to be produced, for example by weaving methods, with significantly higher mechanical and cost outlays than with warp-reinforced fiber compositions - woven fabrics. . In this case, in addition to this, such fabrics can be used only at low areal weight levels and with low warp-weft softening ratios, which is particularly necessary for highly lightweight construction styles. However, there is the added fact that certain fiber types with a risk of breakage cannot be processed into such fibers, namely particularly ultra-modular carbon fibers.

これに対して本発明の課題は、積層体の一定の交差角度
で互いに織成された繊維組織の各々において個別にかつ
無段階に選択可能な糸密度が簡単かつ費用の点で有利な
方法で達せられ、かつ実際にどんな任意の種類の繊維で
も、なかんずく上記の炭素繊維でも問題なく加工するこ
とが可能な繊維組成積層体を造るための方法を造ること
である。
In contrast, the object of the present invention is to provide a thread density that can be individually and steplessly selected in each of the fiber structures interwoven with each other at a constant angle of intersection of the laminate in a simple and cost-effective manner. The object of the present invention is to create a method for producing fiber composition laminates which can be achieved and which in fact can process any arbitrary type of fiber without problems, in particular even the carbon fibers mentioned above.

この課題は本発明によシ特許請求の範囲第1項に記載の
特徴を有する方法によって解決される。
This problem is solved according to the invention by a method having the features of patent claim 1.

本発明により、前進運動および前進運動のためのリード
角を交差角度および糸密度化考慮の下に意図的に違わせ
て予調節することによる連続的なかつ繊維を傷めること
のない巻付は成形方法により僅かな機械上の出費および
経費の支出で繊維組成材料−巻体外皮が得られ、この繊
維組成材料−巻体外皮は所定の交差角度の下に互いに編
組みされた糸組織内での片側におけるより高い繊維補強
関与に対する要求を重量上最適な状態で充足する。所望
の糸密度が達せられるまで大抵スレッドアイの前進運動
および前進運動を何度も行わなければならないので、た
とえスレッドアイが総体的に前進運動を前進運動よりも
頻繁に或いはわずかな頻度で行ったとしても、前進運動
および前進運動の比率は−を基   □準とした違いで
ある。
According to the invention, continuous and non-damaging winding by presetting the forward movement and the lead angle for the forward movement intentionally differently, taking into account the crossing angle and thread density, is a forming method. With little mechanical outlay and expense, a fibrous material-wound shell is obtained, which fibrous material-wound skin is formed on one side in a yarn structure that is interwoven with one another under a predetermined crossing angle. satisfies the demands for higher fiber reinforcement involvement in weight-optimized conditions. Even if the thread eye generally performs forward motions more frequently or less frequently than forward motions, it is often necessary to carry out forward and backward motions of the thread eye many times until the desired thread density is achieved. Even so, the forward motion and the ratio of forward motion are the differences based on - □.

この場合本発明の特に優れた構成にあっては前進運動お
よび前進運動のためのリード角は特許請求の範囲第2項
に記載の方法により極めて簡単に決定され、かつ巻心の
周速度および回転数に対する送り速度の比率は特許請求
の範囲第3項に記載の構成により決定される。
In this case, in a particularly advantageous embodiment of the present invention, the forward movement and the lead angle for the forward movement are determined very simply by the method set forth in claim 2, and the circumferential speed and rotation of the winding core are The ratio of the feed rate to the number is determined by the arrangement according to claim 3.

巻体積層体は特に特許請求の範囲第4項に記載の方法に
よシ裁断され、これにより共通した捻れ様式の繊維組織
の配向変えが達せられる。
The rolled laminate is cut in particular by the method according to claim 4, whereby a reorientation of the fiber structure with a common twist pattern is achieved.

即ち、例えば高い繊維補強関与度を有する繊維組織は巻
体外皮の主応力方向に整向される。巻体積層体もしくは
巻体外皮の糸組織を巻付は成形工程終了後始めて繊維組
成材料の樹脂マトリックスで含浸することは容易に可能
であるが、しかしより以上の方法技術上の簡略化の点で
は、特許請求の範囲第5項に記載の方法により補強糸を
スレッドアイを通過する以前に樹脂で含浸するのが有利
である。極めて軽量な構造様式の点での方法の特別な利
点は、特許請求の範囲第6項【記載の方法により巻体外
皮を超モジュールの炭素系から造ることである。巻体外
皮を極めて高め応力に即応するように構成し、かつ相応
して大きな面積重量を以て造るには、特許請求の範囲第
7項に記載の方法により巻体積層体を特に繰り返される
多層巻付は成形雛形にしたがって巻付は成形を行う。こ
れにより積層体中の補強糸は密な順序で配設されるのみ
ならず上下に重なっても配設される。
That is, for example, a fiber structure with a high fiber reinforcement degree is oriented in the principal stress direction of the winding shell. It is easily possible to impregnate the thread structure of the rolled laminate or the rolled shell with a resin matrix of the fiber composition material only after the winding process has ended, but there are still further technical simplifications. In this case, it is advantageous to impregnate the reinforcing thread with resin before passing through the thread eye by the method according to claim 5. A particular advantage of the method in terms of its extremely lightweight construction is that the winding shell is produced from a supermodular carbon system by the method described in claim 6. In order to make the winding sheath extremely high and stress-responsive and with a correspondingly high areal weight, the winding stack can be produced in particular by repeated multilayer windings by the method according to claim 7. Wrapping and forming are performed according to the forming model. As a result, the reinforcing threads in the laminate are not only arranged in a dense order but also arranged one above the other.

゛以下に添付した図面に図示した実施例につき本発明の
詳細な説明する。
BRIEF DESCRIPTION OF THE DRAWINGS The invention will now be described in detail with reference to embodiments illustrated in the accompanying drawings.

第1図により、交差角度βで互いに編組みされた二つの
繊維組織2,4から成る繊維組成材料−巻体積層体を造
るため、無端の補強糸が交互に相前後して多数回行われ
る前進運動および前進運動で連続して交差角度βの半分
の値に相当するリード角αで、終端側に補強糸の進み方
向を反転させるための端部キャップ(Po1ka−pp
e)8,10を備えた回転する円筒形の巻心6上に、所
望の面積重量が達せられるまで、巻付けられ、その後巻
体積層体は巻体外r3i12(第1b図)内での繊維配
向によって予め与えられる交差線に沿って裁断され、巻
心6から増重される。このようKして形成された巻体外
皮12内にあっては、補強糸の面積重量は同じ割合で繊
維組織2と4に分割されている。即ち、両繊維組織2,
4は同じ繊維密度を有している。
According to FIG. 1, in order to create a laminate of fiber composition material consisting of two fiber structures 2, 4 interwoven with each other at a crossing angle β, endless reinforcing threads are carried out a number of times one after the other in alternation. An end cap (Po1ka-pp
e) onto a rotating cylindrical winding core 6 with 8, 10 until the desired areal weight is reached, the wound laminate is then wound with fibers in the outer winding r3i12 (FIG. 1b). It is cut along the intersection line given in advance by the orientation, and the weight is increased from the winding core 6. In the winding outer skin 12 formed in this manner, the area weight of the reinforcing yarn is divided into fiber structures 2 and 4 at the same ratio. That is, both fiber tissues 2,
4 have the same fiber density.

この実施列の場合、交差角度βは90°であり、即ち、
前進運動および前進運動におけるリード角αは45°で
あり、交差線A−A、B−Bは、巻体外皮12内の繊維
組織2,4が90°10゜の配向を備えるように選択さ
れる。
For this implementation, the crossing angle β is 90°, i.e.
The lead angle α in the forward movement and forward movement is 45°, and the intersecting lines AA, B-B are selected such that the fiber structures 2, 4 in the winding shell 12 have an orientation of 90° 10°. Ru.

本発明による巻付は成形方法を第2図に図示した巻付は
装置をもとに説明する。この巻付け1.装置は、端部キ
ャップ8,10を備えている、回転数nで連続的に回転
する円筒形の巻心6、この巻心6に対して軸平行に前進
運動および前進運動するスレッドアイ14およびこのス
レッドアイの手前に接続されていてかつ含浸ロー218
を備えている含浸槽16とから一般的な様式で構成され
ている。糸ローラ20から引出される補強糸22、例え
ば超モジュールの炭素系は均一な張力で巻心6上に載置
される以前に、含浸ローラに漕って案内されて繊維組成
材料の樹脂マトリックスで含浸される。
The winding and forming method according to the present invention will be explained based on the winding apparatus shown in FIG. This winding 1. The device comprises a cylindrical winding core 6 which rotates continuously at a rotational speed n and is provided with end caps 8, 10, a thread eye 14 which moves forward and forward in axis parallel to this winding core 6, and The impregnated row 218 is connected in front of this thread eye.
The impregnating tank 16 is constructed in a conventional manner. The reinforcing yarn 22, e.g. supermodular carbon-based, drawn out from the yarn roller 20 is guided by impregnation rollers and coated with a resin matrix of fibrous composition material before being placed on the winding core 6 under uniform tension. Impregnated.

スレッドアイ14が交互に相前後して多数回前進運動お
よび前進運動することにより巻心6に、交差角度βで互
いに編組みされる両繊維組織2,4から形成される巻体
積層体く所定の繊維−面積重量が達せられるまで巻付け
が行われる。しかし、同時にこの面積重量は所定の様式
でも両繊維組織2,4上に異なって配分される。
As the thread eyes 14 alternately move forward and backward a number of times, a predetermined winding layered body is formed on the winding core 6 from the two fiber structures 2 and 4 that are interwoven with each other at an intersecting angle β. Winding is carried out until a fiber-area weight of is reached. At the same time, however, this areal weight is distributed differently on the two fiber structures 2, 4 even in a given manner.

即ち、繊維組織2,4の各々に個別的に定まった糸密度
が与えられる。この目的のため、前進運動で巻付は成形
される繊維組織2のためのリード角αV と交差角度β
に対するこのリード角ay  f補完する前進運動で巻
付は成形される繊維組織4のためのリード角αRは、式 (この場合、 X=前進運動で巻付は成形される繊維組織2の前進運動
で巻付は成形される繊維組織4に対する必要とする糸密
度比、 m=スレッドアイ14の前進運動の度数、n=スレッド
アイ14の前進運動の度数。)を満足するように決定さ
れる。
That is, each of the fiber structures 2 and 4 is given an individually determined thread density. For this purpose, in a forward movement the winding is formed with a lead angle αV and a crossing angle β for the fiber structure 2.
This lead angle ay f for the fibrous tissue 4 whose winding is formed with a complementary forward movement is given by the formula (in this case, The winding is determined so as to satisfy the required thread density ratio for the fiber structure 4 to be formed, where m=the number of degrees of forward motion of the thread eye 14, and n=the number of degrees of forward motion of the thread eye 14.

m = n或いはl m −n l = 1とm、n)
Oであるので、 が成シ立ち、 tanα=−ので、 ”V  ”Rx+coaβ (この場合、 TV、R=前進運動もしくは前進運動におけるスレッド
アイ14の送り速度、 ■とnV、R=巻心6の周速度および前進運動度数もし
くは前進運動度数。) が成り立つ。
m = n or l m -n l = 1 and m, n)
Since tanα=-, “V”Rx+coaβ (in this case, TV, R=forward movement or feed rate of thread eye 14 in forward movement, ■ and nV, R=speed of winding core 6 Circumferential velocity and forward motion degree or forward motion degree.) holds true.

交差角度β=900に関して他の簡略式%式% 図示したように繊維組織2の繊維補強関与が繊維組織4
の繊維補強関与の二倍はど大きくする場合、即ちβ=9
0°でx = 2 K I、ようとする場合、αV を
24565°に、そしてα、(=β−αy)f4:61
455°に調節し、円筒形の巻心6の回転数が一定であ
る場合前進運動でのスレッドアイ14の送り速度はそれ
ぞれ前進運動における送り速度より四倍の送り速度に選
択しなければならない。
Regarding the intersection angle β = 900, another simplified formula % formula % As shown in the figure, the involvement of fiber reinforcement in fiber tissue 2 is
When increasing the fiber reinforcement participation by twice as much, i.e. β = 9
If we want x = 2 K I at 0°, then αV to 24565° and α, (=β − αy) f4:61
455° and the rotational speed of the cylindrical winding core 6 is constant, the feed rate of the thread eye 14 in the forward movement must be selected to be four times as great as the feed rate in the forward movement.

このようにして繊維補強部の所望の面積重量Kまで巻付
は成形された巻体積層体(第3a図)は次いで所望の繊
維配向に相当して巻体外皮12に裁断され、この場合第
3図による巻体外FJL12内の交差MA−AとB−B
の場合両繊維組織2,4にとって±45°の繊維配向が
得られ(第3b図参照)、一方繊維組織2.4の糸方向
に対して交差線が平行にもしくは垂直に走っている場合
第30図に図示した巻体外皮12が形成し、この巻体外
F112にあっては繊維組織4は僅かな糸密度をもって
90°の配向を、繊維組織2け二倍程高い繊維補強関与
で0°の配向を有している。
The rolled laminate (FIG. 3a) which has been wound and formed in this way up to the desired areal weight K of the fiber reinforcement is then cut into rolled skins 12 corresponding to the desired fiber orientation, in which case Intersection MA-A and B-B inside FJL12 outside the roll according to Figure 3
A fiber orientation of ±45° is obtained for both fiber structures 2, 4 (see FIG. 3b), whereas if the line of intersection runs parallel or perpendicular to the thread direction of the fiber structures 2.4, The winding outer skin 12 shown in Fig. 30 is formed, and in this winding outer F112, the fiber structure 4 has a 90° orientation with a slight thread density, and a 0° orientation with a fiber reinforcement participation that is twice as high as the fiber structure. It has an orientation of

形された巻体積層体およびこの巻体積層体から裁断され
た巻体外皮の図、 第2図は本発明により巻付は成形方法を説明するための
巻付は装置を著しく概略図示した図、第3a図は本発明
による方法で作られた巻体a図の巻体積層体から異なっ
て裁断された二つの繊維組成材料−巻体外皮の図。
FIG. 2 is a highly schematic diagram of the winding device for explaining the winding and forming method according to the invention; FIG. FIG. 3a is an illustration of two fiber composition material-roll skins cut differently from the roll stack of roll a made by the method according to the invention.

図中符号は、 2.4・・・繊維組織 6 ・・−°・巻心 8.10・−・端部キャップ 12・・・・巻体外皮 14・・−拳スレッドアイ 20・・・・糸ローラThe symbols in the figure are 2.4...Fiber tissue 6...-°・core 8.10・-・End cap 12...roll outer skin 14...-Fist Thread Eye 20... Thread roller

Claims (1)

【特許請求の範囲】 1、少なくとも一本の無端糸を連続的にスレツドアイを
交互に相前後して多数回前進運動および後退運動させて
このスレツドアイに対して相体的に回転する巻心上にこ
の巻心の周速度のスレツドアイの送り速度に対する比率
によつて定まるリード角で巻付けかつこのようにして形
成された巻体積層体を硬化してない状態で巻心から取出
して行う、一方向性で一方の方向に指向している補強糸
から成る第一の繊維組織と一方向性で第二の方向で指向
している補強糸から成る、第一の繊維組織と交差配向し
て編組みされた第二の少なくとも一つの繊維組織から成
る少なくとも一つの糸層から予含浸処理した繊維組成材
料−巻体外皮を造るための方法において、両繊維組織を
、一本或いは多数本の無端糸のリード角がスレツドアイ
の方向変換毎に変え、このリード角を前進運動に関して
は両繊維組織の交差角度と所望の糸密度に依存して定め
、後退運動に関しては上記の決定に対比して交差角度に
相当して異なる値に調節するようにして、異なる糸密度
で巻付け成形することを特徴とする、上記繊維組成材料
−巻体外皮を造るための方法。 2、スレツドアイを同じ度数でおよび/またはより多い
度数で前進運動および後退運動させる際この前進運動お
よび後退運動のためのリード角を以下の式、即ち tanα_V=sinβ/(x+cosβ)とtanα
_R=tan(β−α_V)=sinβ/[(1/x)
+cosβ](この場合、 α_V=前進運動で巻付け成形される繊維組織のための
リード角、 α_R=後退運動で巻付け成形される繊維組織のための
リード角、 β=両繊維組織の交差角度、 x=前進運動で巻付け成形される繊維組 織の後退運動で巻付け成形される繊 維組織に対する糸密度比) が満足されるように選択する、特許請求の範囲第1項に
記載の繊維組成材料−巻体外皮を造るための方法。 3、スレツドアイを同じ度数および/又はより大きな度
数で前進運動および後退運動させる場合、前進運動にお
ける送り速度に対する周速度の後退運動における送り速
度の周速度に対する比率を以下の式、即ち V_V/U_V:V_R/U_R=[(1/x)+co
sβ]/(x+cosβ)(この場合、 V_V_、_R=前進運動および後退運動における繊維
組織の送り速度、 U_V_、_R=前進運動および後退運動における巻心
の周速度、 β=両繊維組織の交差角度、 x=前進運動において巻付け成形される 繊維組織の後退運動において巻付け 成形される繊維組織に対する糸密度 比) を満足するように選択する、特許請求の範囲第1項或い
は第2項に記載の繊維組成材料−巻体外皮を造るための
方法。 4、巻体積層体を巻体外皮内の繊維配向に相当する交差
線で裁断する、特許請求の範囲第1項から第3項までの
いずれか一つに記載の繊維組成材料−巻体外皮を造るた
めの方法。 5、補強糸をこれがスレツドアイを通過する以前に樹脂
で含浸する、特許請求の範囲第1項から第4項までのい
ずれか一つに記載の繊維組成材料−巻体外皮を造るため
の方法。 6、補強糸として超モジュールの炭素系を巻付け成形す
る、特許請求の範囲第1項から第5項までのいずれか一
つに記載の繊維組成材料−巻体外皮を造るための方法。 7、巻体積層体を巻体外皮のより大きな面積重量を得る
ために多層で繰り返される巻付け雛形に従つて巻付け成
形する、特許請求の範囲第1項から第6項までのいずれ
か一つに記載の繊維組成材料−巻体外皮を造るための方
法。
[Claims] 1. At least one endless yarn is continuously moved forward and backward many times by alternating the threaded eyes, so that the threaded yarn is wound on a winding core that rotates relative to the threaded eyes. Unidirectional winding is carried out by winding at a lead angle determined by the ratio of the circumferential speed of the core to the feed speed of the threaded eye, and by taking out the wound laminate thus formed from the core in an uncured state. a first fiber structure consisting of reinforcing yarns oriented in one direction and a first fiber structure consisting of reinforcing yarns unidirectional and oriented in a second direction in a cross-orientation; A method for making a winding shell - a fiber composition material pre-impregnated from at least one yarn layer consisting of at least one second fibrous structure, in which both fibrous structures are combined into a reed of one or more endless threads. The lead angle changes with each change of direction of the thread eye, and this lead angle is determined for the forward movement depending on the crossing angle of both fiber structures and the desired thread density, and for the backward movement corresponds to the crossing angle in contrast to the above determination. A method for producing the above-mentioned fibrous composition material-wound skin, characterized in that the fiber composition is wound and formed with different thread densities so as to be adjusted to different values. 2. When moving the threaded eye forward and backward with the same degree and/or with more degrees, the lead angle for this forward and backward movement is determined by the following formula: tanα_V=sinβ/(x+cosβ) and tanα
_R=tan(β-α_V)=sinβ/[(1/x)
+ cos β] (in this case, α_V = lead angle for the fibrous structure that is wrapped and formed in the forward movement, α_R = lead angle for the fibrous structure that is wrapped and formed in the backward movement, β = intersection angle of both fibrous structures) The fiber composition according to claim 1, which is selected so that the following is satisfied: Materials - Method for constructing the roll shell. 3. When the threaded eye is moved forward and backward at the same degree and/or greater degree, the ratio of the circumferential speed to the feed rate in the forward movement to the feed rate to the circumferential speed in the backward movement is expressed by the following formula: V_V/U_V: V_R/U_R=[(1/x)+co
sβ]/(x+cosβ) (in this case, V_V_, _R = feed rate of the fiber tissue in forward motion and backward motion, U_V_,_R = circumferential speed of the winding core in forward motion and backward motion, β = crossing angle of both fiber structures , x=thread density ratio of the fiber tissue wrapped and formed in the forward motion to the fiber tissue wrapped and formed in the backward motion). Fiber Composition Material - Method for Making a Roll Shell. 4. The fiber composition material according to any one of claims 1 to 3, in which the rolled laminate is cut along a cross line corresponding to the fiber orientation in the rolled outer skin - the rolled outer skin A method for building. 5. A method for making a fibrous composition-wound shell according to any one of claims 1 to 4, characterized in that the reinforcing thread is impregnated with a resin before it passes through the thread eye. 6. A method for making a fibrous composition material-wound shell according to any one of claims 1 to 5, which comprises winding and molding a super-modular carbon-based reinforcing thread. 7. Any one of claims 1 to 6, wherein the rolled laminate is wound and formed according to a winding pattern that is repeated in multiple layers in order to obtain a larger area weight of the rolled body skin. Fiber composition material according to - Method for making a roll skin.
JP61154276A 1985-07-02 1986-07-02 Method for making a fiber composite laminate composed of fiber composite material Expired - Lifetime JPH0749351B2 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE3523570.5 1985-07-02
DE19853523570 DE3523570C1 (en) 1985-07-02 1985-07-02 Process for producing a fibre-composite winding skin

Publications (2)

Publication Number Publication Date
JPS6212581A true JPS6212581A (en) 1987-01-21
JPH0749351B2 JPH0749351B2 (en) 1995-05-31

Family

ID=6274722

Family Applications (1)

Application Number Title Priority Date Filing Date
JP61154276A Expired - Lifetime JPH0749351B2 (en) 1985-07-02 1986-07-02 Method for making a fiber composite laminate composed of fiber composite material

Country Status (3)

Country Link
JP (1) JPH0749351B2 (en)
DE (1) DE3523570C1 (en)
FR (1) FR2584341B1 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2007336779A (en) * 2006-06-19 2007-12-27 Toshiba Corp Electric vehicle drive

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3631975A1 (en) * 1986-09-19 1988-04-07 Eugen Ehs DRYER CONTAINER FOR AN AIR CONDITIONING
DE4107882C2 (en) * 1991-03-12 1994-08-18 Eugen Ehs Method and device for manufacturing pressure vessels and pressure vessels

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS4929903A (en) * 1972-07-20 1974-03-16

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2723705A (en) * 1950-07-21 1955-11-15 Owens Corning Fiberglass Corp Method and apparatus for making reinforced plastic laminates
FR1443872A (en) * 1963-04-11 1966-07-01 Plastrex France Method and device for the manufacture of reinforced synthetic pipes and pipes conforming to those obtained by said method or similar method
JPS5855219A (en) * 1981-09-29 1983-04-01 Mitsubishi Electric Corp Manufacture of fiber-reinforced plastic product

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS4929903A (en) * 1972-07-20 1974-03-16

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2007336779A (en) * 2006-06-19 2007-12-27 Toshiba Corp Electric vehicle drive

Also Published As

Publication number Publication date
FR2584341A1 (en) 1987-01-09
DE3523570C1 (en) 1986-06-26
FR2584341B1 (en) 1988-11-25
JPH0749351B2 (en) 1995-05-31

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