EP0733731A1 - Deformable technical fabric for the manufacture of construction parts or structural components - Google Patents
Deformable technical fabric for the manufacture of construction parts or structural components Download PDFInfo
- Publication number
- EP0733731A1 EP0733731A1 EP96104224A EP96104224A EP0733731A1 EP 0733731 A1 EP0733731 A1 EP 0733731A1 EP 96104224 A EP96104224 A EP 96104224A EP 96104224 A EP96104224 A EP 96104224A EP 0733731 A1 EP0733731 A1 EP 0733731A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- manufacture
- fabric
- structural components
- technical fabric
- fibers
- 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
Links
Images
Classifications
-
- D—TEXTILES; PAPER
- D03—WEAVING
- D03D—WOVEN FABRICS; METHODS OF WEAVING; LOOMS
- D03D15/00—Woven fabrics characterised by the material, structure or properties of the fibres, filaments, yarns, threads or other warp or weft elements used
- D03D15/60—Woven fabrics characterised by the material, structure or properties of the fibres, filaments, yarns, threads or other warp or weft elements used characterised by the warp or weft elements other than yarns or threads
- D03D15/67—Metal wires
Definitions
- the invention relates to a deformable, technical fabric for the production of components or structural parts.
- the invention has for its object to provide a technical fabric that is mechanically deformable and remains in the deformed state.
- Fig. 1 shows a technical fabric in which the warp threads and the weft threads alternately consist of C fibers or metal wire.
- binding wire quality steel, stainless steel, non-ferrous metals (aluminum alloys, titanium, copper) are used as metal wire.
- the wire diameter is 0.1 to 0.4 mm.
Landscapes
- Engineering & Computer Science (AREA)
- Textile Engineering (AREA)
- Woven Fabrics (AREA)
- Laminated Bodies (AREA)
Abstract
Description
Die Erfindung betrifft ein verformbares, technisches Gewebe zur Herstellung von Bauteilen oder Strukturteilen.The invention relates to a deformable, technical fabric for the production of components or structural parts.
Aus der DE 31 44 653 A1 sind Fasergewebe bekannt, bei denen die Kettfäden und die Schußfäden mit elektrisch leitfähigem Material umhüllt sind. Das Fasergewebe bildet eine leitfähige Barriere zur Verteilung von Strömen und soll Flugzeuge vor Blitzschlag-Schäden schützen. Weiter sind Fasergewebe mit eingewebten Aluminium-Drahteinlagen zur Herstellung oder Verbesserung der elektrischen Leitfähigkeit bekannt. Die Drähte sind jedoch so dünn, daß sie dem Gewebe keine Eigensteifigkeit vermitteln. DE 31 44 653 A1 discloses fiber fabrics in which the warp threads and the weft threads are covered with electrically conductive material. The fiber fabric forms a conductive barrier for the distribution of currents and is intended to protect aircraft from lightning damage. Furthermore, fiber fabrics with woven-in aluminum wire inserts for producing or improving the electrical conductivity are known. However, the wires are so thin that they do not impart any inherent stiffness to the fabric.
Der Erfindung liegt die Aufgabe zugrunde, ein technisches Gewebe zu schaffen, das mechanisch verformbar ist und im verformten Zustand verharrt.The invention has for its object to provide a technical fabric that is mechanically deformable and remains in the deformed state.
Diese Aufgabe wird erfindungsgemäß durch den Gegenstand des Hauptanspruchs gelöst. Die Unteransprüche betreffen vorteilhafte Ausgestaltungen der Erfindung.This object is achieved by the subject matter of the main claim. The subclaims relate to advantageous refinements of the invention.
Durch den Gegenstand der Erfindung ergeben sich folgende Vorteile:
- Herstellmöglichkeit von eigensteifen Formelementen aus Faserhalbzeug mit geringen Verformungskräften maschinell und/oder manuell.
- Beschickung der formgebenden Bauvorrichtung (Laminiervorrichtung) mit vorgeformten Faserelementen in kürzester Zeit mittels Roboter und/oder manuell.
- Keine oder nur einzelne Haltepunkte der vorgeformten Faserelemente in der Laminiervorrichtung erforderlich.
- Keine Überspannung von Kanten und Ecken beim Drapieren.
- Erhöhung der Bruchzähigkeit des Faserverbundwerkstoffes durch Metallarmierung.
- Verbesserung des Schadensverhaltens der Bauteile aus diesem Werkstoff.
- Possibility of producing inherently rigid molded elements from semi-finished fiber with low deformation forces by machine and / or manually.
- Loading of the shaping construction device (laminating device) with preformed fiber elements in the shortest possible time by means of robots and / or manually.
- No or only individual breakpoints of the preformed fiber elements in the laminating device are required.
- No over-tensioning of edges and corners when draping.
- Increasing the fracture toughness of the fiber composite material through metal reinforcement.
- Improvement of the damage behavior of the components made from this material.
Die Erfindung wird nachfolgend anhand von Figuren beschrieben.The invention is described below with reference to figures.
Es zeigen:
- Fig. 1
- ein Filamentgewebe mit Drahteinlagen,
- Fig. 2
- ein zweiteiliges Formteil aus vorverformtem, eigensteifen Fasergelege,
- Fig. 3
- einen U-Träger (Holm) mit profiliertem Steg aus vorverformtem, eigensteifen Fasergelege und
- Fig. 4
- zweiteilige Laminierform (Negativform) und Druckschlauch zur Herstellung eines Hohlprofils aus eigensteifen Fasergelegen nach Fig. 2.
- Fig. 1
- a filament fabric with wire inlays,
- Fig. 2
- a two-part molded part made of pre-formed, inherently rigid fiber fabric,
- Fig. 3
- a U-beam (spar) with a profiled web made of pre-formed, inherently stiff fiber fabric and
- Fig. 4
- two-part laminating mold (negative mold) and pressure hose for producing a hollow profile from inherently rigid fiber fabrics according to FIG. 2.
Nachfolgend wird Fig. 1 näher erläutert.
Fig. 1 zeigt ein technisches Gewebe, bei dem die Kettfäden und die Schußfäden jeweils wechselweise aus C-Fasern oder Metalldraht bestehen. Als Metalldraht wird z.B. Bindedrahtqualität, Werkstoff Stahl, nichtrostender Stahl, NE-Metalle (Aluminiumlegierungen, Titan, Kupfer) verwendet. Der Drahtdurchmesser beträgt 0,1 bis 0,4 mm.1 is explained in more detail below.
Fig. 1 shows a technical fabric in which the warp threads and the weft threads alternately consist of C fibers or metal wire. For example, binding wire quality, steel, stainless steel, non-ferrous metals (aluminum alloys, titanium, copper) are used as metal wire. The wire diameter is 0.1 to 0.4 mm.
Claims (4)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE19510980 | 1995-03-24 | ||
DE19510980A DE19510980C2 (en) | 1995-03-24 | 1995-03-24 | Deformable, technical fabric for the production of components or structural parts |
Publications (2)
Publication Number | Publication Date |
---|---|
EP0733731A1 true EP0733731A1 (en) | 1996-09-25 |
EP0733731B1 EP0733731B1 (en) | 1999-07-21 |
Family
ID=7757735
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP96104224A Expired - Lifetime EP0733731B1 (en) | 1995-03-24 | 1996-03-16 | Deformable technical fabric for the manufacture of construction parts or structural components |
Country Status (2)
Country | Link |
---|---|
EP (1) | EP0733731B1 (en) |
DE (1) | DE19510980C2 (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US10220593B2 (en) | 2013-07-26 | 2019-03-05 | Learjet Inc. | Composite material incorporating water ingress barrier |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE3144653A1 (en) * | 1980-11-13 | 1982-07-01 | Brunswick Corp., 60077 Skokie, Ill. | THREAD COMPOSITE CONSTRUCTIONS THAT PROVIDE LIGHTNING AND ELECTROMAGNETIC PROTECTION |
EP0074263A2 (en) * | 1981-09-04 | 1983-03-16 | Lear Fan Corp. | Graphite fiber reinforced laminate structure capable of withstanding lightning strikes |
WO1985000556A1 (en) * | 1983-07-25 | 1985-02-14 | Stern & Stern Textiles Inc. | Electrostatic dissipating fabric |
WO1990014224A1 (en) * | 1989-05-24 | 1990-11-29 | Auburn University | Mixed fiber composite structures: method of preparation, articles therefrom, and uses therefor |
US5171419A (en) * | 1990-01-18 | 1992-12-15 | American Cyanamid Company | Metal-coated fiber compositions containing alloy barrier layer |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE2933926A1 (en) * | 1979-08-22 | 1981-03-12 | Verseidag-Industrietextilien Gmbh, 4150 Krefeld | Prodn. of textile webs armoured by carbon fibres - created in situ by pyrolysing cellulose or acrylic copds. |
US4590122A (en) * | 1980-12-18 | 1986-05-20 | Fiberite Corporation | High conductivity graphite material with electrically conductive filaments wrapped around warp and fill elements |
JPH0823095B2 (en) * | 1989-06-06 | 1996-03-06 | 東レ株式会社 | Reinforcing fiber fabric |
WO1990015175A1 (en) * | 1989-06-08 | 1990-12-13 | Kanebo Ltd. | Textile of long high-purity alumina fiber, long high-purity alumina fiber used for producing said textile, and method of producing them |
-
1995
- 1995-03-24 DE DE19510980A patent/DE19510980C2/en not_active Expired - Fee Related
-
1996
- 1996-03-16 EP EP96104224A patent/EP0733731B1/en not_active Expired - Lifetime
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE3144653A1 (en) * | 1980-11-13 | 1982-07-01 | Brunswick Corp., 60077 Skokie, Ill. | THREAD COMPOSITE CONSTRUCTIONS THAT PROVIDE LIGHTNING AND ELECTROMAGNETIC PROTECTION |
EP0074263A2 (en) * | 1981-09-04 | 1983-03-16 | Lear Fan Corp. | Graphite fiber reinforced laminate structure capable of withstanding lightning strikes |
WO1985000556A1 (en) * | 1983-07-25 | 1985-02-14 | Stern & Stern Textiles Inc. | Electrostatic dissipating fabric |
WO1990014224A1 (en) * | 1989-05-24 | 1990-11-29 | Auburn University | Mixed fiber composite structures: method of preparation, articles therefrom, and uses therefor |
US5171419A (en) * | 1990-01-18 | 1992-12-15 | American Cyanamid Company | Metal-coated fiber compositions containing alloy barrier layer |
Non-Patent Citations (1)
Title |
---|
DR. HORST FREHSEN: "Kohlenstoff- und Graphitfasern, Herstellung, Eigenschaften und Verwendung", MELLIAND TEXTILBERICHTE, vol. 52, no. 1, January 1971 (1971-01-01), HEIDELBERG DE, pages 3 - 10, XP002006562 * |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US10220593B2 (en) | 2013-07-26 | 2019-03-05 | Learjet Inc. | Composite material incorporating water ingress barrier |
Also Published As
Publication number | Publication date |
---|---|
DE19510980C2 (en) | 1998-06-18 |
EP0733731B1 (en) | 1999-07-21 |
DE19510980A1 (en) | 1996-09-26 |
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