Patent Application
20230160527
The present invention relates to the use of a fiber composite material connecting portion to connect a tubular fiber composite material structure to a connecting device, wherein the fiber composite material structure has more circumferential layers than longitudinal threads, wherein the connecting portion has at least one fiber deflecting element in its interior, wherein the course of the longitudinal threads from the fiber composite material component follows the shape of a fiber deflecting portion of a fiber deflecting element so that the fiber direction thereof is deflected at the fiber deflecting portion, and wherein the long fibers do not completely loop around the fiber deflecting elements with which they are associated respectively, wherein the fiber deflecting elements consist of fiber composite material, for a pressure tank.
To connect fiber composite materials to components, the connection methods known for metal materials often cannot be used or can only be used with a loss of strength of the connection. In particular, the strength of the connection between the fiber composite material and the component is reduced by separation and breaking of fibers of the fiber composite material. Such breaks of the fibers occur, for example, when drilling through or trimming the fiber composite material in order to insert the component to be connected through the drilled hole or to glue it to the trimmed edges.
Therefore, fiber composite material connecting portions that connect a fiber composite material structure to a connecting device without severing the long fibers of the fiber composite structure are known.
WO 2016/008858 A1 describes a fiber composite material connecting portion for connecting a fiber composite material structure to a connecting device. The connecting portion in that case has at least one fiber deflecting element in its interior, wherein the course of first long fibers from the fiber composite material component follows the shape of a first fiber deflecting element, so that the fiber direction thereof is deflected at the first fiber deflecting portion. The course of second long fibers from the fiber composite material structure follows a second portion thereof or a second fiber deflecting element so that their fiber direction is deflected at the second fiber deflecting portion. The two fiber deflecting portions are spatially separated from each other, wherein a first securing projection and a second securing projection spatially separated from the first one are formed at the connecting portion in each case to transmit force into the connecting portion, and wherein the first securing projection is formed by the first fiber deflecting element and the first long fibers and the second securing projection is formed by the second fiber deflecting element and the second long fibers. The long fibers running from the fiber composite structure or the fiber composite material component to the securing portion are divided and distributed among a plurality of securing projections. This allows the tensile and compressive forces transmitted to the long fibers to be transmitted to another component. In this case, the fiber composite material component can be formed as a rod or tube as a tension-compression element. In particular, a large proportion of fibers with fiber direction in the longitudinal direction of the rod or tube can be provided.
EP 0 082 021 A2 describes the fastening of a ring, in particular a metal ring, on an object, which has walls or skirts made of fiber-reinforced synthetic resin material. The ring has a plurality of outer grooves. The skirt includes, for each groove, subsequently a first and a second layer of fiber-reinforced resin material. The fibers in the first layer are substantially oriented parallel to the axis of the ring an extend from the skirt into the respective grooves. A second layer is located above the first layer, which second layer consists of annular windings, which extend from the skirt in the direction of the groove. The second layer is at least partially located in the groove for fixing the first layer in the groove. This layering is repeated for each groove, and finally, subsequent hoop windings are wound over the entire product.
The object of the invention is to create profoundly pressure-resistant pressure tanks.
The object is achieved by the use of a fiber composite material connecting portion to connect a tubular fiber composite material structure to a connecting device, wherein the fiber composite material structure has more circumferential layers than longitudinal threads, wherein the connecting portion has at least one fiber deflecting element in its interior, wherein the course of the long fibers from the fiber composite material component follows the shape of a fiber deflecting portion of a fiber deflecting element so that the fiber direction thereof is deflected at the fiber deflecting portion, and wherein the long fibers do not completely loop around the fiber deflecting elements with which they are associated respectively, wherein the fiber deflecting elements consist of fiber composite material, and wherein no firm connection is present between the tubular fiber composite material structure and the connecting device, for a pressure tank.
The pressure tank can be configured as an inner and outer pressure tank. In this case, the pressure tank consists of the tubular fiber composite material structure, which is connected to a connecting device via the fiber composite material connecting portion. To connect the fiber composite material structure to the connecting device, the long fibers from the fiber composite material structure can run along a surface portion of the fiber deflecting elements. There is no need here for the long fibers to wrap around the fiber deflecting elements. The surface portion at least partially forms an outer surface of the connecting portion. The surface portions run at an angle of between 20° and 60°, particularly preferably 45°, from the direction of the long fibers running towards the connecting portion. The long fibers also run with a portion on the adjacent fiber deflecting elements, wherein the portions on the adjacent fiber deflecting elements change direction. After the change in direction, they run along the surfaces of the fiber deflecting elements. Due to the changed fiber direction, the outer surfaces of the fiber deflecting elements can be understood as fiber deflecting portions for the fibers. With regard to the long fibers, due to the curved surface along which the fibers run, the adjacent fiber deflecting elements also each fulfil the function of a fiber deflecting portion.
The fiber deflecting elements can each have a protruding tip in the direction of the connecting device. The long fibers reach here maximally to this tip, so that the long fibers do not completely wrap around the fiber deflecting element. The long fibers do not significantly change direction again after being deflected onto the fiber deflecting element. The surfaces of the fiber deflecting elements along which the long fibers run are planar at least in a portion into the vicinity of the tips and merge, after a deflection of preferably 90°, into a further surface each, said further surfaces running from the tips in the direction of the interior of the connecting portion. At the end of this surface there is in each case a notch, after which the outer surface of the connecting portion continues in the next fiber deflecting element, as far as it is not the last fiber deflecting element. The two surfaces that touch at the tip preferably form the legs of an equilateral triangle. They form a V-shaped depression of the connecting device.
The long fibers each preferably belong to a separate fiber layer. The long fibers can be embedded here in the outer surfaces of the fiber deflecting elements.
Advantageously, the use of tubular fiber composite material structures achieves a weight and cost reduction compared to conventional metal, but also conventionally wound fiber composite material pressure tanks (type 4). This weight and cost reduction is particularly advantageous in the field of H2 high-pressure tanks in mobile applications such as motor vehicles, ships, aircraft and space travel.
The fiber deflecting elements can be configured as independent fiber deflecting elements. Alternatively, the fiber deflecting elements can be configured as a helical, interrelated fiber deflecting element.
Advantageously, in the present invention, smaller diameters of the tubular fiber composite material structure for the pressure tank can be achieved. In this way, the pressure tanks can have diameters < 100 mm. For example, for H2 high-pressure tanks conventionally produced by the winding process, the minimum diameter is determined by the boss part. If this is 100 mm, the outer diameter of the pressure tank cannot be less than approximately 130 mm, since pressure tanks produced in the winding process require a boss part wound with fibers to absorb the longitudinal forces caused by the overpressure. Thus, in addition to the cylindrical portion with internal thread provided to accommodate the safety valve, the boss part must have a pronounced plate-shaped portion of larger diameter, which ultimately serves as a turning zone during winding and additionally absorbs the longitudinal forces caused by the internal pressure. This function of absorbing the longitudinal forces during the transition of the load from the cylindrical composite material region into the often metal dome region is achieved by the present invention in a much more compact manner and with lower stress concentrations.
Advantageously, the tubular fiber composite material structures with the connecting device can be loaded by both internal and external pressure compared to conventionally wound inner pressure tanks. This means that these tubular fiber composite material structures with connecting device are also suitable for use as nested high-pressure tanks, wherein the inner tank can also have a lower internal pressure than the outer tank and thus effectively represents a tank loaded by external pressure. As a rule, these high-pressure tanks have a minimum burst pressure of approximately 1575 bar.
Advantageously, the fiber composite material structure and the connecting device can be connected without adhesive bonding. The force transmission of tensile and compressive forces takes place by way of a form fit between the connecting device and the deflecting elements and the long fibers of the fiber composite material structure. This means that there is no tension in the event of temperature changes. Advantageously, no fibers are broken to secure the connecting device. Such a breaking of fibers can have a negative effect on the strength of the fiber composite material structure. Due to the lack of penetration by connecting elements such as bolts or screws, there is also no stress corrosion. The use of different materials with different temperature expansion coefficients does not lead to tension in the introduction of force between the tubular fiber composite material structure and the connecting device, not even as a result of large temperature differences, because there is no fixed connection, such as with an adhesive bond. For this reason, the pressure tank is also suitable for cryogenic applications, for example cryogenic high-pressure storage. For example, the pressure tank can be configured as a double-walled tank with a cryogenic inner tank, for example for liquid H2, and gaseous H2 in the outer tank. Cryogenic tanks are usually protected by way of very complex vacuum insulation layers against heating of the cryogenic contents. If the cryogenic content, for example H2, becomes warmer than 20 K, part of the content must be blown off in order to cool down the remaining content. This blow-off could then pass from the inner to the outer tank in the case of a double-walled outer pressure/inner pressure tank and could continue to be available there as gaseous H2.
Due to the larger number of circumferential layers of the tubular fiber composite material structure, these can be loaded with a higher internal as well as external pressure. Advantageously, the forces occurring in the cylindrical part of the tank due to the internal or external pressure are absorbed in particular by the circumferential layers. As a result, high-pressure tanks with a burst pressure of, for example, 1575 bar can be produced with the tubular fiber composite material structure. The overall laminate of the tubular fiber composite material structure particularly preferably has twice as many circumferential layers as longitudinal threads.
It is expedient here that the fiber composite material of the fiber deflecting elements mainly consists of circumferential layers.
Preferably, the V-shaped depressions of the connecting device are filled with circumferential layers of fiber composite material. Preferably, the circumferential layers are wound over the entire connecting device in the case of use as a pressure tank, more specifically preferably approximately in the ratio of ⅔ (circumferential layer) to ⅓ (longitudinal layer) with regard to the total wall thickness. The winding of the circumferential layers fixes the long fibers of the tubular fiber composite material structure to the connecting device.
Due to the orientation of the fibers of the fiber deflecting elements in the circumferential direction, tensile, compressive, and torsional forces, which are transmitted to the fiber deflecting elements via the long fibers of the fiber composite material structure, are converted into circumferential forces in the fibers of the fiber deflecting elements on the connecting portion. This allows an advantageous introduction of the forces into the fiber deflecting elements.
Another embodiment of the invention is that the connecting device comprises a dome cap.
The dome cap forms the pressure-resistant closure of a tubular fiber composite material structure. Such a tubular fiber composite material structure with a dome cap is advantageously suitable as a pressure tank. The forces acting on the fiber composite material structure due to the internal or external pressure can be transmitted via the long fibers and the fiber deflecting elements to the connecting device with the dome caps.
In another embodiment of the invention, the fiber composite material structure comprises a liner.
In order to ensure the tightness of the pressure tanks made of tubular fiber composite material structures against the escape or entry of media, for example H2 from the outside, the tubular fiber composite material structures and the connecting device can be provided with a liner. This liner can be applied to the inside or outside of the tubular fiber composite material structures, depending on the direction of pressure. The liner can be a thermoplastic liner, for example HDPE or PA. It can also be made of glass, silicone, or metals. Advantageously, the liner ensures the media tightness of the fiber composite material structure even if intermediate fiber breaks occur in the fiber composite material structure.
An inner liner in combination with the dome caps can form the blank for the manufacture of an inner pressure tank. In this way, an additional core is avoided during manufacture. The liner, which is later connected to the dome caps in a media-tight manner, can be pressurized in the course of manufacture to serve as a core for the winding of the tubular fiber composite material structure. The level of pressure can be adapted here to the relevant requirements. Additional stabilization of the blank (liner and dome caps) during manufacture can be achieved by flooding the liner with a stabilizing medium (polystyrene, sand, hollow spheres, etc.) until the textile structure of the tank is stable.
Another embodiment of the invention is that a plurality of tubular fiber composite material structures are interconnected via the connecting devices.
This results in a structure with a plurality of pressure tanks. The connecting devices can be formed here as connectors between the pressure tanks. The structure formed from modular tank units can be used to make better use of installation space, for example in H2 pressure tanks in vehicle construction. The modular pressure tanks can be oriented here in various arrangements. For example, a plurality of pressure tanks can be arranged in parallel next to each other. Alternatively, for example, a plurality of pressure tanks with liquid H2 can be arranged in a pressure tank with gaseous H2.
According to another embodiment of the invention, it is provided that the liner, depending on the pressure direction, is applied to the tubular fiber composite material structure inside or outside.
One embodiment of the invention is such that the liner serves as a core for the winding of the tubular fiber composite material structure.
Lastly, it is within the scope of the invention that a plurality of tubular fiber composite material structures are interconnected and combined in the form of sub-assemblies.
In the following, embodiments of the device for use according to the invention are explained in greater detail with reference to drawings.
In the drawings
The long fibers 201a, 202a and 203a and correspondingly the portions of the long fibers 201, 202 and 203 consist of ⅓ longitudinal threads and ⅔ circumferential layers.
The fiber deflecting elements 211, 212 and 213 have protruding tips 231, 232 and 233 respectively in the direction of the connecting device 260. In this embodiment, the long fibers 201a, 202a and 203a extend maximally to the tips 231, 232 and 233, respectively. The long fibers 201a, 202a, 203a do not significantly change direction again after being deflected onto the fiber deflecting elements 211, 212 and 213, respectively. The surfaces 221, 222 or 223 of the fiber deflecting elements 211, 212 or 213, along which the long fibers 201a, 202a and 203a run, respectively, are at least approximately planar at least in a portion reaching into the vicinity of the tips 231, 232 and 233. These planar surfaces 221, 222 and 223 each merge, on the other side of the tips 231, 232 and 233 respectively and after a deflection of preferably 90°, into further surfaces 241, 242 and 243 respectively, each running from the tips 231, 232 and 233 respectively towards the interior of the connecting portion 210. At the end of each of these surfaces 241, 242 and 243 there are notches 251, 252 and 253, respectively, after which the outer surface of the connecting portion 210 continues in the next fiber deflecting element, unless it is the last fiber deflecting element 211. The two surfaces that contact at a tip 231, 232 or 233 form a V-shaped depression as shown in
The connecting device 260 comprises a carrier structure 261 to which there is secured an engagement portion 262 which is complementary in shape to the outer surface facing the connecting device 260. The portions of the engagement portion 262 facing the planar surfaces 221, 222, 223, 241, 242 and 243 of the connecting portion 210 are also planar and embodied with the same slope relative to the direction in which force is introduced. In this way, a form fit is achieved in the state in which the connecting portion 210 is secured to the connecting device 260. The connecting device 260 is tapered towards its free end. The side of the carrier structure 261 facing away from the connecting portion 210 is beveled here to form the taper.
Preferably, the connecting portion 210 and the connecting device 260 are embodied as separate elements without an integrally bonded connection. In the case of a transmission of torsional forces, however, it may be expedient to adhesively bond the connecting portion 210 to the connecting device 260. Preferably, at least one fiber layer relative to the connecting portion 210 is then embodied as a +45° layer. If the fiber deflecting element 218 is helical and there is a thread-like connection between the connecting portion 210 and the connecting device 260, torque can be transmitted in the tightening direction of the thread in a position against a threaded stop without the need for adhesive bonding.
The second embodiment differs from the first embodiment in that the long fibers 201a, 202a and 203a extend beyond the tips 231, 232 and 233, respectively, and continue in the sloping, planar surfaces 241, 242 and 243, respectively. They are embedded in these surfaces 241, 242 and 243, respectively. They end at the end of the surfaces 241, 242 and 243, respectively, in the direction of the notches 251, 252 and 253, respectively, or the vicinity thereof. Compared to the first embodiment, there is the additional advantage that the long fibers 201a, 202a and 203a are more firmly connected to the fiber deflecting elements 211, 212 and 213, respectively. Furthermore, the additional fibers make the surfaces 241, 242 or 243 stronger and able to transmit higher compressive forces to the connecting device 260.
As can be seen in the detail in
The third embodiment differs from the second embodiment in that it comprises long fibers 201a, 202a and 203a and, correspondingly, the portions of the long fibers 201, 202 and 203 consist entirely of longitudinal threads. There is an additional long fiber 204a, which wraps completely around the long fibers 201a, 202a and 203a, arranged on the outer surface of the connecting portion 210. This long fiber 204a consists entirely of circumferential layers. In this way, the circumferential layers are separated from the longitudinal layers.
The fourth embodiment differs from the second embodiment by an additional further fiber deflecting element 214 on the connecting portion 210. Said additional further fiber deflecting element is arranged in continuation of the row of fiber deflecting elements 211, 212 and 213 in a direction away from the free end of the connecting portion 210. However, it differs from the other fiber deflecting elements 211, 212 and 213 in that it does not have embedded therein long fibers 201a, 202a and 203a with which the connecting portion 210 is connected, for example, to a component not explicitly shown. However, in the case in which the connecting portion 210 is tubular, fibers are embedded in the circumferential direction in the fiber deflecting element 214 to allow the fiber deflecting element to better absorb forces from the deflection of the long fibers 203a. The forces from the long fibers are converted into circumferential forces by the ring shape. This increases the strength of the connection.
Another difference is that in the fourth embodiment the connecting device 260 is elongated in the direction of its free end. The carrier extension portion 261a, around which the carrier structure 261 is extended, continues the taper shown in
The fifth embodiment differs from the fourth embodiment in that the connecting portion 210 additionally has a support layer 215 between the fiber deflecting element 214 and the fiber layer 203a. This support layer 215 extends away from the free end of the connecting portion 210 beyond the additional fiber deflecting element 214. The support layer 215 further homogenizes the tension in the connecting portion 210, so that said connecting portion has a greater load-bearing capability at only a slightly higher material cost for the support layer 215.
In addition, the fifth embodiment differs from the fourth embodiment in that the long fibers 201a, 202a and 203a are not continued beyond the tips 231, 232 and 233, respectively, into the second sloping surfaces 241, 242 and 243, respectively, as in the first embodiment shown in
| Number | Date | Country | Kind |
|---|---|---|---|
| 10 2020 112 179.2 | May 2020 | DE | national |
This application is the National Stage of PCT/DE2021/100406 filed on May 5, 2021, which claims priority under 35 U.S.C. §119 of German Application No. 10 2020 112 179.2 filed on May 6, 2020, the disclosure of which is incorporated by reference. The international application under PCT article 21(2) was not published in English.
| Filing Document | Filing Date | Country | Kind |
|---|---|---|---|
| PCT/DE2021/100406 | 5/5/2021 | WO |
