DE102007012608B4 - Method and device for producing a preform for a force flow compatible fiber composite structure - Google Patents

Abstract

A method of manufacturing a preform (42) for a flow-compatible fiber composite structure, comprising the following sequence of steps:
a1) providing a flat sliver (14),
c). Cutting a sliver piece (40, 40 ', 40'') from the flat sliver (14),
e) picking up the fiber band piece (40, 40 ', 40'') at a predetermined picking position by means of a laying device (28),
f) placing the fiber band piece (40, 40 ', 40 ") at a predefined position,
g) fixing the fiber band piece (40, 40 ', 40'') by means of a binder material (38),
wherein steps c) to f) are repeated for placing and fixing further fiber ribbon pieces (40, 40 ', 40 ") at other predefined positions, and wherein steps e) and f) are performed by means of a laying head (52) of the laying device (28) automatically from the at least one pick-up position to a first predefined position for placing a first sliver piece (40) and back to the one or more predetermined pick-up positions to receive a second sliver piece (40 ') and then ...

Description

The The invention relates to a method for producing a preform for a force flow Fiber composite structure. Furthermore, the invention relates to the use of such a process in the production of more power flow Composite structures. After all the invention relates to a device for carrying out the Process.

At the Construction of vehicles of all kinds, especially in the construction of air and Spacecraft, but There are always other industries, such as mechanical engineering more the need after resilient, yet lightweight and possible inexpensive Materials. In particular fiber composite materials offer an outstanding lightweight construction potential. The principle is that in particular high-strength and rigid Fibers are embedded in a matrix according to stress, which Components with outstanding mechanical properties arise, those with previous techniques typically 25% lighter than aluminum and 50% lighter than steel structures with comparable performance are. A disadvantage lies in the high material costs and in particular in the elaborate, Mostly manual production.

It There is therefore a desire to create an automated production, which allows a mechanical arrangement of the fibers in the room. These days, fiber-reinforced plastics are becoming increasingly popular when using oriented long fibers, for example carbon fibers, by a very high strength and rigidity at low weight. Furthermore feature she over a high weight-specific energy absorption capacity and good Fatigue properties.

This is achieved so far by the fact that continuous fibers load requirements in a matrix (for example epoxy resin) are inserted. Depending on the direction of reinforcement can anisotropic materials are created, the directional mechanical Have properties. For example, one material may be different in length Have properties as in width. In modern air and Spacecraft already has a high percentage today the structural weight of fiber-reinforced plastics.

The most important manufacturing process is currently based on the so-called Prepreg technology. in this connection become the reinforcing fibers arranged in parallel (unidirectionally) and embedded in a matrix. After a curing step arise semi-finished products as thin Able to be wound up on a roll. When processing will be these layers tailored to the component contour and predominantly by hand layer for Layer laminated in a tool. Subsequently, the curing takes place under Pressure and temperature in an autoclave. The resulting components have a very high lightweight construction potential, the manufacturing is but very expensive and expensive. For several decades employed the material researchers Therefore, the question of how fibers are stressful, three - dimensional and as possible from its contour close to the final Contour of the component arranged in an automated process become.

In order to produce fiber composite structures with fibers arranged in accordance with the force flow, so-called preforms have previously been produced in addition to prepregs for selected applications as semi-finished textile products. These are usually two- or three-dimensional structures with load-oriented fiber alignment. So far, for this purpose, by means of textile technology continuous fibers laid in the loading direction and by means of textile technology, usually by sewing, knitting or the like, prefixed. Examples of apparatus and methods for making such preforms can be found in the DE 30 03 666 A1 , of the DE 196 24 912 A1 of the DE 197 26 831 A1 as well as the DE 100 05 202 A1 ,

From the US 4,952,366 A a comparable method for producing a preform and a composite structure is known therefrom, wherein a prepreg is reinforced with an endless fiber for producing the preform. The continuous fiber is first fixed to the prepreg during its transport with a vacuum suction. A transport of fiber webs on a conveyor belt such that these fiber webs are sucked by vacuum, is thus known from this prior art.

From the DE 30 48 367 C1 For example, a method and apparatus for spreading a fiber strand are known. In this case, a convex surface penetrates into the fiber strand and fanning it as wide as possible.

From the CH 450 239 A Also, a method and an apparatus for spreading a fiber strand are known. Here, the fiber strand is guided meandering over solid strips. A guide surface of the strip is curved arcuately convex.

From the US 2002/0123819 A1 For example, a system for automatically controlling the spreading of a textile layer is known, which textile layer is formed from a plurality of fiber strands. This system has a measuring device for measuring the positions of the longitudinal edges of each fiber strand, a width adjusting device for individually adjusting the width of each fiber strand, a position adjusting device for adjusting the position of each Rope and a control device for controlling the Aufspreizvorganges in the way that the textile layer has a predetermined width and position. The fiber strands are pulled over curved rods.

From the DE 695 00 513 T2 is a segmented fiber laying head for laying and pressing fiber strands to a preform known. Due to the segmentation of the fiber lay head is elastic, so that the contact forces are better adapted to irregular shapes. The laying head has a pressure roller, by means of which individual long fiber strands can be pressed against the preform. To form the segmented fiber laying head, this pressure roller is formed of many individual disks. A total of 16 individual fiber strands are guided over fiber strand guides to the fiber head.

From the EP 0 491 353 A1 For example, a multi-axis fiber applicator machine having a laying head on a robot arm is known. This laying head contains a pressure roller, can be compacted and pressed by means of fiber strands. The laying head rovings into a tape and places the tape on a rotatably mounted preform. The rovings are previously impregnated with resin. The individual elements are temperature controlled to match the tackiness of the resin to the particular processing step. In particular, the compaction roller can be heated to increase the tackiness during pressing. Again, the rovings are guided via fiber guides directly from supply spools to the laying head.

From the FR 2 882 681 A1 Also, a fiber applicator machine for making fiber reinforced composite structures is known. This has a laying head for attaching fiber strands. The laying head also has a loading roller for laying the fibers on a preform. Further, the laying head, which is movably attached to the end of a robot arm, is provided with an applicator for applying resin to each fiber just before laying. This can be applied as a binding material in the head, for example, a thermoplastic. A cutter is also provided in the head for cutting the fiber strands into desired lengths. This cutting device is upstream of the device for applying resin. A transport of fiber strands from the cutting device to the Auflegerolle done with air. In addition, a cooling device is provided for cooling the fiber strands contacting the lay-up roller to adjust the stickiness. In the resin applicator, heaters may be provided to adjust the viscosity of the resin for metering and application. To the laying head, a plurality of fiber strands, which are placed side by side to form a sliver, supplied. For this purpose, there is a transport device through which the endless fiber strands are guided by supply spools up to the laying head.

From the DE 103 01 646 A1 is a thread or fiber fabric and a manufacturing method thereof known. In this case, individual strand pieces of a fiber strand material are stored stress-free. This is done by means of a plurality of combined laying and separating devices, which in addition to the laying function for laying the individual fiber strand also have a separating function for separating the fiber strand piece. The laying and separating device is tubular and can have a certain Aufspreizfunktion in which a originally provided with a round cross-section fiber strand is brought into a flatter, more rectangular cross-section. The filing is usually done with parallel adjacent strand pieces. The fixation of each deposited fiber strand pieces to the ground can be done by means of clamping means, which cause further spreading, or by means of gluing.

however The known methods for producing preforms are complicated in the application and the process technology. Especially with such Components where curved Power flux lines with varying density are to be expected with the previously known methods the preparation of a corresponding Not suitable for flow-oriented components. In particular, the Fibers are not arbitrarily oriented along defined curved paths, and the fiber content leaves do not vary locally.

It is accordingly Object of the invention, a method and an apparatus for producing textile semi-finished products for to create power flow oriented fiber composite structures, where the fibers are easier and better adaptable to complicated Kraftflussverläufe are. In particular, a simpler manufacturing process for a power flow is appropriate designed component allows in which fibers along arbitrarily defined curved paths are orientable and the fiber content is locally variable.

These The task is accomplished by a process for the production of preforms for power flow designed fiber composite structures with the steps of the appended claim 1 and a device for carrying out such a manufacturing method solved with the features of claim 22. An advantageous use the manufacturing process is the subject of the independent claim 21st

advantageous Embodiments of the invention are the subject of the dependent claims.

at the method according to the invention let yourself Produce a preform by first a fiber filament bundle, preferably a roving, spread flat. From this spread fiber filament bundle is then a Fa band piece, in the following description also called patch, preferably with predefined length, cut off. Subsequently becomes the sliver piece taken by means of a laying device and at a predefined Position placed. There is the sliver piece by means of a binder material fixed. The cutting, laying and fixing of fiber band pieces is repeated, wherein the sliver pieces at different predefined Positions are placed and fixed. This is preferably done in such a way that from the several to each other and / or to any further Components of the preform fixed patches the desired preform is formed with appropriate flow-oriented fiber orientation. It leaves For example, this is also an area of a conventionally produced Reinforce preforms in a targeted manner, For example, at particularly heavily loaded patches power flow be filed.

The Invention, which are also called fiber patch preforming technology can, made possible by a special laying process the positionally accurate application of short fiber pieces (Patches). About the Orientation and number of fiber pieces can be the required properties the preform are met.

A Orientation also along stronger curved Webs is made possible by cutting into short pieces of fiber. Investigations have shown that despite the use of short pieces of fiber instead of continuous fiber structures nevertheless - in particular due to the exact orientation and better customizability - very high Strength values are achievable, compared to the purely textile preforming process a substantial simplification of the laying process is possible.

at the method according to the invention can through the storage of splayed, short cut pieces of fiber optimized for flow Preforms are produced. In preferred embodiments, cuts a fiber cutting plant specially prefabricated, binded slivers in short pieces and passes this to a vacuum conveyor. There are the sliver pieces isolated and transported to the laying device. The handover the sliver pieces To a laying head of the Le gevorrichtung preferably takes place flying over a Combination of suction modules and blow-off modules. In a preferred embodiment a heater is provided on the laying head, which the sliver piece during the Heats up transport to the deposit and thereby activates the binder. The laying head presses the sliver piece to the predefined position and solve then preferably with a blow-off. The laying head returns then back to starting position.

The Technology according to the invention and / or of their preferred embodiments allows the fully automatic Production of complex fiber preforms. Parameters such as fiber content, fiber orientation and curve radii can be varied widely.

Prefers The binder material for fixing the sliver piece on the fiber filaments applied, wherein the binder material is preferably a thermally activatable binder material, for example a thermoplastic, is. Process-technically simple realize this when the binder material in the form of powder is present and applied to the Faserfilamente, and there by a short warming adheres. Although possible is the binder material during transport between cutting and placing, it has proven to be easier to implement as a process technology if the binder material previously applied to the Faserfilamente becomes. A good distribution with easy attachment let yourself reach when the binder material between the spreading and the cutting on the spread fiber filament bundle applied becomes.

Around is also able to train complicated three-dimensional designs is more preferably that when placing the sliver piece on a partial area a mold surface for the Preform is pressed. This leaves preferably achieve that a laying temple with a elastic pressing surface is used on the laying head.

ever shorter the sliver pieces or patches are cut, the smaller radii of curvature can be achieved by different orientation of the fiber direction reproduce sliver pieces stored one behind the other. thats why preferably that for forming the sliver piece each a piece of less cut off as about 20 cm, in particular less than about 10 cm becomes. Become the fiber pieces very short, then there are higher requirements to the devices for handling the fiber band pieces, in particular to a cutting device with a correspondingly shorter distance preferably to cut exactly defined, as well as to the laying device, then correspondingly more sliver pieces for a given area of Must relocate Preform. Therefore, the lower value for the length of the Sliver pieces about 10 mm preferred. Depending on the size of the component to be manufactured can these sizes vary accordingly.

A laying head of the laying device is invented According to the invention - preferably automatically - so controlled that it is between at least one or more receiving positions, where the individual sliver pieces are received and the respectively for the individual sliver pieces predetermined positions where the sliver pieces are placed, moved back and forth.

Around the sliver pieces or patches after trimming or with a sufficiently large distance provided to each other so that they are safe one by one from the laying device in succession can be taken If transport by means of a transport device is preferred, the greater transport speed as the conveying speed of the spread fiber filament bundle to a cutting device.

Around the sliver pieces It is further preferred that the individual patches be positioned precisely on the transport device and / or the laying device, in particular held on a laying head thereof. This is preferred with pneumatic forces, in particular by means of suction and blowing, feasible. The Holding by pneumatic suction has the advantage that the individual slivers, which are spread apart, with individual filaments preferably already are pre-fixed by binder material, lie flat without distortions can. Due to the flat spread structure of the sliver piece is clinging easily possible. This would be in particular in knitted or other prefabricated fiber fabrics or Fasergelegen according to the prior art, not the case because these because of their dimensions and because of their air permeability by suction not reliable can be fixed.

When filament bundles, which is spread to provide the starting material is preferably a roving, in particular a carbon roving used.

The Sliver pieces or patches are laid, for example, so that they are on edge areas partially overlap, so that a fixation of the sliver pieces can be done together. On the other hand, the overlap adjacent sliver pieces unwanted from the aspect, that superimposed fibers of adjacent sliver pieces to thickenings to lead can, which impair the strength can. If you cut the patches or slivers along of arcuate Cutting lines, in particular along arcuate cutting lines performs, then let yourself at one end of each sliver piece a concave edge portion and at another end of the sliver piece a complementary convex Edge area received. The slivers can then work with theirs accordingly arc curved Cutting edges are strung together juxtaposed, with overlaps or gaps be minimized. Especially with a circular arc-shaped cutting edge can while the sliver pieces close together with different fiber orientations to each other be oriented without causing thickening or overlapping.

A Fixation of the fiber band pieces at its predetermined position and in its predetermined orientation in the preform, for example, on the left and right adjacent Sliver pieces or Based on an offset applied further layer of slivers, wherein the superposed fiber band piece layers by means of the binding material be fixed, or in particular in the event that the fiber patch technology for areawise reinforcement of preforms is used on other components of the preform, For example, on a conventional fiber fabric, be achieved.

With the method according to the invention let yourself thus a preform in a kind of patchwork laying arrangement under adaptation the number and orientation of each patch.

embodiments The invention will be explained in more detail with reference to the drawings shown. In this shows:

1 a schematic overview of an apparatus for producing a preform for the purpose of producing kraftflussgerechter fiber composite structures;

1a a schematic representation of an alternative embodiment of the device of 1 at a dividing plane indicated by a dot-dash line;

2 a schematic representation of a device according to 1 usable unrolling device for unwinding in accordance with the device 1 processable fiber filament bundle;

3 a schematic perspective view of a in the unwinding of 2 usable position sensor and a graph of its characteristic;

4 a perspective view of a known spreading device for explaining the principle of action in accordance with the device 1 used spreading of a fiber filament bundle;

5 a perspective schematic Representation of the device of 1 usable spreading device;

6a a schematic side view of a device in the 1 usable loosening device;

6b a schematic representation of the principle of action of the loosening of 6a ;

7 a schematic side view of a device in the 1 usable binding device;

8th a schematic side view of one used in an embodiment of a device for producing a preform combination of cutting device and laying device;

9 / 10 schematic representations of the principle of action of the cutting device of 8th ;

11 a schematic representation of predetermined paths for depositing fibers through one of the devices according to 1 or 8th ;

12 a series of through the device according to 1 discarded sliver piece;

13 a schematic representation of one with one of the devices according to 1 or 8th producible preform;

14 a schematic cross-sectional view through a laying device of 8th or 1 usable laying head;

15 a bottom view of the laying head of 14 and;

16 a more detailed schematic perspective view of the laying device 8th ,

In 1 is a total with 10 designated preform manufacturing device shown in the overview. With this preform manufacturing device, a complicated textile semifinished product can be produced in a simple manner with fiber filaments running in accordance with the flow of force for the production of fiber composite structures even with a complicated construction of the semifinished product. Such semi-finished textile products are called preforms. The production of these preforms takes place in the device according to 1 from individual short fiber pieces fixed by means of binder material, which have been previously cut from a specially pre-processed fiber filament strand or sliver. The preform manufacturing device can thus be in a processing group 12 for the preparation of the sliver 14 and into a cutting and laying group 16 for cutting fiber ribbon pieces and laying them divide. With a dash-dotted line is the possible separation 15 between these groups 12 and 16 indicated.

1 shows a first embodiment of such a cutting and laying group 16 ; A second embodiment of such a cutting and laying group 16 is in 8th shown.

First, based on the 1 the overall structure and the mode of action of the preform manufacturing device 10 explained, which then explained with reference to the other figures whose individual modules.

How out 1 can be seen, the preform manufacturing device 10 a rolling device 18 , a spreading device 20 , a binding device 22 , a cutting device 24 , a transport device 26 , a laying device 28 as well as a preform 30 on. These individual devices 18 . 20 . 22 . 24 . 26 . 28 and 30 are each self-negotiable and usable without the other Vorrichtun conditions to fulfill their purposes. The present disclosure therefore also encompasses the respective devices 12 . 16 . 18 . 20 . 22 . 24 . 26 . 28 . 30 each individually and alone.

The unwinding device 18 serves to provide a Faserfilamentstranges, such as a roving 32 , The unwinding device 18 is, as will be explained in more detail below, designed such that a twist-free rolling of the roving 32 is possible. For the production of carbon fiber reinforced (CFRP) components, a carbon roving is used in the illustrated embodiment.

The spreading device 20 serves for the widest possible spreading of the individual filaments of the roving 32 , so as flat as possible sliver 14 from as few layers of adjacent individual filaments to provide. For this purpose, the spreading device 20 , as will be explained in more detail below, a spreader 34 and a loosening device 36 on.

The binding device 22 serves to filaments of the sliver 14 and / or individual sliver pieces thereof with a binder material 38 to provide, which serves to fix the sliver pieces in the preform. In the in 1 illustrated embodiment, the binding device 22 Part of the processing group 12 and thus becomes the provision of the spread sliver 14 with binder material 38 used. In non-illustrated embodiments of the preform manufacturing device 10 can additionally or alternatively a binding device 22 the cutting and laying group 16 then assign the already cut fiber pieces with binder material 38 to provide.

The cutting device 24 is for cutting pieces of defined length from the sliver 14 (Fiber pieces) formed. The individual sliver pieces are referred to as patches below 40 . 40 ' . 40 '' designated.

The transport device 26 is used to separate the patches 40 and for transporting the same to the laying device 28 ,

The laying device 28 is designed to be single patches 40 and to predefined positions, here at the preform 30 can place. The preform 30 serves to the preform 42 to give a given three-dimensional surface design.

The preform manufacturing device 10 also has one here several controls 44a . 44b having a control device 44 on which the individual devices 12 . 18 . 20 . 22 . 26 . 30 so controls, that in the manner of a patchwork blanket or with the individual patches 40 the preform 42 is formed.

With the preform manufacturing device 10 Thus, the following manufacturing method for producing a preform can be achieved 42 automatically carry out a power flow-compatible fiber composite structure:
First, one in the form of roving 32 present Faserfilamentbündel spread and with the in the present embodiment, thermally activated ble binder material 38 Mistake. The so-provided binded sliver 14 is then inserted into the pieces of defined length - patches 40 - cut. The patches 40 are isolated and to the laying device 28 transported. The laying device 28 places every patch 40 at a respectively predefined position 46 at the preform 30 and squeezes the patch 40 on the preform 30 on.

With the preform manufacturing device 10 Thus, a fiber patch preforming technology can be carried out, which enables the positionally accurate application of short pieces of fiber through a special laying process. The required properties of the preform can be determined by the orientation and number of fiber pieces 42 be fulfilled. As a result, fibers can be oriented along defined curved paths; and the fiber content can vary locally.

Through the storage of splayed, short cut slivers - patches 40 - can power flow optimized preforms 42 getting produced. A fiber cutter 48 cuts the specially prefabricated, bonded slivers 14 in short pieces, and passes them to a vacuum conveyor 50 the transport device 26 ,

The handover of the patches 40 from the vacuum conveyor 50 to a laying head 52 the laying device 28 takes place over a combination of suction and blow-off modules. The laying head 52 heats the patch 40 during transport to the deposit location and thereby activates the binding material 38 , The laying head 52 squeezes the patch 40 to the predefined position and then dissolves with a blow-off pulse. The laying head 52 then returns to the starting position.

These Technology allows the fully automatic production of complex Fiber preforms. parameter like fiber content, fiber orientation and curve radii can be largely be varied.

In the embodiments shown here are for producing the preforms 42 spread carbon fibers used instead of textile semi-finished products. The length of the fibers is very short (a few centimeters) compared to prefabricated fabrics using long fibers. By a special positioning of the short fibers - in the patches 40 - Similar high mechanical characteristics can be achieved as with long fiber composites.

The Short fibers can be placed relatively accurately along complex power flow paths. at previously used for the production of such preforms textile Can cut only preferred orientations are set. This can be done with The technology presented here represents extreme geometrical shapes become. The manufacturing process is fully automated and it can thickness variations within a preform and / or altered Fiber volume contents are obtained.

In the in 1 illustrated embodiment of the preform manufacturing device 10 is in the cutting and laying group 16 as a fiber cutter 48 a laser 54 used, the processor controlled exactly relative to the sliver 14 is movable. Next is in 1 as a laying mechanism 184 for movement of the laying head 52, a robot arm indicated. The preform 30 is exact and defines relative to this movable and rotatable to various complex 3D structures of preforms 42 easy to generate.

In summary, a basic idea of the embodiment of fiber patch preforming technology presented here is carbon fiber rovings 32 Spread as wide as possible, coat with binder powder and with a new cutting technique in defined long pieces, so-called patches 40 to cut. These patches 40 become then from the special laying device 28 taken, placed at a predefined position and using the binder material 38 fixed. This makes it possible to produce a wide variety of component geometries and fiber architectures.

In the manufacturing process shown here, spread fibers are used. Fiber spreading provides a basis for avoiding localized accumulation of fiber ends within the composite later, as these may cause stress concentrations and, in the worst case scenario, lead to component failure. Spreading reduces the thickness of the roving 32 , This allows more continuous fibers to reach the sphere of influence of a fiber end and compensate for voltage peaks. Furthermore, when overlapping, the step is at the cut end of a roving 32 reduced. Such a step could be up to 250 microns high in an unspread roving and would result in the deflection of the overlying carbon fiber from the direction of force flow. In addition, there could be a resin-rich zone there, which has a negative effect on the strength of the material.

In order to perform a spreading as effectively as possible, should be twists of the roving 32 be avoided, since transverse filaments could constrict a splayed Ro ving again. The tension within the roving 32 should be constant in the spread state, since voltage spreads could influence the spread width and spread quality.

The unwinding device 18 , which in the following on the basis of 2 is explained in more detail, serves a roving 32 from a supply reel 56 to be able to deliver without twisting and the pendulum movement of the roving 32 when deducted from the supply spool 56 compensate. The unwinding device 18 has a movable storage for this purpose 58 the supply reel 56 such that the supply spool 56 according to the location of the area of the roving being rolled up 32 moved so that the unwinding position remains as constant as possible.

For this purpose, the storage 58 one along a linear guide 60 stored sled 62 on. The sled 62 is by means of stepper motors and in the example shown here by means of a drive spindle in the direction of the axis of rotation of the supply reel 56 movable. The movement of the sled 62 is from a motor 66 driven with integrated control. A sensor 68 watch the current position 70 of the blank 32 and thus controls the rotational movement of the engine 66 ,

As a sensor 68 serves for this purpose a spatially resolving photodiode 72 , in the 3 is shown together with its characteristic. A diode array of the photodiode 72 registers the shadow of the roving 32 and outputs the position via an amplifier circuit (not explicitly shown) as an analog signal. The center of a shadow corresponds to a specific voltage value depending on location. The analog signal is sent as a bipolar voltage signal to the motor control 66 passed, where 0 volts corresponds to the center of the sensor. In addition, the sensor 68 with an IR LED headlamp at a certain frequency, for example, 10 KHz, slit to prevent interference of the measurement signal by ambient light. This sensor 68 is based on the special requirements of a roving's location 32 on the supply reel 56 compensating unrolling optimized and allows even more settings, such as center shift and bending adjustment. The combination of a spatially resolving photodiode 72 and controlled servomotor 66 has the advantage that the counter-movement depending on the current movement speed of the roving 32 is triggered. At slow take-off speeds, relatively slow compensation movements are triggered, while high take-off speeds trigger correspondingly rapid counter-movements. This will be the roving 32 largely free of vibration as a flat ribbon 74 unrolled. At the end of the unwinding device 18 the roving revolves around 32 in an S-shaped motion two rolls 75 , here two waisted Edelstahlröllchen, which additionally calm down last vibrations. The unwinding device 18 can be different than in 1 shown also operate completely autonomous from the other modules and basically requires only one power supply, such as a power connection.

The roving 32 goes through after the unwinding device 18 a spreading distance in the spreading device 20 ,

The spreading device 20 has, as already mentioned above, first the spreader 34 on that in more detail 5 is shown and their principle of action first on the basis of 4 is explained.

4 shows a schematic diagram of an already from the DE 715 801 C known old mechanical spreading principle. Here goes through a fiber strand 14 one bent bar in turn 76 and then a straight rod 78 , The combination of a straight and a curved rod ensures in 4 illustrated, basically known radius spreaders that the tensile force acting on the fiber is redirected. It now also acts a force that presses the fiber on the curved rod. At the highest point of the deflection, the highest force acts on the filaments. With increasing distance from this point, the power is reduced. The In other words, filaments can avoid the strain of moving outward on the curved bar. However, it depends on the tensile force on the fiber, the friction between the fiber and the rod, the position of the rods to each other and from the bending of the rod, as the spreader result looks like. In extreme bending, the difference in the forces acting between the highest point and an outer position is so great that the surface friction of the rod no longer plays a role. The filaments will abruptly move outwards, ie the roving 32 would slip or split. If the bend is too small, then the spread ratio is too low.

Because of that, the in 4 illustrated spreaders for the industrial processing of rovings 32 not suitable for reprocessing for preform production on an industrial scale. In particular, errors would be in roving 32 , such as twists, crevices or folds lead to slipping or splitting in the spread material.

In the 5 Spreader shown 34 solves problems with the material quality of rovings or other aufzuspreizenden fiber filament bundles by the roving 32 or the fiber filament bundle is placed again and again on at least one convexly curved spreading edge. For this purpose, the spreader 34 at least one convexly curved spreading edge 80 on, with at least one directional component perpendicular to the longitudinal extent of the roving 32 or the other fiber filament bundle relative to this moves so that this on the convex arcuate spreading edge 80 is applied under tension and then again with at least one directional component perpendicular to the roving 32 or the fiber filament bundle moved away, so that this of the spreading edge 80 solves.

The at least one spreading edge 80 is in a practical embodiment of a radial projection 82 on a rotary shaft 84 educated.

In the preferred embodiment according to the in 5 illustrated embodiment, at least two edges, of which at least one convexly bent spreading edge 80 is formed, from opposite directions on the roving 32 or the fiber filament bundle to move. In the embodiment, for this purpose, two rotary shafts 84 . 86 with radial projections 82 provided, with the rotary shafts 84 . 86 rotate in opposite directions.

In addition to first radial projections 82 , at which convexly bent spreading edges 80 are formed, in a preferred embodiment, also second radial projections 88 provided, which with rectilinear edges 90 leak. As a result, a spreading device is provided in which at least one convexly curved spreading edge 80 and at least one straight edge 90 from opposite directions on the roving 32 or the filament bundle can move until the roving 32 or the filament bundle similar to the one in 4 shown way between the edges 80 . 90 is spread. The edges 80 . 90 are also to relieve the roving 32 or the fiber filament bundle traceable back in the opposite direction.

This is particularly simple in the embodiment according to 5 realized in that at the opposite, here by means of a gear transmission 92 , driven rotary shafts 84 . 86 several, the radial projections 82 . 88 forming wings 94 are configured, which extend substantially in the axial direction and at the radially outermost regions of the edges 80 or 90 are formed. It follows on a wing 94 with the straight edge 90 in the circumferential direction a wing with the convex radially outwardly bent spreading edge 80 and then another wing 94 with a straight edge 90 etc

In another embodiment, the edges of all wings 94 as a convex radially outwardly bent spreading edges 80 designed. Due to the arrangement of oppositely moving movement organs, in the embodiment, the two rotary shafts 84 . 86 , the fibers are each between two oppositely bent spreading edges 80 spread.

In this way is the spreader 34 formed as a wing spreader, so to speak, for a renewed edition of the roving 32 on spreading edges 80 provides. In addition, a sizing on the roving 32 or the fiber filament bundle broken by the mutual bending, and the filaments 100 can move independently.

In the spreading device 20 follows the spreader designed as a wing spreader 34 in the conveying direction of the roving 32 continue the loosening device 36 , which is designed in the embodiment presented here as a suction chamber according to the so-called Fukui principle. The suction chamber 96 can be of the kind that they are in US 6 032 342 A is described. The loosened and pre-spread roving 32 is characterized by a strong laminar air flow 98 in the suction chamber 96 drawn. The individual filaments 100 are flowed around by air and can relatively easily slide over each other. Furthermore, the suction chamber 96 slight fluctuations in the tension of the roving 32 ausglei chen.

In the manufacture of plastic fibers, the filament bundles are often guided freely and passed through eyelets. This can be parts of the filaments 100 rotate around the rest of the bundle and cause roving constrictions as early as the manufacturing process. After being wound on a roving bobbin, these defects are barely visible at first because the filament bundle is pulled flat. After the loosening of the filament bundles in the spreader 34 However, transverse roving parts are clearly visible. This effect can cause gaps and shifts in roving 32 lead, which influence the spread quality negatively.

In order to achieve the most homogeneous spreading possible, a multistage spreading is provided in a not explicitly illustrated embodiment of the invention, in which the spreading ratio is increased in stages. For this purpose, first a first spreading device 34 and a first loosening device 36 for spreading the roving 32 to a first width dimension, for example to a value between 8 mm and 16 mm. This is followed by another stage with another spreader 34 and another loosening device 36 with larger dimensions than the first spreader and the first loosening device, so as to perform a spread to a greater width, for example a value between 20 mm and 35 mm.

After that lies the roving 32 as a broad thin band, the sliver 14 , in front.

In the further course of this sliver 14 still with a small amount of binder material 38 equipped.

Theoretically, with a perfectly splayed, 30 mm wide 12k roving, only three filaments lie on top of each other. This was a diameter of the filaments 100 of 7 μm and a highest packing density. In reality, a roving indicates 32 However, always spreading errors that can sometimes lead to thicker areas and thus to a higher number of filament ends.

The oversight of the roving thus spread 32 with binder material 38 will be in the in 7 Binding device shown in principle 22 carried out. The binding device 22 is formed by the basic principle according to the form of a powder spreader, as he, for example, in the US Pat. No. 3,518,810 , of the US 2 489 846 A , of the US 2 394 657 A , of the US 2 057 538 A or the US 2 613 633 A is described. He has a funnel 102 , at whose output one with radial elevations 104 provided roller 106 passes.

The roller 106 is in the illustrated embodiment, a knurled steel roller, which takes over the powder transport with its rough surface. This roller 106 in turn is from a spreading brush 108 edited, which is the powdered binder material 38 from the roller 106 removed and on the passing underneath sliver 14 scatters.

Between the sliver 14 and the application mechanism, a voltage U may be applied, so that the powder, as in a powder coating, electrostatically to the sliver 14 invests.

The transport roller 106 as well as the spreading brush 108 are by two separate electric motors 110 and 112 driven in order to set the scattering parameters as freely as possible. The control takes place via a control device 114 , which is part of the control device 44 can be.

To prevent the powder from blocking at bottlenecks and jamming machine parts, the funnel is used 102 not at the rest of the binding device 22 firmly fixed, but on a holder 116 held, the compensatory movements allows. An advantage of the owner 116 is in the process of that funnel 102 can swing during operation and the powder is automatically shaken down. The powder is applied in precisely metered quantity to the surface of the rovings passing below it at a defined speed, for example in the range of 3 to 6 m / min 32 sprinkled. Excess powder falls on the roving 32 passed into a collection container (not shown) and can later be reintroduced into the process.

Measurements have shown that the scattered amount of binder material almost linearly from the rotational speed of the roller 106 depends.

The binding device 22 also has a heating device 118 on to the powder particles of the melting at heating temperatures binder material 38 to the surface of the filaments 100 to fix.

In the illustrated embodiment, the heater 118 an approx. 100 mm to 500 mm long heating section. The preferred embodiment of the heater 118 is with radiant heaters, here with infrared radiant heaters 120 fitted. The heating power of the heater 118 can by the control device 114 be set exactly.

The Binder particles are easily melted and bind to the Fiber surface.

After that - like this in 1a is indicated - the finished sliver 14 on a special one film reel 121 be rolled up and stored for later use.

At the in 1 illustrated embodiment, the so specially prefabricated sliver 14 fed to the cutting device, where it enters the patches 40 . 40 '; 40 '' is divided and then by means of the laying device 28 is relocated.

1a shows a version with separate groups 12 . 16 using the film reels 121 as an example of an intermediate storage. The groups 12 . 16 could also be at separate production sites.

In 8th is a second embodiment of the cutting and laying group 16 shown in more detail. In this embodiment according to 8th has the cutting device 24 a fiber cutter 122 with a knife device 124 and a counter roll 126 and with at least one or, as shown here, a plurality of conveyor rollers 128 on.

The knife device 124 can be adjusted depending on the rotational speed of the counter roll 126 and / or the conveyor rollers 128 for cutting off patches 40 operate with a defined length.

In particular, the knife device 124 a (not shown) coupling mechanism, which drives the knife device 124 with a drive for the rollers 126 . 128 couples.

The knife device 124 is in the example shown with a knife roller 130 provided as a radial projection at least one, here several knife edges 132 having. The knife roller 130 is in the illustrated embodiment, further by the coupling device not shown so to the drive of the backing roll 126 coupled, that the knife edges 132 at the same peripheral speed as the surface of the backing roll 126 move.

In the 8th and in greater detail in 9 The cutting device shown therefore has a coupling cutter 134 on, where two pairs of feed rollers 128 and a rubberized counter roll 126 by means of a motor, not shown, via a central positive gear, for example via a toothed belt (not shown) driven. The conveyor rollers 128 draw an endless fiber ribbon - here in particular the spread sliver 14 - and guide it over the rotating counter roll at the same speed 126 ,

Over the counter roll 126 stands a knife bar 136 in waiting position. If a cut is to be made, an electromagnetic clutch couples the cutter bar 136 in the cutting mechanism movement. In the touch point have the knife bar 136 and the counter roll 126 the same rotational speed. The material to be cut is through a knife blade 138 Broken. Then the knife bar becomes 136 disengaged and with a braking device, for example with an electromagnetic brake - not shown - stopped. The second pair of conveyor rollers 128 transports the blanks.

The coupling cutter 134 allows distortion-free cutting of spread slivers. The cutting cycle, or the cutting length can be changed computer-controlled during operation.

The braking device (not explicitly shown) ensures that the knife roller 130 always locked when the clutch is not switched on. The clutch and brake operation via a common changeover relay (not shown), so the disturbances are excluded by program errors. A non-illustrated sensor device, such as an inductive proximity switch, registers the position of the knife and ensures a braking of the knife in a horizontal position. Is from the connected controller, such as the control device 44 , a cutting command is triggered, the knife roller couples 130 a, accelerates and executes a cut. If, as provided in the embodiment, the knife roller 130 at this moment has the same peripheral speed as the counter roll 126 , the knife blade becomes 138 not bent, and it results in a much longer knife life, comparable to a simple shock knife. After the cutting process, the knife roller 130 disengaged and braked and held in the same position as at the beginning. The cutting length is programmed in a control software.

10 shows the schematic sequence of the cutting unit control. How out 10 can be seen, depending on the feed rate of the cutting unit of the cutting cycle is specified. The minimum cutting length is due to the dimensions of the knife roller 130 and counter roll 126 and is for example in the order of the width of the spread sliver 14 , The maximum cutting length is theoretically unlimited.

In both presented embodiments of the cutting and laying group 16 become the patches 40 . 40 ' . 40 '' after the cutting device 24 to the transport device 26 passed the patches 40 . 40 ' . 40 '' with a greater transport speed than the conveying speed of the sliver 14 to or in the cutting direction 24 from the cutting device 24 transported away. This will make the patches 40 . 40 ' . 40 '' isolated and with sufficient distance from each other. The transport device 26 comes with a holding device that holds the patches 40 . 40 ' . 40 '' holds on the transport device, and provided with a transfer device, the patches 40 . 40 ' . 40 '' to the laying head 52 the laying device 28 passes.

The retaining device and the transfer device are here in the form of the vacuum conveyor belt 50 realized. A large-volume suction chamber 140 distributes the suction of a vacuum source, not shown, for example, a suction fan, over the entire transport device 26 , A provided with many continuous pores band, for example, a polypropylene belt, via a suction chamber 140 covering perforated sheet 142 guided.

The transport device 26 is by a coupling to a conveyor unit of the cutting device 24 driven. In the example shown here is the vacuum conveyor 50 to the positive gear, which the conveyor rollers 128 and the counter roll 126 drives, coupled. In this case, a corresponding transmission ratio, for example a transmission ratio of 1 to 2, ensures a sufficiently large distance between the patches 40 . 40 ' . 40 '' , At the end of the transport route is a suction-Abblaskammer 144 , which is operated with a pneumatic vacuum module. As long as a piece of fiber patch 40 - over the suction blow-off chamber 144 is guided, this is in the suction mode. If the laying stamp at a predetermined transfer position 146 is, a blow-off pulse is triggered at the right moment, the patch 40 on the laying head 52 promoted.

The laying head 52 sucks the patch 40 on, heats it up and transported him with a predetermined orientation to its predetermined position.

It will, as in 11 is shown, the patches 40 . 40 ' . 40 '' along predetermined curved paths 148 on the preform 30 stored. at 150 are along these curved paths 148 with appropriate orientation laid patches and their overlap indicated. In the overlap areas, the patches become 40 through that through the laying head 52 heated binder material 38 fixed together.

With the in 1 illustrated cutting device using the laser 54 (or any other beam cutting method) but can also produce more complicated cutting edge shapes. In 12 is a particularly advantageous cutting edge shape with complementary to each other convex or concave curved cutting edges 152 . 154 shown. The oppositely directed cutting edges 152 . 154 on every patch 40 are curved in a circular arc. This allows the cutting edges 152 . 154 consecutive patches 40 . 40 ' . 40 '' even with angulation of the patches 40 . 40 ' . 40 '' very close to each other, without any gaps or thickening. In this way, with a consistent dense system of fiber pieces and narrower radii of curvature of the webs 148 be assigned with appropriate fiber orientations. The fixation of the patches 40 . 40 ' . 40 '' may be by overlap with adjacent or overlying or underlying patches (not shown).

In this way you can also very complicated preforms 42 represent, for example, in 13 are indicated. Here is a kind of patchwork with the short pieces of fiber a preform 192 for a power flow compatible fiber composite structure for a window funnel, for example, for a fuselage of an aerospace device formed. The patches 40 . 40 ' . 40 '' are oriented according to the power flow lines.

The illustrated ring shape can be procedurally, for example, by a rotatable preform defined 30 reach like this by the arrows 156 in 1 is shown.

Based on 14 - 16 will now be the laying device 28 and their laying head 52 the in 8th illustrated embodiment of the cutting and laying group 16 further explained.

The laying head 52 should fulfill the function, a piece of fiber or patch 40 . 40 ' . 40 '' and to the next predetermined position 46 at the preform 30 where a patch 40 . 40 ' . 40 '' should be moved to transport. For this purpose has the laying head 52 a retaining device. Although other retaining devices are conceivable, in the example shown here, in order to easily receive the patch from the transport device 26 the retaining device as a suction device 158 educated.

Further, it is advantageous if the binder material 38 with which the recorded patch 40 is provided during transport with the laying head 52 is activated. For this purpose, the laying head 52 an activation device for activating the binder material 38 on. The activation device is formed depending on the binder material used. If z. B. an activatable by an additive binder material used, then the laying head has a device for adding this additive. In another, not shown embodiment equal active binder material, such as an adhesive, supplied only during the transport of the patch on the laying head. In such an embodiment, the laying head has a device for adding the binder material. For use in the previously discussed preform manufacturing apparatus 10 , the thermally activated binder material 38 is used, the activation device in the illustrated embodiment as a heater 160 educated.

Further, it is advantageous if the laying head 152 the patch 40 . 40 ' . 40 '' certainly also to more complicated three-dimensional surface designs of the preform 30 can attach. This is the laying head 52 with a pressing device 162 provided for pressing the transported patch 40 suitable for different surface designs. The pressing device 162 In a preferred embodiment has a flexible surface 164 on the patch 40 can be held by the retaining device on. The flexible surface 164 is werter preferred on an elastic support member 166 educated.

14 shows a cross section through a laying temple 168 of the laying head 52 which unites the retaining device, the activation device and the pressing device. The in 14 illustrated laying stamp 168 thus has the suction device 158 , the heater 160 as well as the pressing device 162 with the flexible surface 164 on the elastic support element 166 on.

15 shows a bottom view of the flexible surface 164 ,

With the laying stamp 168 can be used for fiber patch preforming technology (FPP) and fiber pieces (patches) cut in defined geometries according to a layout plan (for example, the in 11 reproduced laying plan) are stored with exact position. The laying temple 168 is a central component of the laydown technique and can also be used in other geometric variations. There are z. B. cuboid or roll-shaped laying temple conceivable.

In the concrete embodiment according to 14 is the laying stamp 168 designed as a silicone stamp. The surface fit of the silicone die is similar to the tampon printing technique. However, here is the appropriate application in a technologically completely different area.

The laying temple 168 is able to cut fiber through an integrated suction - suction device 158 - pick up quickly and gently and transport to a defined storage location. During transport, one in the contact surface heats - flexible surface 164 - integrated heating - heating device 160 - activates the material and thereby activates a binder - binder material 38 - on the fiber blank. The fiber blank is pressed onto the surface, with the soft stamp material conforming to the surface geometry. When the laying temple 168 removed from the surface, a blow-off pulse is triggered, the binder material 38 cooled, and the fiber material remains at the storage location.

The laying temple 168 enables the production of fiber patch preforms 42 ,

In the 14 is the elastic support element 166 - elastic pressure body - with an air distribution 170 shown, the part of the suction device 158 is. The not shown part of the suction device 158 is provided with common pneumatic sources and pneumatic controls (not shown). Next is the flexible surface 164 as elastic heating surface 172 with intake and exhaust ducts 174 shown.

The elastic support element 166 sits on a clutch plate 4 with detachable fasteners (not shown) for fixing the laying punch 168 at a positioning device 176 (please refer 16 ) is provided.

Next is a thermocouple 178 as a control part of the heater 160 intended. A highly flexible power line 180 connects the thermocouple 178 with the elastic heating surface 172 ,

In 15 is the suction surface - flexible surface 164 - with the intake and exhaust ducts 174 shown.

The following is the application of the laying stamp 168 as well as further details of the laying device 28 based on their use in the preform manufacturing device 10 explained in more detail.

The fiber patch preforming technology presented here becomes single fiber patches 40 to a three-dimensional preform 42 . 192 arranged. For this purpose, a suitable laying technique converts the construction plan into reality. The laying device 28 takes over the tied and cut fiber patches 40 from the vacuum conveyor 50 , that of the cutting device 24 is assigned, and places the fiber patches 40 in the fastest possible time on a surface. In the illustrated embodiment, the fiber patches 40 . 40 ' . 40 '' on a surface of the preform 30 stored.

It should the patches 40 . 40 ' . 40 '' to form a stable preform 42 pressed onto the shaping surface. The laying temple 168 should be as wel as possible in order to be able to adapt to a three-dimensional surface with uniform force. It is also advantageous for the embodiment shown here that just before depositing a certain amount of heat to activate the binder material 38 can be made available. This is the flexible surface 164 with the heater 160 equipped, which influences the mechanical properties of the stamp material as little as possible. Similar to the vacuum conveyor 50 is also at the legend temple 168 a flat fixation of filigree fiber patches 40 advantageous. This is due to the flexible surface 164 also a suction function.

The production of the laying temple 168 leans on the production of tampon printing stamps from the printing technology. There are a number of specialty silicones available for the production of tampon plungers that can withstand the constant mechanical cycling for a long time. From these silicones, a silicone rubber is selected that meets the additional requirements due to the heater 160 as well as the contact with binder material 38 as well as possible. There in the laying temple 168 a heater is integrated, attempts were made to temperature stability of the stamp material. It is advantageous if the laying temple 168 Continuous temperatures up to 200 ° C can endure. A plasticizer for the silicone material is selected according to these requirements.

To the laying surface of the laying temple 168 To heat are different heaters 160 used. It come z. As electric heaters, fluid circuits or hot air in question. Manufacturing technology is the simplest variant of an electric heater 160 implement. This also offers the possibility of very high heat outputs with exact temperature setting.

To the flexibility of the elastic support element 166 not to influence, are the power lines 180 advantageously formed by means of a Kohlenstoffasergarns. The high flexibility of such a yarn does not lead to a stiffening of the flexible surface 164 , Furthermore, such a fiber can withstand several 100,000 load cycles.

The thermal conductivity of the elastic support element 166 can be increased by adding heat transfer agents into the silicone.

For example, the flexible surface has a heat conductivity of about 10-30 weight percent sufficient thermal conductivity, so that a heating element of the heater 160 and the flexible surface 164 can be kept at approximately the same temperature.

In the flexible surface 164 of the laying temple 168 were the intake and Abblaskanäle 174 integrated in the interior of the laying temple 168 over a chamber 182 to merge. In the chamber 168 is a Saugvlies (not shown) inserted, which collapse when pressing the laying temple 168 prevented.

To avoid electrostatic charges, it is advantageous if the flexible surface 164 is formed of a flexible material with antistatic properties.

The following is still based on the 16 the depositing mechanism of the laying device 28 explained in more detail.

In the 16 reproduced laying mechanism 184 serves to move the laying temple 168 to fiber patches 40 from the cutting device 24 to the predefined position 46 to transport. The laying mechanics 184 allows a quick laying cycle and an adjustable deflection angle.

As previously explained, the patch will be 40 non-contact from the vacuum conveyor 50 on the laying temple 168 to hand over. For this purpose, the control device triggers 44 after a set delay time as a function of a cutting command, a blow-off pulse of the suction / blow-off chamber 144 of the vacuum conveyor 50 out. The patch 40 is applied over a few millimeters (about 0.5-10 mm) amount of air to the sucking Legestempel 168 transfer. Thereafter, the movement sequence of the laying mechanics begins 184 ,

The laying mechanics 184 has a first translational drive for transporting the laying temple 168 from the pickup position to a position above the predetermined position. This first drive is in the illustrated Ausfüh tion form the laying mechanics 184 as a horizontal pneumatic cylinder 186 executed. This horizontal pneumatic cylinder 186 can the laying temple 168 move from its pickup position over the depository. A second drive, here in the form of a vertical pneumatic cylinder 188 , presses the laying temple 168 , preferably with adjustable pressure, on the surface.

During the shifting process, the plunger surface is kept permanently at an adjustable temperature so that the binder can activate its stickiness. As soon as the patch 40 the surface touches, cools the binder material 38 off and gets stuck. Controlled by the control device 44 then a blow-off pulse in the suction device 158 of the laying temple 168 triggered; the legestem pel dissolves and then returns to its starting position. The separating properties of the silicone are advantageous because no binder material 38 remains on the stamp.

Via a third drive, which in the embodiment in the form of a stepper motor 190 with spline system 191 is formed, the laying stamp 168 to be turned around. Thus, even traces of oblique patches 40 be generated without the entire laying head (eg laying stamp 168 with laying mechanics 184 ) must be turned.

To achieve an economical laying process, a very high cycle rate of more than two laying operations per second has been planned. For example, five laying operations per second or more are performed. With a patch length of 60 mm and using a 12k roving, this results in a theoretical fiber throughput of 14.4 g / min. For example, if you want a square meter with fiber patches 40 in the thickness of a Biaxialgeleges (about 500 gr / sqm) occupy, so would the preform manufacturing device 10 need about 35 minutes. Shorter times can be achieved by using multiple laying devices 28 , for example, using multiple robots that work together on a surface.

Due to the currently still relatively low achievable speeds, the FPP technology in the currently presented form is particularly suitable for the reinforcement of other preform types as well as for thin-walled and complex components. So z. B. to think of the reinforcement of hole edges on Mulitaxialgelegen or tissues. A window funnel whose preform 192 in 13 is illustrated, would also be very thin-walled and produced with a defined fiber layer.

For certain preform types, fewer degrees of freedom are achieved on a FPP system - preform manufacturing device 10 - needed. Should z. B. only reinforcing profiles are produced, then the individual modules can be simplified and combined into a production line. Unused assemblies may be omitted, or the device may be separated into multiple assemblies with intermediate storage of the semifinished product.

Thereby can both the plant costs are lowered, and the productivity can be increased.

10

Preform manufacturing

12

treatment group

14

tow

16

cutting and laying group

18

unrolling

20

spreading

22

binder impregnation device

24

cutter

26

transport means

28

positioning device

30

preform

32

roving

34

spreading

36

loosening device

38

binder material

40 40 ', 40' '

patch (Sections of a sliver;

42

preform

44

control device

46

predefined position

48

Fiber cutting tool

50

vacuum conveyor Belt

52

laying head

54

laser

56

supply spool

58

storage

60

linear guide

62

carriage

64

drive spindle

66

engine

68

sensor

70

position

72

photodiode

74

flat ribbon

75

roll

76

curved pole

78

just pole

80

spreading edge

82

first radial projection

84

rotary shaft

86

rotary shaft

88

second radial projection

90

straight edge

92

gear transmission

94

wing

96

suction chamber

98

laminar airflow

100

filaments

102

funnel

104

radial surveys

106

roller

108

Ausbürstwalze

110

electric motor

112

electric motor

114

control device

116

holder

118

heater

120

IR heaters

122

Fiber cutting tool

124

Knife device

126

backing roll

128

conveyor roller

130

knife roll

132

knife edge

134

Coupled cutting system

136

cutter bar

138

knife blade

140

suction chamber

142

perforated sheet

144

Suction / blow-off

146

Transfer position

148

curved tracks

150

overlapping patches

152

cutting edge

154

cutting edge

156

mobility the preform - multidimensional -

158

suction

160

heater

162

presser

164

flexible surface

166

elastic support element

168

laying die

170

air distribution

172

elastic heating surface

174

intake and blow-off channels

175

clutch plate

176

positioning

178

thermocouple

180

power line

182

chamber

184

put mechanics

186

horizontally Pneumatic cylinder (first drive)

188

vertical Pneumatic cylinder (second drive)

190

stepper motor (third drive)

191

Spline system

192

Fenstertrichterpreform

Claims (39)

Method for producing a preform ( 42 ) for a power flow compatible fiber composite structure, comprising the following sequence of steps: a1) providing a flat fiber ribbon ( 14 c). Cutting a sliver piece ( 40 . 40 ' . 40 '' ) from the flat sliver ( 14 ), e) picking up the sliver piece ( 40 . 40 ' . 40 '' ) at a predetermined picking position by means of a laying device ( 28 ), f) placing the sliver piece ( 40 . 40 ' . 40 '' ) at a predefined position, g) fixing the fiber band piece ( 40 . 40 ' . 40 '' ) by means of a binder material ( 38 ), wherein the steps c) to f) for placing and fixing further fiber band pieces ( 40 . 40 ' . 40 '' ) are repeated at other predefined positions and wherein the steps e) and f) by means of a laying head ( 52 ) of the laying device ( 28 ), which automatically moves from the at least one pickup position to a first predefined position for placing a first sliver piece (Fig. 40 ) and back to the or one of a plurality of predetermined picking positions for picking up a second piece of fiber tape ( 40 ' ) and then to a second predefined position for placing the second sliver piece ( 40 ' ) moves. A method according to claim 1, characterized in that step a1) comprises the step: a) spreading a fiber filament bundle ( 32 ) of fiber filaments ( 100 ) to a flat sliver ( 14 ) contains. A method according to claim 2, characterized by the step to be carried out at some point between step a) and step f): b) attaching the binder material ( 38 ) on fiber filaments ( 100 ). Method according to claim 3, characterized that step b) is performed before step c). Method according to one of claims 1 to 4, characterized in that a heat activatable binder material ( 38 ) is used, and that for carrying out the step g) the cut fiber band piece ( 40 . 40 ' . 40 '' ) is heated. Method according to claim 5, characterized in that the laying head ( 50 ) is heated during its movement between the receiving position and the predefined position in order to remove the binder material ( 38 ) to activate. Method according to one of the preceding claims, characterized in that in step f) the sliver piece ( 40 . 40 ' . 40 '' ) to a portion of a molding surface ( 30 ) for the preform ( 42 ) is pressed to the sliver piece ( 40 . 40 ' . 40 '' ) to give a desired three-dimensional surface design. A method according to claim 7, characterized in that the pressing against the molding surface ( 30 ) by means of an elastically deformable receiving surface ( 164 ) of the laying head ( 52 ) is carried out, at which the fiber band piece ( 40 ) is held flat fitting during the laying process and Andrückvorganges. Method according to one of the preceding claims, characterized in that in step c) for forming the sliver piece ( 40 . 40 ' . 40 '' ) a piece of defined length, preferably less than about 20 cm, in particular less than about 10 cm, is cut off. Method according to one of the preceding claims, characterized in that the sliver piece ( 40 ) during the laying process pneumatically on the laying head ( 52 ). Method according to one of the preceding claims, characterized in that in step f) the placed fiber band piece ( 40 . 40 ' . 40 '' ) by means of a pneumatic pulse from the laying head ( 52 ) is solved. Method according to one of the preceding claims, characterized by the step to be carried out between step c) and step e): d) transporting the sliver piece ( 40 . 40 ' . 40 '' ) of a cutting device used to carry out the step c) to the receiving position of the laying device. A method according to claim 12, characterized in that the transport speed in step d) is greater than a conveying speed of the flat sliver ( 14 ) is to subsequently cut fiber band pieces ( 40 . 40 ' . 40 '' ) to separate from each other. Method according to one of claims 12 or 13, characterized in that the sliver piece ( 40 . 40 ' . 40 '' ) for transporting pneumatically on a conveyor belt ( 50 ). A method according to claim 14, characterized in that the sliver piece ( 40 . 40 ' . 40 '' ) by means of a pneumatic pulse from the conveyor belt ( 50 ) to the laying head ( 52 ). Method according to one of claims 2 to 15, characterized in that in step a) the filaments ( 100 ) of a roving ( 32 ), in particular a carbon roving, be spread. Method according to one of the preceding claims, characterized in that sliver pieces ( 40 . 40 ' . 40 '' ) with its fiber direction along predefined curved paths ( 148 ) are placed oriented. Method according to one of the preceding claims, characterized in that at different partial areas of the preform ( 42 ) a different number of slivers ( 40 . 40 ' . 40 '' ) is placed to different fiber contents at the sub-areas of the preform ( 42 ) to obtain. Method according to one of the preceding claims, characterized in that in step c) the sliver piece ( 40 . 40 ' . 40 '' ) is cut off each along an arcuate section line. A method according to claim 19, characterized in that in step f) sliver pieces ( 40 . 40 ' . 40 '' ) with mutually complementary arcuate cutting edges ( 152 . 154 ) are placed one behind the other without overlay. Use of a method according to one of the preceding claims for producing a power flow-compatible fiber composite structure which is in contact with the preform produced by the method (US Pat. 42 ) is constructed. Contraption ( 10 ) for carrying out the method according to one of the preceding claims, comprising: a cutting device ( 24 ) for cutting a flat sliver ( 14 ) into several slivers ( 40 . 40 ' . 40 '' ), a relative to the cutting device movable laying device for receiving individual sliver pieces ( 40 . 40 ' . 40 '' ) and placing them at predefined positions with predetermined orientation, and a control device ( 44 ) used for such control of the laying device ( 28 ) is formed such that the sliver pieces ( 40 . 40 ' . 40 '' ) along predetermined paths ( 148 ) oriented are deposited, wherein the laying device ( 28 ) a laying head ( 52 ) controlled by the control device ( 44 . 44b ) of at least one predetermined pickup position ( 146 ) is movable to different predefined positions and backwards to move from the cutting device ( 24 ) cut slivers ( 40 . 40 ' . 40 '' ) at the at least one receiving position and store at the predefined positions. Apparatus according to claim 22, characterized by a spreading device ( 20 ) for spreading at least one roving ( 32 ) to a flat sliver ( 14 ). Device according to claim 23, characterized in that the spreading device ( 20 ) with at least one convexly curved spreading edge ( 80 ) provided with at least one directional component perpendicular to the longitudinal extent of a Faserfilamentbündels aufzuspreizenden ( 32 ) is movable relative thereto, so that the fiber filament bundle ( 32 ) on the convexly curved spreading edge ( 80 ) is placed under tension, and then again with at least one directional component perpendicular to the fiber filament bundle ( 32 ) is movable away from this by the spreading edge ( 80 ) to solve. Apparatus according to claim 24, characterized ge indicates that the at least one spreading edge ( 80 ) on one of a rotary shaft ( 84 ) rotatable radial projection ( 82 ) is trained. Device according to one of claims 24 or 25, characterized in that it has at least two edge regions, of which at least one convexly bent spreading edge ( 80 ) and that from opposite directions on the fiber filament bundle ( 32 ) are too movable. Device according to claim 26, characterized in that two rotary shafts ( 84 . 86 ) with radial projections ( 82 ) are provided, wherein the rotary shafts ( 84 . 86 ) rotate in opposite directions. Apparatus according to claim 27, characterized in that the counter-rotating, in particular by means of a gear transmission ( 92 ), driven rotary shafts ( 84 . 86 ) several, the radial projections ( 82 . 88 ) forming wings ( 94 ) are configured which extend substantially in the axial direction erstre and at the radially outermost region of the edge regions ( 80 . 90 ) are formed. Device according to one of claims 26 to 28, characterized in that a plurality of edge portions serving for spreading as a convex radially outwardly bent spreading edges ( 80 ), wherein one after the other on the fiber filament bundle ( 32 ) aufzusetzende edge portions are arranged on counter-rotating movement organs so that the fibers between each two oppositely bent spreading edges ( 80 ) are spreadable. Device according to one of claims 24 to 29, characterized in that the spreading device ( 20 ) in the conveying direction of the fiber filament bundle ( 32 ) behind one the at least one spreading edge ( 80 ) having a spreading device ( 34 ) relaxation device ( 36 ) for loosening the spread fiber filament bundles ( 32 ) having. Apparatus according to claim 30, characterized in that the loosening device ( 36 ) a suction chamber ( 96 ) having. Device according to one of Claims 22 to 31, characterized by a binder material application device ( 22 ), with the binder material ( 38 ) for fixing the fiber band pieces ( 40 . 40 ' . 40 '' ) on filaments ( 100 ) is orderable. Device according to claim 32 and one of claims 23 to 31, characterized in that the binder material application device ( 22 ) of the spreading device ( 20 ) is assigned to binder material ( 38 ) on filaments ( 100 ) of the spread sliver ( 14 ) apply. Device according to one of claims 32 or 33, characterized in that the binder material application device ( 22 ) for applying powdery binder material ( 38 ) is trained. Device according to one of claims 22 to 34, characterized by a transport device ( 26 ), by means of which the cut fiber band pieces ( 40 . 40 ' . 40 '' ) and to the laying device ( 28 ) are transportable. Apparatus according to claim 35, characterized in that the transport device ( 26 ) a vacuum conveyor belt ( 50 ), on which the sliver pieces ( 40 . 40 ' . 40 '' ) are held transportable using a suction pressure. Device according to one of claims 35 or 36, characterized by a combination of suction and blow-off modules ( 140 . 142 . 144 . 174 ) for performing a smooth transfer of the sliver pieces of the transport device ( 26 ) to the laying device ( 28 ) is trained. Device according to one of claims 22 to 37, characterized by at least one heating device ( 160 ) for activating on filaments ( 100 ) applied binder material ( 38 ). Apparatus according to claim 38, characterized in that the heating device ( 160 ) or at least one of a plurality of heaters on the laying head ( 52 ) is arranged to heat up received fiber band pieces.