DE4004473A1 - Composite component prodn. with braided and unidirectional fibres - Google Patents
Composite component prodn. with braided and unidirectional fibresInfo
- Publication number
- DE4004473A1 DE4004473A1 DE4004473A DE4004473A DE4004473A1 DE 4004473 A1 DE4004473 A1 DE 4004473A1 DE 4004473 A DE4004473 A DE 4004473A DE 4004473 A DE4004473 A DE 4004473A DE 4004473 A1 DE4004473 A1 DE 4004473A1
- Authority
- DE
- Germany
- Prior art keywords
- fibers
- unidirectional
- braiding
- braided
- component
- 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.)
- Withdrawn
Links
Classifications
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- D—TEXTILES; PAPER
- D04—BRAIDING; LACE-MAKING; KNITTING; TRIMMINGS; NON-WOVEN FABRICS
- D04C—BRAIDING OR MANUFACTURE OF LACE, INCLUDING BOBBIN-NET OR CARBONISED LACE; BRAIDING MACHINES; BRAID; LACE
- D04C1/00—Braid or lace, e.g. pillow-lace; Processes for the manufacture thereof
- D04C1/06—Braid or lace serving particular purposes
-
- A—HUMAN NECESSITIES
- A61—MEDICAL OR VETERINARY SCIENCE; HYGIENE
- A61F—FILTERS IMPLANTABLE INTO BLOOD VESSELS; PROSTHESES; DEVICES PROVIDING PATENCY TO, OR PREVENTING COLLAPSING OF, TUBULAR STRUCTURES OF THE BODY, e.g. STENTS; ORTHOPAEDIC, NURSING OR CONTRACEPTIVE DEVICES; FOMENTATION; TREATMENT OR PROTECTION OF EYES OR EARS; BANDAGES, DRESSINGS OR ABSORBENT PADS; FIRST-AID KITS
- A61F2/00—Filters implantable into blood vessels; Prostheses, i.e. artificial substitutes or replacements for parts of the body; Appliances for connecting them with the body; Devices providing patency to, or preventing collapsing of, tubular structures of the body, e.g. stents
- A61F2/02—Prostheses implantable into the body
- A61F2/30—Joints
- A61F2/3094—Designing or manufacturing processes
- A61F2/30965—Reinforcing the prosthesis by embedding particles or fibres during moulding or dipping
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C53/00—Shaping by bending, folding, twisting, straightening or flattening; Apparatus therefor
- B29C53/56—Winding and joining, e.g. winding spirally
- B29C53/564—Winding and joining, e.g. winding spirally for making non-tubular articles
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C53/00—Shaping by bending, folding, twisting, straightening or flattening; Apparatus therefor
- B29C53/56—Winding and joining, e.g. winding spirally
- B29C53/58—Winding and joining, e.g. winding spirally helically
- B29C53/60—Winding and joining, e.g. winding spirally helically using internal forming surfaces, e.g. mandrels
- B29C53/62—Winding and joining, e.g. winding spirally helically using internal forming surfaces, e.g. mandrels rotatable about the winding axis
- B29C53/64—Winding and joining, e.g. winding spirally helically using internal forming surfaces, e.g. mandrels rotatable about the winding axis and moving axially
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C53/00—Shaping by bending, folding, twisting, straightening or flattening; Apparatus therefor
- B29C53/80—Component parts, details or accessories; Auxiliary operations
- B29C53/8008—Component parts, details or accessories; Auxiliary operations specially adapted for winding and joining
- B29C53/8016—Storing, feeding or applying winding materials, e.g. reels, thread guides, tensioners
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C53/00—Shaping by bending, folding, twisting, straightening or flattening; Apparatus therefor
- B29C53/80—Component parts, details or accessories; Auxiliary operations
- B29C53/8008—Component parts, details or accessories; Auxiliary operations specially adapted for winding and joining
- B29C53/805—Applying axial reinforcements
- B29C53/8058—Applying axial reinforcements continuously
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
- B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
- B29C70/06—Fibrous reinforcements only
- B29C70/08—Fibrous reinforcements only comprising combinations of different forms of fibrous reinforcements incorporated in matrix material, forming one or more layers, and with or without non-reinforced layers
- B29C70/083—Combinations of continuous fibres or fibrous profiled structures oriented in one direction and reinforcements forming a two dimensional structure, e.g. mats
-
- D—TEXTILES; PAPER
- D04—BRAIDING; LACE-MAKING; KNITTING; TRIMMINGS; NON-WOVEN FABRICS
- D04C—BRAIDING OR MANUFACTURE OF LACE, INCLUDING BOBBIN-NET OR CARBONISED LACE; BRAIDING MACHINES; BRAID; LACE
- D04C3/00—Braiding or lacing machines
- D04C3/02—Braiding or lacing machines with spool carriers guided by track plates or by bobbin heads exclusively
- D04C3/12—Braiding or lacing machines with spool carriers guided by track plates or by bobbin heads exclusively with means for introducing core threads
-
- D—TEXTILES; PAPER
- D04—BRAIDING; LACE-MAKING; KNITTING; TRIMMINGS; NON-WOVEN FABRICS
- D04C—BRAIDING OR MANUFACTURE OF LACE, INCLUDING BOBBIN-NET OR CARBONISED LACE; BRAIDING MACHINES; BRAID; LACE
- D04C3/00—Braiding or lacing machines
- D04C3/48—Auxiliary devices
-
- A—HUMAN NECESSITIES
- A61—MEDICAL OR VETERINARY SCIENCE; HYGIENE
- A61F—FILTERS IMPLANTABLE INTO BLOOD VESSELS; PROSTHESES; DEVICES PROVIDING PATENCY TO, OR PREVENTING COLLAPSING OF, TUBULAR STRUCTURES OF THE BODY, e.g. STENTS; ORTHOPAEDIC, NURSING OR CONTRACEPTIVE DEVICES; FOMENTATION; TREATMENT OR PROTECTION OF EYES OR EARS; BANDAGES, DRESSINGS OR ABSORBENT PADS; FIRST-AID KITS
- A61F2/00—Filters implantable into blood vessels; Prostheses, i.e. artificial substitutes or replacements for parts of the body; Appliances for connecting them with the body; Devices providing patency to, or preventing collapsing of, tubular structures of the body, e.g. stents
- A61F2/02—Prostheses implantable into the body
- A61F2/30—Joints
- A61F2/30767—Special external or bone-contacting surface, e.g. coating for improving bone ingrowth
- A61F2/30907—Nets or sleeves applied to surface of prostheses or in cement
-
- A—HUMAN NECESSITIES
- A61—MEDICAL OR VETERINARY SCIENCE; HYGIENE
- A61F—FILTERS IMPLANTABLE INTO BLOOD VESSELS; PROSTHESES; DEVICES PROVIDING PATENCY TO, OR PREVENTING COLLAPSING OF, TUBULAR STRUCTURES OF THE BODY, e.g. STENTS; ORTHOPAEDIC, NURSING OR CONTRACEPTIVE DEVICES; FOMENTATION; TREATMENT OR PROTECTION OF EYES OR EARS; BANDAGES, DRESSINGS OR ABSORBENT PADS; FIRST-AID KITS
- A61F2/00—Filters implantable into blood vessels; Prostheses, i.e. artificial substitutes or replacements for parts of the body; Appliances for connecting them with the body; Devices providing patency to, or preventing collapsing of, tubular structures of the body, e.g. stents
- A61F2/02—Prostheses implantable into the body
- A61F2/30—Joints
- A61F2/3094—Designing or manufacturing processes
-
- A—HUMAN NECESSITIES
- A61—MEDICAL OR VETERINARY SCIENCE; HYGIENE
- A61F—FILTERS IMPLANTABLE INTO BLOOD VESSELS; PROSTHESES; DEVICES PROVIDING PATENCY TO, OR PREVENTING COLLAPSING OF, TUBULAR STRUCTURES OF THE BODY, e.g. STENTS; ORTHOPAEDIC, NURSING OR CONTRACEPTIVE DEVICES; FOMENTATION; TREATMENT OR PROTECTION OF EYES OR EARS; BANDAGES, DRESSINGS OR ABSORBENT PADS; FIRST-AID KITS
- A61F2/00—Filters implantable into blood vessels; Prostheses, i.e. artificial substitutes or replacements for parts of the body; Appliances for connecting them with the body; Devices providing patency to, or preventing collapsing of, tubular structures of the body, e.g. stents
- A61F2/02—Prostheses implantable into the body
- A61F2/30—Joints
- A61F2/32—Joints for the hip
- A61F2/36—Femoral heads ; Femoral endoprostheses
- A61F2/3662—Femoral shafts
-
- A—HUMAN NECESSITIES
- A61—MEDICAL OR VETERINARY SCIENCE; HYGIENE
- A61F—FILTERS IMPLANTABLE INTO BLOOD VESSELS; PROSTHESES; DEVICES PROVIDING PATENCY TO, OR PREVENTING COLLAPSING OF, TUBULAR STRUCTURES OF THE BODY, e.g. STENTS; ORTHOPAEDIC, NURSING OR CONTRACEPTIVE DEVICES; FOMENTATION; TREATMENT OR PROTECTION OF EYES OR EARS; BANDAGES, DRESSINGS OR ABSORBENT PADS; FIRST-AID KITS
- A61F2/00—Filters implantable into blood vessels; Prostheses, i.e. artificial substitutes or replacements for parts of the body; Appliances for connecting them with the body; Devices providing patency to, or preventing collapsing of, tubular structures of the body, e.g. stents
- A61F2/02—Prostheses implantable into the body
- A61F2/30—Joints
- A61F2/32—Joints for the hip
- A61F2/36—Femoral heads ; Femoral endoprostheses
- A61F2/3662—Femoral shafts
- A61F2/367—Proximal or metaphyseal parts of shafts
-
- A—HUMAN NECESSITIES
- A61—MEDICAL OR VETERINARY SCIENCE; HYGIENE
- A61F—FILTERS IMPLANTABLE INTO BLOOD VESSELS; PROSTHESES; DEVICES PROVIDING PATENCY TO, OR PREVENTING COLLAPSING OF, TUBULAR STRUCTURES OF THE BODY, e.g. STENTS; ORTHOPAEDIC, NURSING OR CONTRACEPTIVE DEVICES; FOMENTATION; TREATMENT OR PROTECTION OF EYES OR EARS; BANDAGES, DRESSINGS OR ABSORBENT PADS; FIRST-AID KITS
- A61F2/00—Filters implantable into blood vessels; Prostheses, i.e. artificial substitutes or replacements for parts of the body; Appliances for connecting them with the body; Devices providing patency to, or preventing collapsing of, tubular structures of the body, e.g. stents
- A61F2/02—Prostheses implantable into the body
- A61F2/30—Joints
- A61F2002/30001—Additional features of subject-matter classified in A61F2/28, A61F2/30 and subgroups thereof
- A61F2002/30003—Material related properties of the prosthesis or of a coating on the prosthesis
- A61F2002/30004—Material related properties of the prosthesis or of a coating on the prosthesis the prosthesis being made from materials having different values of a given property at different locations within the same prosthesis
- A61F2002/30009—Material related properties of the prosthesis or of a coating on the prosthesis the prosthesis being made from materials having different values of a given property at different locations within the same prosthesis differing in fibre orientations
-
- A—HUMAN NECESSITIES
- A61—MEDICAL OR VETERINARY SCIENCE; HYGIENE
- A61F—FILTERS IMPLANTABLE INTO BLOOD VESSELS; PROSTHESES; DEVICES PROVIDING PATENCY TO, OR PREVENTING COLLAPSING OF, TUBULAR STRUCTURES OF THE BODY, e.g. STENTS; ORTHOPAEDIC, NURSING OR CONTRACEPTIVE DEVICES; FOMENTATION; TREATMENT OR PROTECTION OF EYES OR EARS; BANDAGES, DRESSINGS OR ABSORBENT PADS; FIRST-AID KITS
- A61F2250/00—Special features of prostheses classified in groups A61F2/00 - A61F2/26 or A61F2/82 or A61F9/00 or A61F11/00 or subgroups thereof
- A61F2250/0014—Special features of prostheses classified in groups A61F2/00 - A61F2/26 or A61F2/82 or A61F9/00 or A61F11/00 or subgroups thereof having different values of a given property or geometrical feature, e.g. mechanical property or material property, at different locations within the same prosthesis
- A61F2250/0028—Special features of prostheses classified in groups A61F2/00 - A61F2/26 or A61F2/82 or A61F9/00 or A61F11/00 or subgroups thereof having different values of a given property or geometrical feature, e.g. mechanical property or material property, at different locations within the same prosthesis differing in fibre orientations
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
- B29L2031/00—Other particular articles
- B29L2031/753—Medical equipment; Accessories therefor
- B29L2031/7532—Artificial members, protheses
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- D—TEXTILES; PAPER
- D10—INDEXING SCHEME ASSOCIATED WITH SUBLASSES OF SECTION D, RELATING TO TEXTILES
- D10B—INDEXING SCHEME ASSOCIATED WITH SUBLASSES OF SECTION D, RELATING TO TEXTILES
- D10B2505/00—Industrial
- D10B2505/02—Reinforcing materials; Prepregs
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Health & Medical Sciences (AREA)
- Textile Engineering (AREA)
- Manufacturing & Machinery (AREA)
- Heart & Thoracic Surgery (AREA)
- General Health & Medical Sciences (AREA)
- Oral & Maxillofacial Surgery (AREA)
- Transplantation (AREA)
- Biomedical Technology (AREA)
- Orthopedic Medicine & Surgery (AREA)
- Vascular Medicine (AREA)
- Life Sciences & Earth Sciences (AREA)
- Animal Behavior & Ethology (AREA)
- Cardiology (AREA)
- Public Health (AREA)
- Veterinary Medicine (AREA)
- Chemical & Material Sciences (AREA)
- Composite Materials (AREA)
- Prostheses (AREA)
- Yarns And Mechanical Finishing Of Yarns Or Ropes (AREA)
- Multicomponent Fibers (AREA)
- Braiding, Manufacturing Of Bobbin-Net Or Lace, And Manufacturing Of Nets By Knotting (AREA)
Abstract
Description
Die Erfindung bezieht sich auf ein Verfahren zur Herstellung von Bauteilen mit mindestens einer Lage aus längs des Bau teiles gerichteten unidirektionalen Fasern, bei dem ein Stützkern hergestellt wird, der anschließend zusammen mit das Bauteil zumindest teilweise umgebenden, unter Spannung gehaltenen unidirektonalen Fasern durch eine Vorrichtung geführt wird, derart, daß die unidirektionalen Fasern auf das Bauteil aufgelegt und mittels Harz verklebt werden.The invention relates to a method of manufacture of components with at least one layer along the construction part directional unidirectional fibers, in which a Support core is produced, which then together with at least partially surrounding the component, under tension held unidirectonal fibers by a device is performed such that the unidirectional fibers on the component is placed and glued with resin.
Ein Verfahren dieser Art ist aus der DE 34 13 601 A1 bekannt, bei dem zur Herstellung von Verbundprofilen ein vorgefertig ter Stützkern zusammen mit umgebenden Verstärkungsfasern in einen Formkanal eingeführt, mit flüssigem Kunstharz getränkt und anschließend einem Aushärtungsprozeß unterworfen wird. Hierdurch können Bauteile mit längs des Bauteiles gerichte ten, sogenannten unidirektionalen Fasern fertigungstechnisch einfach umgeben werden. Allerdings ist das Verfahren nur bei Bauteilen geeignet, die einen konstanten Querschnitt haben.A method of this type is known from DE 34 13 601 A1, in which a prefabricated for the production of composite profiles ter support core together with surrounding reinforcing fibers in introduced a mold channel, impregnated with liquid synthetic resin and then subjected to a curing process. This allows components to be aligned along the component ten, so-called unidirectional fibers manufacturing technology just be surrounded. However, the procedure is only for Suitable components that have a constant cross section.
Dieser Mangel wird gemäß einem Vorschlag nach der DE 39 19 508 dadurch behoben, daß anstelle der starren Form eine Membran verwendet wird, deren Öffnung sich automatisch an die Kontur des durchzuführenden Bauteiles anpaßt. This shortcoming is allegedly proposed according to the DE 39 19 508 resolved that instead of the rigid form a membrane is used, the opening of which is automatic adapts to the contour of the component to be carried out.
Bei Anwendung dieser Methode können sich jedoch noch Pro bleme mit gekrümmten Bauteilen ergeben. Die den Kern umgebenden, unter Spannung gehaltenen Fasern werden bei Krümmungen des Stützkernes den kürzeren Weg einnehmen wollen, wodurch ein Verrutschen der Faser zur konkaven Seite des Bauteiles sowie das Abheben der Fasern an kon kaven Seiten möglich ist.When using this method, however, Pro arise with curved components. The core surrounding, kept under tension fibers Curvatures of the support core take the shorter path want, causing the fiber to slip to the concave Side of the component and the lifting of the fibers at con kaven sides is possible.
Der Erfindung liegt die Aufgabe zugrunde, ein Verfahren der eingangs genannten Art dahingehend zu verbessern, daß damit Bauteile jeder Konfiguration unter Beibehaltung der ferti gungstechnischen Einfachheit mit unidirektionalen Fasern überzogen werden können.The invention has for its object a method of to improve the type mentioned in such a way that Components of any configuration while maintaining the ferti engineering simplicity with unidirectional fibers can be covered.
Die Aufgabe wird erfindungsgemäß mit den Merkmalen des Anspruchs 1 gelöst.The object is achieved with the features of Claim 1 solved.
Die Fasern des Flechtwerkes winden sich automatisch um den Kern herum und drücken dabei zwischen Kern und Flechtfasern befindliche unidirektionale Fasern an den Kern. Hierbei ersetzen die Flechtfasern nicht nur die bei dem bekannten Verfahren verwendete starre Form bzw. Membran, sondern sie bilden gleichzeitig einen Torsionskasten für das Bauteil, der die bei Belastung auftretenden Radialkräfte aufnimmt.The fibers of the wickerwork automatically wind around the Core around and press between the core and braided fibers located unidirectional fibers to the core. Here The braided fibers do not only replace the known ones Process used rigid form or membrane, but they at the same time form a torsion box for the component, which absorbs the radial forces occurring under load.
Mit dem Verfahren wird außerdem eine Führung der unidirek tionalen Fasern bewirkt, indem diese oder Teile davon bei Bedarf gleichzeitig mit umflochten werden. Auf diese Weise wird gleichzeitig ein Verrutschen in Umfangsrichtung der unidirektionalen Fasern verhindert. The procedure also leads unidirek tional fibers caused by these or parts thereof Need to be braided at the same time. In this way is at the same time slipping in the circumferential direction of the unidirectional fibers prevented.
Gemäß einer Ausgestaltung der Erfindung sind die unidirek tionalen Fasern zwischen dem Stützkern und den Flechtfasern ge führt. Diese Ausgestaltung hat den Vorteil, daß die uni direktionalen Fasern zur optimalen Nutzung der Faserfestig keit in gespannter Form in das Bauteil eingebracht werden, während sich das Flechtwerk um die unidirektionale Faser lage legt.According to one embodiment of the invention, the unidirek tional fibers between the support core and the braided fibers leads. This configuration has the advantage that the uni directional fibers for optimal use of fiber strength be introduced into the component in a tensioned form, while the wattle around the unidirectional fiber location.
Gemäß einer weiteren Ausgestaltung der Erfindung, kann zumindest ein Teil der unidirektionalen Fasern in das Flechtwerk einbezogen werden, wodurch deren Führung entlang der Mantellinie des Bauteiles gegeben ist. Diese Ausgestal tung eignet sich insbesondere für stark gekrümmte Bauteile, bei denen eine möglichst genaue Führung der unidirektionalen Fasern entlang der Mantellinien gewünscht wird.According to a further embodiment of the invention, at least part of the unidirectional fibers in that Wickerwork can be included, thereby guiding it along the surface line of the component is given. This shape device is particularly suitable for strongly curved components, where the most accurate guidance of the unidirectional Fibers along the surface lines is desired.
In diesem Fall werden die gewählten unidirektionalen Fasern mit Flechtfasern unterlegt, so daß diese Fasern in ihrer Wirkung an Festigkeit einbüßen. Ein Ausgleich kann aller dings durch Anhebung der Faserlagenzahl erreicht werden. Es ist aber auch möglich, durch Wahl sehr dünner Flecht fasern die Festigkeitseinbußen zu verringern.In this case, the chosen unidirectional fibers underlaid with braided fibers, so that these fibers in their Loss of strength. Anyone can compensate dings can be achieved by increasing the number of fiber layers. But it is also possible to choose very thin braiding fibers to reduce the loss of strength.
Es ist selbstverständlich jede Kombination möglich, bei der mehr oder weniger unidirektionale Fasern zwischen dem Kern und den Flechtfasern bzw. innerhalb des Geflechtes geführt werden. Of course, any combination is possible in which more or less unidirectional fibers between the Core and the braided fibers or within the braid be performed.
Die Einbringung eines Harzes erfolgt nach konventionellen Methoden, z. B. durch Tränken der Fasern vor oder nach deren Aufbringung auf den Stützkern. Das nach dem oben beschriebenen Verfahren hergestellte Bauteil wird an schließend oder während des Durchziehens durch das Fadenauge einer Wärmebehandlung unterzogen, um das Harz auszuhärten.A resin is introduced according to conventional methods Methods, e.g. B. by soaking the fibers before or after their application to the support core. That after the above Component manufactured described is to closing or while pulling through the thread eye subjected to heat treatment to cure the resin.
Die Erfindung erstreckt sich auf die Anwendung des er findungsgemäßen Verfahrens zur Herstellung von Knochen implantaten, insbesondere zur Herstellung des Schaftes für eine Hüftgelenk-Endoprothese. Ein vorgefertigter Kern wird vorzugsweise vollständig mit straffgezogenen unidirektiona len Fasern umlegt, wobei die Flechtfasern die unidirektiona len Fasern umgeben.The invention extends to the application of the Process according to the invention for the production of bones implants, in particular for the manufacture of the shaft for a hip joint endoprosthesis. A pre-made core will preferably completely with taut unidirectional len fibers, the braided fibers the unidirectional len fibers surround.
Aufgrund der Krümmung, die ein Implantatschaft aufweist, können zumindest ein Teil der unidirektionalen Fasern um flochten werden, um diese entsprechend in der Krümmung führen zu können. Die Enden des Schaftes können ausschließ lich aus den unidirektionalen und den Flechtfasern bestehen, wobei der Stützkern lediglich als Verdrängerkörper zur Bildung des Bereiches mit dickerem Querschnitt verwendet wird.Because of the curvature that an implant shaft has, can um at least part of the unidirectional fibers be braided to match this in the curvature to be able to lead. The ends of the shaft can exclude consist of unidirectional and braided fibers, the support core only as a displacement body Formation of the area with a thicker cross section is used becomes.
Zur Anwendung des erfindungsgemäßen Verfahrens kann eine im Handel erhältliche Flechtmaschine verwendet werden, die um Faserführungen für die unidirektionalen Fasern erweitert wird.One can use the method according to the invention commercially available braiding machine can be used, the expanded with fiber guides for the unidirectional fibers becomes.
Die Erfindung wird anhand von in der Zeichnung schematisch dargestellten Ausführungsbeispielen näher beschrieben. Es zeigen:The invention is illustrated schematically in the drawing illustrated embodiments described in more detail. Show it:
Fig. 1 und 2 eine Anlage zum Durchführen des Verfahrens im Schnitt bzw. in Draufsicht, Fig. 1 and 2, a plant for carrying out the method in section and in plan view,
Fig. 3 den Faserverlauf an einem Bauteil und Fig. 3 shows the fiber course on a component and
Fig. 4 und 5 je einen Querschnitt eines fertigen Bauteiles. FIGS. 4 and 5 each shows a cross section of a finished component.
In Fig. 1 ist die Herstellung eines Prothesenschaftes ge zeigt, der zunächst aus einem vorgefertigten Stützkern 10 besteht. Der Stützkern 10 wird durch ein Fadenauge 11 einer Flechtmaschine 12 mittels eines Greifers 13 durchgezogen. Die Flechtmaschine 12 besteht aus einem Führungsring 14, auf dem zwei sinusförmige Führungsschienen 15 bzw. 16 (Fig. 2) vorgesehen sind. In der einen Schiene 15 wird eine bestimmte Anzahl von Klöppel 17 einer ersten Gruppe in eine Rich tung 18 geführt, während eine zweite Gruppe Klöppel 19 auf der zweiten Schiene 16 in die Gegenrichtung 20 geführt wird.In Fig. 1, the manufacture of a prosthesis socket is shown, which initially consists of a prefabricated support core 10 . The support core 10 is pulled through a thread eye 11 of a braiding machine 12 by means of a gripper 13 . The braiding machine 12 consists of a guide ring 14 on which two sinusoidal guide rails 15 and 16 ( FIG. 2) are provided. In one rail 15 , a certain number of clappers 17 of a first group are guided in one direction 18 , while a second group of clappers 19 are guided on the second rail 16 in the opposite direction 20 .
Bei der so beschriebenen Bewegung der Klöppel 17 bzw. 19 wird jede einzelne Faser 21 einmal unter eine andere Faser und einmal über eine andere Faser gelegt. Zusätzlich zu den Flechtfasern 21, 22 der beiden Klöppelgruppen 17, 19 sind über einen inneren Ring 50 (Fig. 2) geführte uni direktionale Fasern 25 vorgesehen, die zwischen dem Kern 10 und den Flechtfasern 21, 22 durch das Fadenauge 11 durch gezogen werden. Sämtliche Faserenden werden mit dem Greifer 13 verbunden, der gleichzeitig den Stützkern 10 trägt und ihn mit einer vorgegebenen Geschwindigkeit vom Fadenauge 11 wegbewegt. Für gekrümmte oder unregelmäßige Bauteile, wie es beim Prothesenschaft der Fall ist, ist der Greifer 13 mit Gelenken 30, Teleskopeinrichtung 31 oder dergleichen ausgerüstet, um zusätzlich zur Vorschubbewegung 32 auch noch Schwenkbewegungen durchführen zu können. Damit kann das Bauteil jeweils so gerichtet werden, daß die Achse des Bauteilbereiches, das gerade auf der Fadenaugenebene liegt, auf der Flechtmaschinenachse steht. Auf diese Weise werden die unter Spannung gehaltenen unidirektionalen Fasern 25 stets den Mantellinien 35 (Fig. 3) des Bauteiles folgen.During the movement of the clappers 17 and 19 described in this way , each individual fiber 21 is placed once under another fiber and once over another fiber. In addition to the braiding fibers 21 , 22 of the two bobbin groups 17 , 19 , uni-directional fibers 25 are provided via an inner ring 50 ( FIG. 2), which are drawn between the core 10 and the braiding fibers 21 , 22 through the thread eye 11 . All fiber ends are connected to the gripper 13 , which at the same time carries the support core 10 and moves it away from the thread eye 11 at a predetermined speed. For curved or irregular components, as is the case with the prosthetic socket, the gripper 13 is equipped with joints 30 , telescopic device 31 or the like in order to be able to carry out swiveling movements in addition to the feed movement 32 . In this way, the component can be aligned in such a way that the axis of the component area that is currently on the thread eye plane is on the braiding machine axis. In this way, the unidirectional fibers 25 kept under tension will always follow the surface lines 35 ( FIG. 3) of the component.
Die einzelnen Flechtfasern 21 bzw. 22 beschreiben im Verlauf des Flechtprozesses eine Schraubenlinie, wie sie in Fig. 3 mit der dickgezeichneten Faser 21 gezeigt ist. Bei diesem Verlauf drückt die Flechtfaser 21 die unidirektionalen Fasern, die der Mantellinie 35 des Stützkernes 10′ folgen, an den Stützkern 10 bzw. 10′. Die Steigung der umwickelten Flechtfasern bzw. deren Orientierung am fertigen Bauteil wird durch die geometrischen Verhältnisse der Flechtmaschine 12, dem Querschnitt des Bauteiles bzw. Stützkernes 10 und der Geschwindigkeit, mit der das Bauteil 10 bewegt wird, be stimmt. Durch Automatisierung und Programmierung des Greiferbewegungsmechanismus kann die Vorschubgeschwindigkeit entsprechend der Geometrie bzw. dem Querschnitt des Bau teiles 10 verändert werden, um die gewünschte Orientierung der Flechtfasern 21, 22 über das gesamte Bauteil zu erhal ten. The individual braiding fibers 21 and 22 describe a helix in the course of the braiding process, as is shown in FIG. 3 with the thick-drawn fiber 21 . In this course, the braiding fiber 21 presses the unidirectional fibers, which follow the surface line 35 of the support core 10 ', to the support core 10 or 10 '. The gradient of the wrapped braiding fibers or their orientation on the finished component is determined by the geometric conditions of the braiding machine 12 , the cross section of the component or support core 10 and the speed at which the component 10 is moved. By automating and programming the gripper movement mechanism, the feed speed can be changed in accordance with the geometry or the cross section of the construction part 10 in order to obtain the desired orientation of the braided fibers 21 , 22 over the entire component.
Sowohl die Flechtfasern 21 als auch die unidirektionalen Fasern 25 können vorab durch Tränkeinrichtungen mit einer Matrix getränkt werden. Die Aushärtung des Harzes wird mittels der über dem Fadenauge 11 vorgesehenen Heizeinrich tung 37 bewirkt. Die Einführung des Matrixmaterials sowie deren Härtung kann auch auf jede andere bekannte Art durch geführt werden.Both the braided fibers 21 and the unidirectional fibers 25 can be impregnated with impregnation devices with a matrix beforehand. The curing of the resin is effected by means of the Heizeinrich device 37 provided above the thread eye 11 . The introduction of the matrix material and its hardening can also be carried out in any other known way.
Bei den bisher beschriebenen Schritten bilden die uni direktionalen Fasern 25 eine innere Faserschicht, die von dem Flechtwerk 55 umgeben ist. In einem Längsschnitt durch das fertige Bauteil 40, wie in Fig. 4 gezeigt, ist an der Oberfläche 41 des Stützkernes 10 eine Längsfaser 25 zu sehen, auf der sich die Flechtfasern 21 bzw. 22 befinden. In diesem Fall legt sich die unidirektionale Faser 25 genau parallel an die Mantellinie 35 des Stützkernes 10 an. Sie ist dabei gestreckt, wodurch das Bauteil die optimale Festigkeit für Druck/Zug-Belastungen hat.In the steps described so far, the uni-directional fibers 25 form an inner fiber layer which is surrounded by the wattle 55 . In a longitudinal section through the finished component 40 , as shown in FIG. 4, a longitudinal fiber 25 can be seen on the surface 41 of the support core 10 , on which the braided fibers 21 and 22 are located. In this case, the unidirectional fiber 25 lies exactly parallel to the surface line 35 of the support core 10 . It is stretched, which means that the component has the optimum strength for compressive / tensile loads.
Wenn ein Bauteil starke Krümmungen aufweist, wie es z. B. beim Prothesenschaft der Fall sein kann, wäre zusätzlich zur radialen Führung der unidirektionalen Fasern 25 eine tangentiale Führung zweckmäßig, um ein Abrutschen der unter Zugspannung stehenden Fasern 25 in den Krümmungs bereichen 38 des Stützkernes 10 zu vermeiden. In diesem Fall wird ein Teil der unidirektionalen Fasern 25 nicht inner halb des, sondern durch den Flechtring 14 geführt. Dieses ist in Fig. 2 näher gezeigt, bei dem der innere Ring 50 nicht alle, wie oben beschrieben, sondern nur einen Großteil der unidirektionalen Fasern 25 führt, während im Flechtring 14 stehende Fadenaugen 51 für unidirektionale Fasern 25, vorgesehen sind. Diese Fasern 25′ werden abwechselnd von der einen Klöppelgruppe 17 unterfahren und von der anderen Klöppelgruppe 19 überfahren, so daß diese unidirektionalen Fasern 25′ zusätzlich zur radialen Führung durch die Flechtfasern 21, 22 auch eine tangentiale Führung, wie in Fig. 3 mit den Pfeilen 52 angedeutet, erfahren. Damit wer den sie in ihrer Position, d. h. entlang der entsprechenden Mantellinie 35 des Stützkernes 10′ gehalten.If a component has strong curvatures, such as. May be for example in the prosthesis shaft the case would be in addition to the radial guide of the unidirectional fibers 25, a tangential guide expedient to slippage of the fibers under tensile stress areas 25 in the curve 38 of the support core 10 to be avoided. In this case, a part of the unidirectional fibers 25 is not within, but led through the braid ring 14 . This is shown in more detail in FIG. 2, in which the inner ring 50 does not guide all, as described above, but rather only a large part of the unidirectional fibers 25 , while thread eyes 51 for unidirectional fibers 25 are provided in the ring 14 . These fibers 25 'are alternately passed under by one bobbin group 17 and passed over by the other bobbin group 19 , so that these unidirectional fibers 25 ' in addition to the radial guidance through the braided fibers 21 , 22 also a tangential guidance, as in Fig. 3 with the arrows 52 indicated, experienced. So who the they held in their position, ie along the corresponding surface line 35 of the support core 10 '.
In diesem Fall wird, wie in Fig. 5 gezeigt, die entsprechen de unidirektionale Faser 25′ stellenweise durch Flecht fasern 21 unterlegt und dazwischen mit Flechtfasern 22 umwickelt, so daß die unidirektionale Faser 25′ ihre opti male gespannte Lage verliert. Mit sehr dünnen Flecht fasern 21 bzw. 22 kann dieser Nachteil minimiert werden, wenn es darauf ankommt. Das Verhältnis der durch den inne ren Ring 50 und dem Flechtring 14 geführten unidirektionalen Fasern 25 bzw. 25′ kann beliebig gewählt werden. Es wird sich in der Regel nach dem jeweiligen Anwendungsfall und dessen Anforderungen richten.In this case, as shown in Fig. 5, the corresponding de unidirectional fiber 25 'underlaid in places by braiding fibers 21 and wrapped in between with braiding fibers 22 , so that the unidirectional fiber 25 ' loses its optimal tensioned position. With very thin braiding fibers 21 and 22 , this disadvantage can be minimized when it matters. The ratio of the unidirectional fibers 25 and 25 'guided by the inner ring 50 and the braid ring 14 ' can be chosen as desired. It will usually depend on the respective application and its requirements.
Für die Herstellung eines Schaftes für ein Hüftgelenk- Implantat mit unidirektionalen Fasern wird man das Verhält nis zwischen im Innenring 50 und im Flechtring 14 geführten unidirektionalen Fasern 25 bzw. 25′ möglichst groß wählen.For the manufacture of a shaft for a hip joint implant with unidirectional fibers, the ratio between the inner ring 50 and the braid ring 14 guided unidirectional fibers 25 and 25 'should be chosen as large as possible.
Claims (5)
Priority Applications (7)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE4004473A DE4004473A1 (en) | 1990-02-14 | 1990-02-14 | Composite component prodn. with braided and unidirectional fibres |
ES90124369T ES2072358T3 (en) | 1990-02-14 | 1990-12-17 | PROCEDURE FOR THE MANUFACTURE OF COMPONENTS COMPOSED OF FIBERS. |
AT90124369T ATE122962T1 (en) | 1990-02-14 | 1990-12-17 | METHOD FOR PRODUCING FIBER COMPOSITE COMPONENTS. |
EP90124369A EP0442092B1 (en) | 1990-02-14 | 1990-12-17 | Method of manufacturing fibre reinforced products |
DE59009143T DE59009143D1 (en) | 1990-02-14 | 1990-12-17 | Process for the production of fiber composite components. |
DE4124015A DE4124015A1 (en) | 1990-02-14 | 1991-07-19 | Prodn. of wound fibre components |
EP92111292A EP0523471A1 (en) | 1990-02-14 | 1992-07-03 | Method of manufacturing fibre reinforced products |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE4004473A DE4004473A1 (en) | 1990-02-14 | 1990-02-14 | Composite component prodn. with braided and unidirectional fibres |
Publications (1)
Publication Number | Publication Date |
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DE4004473A1 true DE4004473A1 (en) | 1991-08-22 |
Family
ID=6400082
Family Applications (2)
Application Number | Title | Priority Date | Filing Date |
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DE4004473A Withdrawn DE4004473A1 (en) | 1990-02-14 | 1990-02-14 | Composite component prodn. with braided and unidirectional fibres |
DE59009143T Expired - Fee Related DE59009143D1 (en) | 1990-02-14 | 1990-12-17 | Process for the production of fiber composite components. |
Family Applications After (1)
Application Number | Title | Priority Date | Filing Date |
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DE59009143T Expired - Fee Related DE59009143D1 (en) | 1990-02-14 | 1990-12-17 | Process for the production of fiber composite components. |
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AT (1) | ATE122962T1 (en) |
DE (2) | DE4004473A1 (en) |
ES (1) | ES2072358T3 (en) |
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102005027879A1 (en) * | 2005-06-09 | 2006-12-14 | Deutsche Institute für Textil- und Faserforschung Stuttgart - Stiftung des öffentlichen Rechts | Rod-shaped fiber composite material, method and apparatus for its production |
EP2189273A1 (en) * | 2007-08-10 | 2010-05-26 | Toyota Jidosha Kabushiki Kaisha | Fiber-reinforced resin member, process for producing the same, and apparatus for producing woven fiber fabric |
DE102010049563A1 (en) * | 2010-10-25 | 2012-04-26 | Daimler Ag | Method for manufacturing torsion bar spring of motor car, involves thermally melting matrix material during and/or after braiding and/or wrapping of core, and connecting component to torsion bar spring |
DE102012222762A1 (en) * | 2012-12-11 | 2014-06-12 | Sgl Kümpers Gmbh & Co. Kg | Braiding machine for manufacturing braided fabric structures, has ring-shaped structure arranged in section between discharge eyelets of bobbins and braiding ring, where outer diameter of structure is larger than inner diameter of ring |
DE102016122522A1 (en) * | 2016-11-22 | 2018-05-24 | Mt Aerospace Ag | Thread eye of a winding machine, a method for producing the thread eye and its use |
DE102017009839A1 (en) * | 2017-07-12 | 2019-01-17 | Oke Kunststofftechnik Gmbh & Co. Kg | Method for producing a composite profile and composite profile |
DE102018211793A1 (en) * | 2018-07-16 | 2020-01-16 | Sgl Carbon Se | Process for producing a hollow profile with variable curvatures and cross sections |
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- 1990-02-14 DE DE4004473A patent/DE4004473A1/en not_active Withdrawn
- 1990-12-17 DE DE59009143T patent/DE59009143D1/en not_active Expired - Fee Related
- 1990-12-17 AT AT90124369T patent/ATE122962T1/en not_active IP Right Cessation
- 1990-12-17 ES ES90124369T patent/ES2072358T3/en not_active Expired - Lifetime
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Cited By (12)
Publication number | Priority date | Publication date | Assignee | Title |
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DE102005027879A1 (en) * | 2005-06-09 | 2006-12-14 | Deutsche Institute für Textil- und Faserforschung Stuttgart - Stiftung des öffentlichen Rechts | Rod-shaped fiber composite material, method and apparatus for its production |
US8104392B2 (en) | 2005-06-09 | 2012-01-31 | Deutsche Institute Fur Textil-Und Faserforschung Denkendorf Stiftung Des Oeffentlichen Rechts | Rod-shaped fibre composite, and method and device for the production thereof |
EP2189273A1 (en) * | 2007-08-10 | 2010-05-26 | Toyota Jidosha Kabushiki Kaisha | Fiber-reinforced resin member, process for producing the same, and apparatus for producing woven fiber fabric |
EP2189273A4 (en) * | 2007-08-10 | 2010-12-15 | Toyota Motor Co Ltd | Fiber-reinforced resin member, process for producing the same, and apparatus for producing woven fiber fabric |
US8006601B2 (en) | 2007-08-10 | 2011-08-30 | Toyota Jidosha Kabushiki Kaisha | Fiber reinforced resin member and method of manufacturing the same, and apparatus manufacturing fiber fabric |
DE102010049563A1 (en) * | 2010-10-25 | 2012-04-26 | Daimler Ag | Method for manufacturing torsion bar spring of motor car, involves thermally melting matrix material during and/or after braiding and/or wrapping of core, and connecting component to torsion bar spring |
DE102010049563B4 (en) * | 2010-10-25 | 2017-09-14 | Daimler Ag | Method for producing a torsion spring |
DE102012222762A1 (en) * | 2012-12-11 | 2014-06-12 | Sgl Kümpers Gmbh & Co. Kg | Braiding machine for manufacturing braided fabric structures, has ring-shaped structure arranged in section between discharge eyelets of bobbins and braiding ring, where outer diameter of structure is larger than inner diameter of ring |
DE102016122522A1 (en) * | 2016-11-22 | 2018-05-24 | Mt Aerospace Ag | Thread eye of a winding machine, a method for producing the thread eye and its use |
DE102017009839A1 (en) * | 2017-07-12 | 2019-01-17 | Oke Kunststofftechnik Gmbh & Co. Kg | Method for producing a composite profile and composite profile |
CN110678308A (en) * | 2017-07-12 | 2020-01-10 | Oke集团有限责任公司 | Method for producing a composite molded part and composite molded part |
DE102018211793A1 (en) * | 2018-07-16 | 2020-01-16 | Sgl Carbon Se | Process for producing a hollow profile with variable curvatures and cross sections |
Also Published As
Publication number | Publication date |
---|---|
ES2072358T3 (en) | 1995-07-16 |
DE59009143D1 (en) | 1995-06-29 |
ATE122962T1 (en) | 1995-06-15 |
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