EP2140052A1 - Dispositif d'ecartement servant a ecarter des faisceaux de filaments de fibres, et procede d'ecartement pouvant etre mis en oeuvre au moyen de ce dispositif d'ecartement - Google Patents

Dispositif d'ecartement servant a ecarter des faisceaux de filaments de fibres, et procede d'ecartement pouvant etre mis en oeuvre au moyen de ce dispositif d'ecartement

Info

Publication number
EP2140052A1
EP2140052A1 EP08717708A EP08717708A EP2140052A1 EP 2140052 A1 EP2140052 A1 EP 2140052A1 EP 08717708 A EP08717708 A EP 08717708A EP 08717708 A EP08717708 A EP 08717708A EP 2140052 A1 EP2140052 A1 EP 2140052A1
Authority
EP
European Patent Office
Prior art keywords
spreading
fiber
laying
edge
filament bundle
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
EP08717708A
Other languages
German (de)
English (en)
Other versions
EP2140052B1 (fr
Inventor
Oliver Meyer
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
EADS Deutschland GmbH
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 EADS Deutschland GmbH filed Critical EADS Deutschland GmbH
Publication of EP2140052A1 publication Critical patent/EP2140052A1/fr
Application granted granted Critical
Publication of EP2140052B1 publication Critical patent/EP2140052B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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Classifications

    • D—TEXTILES; PAPER
    • D02—YARNS; MECHANICAL FINISHING OF YARNS OR ROPES; WARPING OR BEAMING
    • D02J—FINISHING OR DRESSING OF FILAMENTS, YARNS, THREADS, CORDS, ROPES OR THE LIKE
    • D02J1/00—Modifying the structure or properties resulting from a particular structure; Modifying, retaining, or restoring the physical form or cross-sectional shape, e.g. by use of dies or squeeze rollers
    • D02J1/18—Separating or spreading
    • D—TEXTILES; PAPER
    • D04—BRAIDING; LACE-MAKING; KNITTING; TRIMMINGS; NON-WOVEN FABRICS
    • D04H—MAKING TEXTILE FABRICS, e.g. FROM FIBRES OR FILAMENTARY MATERIAL; FABRICS MADE BY SUCH PROCESSES OR APPARATUS, e.g. FELTS, NON-WOVEN FABRICS; COTTON-WOOL; WADDING ; NON-WOVEN FABRICS FROM STAPLE FIBRES, FILAMENTS OR YARNS, BONDED WITH AT LEAST ONE WEB-LIKE MATERIAL DURING THEIR CONSOLIDATION
    • D04H3/00—Non-woven fabrics formed wholly or mainly of yarns or like filamentary material of substantial length
    • D04H3/002—Inorganic yarns or filaments
    • D—TEXTILES; PAPER
    • D04—BRAIDING; LACE-MAKING; KNITTING; TRIMMINGS; NON-WOVEN FABRICS
    • D04H—MAKING TEXTILE FABRICS, e.g. FROM FIBRES OR FILAMENTARY MATERIAL; FABRICS MADE BY SUCH PROCESSES OR APPARATUS, e.g. FELTS, NON-WOVEN FABRICS; COTTON-WOOL; WADDING ; NON-WOVEN FABRICS FROM STAPLE FIBRES, FILAMENTS OR YARNS, BONDED WITH AT LEAST ONE WEB-LIKE MATERIAL DURING THEIR CONSOLIDATION
    • D04H3/00—Non-woven fabrics formed wholly or mainly of yarns or like filamentary material of substantial length
    • D04H3/02—Non-woven fabrics formed wholly or mainly of yarns or like filamentary material of substantial length characterised by the method of forming fleeces or layers, e.g. reorientation of yarns or filaments
    • D04H3/04—Non-woven fabrics formed wholly or mainly of yarns or like filamentary material of substantial length characterised by the method of forming fleeces or layers, e.g. reorientation of yarns or filaments in rectilinear paths, e.g. crossing at right angles
    • D—TEXTILES; PAPER
    • D04—BRAIDING; LACE-MAKING; KNITTING; TRIMMINGS; NON-WOVEN FABRICS
    • D04H—MAKING TEXTILE FABRICS, e.g. FROM FIBRES OR FILAMENTARY MATERIAL; FABRICS MADE BY SUCH PROCESSES OR APPARATUS, e.g. FELTS, NON-WOVEN FABRICS; COTTON-WOOL; WADDING ; NON-WOVEN FABRICS FROM STAPLE FIBRES, FILAMENTS OR YARNS, BONDED WITH AT LEAST ONE WEB-LIKE MATERIAL DURING THEIR CONSOLIDATION
    • D04H3/00—Non-woven fabrics formed wholly or mainly of yarns or like filamentary material of substantial length
    • D04H3/08—Non-woven fabrics formed wholly or mainly of yarns or like filamentary material of substantial length characterised by the method of strengthening or consolidating
    • D04H3/12—Non-woven fabrics formed wholly or mainly of yarns or like filamentary material of substantial length characterised by the method of strengthening or consolidating with filaments or yarns secured together by chemical or thermo-activatable bonding agents, e.g. adhesives, applied or incorporated in liquid or solid form

Definitions

  • Spreading device for spreading fiber filament bundles as well as spreading method that can be carried out therewith
  • the invention relates to a Sp Schwarzvorhchtung for spreading fiber filament bundles to a flat sliver.
  • the spreading device according to the invention is particularly suitable for use in a method for producing a preform for a force flow compatible fiber composite structure.
  • the invention relates to a spreading method that can be carried out with such a spreading device.
  • fiber composite materials offer an outstanding lightweight construction potential.
  • the principle is that in particular high-strength and stiff fibers are embedded in a matrix in a load-compatible manner, resulting in components with outstanding mechanical properties, which are typically 25% lighter than aluminum and 50% lighter than comparable performance steel structures.
  • a disadvantage lies in the high material costs and in particular in the complex, mostly manual production.
  • fiber-reinforced plastics in particular when using oriented long fibers, for example carbon fibers, are characterized by very high strength and rigidity with low weight. In addition, they have a high weight-specific energy absorption capacity and good fatigue properties. This has hitherto been achieved by inserting endless fibers into a matrix (for example epoxy resin) in accordance with the load.
  • a matrix for example epoxy resin
  • anisotropic materials can be produced which have direction-dependent mechanical properties. For example, a material may have different properties in length than in width. In modern aircraft and spacecraft, a high percentage of the structural weight is already made of fiber-reinforced plastics today.
  • the reinforcing fibers are arranged in parallel (unidirectional) and embedded in a matrix.
  • semi-finished products are produced, which are wound up as a thin layer onto a roll.
  • these layers are cut according to the component contour and laminated mainly by hand layer by layer in a tool.
  • the curing takes place under pressure and temperature in an autoclave.
  • the resulting components have a very high lightweight potential, but the production is very complex and expensive.
  • the material researchers have therefore been investigating the question of how fibers are arranged in a load-bearing, three-dimensional and contoured manner as close as possible to the final contour of the component in an automated process.
  • preforms 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 devices and methods for producing such preforms can be found in DE 30 03 666 A1, DE 196 24 912, DE 197 26 831 A1 and DE 100 05 202 A1. However, the known processes for producing preforms are complicated in application and process technology.
  • the fibers can not be oriented arbitrarily along defined curved paths, and the fiber content can not be varied locally.
  • rovings are woven into the textile preform in the above-described previously known preform production process.
  • 12k rovings with 12000 individual filaments are used.
  • a uniform penetration of such rovings with the material of the matrix is very difficult to accomplish.
  • Fig. 4 shows a schematic diagram of an already known from DE 715801 A old mechanical spreading principle.
  • a fiber strand 14 successively passes through a bent rod 76 and then a straight rod 78.
  • the combination of a straight and a curved rod provides in Fig. 4, 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. That is, filaments can avoid the load as they move outward on the curved bar.
  • the spreader result 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. At an extreme bend, the difference is the acting one Forces between the highest point and an outer position are so great that the surface friction of the rod no longer plays a role.
  • the filaments will abruptly move outward, ie the fiber strand 14 would slip or split. If the bend is too small, then the spread ratio is too low. Thus, the spreader result is very irregular, it results in an irregular fiber distribution. In particular, the spreading result depends very much on the material quality.
  • the spreading device has at least one convexly curved spreading edge, which moves with at least one directional component perpendicular to the longitudinal extent of the fiber filament bundle relative to this so that this is placed on the convexly curved spreading edge under tension and then again with at least one directional component perpendicular to the Moved fiber filament bundle, so that it dissolves from the spreading edge.
  • a preform in a preferred method of use of the spreading device, can be prepared by first a fiber filament bundle, preferably a roving is spread flat. From this spread fiber filament bundle then a sliver piece, in the following description also called patch, preferably cut with a predefined length. Subsequently, the sliver piece is picked up by means of a laying device and placed at a predefined position. There, the sliver piece is fixed by means of a binder material. The cutting, laying and fixing of sliver pieces is repeated with the sliver pieces being placed and fixed at different predefined positions.
  • the desired preform with appropriate force-flow-oriented fiber orientation is formed from the plurality of patches fixed to one another and / or to additional components of the preform.
  • This also makes it possible, for example, to selectively reinforce a region of a conventionally produced preform, for example by depositing patches at particularly stressed points in accordance with the flow of forces.
  • such a method which can also be called fiber patch preforming technology, allows the positionally accurate application of short fiber pieces (patches) by means of a special laying process.
  • the required properties of the preform can be fulfilled by the earthing and number of fiber pieces.
  • a fiber filament bundle in particular a roving
  • a fiber filament bundle can be spread particularly flat and evenly.
  • thickening or other undesired fiber concentrations can be avoided, and the individual filaments can be better embedded in the matrix.
  • the invention is also useful for other applications where a shallow and uniform spreading of fiber bundles formed from individual fibers is desirable.
  • a roving in particular a carbon roving is preferably used.
  • the spreading device according to the invention in particular a wider spreading of the individual filaments of a roving than with previously known techniques is possible.
  • the spreading device for this purpose has a spreading device and a downstream loosening device.
  • FIG. 1 is a schematic overview of an apparatus for producing a preform for the purpose of producing power flow-compatible fiber composite structures
  • FIG. 1a is a schematic representation of an alternative embodiment of the device of Figure 1 at a direction indicated by a knotted-dotted line dividing plane ..;
  • FIG. 2 shows a schematic illustration of an unrolling device which can be used in the device according to FIG. 1 for unrolling a fiber filament bundle which can be processed in the device according to FIG. 1;
  • FIG. 3 shows a schematic perspective view of a position sensor which can be used in the unwinding device of FIG. 2 and a diagram of its characteristic curve;
  • FIG. 4 shows a perspective view of a spreading device known per se for explaining the principle of action of a spread of a fiber filament bundle used in the device according to FIG. 1;
  • 5 shows a perspective schematic illustration of a spreading device which can be used in the device of FIG. 1;
  • FIG. 6a is a schematic side view of a loosening device usable in the device of FIG. 1;
  • Fig. 6b is a schematic representation of the principle of operation of the loosening device of Fig. 6a;
  • Fig. 7 is a schematic side view of a bonder used in the apparatus of Fig. 1;
  • FIG. 8 shows a schematic side view of a combination of cutting device and laying device used in one embodiment of a device for producing a preform
  • Fig. 9/10 are schematic representations of the principle of operation of the cutting device of Fig. 8;
  • FIG. 11 shows a schematic illustration of predetermined webs for depositing fibers through one of the devices according to FIG. 1 or FIG. 8;
  • FIG. 11 shows a schematic illustration of predetermined webs for depositing fibers through one of the devices according to FIG. 1 or FIG. 8;
  • Fig. 12 is a series of laid by the apparatus of FIG. 1 sliver pieces
  • FIG. 13 a schematic illustration of a preform producible with one of the devices according to FIG. 1 or FIG. 8;
  • FIG. 14 shows a schematic cross-sectional view through a laying head which can be used in the laying device of FIG. 8 or FIG. 1;
  • Fig. 15 is a bottom view of the laying head of Fig. 14 and; 16 is a more detailed schematic perspective view of the laying device of FIG. 8.
  • a generally designated 10 preform manufacturing device is shown in the overview.
  • 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 apparatus according to FIG. 1 from individual short fiber pieces fixed by means of binder material, which have previously been cut off from a specially pre-processed fiber filament strand or sliver.
  • the preform manufacturing device can thus be divided into a processing group 12 for processing the sliver 14 and into a cutting and laying group 16 for cutting slivers and laying them. With a dot-dash line the possible separation 15 between these groups 12 and 16 is indicated.
  • Fig. 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 shown in Fig. 8.
  • the preform manufacturing device 10 has a unwinding device 18, a spreading device 20, a binding device 22, a cutting device 24, a transporting device 26, a laying device 28 and a preform 30.
  • These individual devices 18, 20, 22, 24, 26, 28 and 30 are each marketable and usable without the respective other devices to fulfill their purposes.
  • the unwinding device 18 is used to supply a fiber filament strand, for example a roving 32.
  • the unwinding device 18 is, as will be explained in more detail below, designed such that a twist-free unrolling of the roving 32 is made possible.
  • a carbon roving is used in the illustrated embodiment.
  • the spreading device 20 serves to spread the individual filaments of the roving 32 as widely as possible, so as to provide as flat a sliver 14 as possible of as few layers of adjacent individual filaments.
  • the spreading device 20 as will be explained in more detail below, a spreader 34 and a loosening device 36.
  • the binding device 22 serves to provide filaments of the sliver 14 and / or individual slivers thereof with a binder material 38 which serves to fix the sliver pieces in the preform.
  • the binding device 22 is part of the dressing group 12 and is thus used to provide the spread fiber sliver 14 with binder material 38.
  • a binding device 22 can be assigned to the cutting and laying group 16 in order then to provide the already cut fiber pieces with binder material 38.
  • the cutting device 24 is designed to cut pieces of defined length from the sliver 14 (fiber pieces).
  • the individual fiber band pieces are referred to below as patches 40, 40 ' , 40 " .
  • the transport device 26 is used to singulate the patches 40 and transport them to the laying device 28.
  • the laying device 28 is designed such that it can detect individual patches 40 and place them at predefined positions, here on the preform 30.
  • the preform 30 serves to give the preform 42 a predetermined three-dimensional surface design.
  • the preform manufacturing device 10 further comprises a control device 44 here having a plurality of controls 44a, 44b, which controls the individual devices 12, 18, 20, 22, 26, 30 in such a manner that, in the manner of a patchwork blanket or with the individual patches 40 the preform 42 is formed.
  • the preform production device 10 can thus be used to automatically carry out the following production method for producing a preform 42 for a force flow-compatible fiber composite structure:
  • a fiber filament bundle in the form of the roving 32 is spread and provided with the binder material 38 that can be thermally activated in the present exemplary embodiment.
  • the thus-provided tied fiber sliver 14 is then cut into the pieces of defined length - patches 40 -.
  • the patches 40 are singulated and transported to the laying device 28.
  • the laying device 28 places each patch 40 at a respectively predefined position 46 on the preform 30 and presses the patch 40 onto the preform 30.
  • preform manufacturing device 10 can thus be a fiber patch
  • a fiber cutting unit 48 cuts the specially prefabricated, tied fiber slivers 14 into short pieces, and transfers them to a vacuum conveyor 50 of the transport device 26.
  • the transfer of the patches 40 from the vacuum conveyor 50 to a laying head 52 of the laying device 28 takes place over a combination of suction and Abblasmodulen.
  • the laying head 52 heats the patch 40 during transport to the place of deposition and thereby activates the binding material 38.
  • the laying head 52 presses the patch 40 to the predefined location and then releases with a blow-off pulse. The laying head 52 then returns to the starting position.
  • 42 expanded carbon fibers are used instead of semi-finished textile products for producing the preforms.
  • the length of the fibers is very short (a few centimeters) compared to prefabricated fabrics using long fibers.
  • the short fibers can be placed relatively accurately along complex power flow paths.
  • textile blanks In previously used for the production of such preforms textile blanks only preferred orientations can be adjusted. As a result, extreme geometric shapes can be represented with the technology presented here.
  • the production process is fully automated and thickness variations within a preform and / or altered fiber volume contents can be obtained.
  • a laser 54 is used in the cutting and laying group 16 as the fiber cutting unit 48, which processor is controlled to move exactly relative to the sliver 14.
  • a robot arm is indicated in FIG. 1 as a laying mechanism 184 for moving the laying head 52.
  • the preform 30 is precise and rotatable relative thereto and is rotatable to easily create various complex 3-D structures of preforms 42.
  • a basic idea of the embodiment of fiber patch preforming technology presented here is to spread carbon fiber rovings 32 as broadly as possible, coat them with binder powder and cut them into defined long pieces, so-called patches 40, using a new cutting technique. These patches 40 are then picked up by the special laying device 28, placed at a predefined position and fixed by the binder material 38. This makes it possible to produce a wide variety of component geometries and fiber architectures.
  • 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.
  • more continuous fibers can reach the area of influence of a fiber end and compensate for voltage peaks.
  • the step at the cut end of a roving 32 is reduced.
  • Such a step could be up to 250 ⁇ m high in an unspread roving and would result in deflection of the overlying carbon fiber from the direction of force flow.
  • twists of the roving 32 should be avoided, since transverse filaments could constrict a splayed roving again.
  • the tension inside the roving 32 should be in be spread state constant, as by voltage differences, the spread width and spread quality could be influenced.
  • the unwinding device 18 which is explained in more detail below with reference to FIG. 2, serves to be able to deliver a roving 32 from a supply spool 56 without rotation and to compensate for the oscillating movement of the roving 32 during the withdrawal from the supply spool 56.
  • the unwinding device 18 has a movable mounting 58 of the supply reel 56 such that the supply reel 56 moves in accordance with the position of the region of the roving 32 that is about to be unrolled, so that the unwinding position remains as constant as possible.
  • the bearing 58 has a carriage 62 mounted along a linear guide 60.
  • the carriage 62 is movable 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 coil 56.
  • the movement of the carriage 62 is driven by a motor 66 with integrated control.
  • a sensor 68 observes the current position 70 of the blank 32 and thus controls the rotational movement of the motor 66.
  • a sensor 68 serves a spatially resolving photodiode 72, which is shown in Fig. 3 together with their 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 passed as a bipolar voltage signal to the control of the motor 66, wherein 0 volts corresponds to the sensor center.
  • the sensor 68 is flashed with an IR LED headlamp at a certain frequency, for example 10 KHz, in order to prevent the measurement signal from being influenced by ambient light.
  • This sensor 68 is optimized for the special requirements of an unrolling compensating for the position of the roving 32 on the supply reel 56 and permits further adjustments, such as, for example, mid-point displacement and bending adaptation.
  • the combination of spatially resolving photodiode 72 and controlled servomotor 66 has the advantage that the countermovement in dependence 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. As a result, the roving 32 is largely unrolled as a flat ribbon 74 unrolled.
  • the roving 32 rotates in an S-shaped movement two rolls 75, here two waisted Brassröllchen, which additionally calm down last vibrations.
  • the unwinding device 18 can also be operated completely autonomously from the remaining modules and basically only requires one power supply, for example a power connection.
  • the roving 32 passes through an unwinding path in the spreading device 20 following the unwinding device 18.
  • the spreading device 20 has, as already mentioned above, first the spreading device 34, which is shown in more detail in Fig. 5 and the principle of action is first explained with reference to FIG. 4.
  • Fig. 4 shows a schematic diagram of an already known from DE 715801 A old mechanical spreading principle.
  • a fiber strand 14 successively passes through a bent rod 76 and then a straight rod 78.
  • the combination of a straight and a curved rod provides in Fig. 4, 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 bent 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. That is, filaments can avoid the load as they move outward on the curved bar.
  • the radius spreader shown in Fig. 4 is not suitable for industrial processing of rovings 32 for preparation for preform production on an industrial scale.
  • errors in the roving 32 such as twists, crevices or folds, would result in slippage or splitting in the spread material.
  • the spreader 34 shown in FIG. 5 solves problems with the material quality of rovings or of other fiber filament bundles to be spread, by repeatedly placing the roving 32 or the fiber filament bundle on at least one convexly curved spreading edge.
  • the spreading device 34 has at least one convexly curved spreading edge 80, which moves with at least one directional component perpendicular to the longitudinal extent of the roving 32 or of the other fiber filament bundle relative thereto, so that it is placed under stress on the convexly curved spreading edge 80 and is then moved away again with at least one directional component perpendicularly from the roving 32 or the fiber filament bundle, so that it dissolves from the spreading edge 80.
  • the at least one spreading edge 80 is formed in a practical embodiment on a radial projection 82 on a rotary shaft 84.
  • At least two edges are movable from opposite directions onto the roving 32 or the fiber filament bundle.
  • two rotary shafts 84, 86 with radial projections 82 are provided for this purpose, with the rotary shafts 84, 86 rotating in opposite directions.
  • second radial projections 88 are also provided, which terminate with straight edges 90.
  • the edges 80, 90 can also be returned in the opposite direction to relieve the load on the roving 32 or the fiber filament bundle.
  • edges of all the wings 94 are designed as convexly radially outwardly bent spreading edges 80.
  • the fibers are in each case spread between two oppositely bent spreading edges 80.
  • the spreader 34 is formed, so to speak, as a wing spreader, which ensures a constantly renewed support of the roving 32 on spreading edges 80.
  • a sizing on the roving 32 or the fiber filament bundle is broken by the mutual bending, and the filaments 100 can move independently of each other.
  • the spreading device 20 is followed by the spreading device 34 designed as a wing spreader in the conveying direction of the roving 32 further the loosening device 36, which is configured in the embodiment presented here as a suction chamber according to the so-called Fukui principle.
  • the suction chamber 96 may be of the type described in US-A-6 032 342.
  • the loosened and pre-spread roving 32 is thereby pulled by a strong laminar air flow 98 into the suction chamber 96.
  • the individual filaments 100 are flowed around by air and can relatively easily slide over one another.
  • the suction chamber 96 can compensate for slight variations in the voltage of the roving 32.
  • the filament bundles are often guided freely and passed through eyelets.
  • parts of the filaments 100 can rotate around the rest of the bundle and lead to Rovingeinschnürungen already in the production.
  • these defects are barely visible at first because the filament bundle is pulled flat.
  • transverse roving parts are clearly visible. This effect can lead to gaps and displacements in the roving 32, which negatively affect the spreading quality.
  • a multi-stage spreading is provided in a not explicitly illustrated embodiment of the invention, in which the spreading ratio is increased gradually.
  • a first spreading device 34 and a first loosening device 36 are provided for spreading the roving 32 to a first width dimension, for example to a value between 8 and 16 mm.
  • a further spreading device 34 and a further loosening device 36 with larger dimensions than the first spreading device and the first loosening device so as to perform a spreading to a greater width, for example a value between 20 and 35 mm.
  • the roving 32 as a wide thin band, the sliver 14, before.
  • this sliver 14 is still equipped with a small amount of the binder material 38.
  • the bonder 22 is constructed in the basic form of a powder spreader such as disclosed, for example, in US-A-3 518 810, US-A-2 489 846, US-A-2 394 657, US-A-2 057 538 or US-A-2 613 633. He has therefore a funnel 102, at the output of a provided with radial elevations 104 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 is in turn processed by a spreading roller 108, which removes the powdered binder material 38 from the roller 106 and spreads on the sliver 14 passing below it.
  • a voltage U can be applied between the sliver 14 and the application mechanism, so that the powder, as in the case of a powder coating, electrostatically adheres to the sliver 14.
  • the transport roller 106 and the Ausbürstwalze 108 are driven by two separate electric motors 110 and 112 in order to set the scattering parameters as free as possible.
  • the control takes place via a control device 114, which may be part of the control device 44.
  • the hopper 102 is not fixedly secured to the remainder of the binding device 22, but held to a holder 116 that allows for compensating movements.
  • An advantage of the holder 116 is that the funnel 102 can oscillate during operation and the powder is shaken automatically downwards.
  • the powder is sprinkled in an exactly metered amount onto the surface of the rovings 32 passing through it at a defined speed, for example in the range of 3 to 6 m / min. Excess powder falls past the roving 32 in a receiver (not shown) and can later be re-introduced into the process.
  • the binding device 22 also has a heating device 118 in order to fix the powder particles of the binder material 38, which melts at heating temperatures, to the surface of the filaments 100.
  • the heater 118 has an approximately 100 to 500 mm long heating section.
  • the preferred embodiment of the heater 118 is equipped with radiant heaters, here with infrared radiant heaters 120.
  • the heating power of the heater 118 can be accurately adjusted by the controller 114.
  • the binder particles are easily melted and bind to the fiber surface.
  • the finished sliver 14 can be rolled up onto a special film spool 121 and temporarily stored for later use.
  • the so-specially prefabricated sliver 14 is fed to the cutting device, where it is inserted into the patches 40, 40 ' . 40 "is divided and then moved by means of the laying device 28.
  • Fig. 1a shows an embodiment with separate groups 12, 16 using the film spools 121 as an example of intermediate storage.
  • the groups 12, 16 could also be at separate production sites.
  • the cutting device 24 has a fiber cutting unit 122 with a knife device 124 and a counter-roller 126 as well as with at least one or a plurality of conveying rollers 128, as shown here.
  • the knife device 124 can be actuated depending on the rotational speed of the counter-roller 126 and / or the conveyor rollers 128 for cutting patches 40 with a defined length.
  • the knife device 124 has a (not shown) coupling mechanism which couples a drive of the blade device 124 with a drive for the rollers 126, 128.
  • the knife device 124 is provided in the illustrated example with a knife roller 130, which has at least one, here several knife edge 132 as a radial projection.
  • the knife roller 130 is in the illustrated embodiment further coupled by the coupling device not shown so to the drive of the backing roll 126, that the knife edge 132 at the same peripheral speed as the surface of the backing roll 126 move.
  • the cutting device shown in Fig. 8 and in greater detail in Fig. 9 therefore has a coupling cutter 134, in which two pairs of conveyor rollers 128 and a rubberized backing roll 126 by means of a motor not shown via a central positive gear, for example via a toothed belt (not shown) is driven.
  • the conveyor rollers 128 pull in an endless fiber belt - here in particular the spread fiber sliver 14 - and guide it over the counter-roller 126 rotating at the same speed.
  • a cutter bar 136 in waiting position. If a cut is to be made, an electromagnetic clutch engages the cutter bar 136 in the cutterbar movement. At the point of contact, the cutter bar 136 and the counter roller 126 have the same rotational speed. The material to be cut is broken by a knife blade 138. Thereafter, the cutter bar 136 is disengaged and with a braking device, for example with an electromagnetic brake - not shown - stopped.
  • the second pair of conveyor rollers 128 transport the blanks.
  • the coupling cutter 134 enables the distortion-free cutting of spread slivers.
  • the cutting cycle, or the cutting length can be changed computer-controlled during operation.
  • the braking device ensures that the knife roller 130 is always locked when the clutch is not turned 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. If a cutting command is triggered by the connected controller, for example the control device 44, the knife roller 130 engages, accelerates and makes a cut. If, as provided in the embodiment, the knife roller 130 at this moment the same Circumferential speed has like the counter-roller 126, the knife blade 138 is not bent, and there is a much longer knife life, comparable to a simple shock knife. After the cutting process, the knife roller 130 is disengaged and braked and held in the same position as at the beginning. The cutting length is programmed in a control software.
  • the cutting cycle is predetermined as a function of the feed rate of the cutting unit.
  • the minimum cutting length is due to the dimensions of the knife roller 130 and counter roller 126 and is for example in the order of the width of the spread sliver 14.
  • the maximum cutting length is theoretically unlimited.
  • the patches 40, 40 ' , 40 " are forwarded after the cutting device 24 to the transport device 26, the patches 40, 40 ' , 40 " with a greater transport speed than the conveying speed of the sliver 14 transported to or in the cutting device 24 of the cutting device 24 away.
  • the patches 40, 40 ' , 40 " are separated and provided with a sufficiently large distance from one another.
  • the transport device 26 is provided with a holding device which holds the patches 40, 40 ' , 40 " to the transport device and with a transfer device, which the patches 40, 40 ' , 40 " passes to the laying head 52 of the laying device 28.
  • the retaining device and the transfer device are realized here in the form of the vacuum conveyor belt 50.
  • a large-volume suction chamber 140 distributes the suction power of a vacuum source, not shown, for example, a suction fan, over the entire transport device 26.
  • a provided with many continuous pores band, such as a polypropylene belt, is guided over a 140 covering the suction chamber 140 perforated plate.
  • the transport device 26 is driven by a coupling to a conveying unit of the cutting device 24.
  • the vacuum conveyor belt 50 is coupled to the positive-locking gear which drives the conveyor rollers 128 and the counter-roller 126.
  • a corresponding LJ conversion ratio for example a gear ratio of 1 to 2, ensures a sufficiently large distance between the patches 40, 40 ' , 40 " .
  • a suction blow-off chamber 144 which is operated with a pneumatic vacuum module As long as a fiber piece - patch 40 - is guided over the suction-blow-off chamber 144, it is in suction mode
  • a blow-off pulse is triggered at the right moment, which carries the patch 40 onto the laying head 52 ,
  • the laying head 52 sucks the patch 40, heats it up and transports it with a predetermined orientation to its predetermined position.
  • the patches 40, 40 ' , 40 "of predetermined curved paths 148 are deposited on the preform 30.
  • patches and their overlapping laid along these curved paths 148 with the corresponding orientation are indicated.
  • the patches 40 are fixed to one another by the binder material 38 heated by the laying head 52.
  • FIG. 12 shows a particularly advantageous cutting edge shape with cutting edges 152, 154 that are complementary to each other in a convex or concave manner.
  • the oppositely directed cutting edges 152, 154 on each patch 40 are curved in a circular arc.
  • the cutting edges 152, 154 of patches 40, 40 ' , 40 " lying one behind the other can be very closely juxtaposed even when the patches 40, 40 ' , 40 " are bent, without any gaps or thickening.
  • To this Way can be occupied with a corresponding dense system of fiber pieces and narrower radii of curvature of the tracks 148 with corresponding fiber orientations.
  • the fixation of the patches 40, 40 ' , 40 " can be done by overlapping with adjacent or overlying or underlying patches (not shown).
  • a preform 192 is designed for a power flow-compatible fiber composite structure for a window funnel, for example for a fuselage of an aerospace device.
  • the patches 40, 40 ' , 40 " are oriented according to the power flow lines.
  • the illustrated ring shape can be achieved in terms of process technology, for example, by a defined rotatable preform 30, as shown by the arrows 156 in FIG.
  • the laying device 28 and its laying head 52 of the embodiment of the cutting and laying group 16 illustrated in more detail in FIG. 8 will now be explained in more detail with reference to FIGS. 14-16.
  • the laying head 52 is intended to fulfill the function of receiving a piece of fiber or patch 40, 40 ' , 40 " and to transport it to the next predetermined position 46 on the preform 30 where a patch 40, 40 ' , 40 " is to be laid.
  • the laying head 52 has a retaining device.
  • the retaining device is designed as a suction device 158.
  • the binder material 38 is activated during transport with the laying head 52.
  • the laying head 52 has an activating device for activating of binder material 38.
  • 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.
  • the same active binder material such as an adhesive, supplied only during the transport of the patch on the laying head.
  • the laying head has a device for adding the binder material.
  • the activation device is designed as a heating device 160 in the illustrated embodiment.
  • the laying head 152 can securely attach the patch 40, 40 ' , 40 " to more complicated three-dimensional surface configurations of the preform 30.
  • the laying head 52 is provided with a pressing device 162 which is used to press the transported patch 40 to different positions
  • the pressing device 162 has a flexible surface 164, on which the patch 40 can be retained by means of the retaining device.
  • FIG. 14 shows a cross section through a laying punch 168 of the laying head 52, which unites the holding device, the activation device and the pressing device.
  • the laying punch 168 shown in FIG. 14 thus has the suction device 158, the heating device 160 and the pressing device 162 with the flexible surface 164 on the elastic support element 166.
  • FIG. 15 shows a bottom view of the flexible surface 164.
  • the laying die 168 fibrous pieces (patches), which are bound in the Fiber-Patch-Preforming Technology (FPP) and cut into defined geometries, can be deposited with exact positioning according to a laying plan (for example of the laying plan shown in FIG. 11).
  • the laying stamp 168 is one central component of the laying technique and can also be used in other geometric variations. There are z. B. cuboid or roll-shaped laying temple conceivable.
  • the laying punch 168 is designed as a silicone stamp.
  • the surface fit of the silicone die is similar to the tampon printing technique. However, here the appropriate application is made in a technologically completely different area.
  • the laying punch 168 is able to take fiber blanks quickly and gently via an integrated intake-suction device 158-and to transport them to a defined storage location.
  • a heater integrated into the contact surface - flexible surface 164 - heater 160 - heats 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.
  • a blow-off pulse is triggered, the binder material 38 is cooled, and the fiber material remains at the deposit location.
  • the laying die 168 enables the production of fiber patch preforms 42.
  • the elastic support element 166 - elastic pressure element - is shown with an air distribution 170, which is part of the suction device 158.
  • the non-illustrated part of the suction device 158 is provided with conventional pneumatic sources and pneumatic controls (not shown).
  • the flexible surface 164 is shown as an elastic heating surface 172 with suction and Abblaskanälen 174.
  • the elastic support member 166 is seated on a coupling plate 4 provided with releasable fasteners (not shown) for securing the laying punch 168 to a positioning means 176 (see Fig. 16). Further, a thermocouple 178 is provided as a control part of the heater 160. A highly flexible power line 180 connects the thermocouple 178 to the elastic heating surface 172.
  • individual fiber patches 40 are arranged to form a three-dimensional preform 42, 192.
  • 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 belt 50, which is associated with the cutting device 24, and places the fiber patches 40 on a surface as fast as possible.
  • the fiber patches 40, 40 ' , 40 "are deposited on a surface of the preform 30.
  • the patches 40, 40 ' , 40 "are to be pressed onto the shaping surface to form a stable preform 42.
  • the laying punch 168 should be as soft as possible in order to be able to adapt to a three-dimensional surface with uniform force 1, that a certain amount of heat can be provided shortly before depositing to activate the binder material 38.
  • the flexible surface 164 is equipped with the heating device 160, which influences the mechanical properties of the stamp material as little as possible 50, a planar fixation of the filigree fiber patches 40 is also advantageous in the case of the laying punch 168.
  • the flexible surface 164 also has a suction function.
  • the production of the laying die 168 is based on the production of tampon printing stamps from printing technology.
  • silicones available for the production of tampon plungers, which can withstand the constant mechanical load changes for a long time. From these silicones, a silicone rubber is selected which corresponds as well as possible to the additional requirements due to the heating device 160 and the contact with binder material 38. As a heater is integrated into the laying die 168, attempts have been made to temperature stability of the stamp material. It is advantageous if the laying punch 168 can endure continuous temperatures up to 200 0 C. A plasticizer for the silicone material is selected according to these requirements.
  • various heating devices 160 can be 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.
  • the power lines 180 are advantageously formed by means of a carbon fiber yarn.
  • the high flexibility of such a yarn does not lead to a stiffening of the flexible surface 164.
  • such a fiber can withstand several 100,000 load cycles.
  • the thermal conductivity of the elastic support member 166 can be increased by adding heat conduction in the silicone.
  • the flexible surface has a dressing portion 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 maintained at approximately the same temperature.
  • the suction and Abblaskanäle 174 were integrated, which merge inside the laying block 168 via a chamber 182.
  • a suction flow (not shown) is inserted, which prevents collapse when pressing the laying punch 168.
  • the flexible surface 164 is formed of a flexible material having antistatic properties.
  • the depositing mechanism of the laying device 28 will be explained in more detail below with reference to FIG. 16.
  • the laying mechanism 184 reproduced in FIG. 16 serves to move the laying punch 168 in order to transport fiber patches 40 from the cutting device 24 to the predefined position 46.
  • the laying mechanics 184 allows a fast laying cycle and an adjustable deflection angle.
  • the patch 40 is transferred non-contact from the vacuum conveyor 50 to the laying die 168.
  • the control device 44 triggers a blow-off pulse of the suction / blow-off chamber 144 of the vacuum conveyor 50 after a set delay time as a function of a cutting command.
  • the patch 40 is transferred to the absorbent laying die 168 via a few millimeters (about 0.5 - 10 mm) airway. Thereafter, the sequence of movements of the laying mechanism 184 begins.
  • the laying mechanism 184 has a first translational drive for transporting the laying punch 168 from the receiving position to a position above the predetermined position.
  • This first drive is in the illustrated embodiment tion form the laying mechanism 184 designed as a horizontal pneumatic cylinder 186.
  • This horizontal pneumatic cylinder 186 can move the laying punch 168 from its receiving position over the deposit.
  • a second drive here in the form of a vertical pneumatic cylinder 188, presses the laying punch 168, preferably with adjustable pressure, on the surface.
  • the plunger surface is kept permanently at an adjustable temperature so that the binder can activate its stickiness.
  • the binder material 38 cools and solidifies. Controlled by the control device 44, a blow-off pulse is triggered in the suction device 158 of the die 168; The laying temple dissolves thereby and then moves back to its starting position.
  • the separating properties of the silicone are advantageous because no binder material 38 remains on the stamp.
  • a third drive which is designed in the embodiment in the form of a stepping motor 190 with spline system 191
  • the laying punch 168 can be rotated.
  • 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 one wishes to cover one square meter with fiber patches 40 in the thickness of a biaxial scrim (approximately 500 gsm), then the preform production device 10 would require approximately 35 minutes for this. Shorter times can be achieved by using multiple laying devices 28, for example, using multiple robots that work together on a surface.
  • 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. For example, think of the reinforcement of hole edges on multi-axial surfaces or weaving. A window funnel, the preform 192 of which is shown in FIG. 13, would likewise be very thin-walled and can be produced with a defined fiber layer.

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  • Engineering & Computer Science (AREA)
  • Textile Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Inorganic Chemistry (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • General Chemical & Material Sciences (AREA)
  • Nonwoven Fabrics (AREA)
  • Moulding By Coating Moulds (AREA)

Abstract

L'invention concerne un dispositif d'écartement (20) et un procédé d'écartement pour écarter des faisceaux de filaments de fibres (32) de manière à former une bande de fibres plate (14). L'objectif de cette invention est de résoudre les problèmes relatifs à la qualité de la matière des faisceaux de filaments de fibres (32) à écarter. A cet effet, le faisceau de filaments de fibres (32) est disposé de manière répétée sur au moins une arête d'écartement convexe (80).
EP08717708.5A 2007-03-13 2008-03-12 Dispositif d'ecartement servant a ecarter des faisceaux de filaments de fibres, et dispositif correspondant de fabrication de préformes Active EP2140052B1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE102007012607A DE102007012607B4 (de) 2007-03-13 2007-03-13 Spreizvorrichtung zum Aufspreizen von Faserfilamentbündeln sowie damit versehene Preform-Herstellvorrichtung
PCT/EP2008/052963 WO2008110582A1 (fr) 2007-03-13 2008-03-12 Dispositif d'écartement servant à écarter des faisceaux de filaments de fibres, et procédé d'écartement pouvant être mis en oeuvre au moyen de ce dispositif d'écartement

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EP2140052A1 true EP2140052A1 (fr) 2010-01-06
EP2140052B1 EP2140052B1 (fr) 2013-12-11

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US (1) US8191215B2 (fr)
EP (1) EP2140052B1 (fr)
CN (1) CN101680136B (fr)
CA (1) CA2680457C (fr)
DE (1) DE102007012607B4 (fr)
DK (1) DK2140052T3 (fr)
ES (1) ES2451016T3 (fr)
WO (1) WO2008110582A1 (fr)

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Also Published As

Publication number Publication date
WO2008110582A1 (fr) 2008-09-18
DK2140052T3 (da) 2014-01-27
EP2140052B1 (fr) 2013-12-11
DE102007012607B4 (de) 2009-02-26
US20100107384A1 (en) 2010-05-06
US8191215B2 (en) 2012-06-05
ES2451016T3 (es) 2014-03-26
CA2680457C (fr) 2013-08-13
CN101680136B (zh) 2011-09-14
CA2680457A1 (fr) 2008-09-18
CN101680136A (zh) 2010-03-24
DE102007012607A1 (de) 2008-09-18

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