WO1997000167A1 - Process for joining an in particular non-textile cellular structure to textile coating layers - Google Patents
Process for joining an in particular non-textile cellular structure to textile coating layers Download PDFInfo
- Publication number
- WO1997000167A1 WO1997000167A1 PCT/EP1996/002607 EP9602607W WO9700167A1 WO 1997000167 A1 WO1997000167 A1 WO 1997000167A1 EP 9602607 W EP9602607 W EP 9602607W WO 9700167 A1 WO9700167 A1 WO 9700167A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- textile
- thread
- sandwich
- cell
- layers
- Prior art date
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B3/00—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar form; Layered products having particular features of form
- B32B3/10—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar form; Layered products having particular features of form characterised by a discontinuous layer, i.e. formed of separate pieces of material
- B32B3/12—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar form; Layered products having particular features of form characterised by a discontinuous layer, i.e. formed of separate pieces of material characterised by a layer of regularly- arranged cells, e.g. a honeycomb structure
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B5/00—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
- B32B5/22—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed
- B32B5/24—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer
- B32B5/26—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer another layer next to it also being fibrous or filamentary
-
- 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
- B29C70/10—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres
- B29C70/16—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length
- B29C70/20—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length oriented in a single direction, e.g. roofing or other parallel fibres
-
- D—TEXTILES; PAPER
- D04—BRAIDING; LACE-MAKING; KNITTING; TRIMMINGS; NON-WOVEN FABRICS
- D04B—KNITTING
- D04B21/00—Warp knitting processes for the production of fabrics or articles not dependent on the use of particular machines; Fabrics or articles defined by such processes
- D04B21/14—Fabrics characterised by the incorporation by knitting, in one or more thread, fleece, or fabric layers, of reinforcing, binding, or decorative threads; Fabrics incorporating small auxiliary elements, e.g. for decorative purposes
- D04B21/16—Fabrics characterised by the incorporation by knitting, in one or more thread, fleece, or fabric layers, of reinforcing, binding, or decorative threads; Fabrics incorporating small auxiliary elements, e.g. for decorative purposes incorporating synthetic threads
-
- D—TEXTILES; PAPER
- D04—BRAIDING; LACE-MAKING; KNITTING; TRIMMINGS; NON-WOVEN FABRICS
- D04H—MAKING TEXTILE FABRICS, e.g. FROM FIBRES OR FILAMENTARY MATERIAL; FABRICS MADE BY SUCH PROCESSES OR APPARATUS, e.g. FELTS, NON-WOVEN FABRICS; COTTON-WOOL; WADDING ; NON-WOVEN FABRICS FROM STAPLE FIBRES, FILAMENTS OR YARNS, BONDED WITH AT LEAST ONE WEB-LIKE MATERIAL DURING THEIR CONSOLIDATION
- D04H1/00—Non-woven fabrics formed wholly or mainly of staple fibres or like relatively short fibres
- D04H1/40—Non-woven fabrics formed wholly or mainly of staple fibres or like relatively short fibres from fleeces or layers composed of fibres without existing or potential cohesive properties
- D04H1/44—Non-woven fabrics formed wholly or mainly of staple fibres or like relatively short fibres from fleeces or layers composed of fibres without existing or potential cohesive properties the fleeces or layers being consolidated by mechanical means, e.g. by rolling
- D04H1/52—Non-woven fabrics formed wholly or mainly of staple fibres or like relatively short fibres from fleeces or layers composed of fibres without existing or potential cohesive properties the fleeces or layers being consolidated by mechanical means, e.g. by rolling by applying or inserting filamentary binding elements
-
- D—TEXTILES; PAPER
- D04—BRAIDING; LACE-MAKING; KNITTING; TRIMMINGS; NON-WOVEN FABRICS
- D04H—MAKING TEXTILE FABRICS, e.g. FROM FIBRES OR FILAMENTARY MATERIAL; FABRICS MADE BY SUCH PROCESSES OR APPARATUS, e.g. FELTS, NON-WOVEN FABRICS; COTTON-WOOL; WADDING ; NON-WOVEN FABRICS FROM STAPLE FIBRES, FILAMENTS OR YARNS, BONDED WITH AT LEAST ONE WEB-LIKE MATERIAL DURING THEIR CONSOLIDATION
- D04H3/00—Non-woven fabrics formed wholly or mainly of yarns or like filamentary material of substantial length
- D04H3/02—Non-woven fabrics formed wholly or mainly of yarns or like filamentary material of substantial length characterised by the method of forming fleeces or layers, e.g. reorientation of yarns or filaments
- D04H3/04—Non-woven fabrics formed wholly or mainly of yarns or like filamentary material of substantial length characterised by the method of forming fleeces or layers, e.g. reorientation of yarns or filaments in rectilinear paths, e.g. crossing at right angles
-
- D—TEXTILES; PAPER
- D04—BRAIDING; LACE-MAKING; KNITTING; TRIMMINGS; NON-WOVEN FABRICS
- D04H—MAKING TEXTILE FABRICS, e.g. FROM FIBRES OR FILAMENTARY MATERIAL; FABRICS MADE BY SUCH PROCESSES OR APPARATUS, e.g. FELTS, NON-WOVEN FABRICS; COTTON-WOOL; WADDING ; NON-WOVEN FABRICS FROM STAPLE FIBRES, FILAMENTS OR YARNS, BONDED WITH AT LEAST ONE WEB-LIKE MATERIAL DURING THEIR CONSOLIDATION
- D04H3/00—Non-woven fabrics formed wholly or mainly of yarns or like filamentary material of substantial length
- D04H3/08—Non-woven fabrics formed wholly or mainly of yarns or like filamentary material of substantial length characterised by the method of strengthening or consolidating
- D04H3/10—Non-woven fabrics formed wholly or mainly of yarns or like filamentary material of substantial length characterised by the method of strengthening or consolidating with bonds between yarns or filaments made mechanically
- D04H3/115—Non-woven fabrics formed wholly or mainly of yarns or like filamentary material of substantial length characterised by the method of strengthening or consolidating with bonds between yarns or filaments made mechanically by applying or inserting filamentary binding elements
-
- D—TEXTILES; PAPER
- D04—BRAIDING; LACE-MAKING; KNITTING; TRIMMINGS; NON-WOVEN FABRICS
- D04H—MAKING TEXTILE FABRICS, e.g. FROM FIBRES OR FILAMENTARY MATERIAL; FABRICS MADE BY SUCH PROCESSES OR APPARATUS, e.g. FELTS, NON-WOVEN FABRICS; COTTON-WOOL; WADDING ; NON-WOVEN FABRICS FROM STAPLE FIBRES, FILAMENTS OR YARNS, BONDED WITH AT LEAST ONE WEB-LIKE MATERIAL DURING THEIR CONSOLIDATION
- D04H5/00—Non woven fabrics formed of mixtures of relatively short fibres and yarns or like filamentary material of substantial length
- D04H5/08—Non woven fabrics formed of mixtures of relatively short fibres and yarns or like filamentary material of substantial length characterised by the method of forming fleeces or layers, e.g. reorientation of fibres or yarns
-
- 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
- D10B2403/00—Details of fabric structure established in the fabric forming process
- D10B2403/02—Cross-sectional features
- D10B2403/024—Fabric incorporating additional compounds
- D10B2403/0241—Fabric incorporating additional compounds enhancing mechanical properties
- D10B2403/02412—Fabric incorporating additional compounds enhancing mechanical properties including several arrays of unbent yarn, e.g. multiaxial fabrics
-
- 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
Definitions
- the invention relates to a method for connecting an in particular non-textile cell structure with textile cover layers to form a sandwich structure according to the preamble of claim 1.
- any material combinations such as Textiles, plastics, metals are connected.
- the good bond that can be achieved between the textiles reduces the risk of detachment due to shear stresses, with fiber composite materials in particular delamination being critical with regard to the greatly reduced strength.
- this known method one obtains three-dimensional reinforced textile.
- the main disadvantage of the described method is that the combination of the different textiles as the end product in turn results in a semi-finished textile product.
- Sandwich materials such as those used in lightweight construction with a rapidly increasing tendency, generally have cover surfaces which are glued to an inlay.
- the inlay glued between the cover surfaces need not be of a textile nature. So far, mainly foams and aluminum or paper honeycomb structures, the so-called honeycombs, have been used as inlays.
- cover surfaces are first manufactured. This can be, for example, a semi-finished textile as reinforcement for a fiber composite. Then the cover surfaces are glued to the inlay. Such cover surface laminates are used in particular for aircraft floors. In addition to the complex manufacturing technology, there is also the disadvantage that the mechanical properties of the sandwich composite cannot be optimally adjusted. There is a risk of premature failure of the sandwich material due to delamination between the top surface and the inlay.
- a flexible composite blanket is also known from EP 0 526 363 A2, which is used for thermal insulation purposes.
- a silicon carbide base fabric and multiple alternating layers of individual aluminized layers and / or honeycomb-like foils are held together by a suitable thread system in the form of a stitched seam, for which purpose two threads are required.
- Temperature-resistant ceramic thread is used as the sewing thread.
- the honeycomb structure used Ren serve as spacers to reduce the thermal conduction properties of the heat-insulating ceiling.
- Honeycombs with cell walls inclined up to 60 ° in relation to the longitudinal direction are used as the cell structure.
- a sandwich structure is described in WO 80/02253, which consists of cover layers which enclose a soft foam insert between them and are sewn together.
- cover layers which enclose a soft foam insert between them and are sewn together.
- sections of high-strength fibers are drawn through the outer layers covering the foam insert on opposite outer sides of the foam insert.
- these high-strength fibers are Fibers are used, which the sewing fiber cannot be drawn into the soft foam core.
- the type of cover layers is designed as a thin skin, ie forms a relatively closed outer surface.
- the foam core serves to form a rigid cell-like resin structure in the interior of the composite material after impregnation with a curable resin.
- DE 34 18 913 C2 describes a laminar block which consists of a multiplicity of laminated plate-shaped elements made of inorganic fibers. This large number of plates or disk-shaped elements stacked on top of one another is integrated into a laminar body by sewing. Such a laminar body is primarily used for lining heat-insulating constructions and is not intended as an intermediate product for the production of a hardened sandwich material. Because there is no cell structure inside, the main disadvantage of such a laminar block is that it may not be able to penetrate the resin completely, especially when several layers are arranged one above the other, and therefore does not cure to achieve a hard composite material is accessible.
- the achievable thread density of the thread system is also limited by the relatively large needle spacing caused by the needle heads, which places limits on the interlaminar shear strength. It is therefore the object of the invention to provide a method for connecting an in particular non-textile cell structure with in particular textile cover layers to form a sandwich structure as a starting product for a composite material, which is easy to handle, a drastic reduction in the process steps required for its production enables and moreover the risk of delamination of the finished composite material under load is substantially eliminated by increasing the interlamina ⁇ ren shear strength.
- the method according to the invention represents a method for connecting an in particular non-textile cell structure, which is preferably a honeycomb structure, with at least one textile upper layer and one textile lower layer to form a sandwich structure by means of a thread system.
- the thread system is preferably produced by the knitting technique.
- the cell structure located between the textile outer layers or cover layers has essentially vertical walls and is continuous over the entire width of the sandwich structure.
- the textile cover layers preferably consist of at least two multiaxial fabrics, preferably of inorganic materials, such as glass wool, ceramic fibers or other mineral wool.
- the multiaxial fabrics are preferably produced on a warp knitting machine with multiaxial weft insertion systems (System LIBA), which is fed to the honeycomb structure, which is still relatively flexible before processing, in such a way that it is arranged between the cover layers.
- System LIBA multiaxial weft insertion systems
- the number of scrims used for the cover layers may also be significantly higher than two.
- a high-performance fiber is used as the machine thread. If the flexible mat-like structure serving as an intermediate product is to be processed into hardened flat sandwich panels, which are used above all in aircraft construction as aircraft floors, it is particularly preferred in a subsequent online process step to remove the forfeited sandwich To guide structure over a device for impregnation with a curable or meltable carrier matrix, a curing device or a downstream cooling device. Panel elements of the desired length can then be cut to standard sizes or any lengths.
- An important advantage of the method or of the product obtained with the method is that, especially in sandwich manufacturing, instead of a large number of individual parts to be assembled beforehand in individual steps, the semi-finished sandwich product is produced directly in a single operation can.
- the mechanical properties of the composite material can be optimized or oversizing avoided.
- Another advantage is the good drapability in cases in which, above all, curved components are to be obtained from the sandwich structure, the intermediate structure is brought to the place of processing with extremely easy handling and pressed into the respective shape can be what the actual impregnation and curing or cooling follow.
- the advantages consist precisely in the fact that individual layers do not have to be applied individually at such locations, and in addition that delamination of the top layers and inlay layer is avoided, above all, even in the case of curved components with increased stress due to the narrow knitting thread system.
- the vertical arrangement of the walls of the honeycomb structure largely prevents damage to the walls of the honeycomb structure by the needles during the knitting process.
- the feed movement of the cell structure into the knitting machine is synchronized with the needle position so that essentially the same number of threads is drawn through each cell of the honeycomb structure and the walls remain largely undamaged, i.e. not to be hit by the needles.
- the figure shows a sandwich structure produced with the method according to the invention, which consists of cover layers 1, 3 formed as a laid scrim with a honeycomb structure 2 in between by interlocking on the basis of warp knitting technology with multiaxial weft insertion systems, e.g. according to the LIBA system.
- the material combination of the sandwich structure shown in the figure shows a lower layer 1 as the lower layer 1 and a cover layer 3, which each consists of two layers and is arranged at different angles to each other.
- the alignment of the lay-up layers with respect to one another and with respect to the feed movement of the sandwich product to be produced is different for the underlayer 1 and the top layer 2.
- the scrim of the lower layer 1 is superimposed on one another in a 45 ° angle arrangement with respect to the conveying direction, while the two scrim layers of the cover layer 2 are placed in a 90 ° arrangement to one another.
- the different orientations of the fabrics serve to further increase the strength of the finished sandwich structure without increasing the material expenditure.
- Inorganic fibers such as glass wool, mineral wool and others are preferably used as the material for the layers of the cover layers 1, 3.
- the materials stacked in this way are fed to a knitting machine and connected to one another to form a unit.
- the arrangement of the individual lay-up strands can preferably be matched to the spacing of the needles 4, so that when they are knocked in synchronism between the feed movement of the material package 5 and the honeycomb structure dimension and the lay-up strand thickness, the individual components of the sandwich structure are knocked as free of injuries as possible.
- the connecting threads which extend through the entire material, soak during the impregnation with the hardenable carrier matrix by capillary action full of resin and thus serve as a safeguard against delamination of the top and bottom layers 1, 3 from the honeycomb. Structure 3 of an additional support and thus increasing the strength of the fully hardened sandwich structure.
- the sandwich structure produced with the method according to the invention achieves an interlaminar shear strength that is at least 15% higher.
Abstract
Description
Claims
Priority Applications (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP96922818A EP0776268A1 (en) | 1995-06-16 | 1996-06-17 | Process for joining an in particular non-textile cellular structure to textile coating layers |
AU63562/96A AU6356296A (en) | 1995-06-16 | 1996-06-17 | Process for joining an in particular non-textile cellular structure to textile coating layers |
KR1019970701031A KR970705468A (en) | 1995-06-16 | 1996-06-17 | A method of connecting a special nonwoven porous structure to a fabric covering layer (PROCESS FOR JOINING AN IN PARTICULAR NON-TEXTILE CELLULAR STRUCTURE TO TEXTILE COATING LAYERS) |
NO970636A NO970636D0 (en) | 1995-06-16 | 1997-02-11 | Method of connecting in particular a non-textile-based structure to textile cover sheets |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE19521946A DE19521946A1 (en) | 1995-06-16 | 1995-06-16 | Method for connecting an in particular non-textile cell structure with textile cover layers |
DE19521946.5 | 1995-06-16 |
Publications (1)
Publication Number | Publication Date |
---|---|
WO1997000167A1 true WO1997000167A1 (en) | 1997-01-03 |
Family
ID=7764539
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/EP1996/002607 WO1997000167A1 (en) | 1995-06-16 | 1996-06-17 | Process for joining an in particular non-textile cellular structure to textile coating layers |
Country Status (6)
Country | Link |
---|---|
EP (1) | EP0776268A1 (en) |
KR (1) | KR970705468A (en) |
AU (1) | AU6356296A (en) |
DE (1) | DE19521946A1 (en) |
NO (1) | NO970636D0 (en) |
WO (1) | WO1997000167A1 (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20110169184A1 (en) * | 2008-09-23 | 2011-07-14 | Endress + Hauser Wetzer Gmbh + Co. Kg | Method for manufacturing a measuring apparatus and method for casting in a mold |
WO2019071266A1 (en) | 2017-10-06 | 2019-04-11 | Power Distribution, Inc. | Universal tap-off box |
Families Citing this family (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE19902368B4 (en) * | 1999-01-21 | 2004-09-02 | Lutze, Hans, Prof. Dr.-Ing.habil. | composite |
ATE203953T1 (en) * | 1999-03-03 | 2001-08-15 | Heimbach Gmbh Thomas Josef | PRESS PAD |
PT1033237E (en) * | 1999-03-03 | 2004-10-29 | Heimbach Gmbh Thomas Josef | COMPRESSION PAD |
DE19913647B4 (en) * | 1999-03-25 | 2004-04-01 | Liba Maschinenfabrik Gmbh | Method and device for the continuous production of knitted / sewn muilti-axial scrims from several layers of threads |
DE10110115A1 (en) * | 2001-03-02 | 2002-09-05 | Audi Ag | Sandwich structure material, e.g. for use in vehicles, is produced using textile or non-textile shape retaining carrier layer and fibre fleece cover layer |
DE102004032833B4 (en) * | 2004-07-06 | 2010-04-22 | Herbert Olbrich Gmbh & Co. Kg | Multi-layer molding and method for its production |
DE102004062895A1 (en) * | 2004-12-20 | 2006-06-29 | Technische Universität Dresden | Textile spacing structure for multilaminar sandwich elements has at least one flat textiles strip and at least one meandering or corrugated folded strip |
JP4699425B2 (en) * | 2007-06-22 | 2011-06-08 | 株式会社ジャムコ | Sandwich panel |
DE102008019065B4 (en) | 2008-04-15 | 2011-06-16 | Airbus Operations Gmbh | Process for producing a core composite provided with cover layers on both sides and core composite |
Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO1980002253A1 (en) * | 1979-04-16 | 1980-10-30 | Int Harvester Co | An improved rigidized resinous foam core sandwich structure |
US4331495A (en) * | 1978-01-19 | 1982-05-25 | Rockwell International Corporation | Method of fabricating a reinforced composite structure |
FR2602178A1 (en) * | 1986-08-01 | 1988-02-05 | Chomarat & Cie | Material for the reinforcement of laminated articles |
EP0355912A2 (en) * | 1988-08-15 | 1990-02-28 | Adprotech B.V. | Flat sandwich-shaped body |
EP0361796A2 (en) * | 1988-09-26 | 1990-04-04 | Tech Textiles International Limited | Method of producing a formable composite material |
EP0526363A2 (en) * | 1991-08-01 | 1993-02-03 | GOVERNMENT OF THE UNITED STATES OF AMERICA as represented by THE ADMINISTRATOR OF THE NATIONAL AERONAUTICS AND SPACE ADM. | Composite flexible blanket insulation |
Family Cites Families (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CS163081B1 (en) * | 1973-05-15 | 1975-07-31 | Jan Zelezny | Non-woven textile fabric and method of its production |
DE4328705C2 (en) * | 1993-08-26 | 2000-11-16 | Saechsisches Textilforsch Inst | Process for the production of reinforced warp knitted fabrics, in particular sewing knitted fabrics |
-
1995
- 1995-06-16 DE DE19521946A patent/DE19521946A1/en not_active Withdrawn
-
1996
- 1996-06-17 WO PCT/EP1996/002607 patent/WO1997000167A1/en not_active Application Discontinuation
- 1996-06-17 KR KR1019970701031A patent/KR970705468A/en not_active Application Discontinuation
- 1996-06-17 AU AU63562/96A patent/AU6356296A/en not_active Abandoned
- 1996-06-17 EP EP96922818A patent/EP0776268A1/en not_active Withdrawn
-
1997
- 1997-02-11 NO NO970636A patent/NO970636D0/en unknown
Patent Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4331495A (en) * | 1978-01-19 | 1982-05-25 | Rockwell International Corporation | Method of fabricating a reinforced composite structure |
WO1980002253A1 (en) * | 1979-04-16 | 1980-10-30 | Int Harvester Co | An improved rigidized resinous foam core sandwich structure |
FR2602178A1 (en) * | 1986-08-01 | 1988-02-05 | Chomarat & Cie | Material for the reinforcement of laminated articles |
EP0355912A2 (en) * | 1988-08-15 | 1990-02-28 | Adprotech B.V. | Flat sandwich-shaped body |
EP0361796A2 (en) * | 1988-09-26 | 1990-04-04 | Tech Textiles International Limited | Method of producing a formable composite material |
EP0526363A2 (en) * | 1991-08-01 | 1993-02-03 | GOVERNMENT OF THE UNITED STATES OF AMERICA as represented by THE ADMINISTRATOR OF THE NATIONAL AERONAUTICS AND SPACE ADM. | Composite flexible blanket insulation |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20110169184A1 (en) * | 2008-09-23 | 2011-07-14 | Endress + Hauser Wetzer Gmbh + Co. Kg | Method for manufacturing a measuring apparatus and method for casting in a mold |
US9228904B2 (en) * | 2008-09-23 | 2016-01-05 | Endress + Hauser Wetzer Gmbh + Co. Kg | Method for manufacturing a measuring apparatus and method for casting in a mold |
WO2019071266A1 (en) | 2017-10-06 | 2019-04-11 | Power Distribution, Inc. | Universal tap-off box |
US11641097B2 (en) | 2017-10-06 | 2023-05-02 | Power Distribution, Inc. | Current/voltage sensor and universal tap-off box |
US11973331B2 (en) | 2017-10-06 | 2024-04-30 | Power Distribution, Inc. | Current/voltage sensor and universal tap-off box |
Also Published As
Publication number | Publication date |
---|---|
EP0776268A1 (en) | 1997-06-04 |
AU6356296A (en) | 1997-01-15 |
KR970705468A (en) | 1997-10-09 |
NO970636L (en) | 1997-02-11 |
DE19521946A1 (en) | 1996-12-19 |
NO970636D0 (en) | 1997-02-11 |
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