Method for producing a composite material component with an integrated electrical conductor circuit

Abstract

For the purpose of simple integration of conductor circuits into composite material components, a method and an apparatus for producing composite material components of this kind are proposed, wherein a conductor circuit is printed onto or applied in some other way to a support, is provided with a thermally activatable adhesive and then the support is applied to a blank of the composite material component for joint curing. The curing at high pressure and high temperature creates a strong connection between the conductor circuit and the composite material component.

Claims

1. A method for producing a composite material component with an integrated electrical conductor circuit, comprising: a) applying the electrical conductor circuit to a surface of a support, b) applying a thermally activatable adhesive to the conductor circuit with a print head, wherein a position of the print head can be controlled in order to follow a profile of elements or conductor tracks of the conductor circuit, c) placing the surface of the support, which surface is provided with the conductor circuit, onto a component blank composed of composite material which is still to be cured, and d) curing the component blank in an autoclave at a temperature above the activation temperature of the adhesive, so that the adhesive is activated and adhesively bonds the conductor circuit to the component.

2. The method according to claim 1, wherein step a) comprises at least one or more of the steps: a1) printing the electrical conductor circuit onto the surface, a2) applying the electrical conductor circuit to a separating film as the support, a3) structuring the electrical circuit on the support, a4) selecting the support and a manner of application in such a way that an adhesion force between the support and the electrical conductor circuit is lower than the adhesion force of the adhesive in an activated state, a5) applying a prespecified layout of conductor tracks as the conductor circuit, or a6) applying conductor tracks, which are formed from metal, to the surface of the support.

3. The method according to claim 1, wherein step b) comprises at least one or more of the following steps: b1) selectively applying the adhesive only to the surface of the conductor circuit, which surface is averted from the support, b2) applying the adhesive before step c), b3) applying the adhesive while carrying out step c), or b4) applying the adhesive in free-flowing form.

4. The method according to claim 1, wherein step c) comprises at least one or more of the steps: c1) providing a component blank composed of carbon fiber-reinforced composite material, c2) providing a component blank pre-formed from a prepreg, c3) providing a component blank with a fiber weave or a fiber scrim, c4) placing the support onto an outer or inner surface of the component blank, which surface is to be provided with the electrical conductor circuit, c5) rotating the support after the conductor circuit is applied to an upper surface and this surface is placed onto a top-most layer of the component blank, c6) placing the support, by way of the surface which is averted from the conductor circuit, onto a mold and inserting the component blank into the mold, c7) pressing a mold surface onto that region of the component blank which is provided with the support, or c8) providing a composite material panel blank, comprising fibers and curable matrix material, in such a way that a composite material panel can be obtained from the composite material panel blank by compression molding at elevated temperature.

5. The method according to claim 1, wherein step d) comprises at least one or more of the steps: d1) curing the component in a mold, or d2) curing the component in a molding press.

6. The method according to claim 1, further comprising the step e) removing the support from the component, which takes place after step d).

Description

BRIEF DESCRIPTION OF THE DRAWINGS

(1) Exemplary embodiments of the invention will be explained in more detail below with reference to the appended drawings, in which:

(2) FIG. 1 shows a schematic illustration of a separating foil as a preferred embodiment of a support;

(3) FIG. 2 shows a schematic perspective illustration of an embodiment of a conductor circuit application device for applying an electrical conductor circuit to the support;

(4) FIG. 3 shows a schematic perspective illustration of an exemplary embodiment of an adhesive application device for applying an adhesive to the electrical conductor circuit;

(5) FIG. 4 shows the separating foil, which is provided with the conductor circuit and the adhesive, as an example of a support during the course of a transfer;

(6) FIG. 5 shows a composite material component blank to which the support is applied;

(7) FIG. 6 shows an exemplary embodiment of a curing device in order to produce a composite material component from the composite material component blank by curing;

(8) FIG. 7 shows a schematic illustration of a further method step which is carried out after the curing;

(9) FIG. 8 shows an airplane as an exemplary embodiment of a vehicle, in particular aircraft, which contains a composite material component which is provided with a conductor circuit; and

(10) FIG. 9 shows a wind power installation which contains a composite material component which is provided with an electrical conductor circuit.

DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS

(11) FIGS. 1 to 7 show different stages of a method for producing a composite material component 10 with an integrated electrical conductor circuit 12. The different devices 22, 26, 32, 34, 42, 46, 54, 56, 70 illustrated in FIGS. 1 to 7 for carrying out the method are part of an apparatus, designated 14 in its entirety, for producing the composite material component with an integrated electrical conductor circuit 12. FIG. 9 shows application examples of a composite material component 10 of this kind. The apparatus 14 can be, for example, a production installation for producing composite material components 10, as are already used, in principle, in airplane manufacture for example, but which has the modifications outlined below.

(12) FIG. 1 provides a support 16 to which the conductor circuit 12 is initially applied. The support 16 used is, in particular, a separating film 18 or pull-off film. The separating film 18 used is, for example, a separating film as is currently used in a similar way in the production of composite components.

(13) As illustrated in FIG. 2, the electrical conductor circuit 12 is then applied to a first surface 20 of the support 16. The application takes place, in particular, by means of printing.

(14) FIG. 2 illustrates an exemplary embodiment of a conductor circuit application device 22 by means of which a predetermined pattern of conductor tracks 24 is applied by selective application of conductive material, in particular metal.

(15) To this end, the conductor circuit application device 22 has, in particular, a conductor circuit printing device 26 for printing the conductor circuit 12. The conductor circuit printing device 26 has a conductor circuit application controller 28 in which patterns to be manufactured are stored in a memory as corresponding files and which is configured to move a movement apparatus 30 (for example, robot arm) of the conductor circuit printing device 26 and to actuate a metal material provision device 32, which is configured as a printing nozzle, in particular, for providing the metal material for the conductor tracks 24.

(16) FIG. 2 also further indicates a separating film provision device 34 by means of which the separating film 18 can be provided for printing purposes. By way of example, a separating film 18 can be unrolled from an appropriate supply roll 36.

(17) As illustrated in FIG. 2, a printing head 38 is, in a manner controlled by means of the conductor circuit application controller 28 in accordance with the pattern stored therein for forming the conductor circuit 12, moved over the first surface 20 of the separating film 18 and actuated for correspondingly printing the conductor tracks 24.

(18) Therefore, an electrical conductor circuit 12 can be produced in a highly accurate manner with high-quality conductive materials under controlled laboratory conditions.

(19) According to FIG. 3, a thermally activatable adhesive 40 is then applied to the conductor circuit 12.

(20) To this end, an exemplary embodiment of an adhesive application device 42 is illustrated in FIG. 3.

(21) The adhesive application device 42 has an adhesive application controller 44 for controlling the application process for the adhesive 40. By way of example, the adhesive application controller 44 is connected to or jointly configured with the conductor circuit application controller 28, so that the prespecified pattern of conductor tracks 24 can also be used for movement control of the adhesive application device 42.

(22) The adhesive application device 42 has an adhesive provision device 46 for providing the adhesive 40 in free-flowing form.

(23) The adhesive 40 provided is a thermally sensitive adhesive. In particular, an adhesive 40 is provided which is activated at temperatures above a predetermined activation temperature and cures at such temperatures. In particular, a thermoset adhesive is provided.

(24) The adhesive application device 42 has an application tool 48, for example with a nozzle 50, a brush (not illustrated) or the like, which application tool, in terms of its position, can be controlled by a further movement apparatus 52 (for example, gantry system) in order to follow the profile of conductor tracks 24 of the conductor circuit 12.

(25) The adhesive application device 42 can be arranged in the same location (for example production station of the apparatus 14) or at another station, such as the conductor circuit application device 22. In the latter case, the support 16, which is configured as the separating film 18 for example, is transported from the conductor circuit application device 22, illustrated in FIG. 2, to the adhesive application device 42, illustrated in FIG. 3, by means of suitable transfer devices 54.

(26) The application of the adhesive 40 takes place on that side of the conductor tracks 24 and/or of the other elements of the conductor circuit 12 which is averted from the separating film 18.

(27) In this way, a temperature-sensitive adhesive 40 is applied to the conductor circuit 12 by means of the adhesive application device 42. In a comparable manner, an insulation, which is formed from several layers, and protective materials can also be added at this station.

(28) The transfer device 54 or a further transfer device 54 transports the support 16 from the adhesive application device 42 to a composite material component blank provision device 56, wherein a composite material component blank 58 is provided. The transfer step is illustrated in FIGS. 4 and 5, wherein FIG. 4 further illustrates that the first surface 20 which is provided with the conductor circuit 12 and initially faces upward is directed, by appropriately turning over or otherwise orienting the support 16, toward that component surface 60 of the composite material component blank 58 which is to be provided with the conductor circuit 12.

(29) The composite material component blank provision device 56 can be any production device which provides a blank for fiber-reinforced composite materials comprising fibers embedded in matrix material. By way of example, components for aircraft 62, in particular airplanes 64, or components of wind power installations 66, as are illustrated in FIGS. 8 and 9, are pre-formed by means of provision devices 56 of this kind.

(30) The support 16, which is configured as a separating film 18 for example, is turned over and applied directly in contact with the last layer of the composite material component blank 58 during the otherwise usual production of composite material components 10 of this kind by means of an appropriate function of the transfer device 54 in particular. The subsequent composite material component 10, which is to be produced from the composite material component blank 58 by curing, can be, in particular, a panel for the airplane 64 or for vanes 68 of the wind power installation 66, which panel is formed from fiber-reinforced plastics, such as carbon fiber-reinforced plastic or glass fiber-reinforced plastic for example.

(31) In FIG. 5, direct contact is preferably made on a component surface 60 which is directed outwards or inwards during subsequent operation. The support 16 is preferably applied to a component surface 60 which is later surrounded by a vacuum pack (bag side).

(32) The separating film 18 can also be placed on a tool side, which faces a molding tool (tool side), or on inner surfaces, such as flanges or the like.

(33) When contact is made, the first surface 20 and, in particular, the conductor circuit 12 which is applied to it, are brought into contact with this component surface 60, wherein an adhesive 40 is inserted therebetween.

(34) FIG. 6 shows a step of curing the composite material component blank 58, as a result of which the composite material component 10 is produced. A curing device 70, which has, in a known manner, a mold 72 (for example the molding tool), an autoclave 74 or furnace and possibly a press 76 or vacuum packing device (not illustrated), is used for this purpose.

(35) The curing device 70 is further provided with a temperature control device 78 which controls the temperature on the composite material component 10 by means of a heating device during curing. A temperature which lies above the activation temperature of the adhesive 40 is reached in the process.

(36) Furthermore, the support 16 is pressed together with the composite material component blank 58 by the press 76 and/or an appropriate pressure in the autoclave 74which can likewise be controlled, so that, at the same time as the composite material component blank 58 is cured, the adhesive 40 is cured at high temperature and high pressure.

(37) In one procedure, the composite material component blank 58 is packed in a film together with the separating film 18 applied to it and subjected to the action of a vacuum, so that a very tight package is produced and the mold is consolidated. This composite is then moved to the autoclave 74 for curing purposes. In the autoclave 74, the high temperaturefor example 120 C. to 180 C.activates the adhesive 40, this ensuring a good adhesive connection between the conductor circuit 12 and the composite material component 10.

(38) As illustrated in FIG. 6, the composite material component 10 is removed from the autoclave 74 when the curing step has been completed.

(39) The support 16, which is configured as a separating film 18 for example, is removed from the composite material component 10, wherein the conductor circuit 12 remains strongly adhesively bonded to the component surface 60.

(40) The printed conductor circuit 12 remains strongly connected to the composite material component 10 in this way after the separating film 18 is removed.

(41) Accordingly, composite material components 10 which are provided with a conductor circuit 12 can be used for different purposes.

(42) FIG. 8 shows, as an application example, the airplane 64 as an example of a vehicle, in particular, an aircraft. Here, for example, panels, which form subregions of the wing for example, can be formed by an appropriate composite material component 10, so that electrical devices on the wing can be actuated by means of the conductor circuit 12.

(43) FIG. 9 shows a wind power installation 66 as a further example of a possible use of the composite material component 10 which is provided with the conductor circuit 12. By way of example, the vanes 68 of the wind power installation 66 are constructed from composite material components 10 which are configured as panels. The conductor circuit 12 integrated therein can be used for actuating position lamps 80 on the vane tips. Sensors which can transmit wire-bound signals via the conductor circuit 12 and can accordingly be actuated via the conductor circuit can also be fitted to the vanes 68.

(44) It goes without saying that actuators or the like can also be supplied with power and/or control signals via the conductor circuit 12 in all application examples.

(45) While at least one exemplary embodiment of the present invention(s) is disclosed herein, it should be understood that modifications, substitutions and alternatives may be apparent to one of ordinary skill in the art and can be made without departing from the scope of this disclosure. This disclosure is intended to cover any adaptations or variations of the exemplary embodiment(s). In addition, in this disclosure, the terms comprise or comprising do not exclude other elements or steps, the terms a or one do not exclude a plural number, and the term or means either or both. Furthermore, characteristics or steps which have been described may also be used in combination with other characteristics or steps and in any order unless the disclosure or context suggests otherwise. This disclosure hereby incorporates by reference the complete disclosure of any patent or application from which it claims benefit or priority.

LIST OF REFERENCE SYMBOLS

(46) 10 Composite material component 12 Conductor circuit 14 Apparatus 16 Support 18 Separating film 20 First surface 22 Conductor circuit application device 24 Conductor track 26 Conductor circuit printing device 28 Conductor circuit application controller 30 Movement apparatus 32 Metal material provision device 34 Separating film provision device 36 Supply roll 38 Printing head 40 Adhesive 42 Adhesive application device 44 Adhesive application controller 46 Adhesive provision device 48 Application tool 50 Nozzle 52 Further movement apparatus 54 Transfer device 56 Composite material component blank provision device 58 Composite material component blank 60 Component surface 62 Aircraft 64 Airplane 66 Wind power installation 68 Vane 70 Curing device 72 Mold 74 Autoclave 76 Press 78 Temperature control device 80 Position lamp