EP0299308A2 - Elément de construction à base d'un tissu de velours et procédé de fabrication - Google Patents

Elément de construction à base d'un tissu de velours et procédé de fabrication Download PDF

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Publication number
EP0299308A2
EP0299308A2 EP88110601A EP88110601A EP0299308A2 EP 0299308 A2 EP0299308 A2 EP 0299308A2 EP 88110601 A EP88110601 A EP 88110601A EP 88110601 A EP88110601 A EP 88110601A EP 0299308 A2 EP0299308 A2 EP 0299308A2
Authority
EP
European Patent Office
Prior art keywords
component
particular according
webs
intermediate webs
fabric
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
Application number
EP88110601A
Other languages
German (de)
English (en)
Other versions
EP0299308B1 (fr
EP0299308A3 (en
Inventor
Wolfgang Böttger
Werner Pensel
Kurt Biedermann
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Vorwerk and Co Interholding GmbH
Original Assignee
Vorwerk and Co Interholding GmbH
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Vorwerk and Co Interholding GmbH filed Critical Vorwerk and Co Interholding GmbH
Priority to AT88110601T priority Critical patent/ATE72471T1/de
Publication of EP0299308A2 publication Critical patent/EP0299308A2/fr
Publication of EP0299308A3 publication Critical patent/EP0299308A3/de
Application granted granted Critical
Publication of EP0299308B1 publication Critical patent/EP0299308B1/fr
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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Classifications

    • D—TEXTILES; PAPER
    • D06—TREATMENT OF TEXTILES OR THE LIKE; LAUNDERING; FLEXIBLE MATERIALS NOT OTHERWISE PROVIDED FOR
    • D06M—TREATMENT, NOT PROVIDED FOR ELSEWHERE IN CLASS D06, OF FIBRES, THREADS, YARNS, FABRICS, FEATHERS OR FIBROUS GOODS MADE FROM SUCH MATERIALS
    • D06M17/00—Producing multi-layer textile fabrics
    • D—TEXTILES; PAPER
    • D06—TREATMENT OF TEXTILES OR THE LIKE; LAUNDERING; FLEXIBLE MATERIALS NOT OTHERWISE PROVIDED FOR
    • D06N—WALL, FLOOR, OR LIKE COVERING MATERIALS, e.g. LINOLEUM, OILCLOTH, ARTIFICIAL LEATHER, ROOFING FELT, CONSISTING OF A FIBROUS WEB COATED WITH A LAYER OF MACROMOLECULAR MATERIAL; FLEXIBLE SHEET MATERIAL NOT OTHERWISE PROVIDED FOR
    • D06N7/00—Flexible sheet materials not otherwise provided for, e.g. textile threads, filaments, yarns or tow, glued on macromolecular material
    • E—FIXED CONSTRUCTIONS
    • E04—BUILDING
    • E04C—STRUCTURAL ELEMENTS; BUILDING MATERIALS
    • E04C2/00—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels
    • E04C2/02—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by specified materials
    • E04C2/10—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by specified materials of wood, fibres, chips, vegetable stems, or the like; of plastics; of foamed products
    • E04C2/16—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by specified materials of wood, fibres, chips, vegetable stems, or the like; of plastics; of foamed products of fibres, chips, vegetable stems, or the like
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S428/00—Stock material or miscellaneous articles
    • Y10S428/902—High modulus filament or fiber
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00—Stock material or miscellaneous articles
    • Y10T428/24—Structurally defined web or sheet [e.g., overall dimension, etc.]
    • Y10T428/24025—Superposed movable attached layers or components
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00—Stock material or miscellaneous articles
    • Y10T428/24—Structurally defined web or sheet [e.g., overall dimension, etc.]
    • Y10T428/24058—Structurally defined web or sheet [e.g., overall dimension, etc.] including grain, strips, or filamentary elements in respective layers or components in angular relation
    • Y10T428/24074—Strand or strand-portions
    • Y10T428/24116—Oblique to direction of web
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00—Stock material or miscellaneous articles
    • Y10T428/24—Structurally defined web or sheet [e.g., overall dimension, etc.]
    • Y10T428/24058—Structurally defined web or sheet [e.g., overall dimension, etc.] including grain, strips, or filamentary elements in respective layers or components in angular relation
    • Y10T428/24124—Fibers
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00—Stock material or miscellaneous articles
    • Y10T428/24—Structurally defined web or sheet [e.g., overall dimension, etc.]
    • Y10T428/24149—Honeycomb-like
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00—Stock material or miscellaneous articles
    • Y10T428/24—Structurally defined web or sheet [e.g., overall dimension, etc.]
    • Y10T428/24174—Structurally defined web or sheet [e.g., overall dimension, etc.] including sheet or component perpendicular to plane of web or sheet
    • Y10T428/24182—Inward from edge of web or sheet
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00—Stock material or miscellaneous articles
    • Y10T428/24—Structurally defined web or sheet [e.g., overall dimension, etc.]
    • Y10T428/24802—Discontinuous or differential coating, impregnation or bond [e.g., artwork, printing, retouched photograph, etc.]
    • Y10T428/2481—Discontinuous or differential coating, impregnation or bond [e.g., artwork, printing, retouched photograph, etc.] including layer of mechanically interengaged strands, strand-portions or strand-like strips
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00—Stock material or miscellaneous articles
    • Y10T428/30—Self-sustaining carbon mass or layer with impregnant or other layer

Definitions

  • the invention relates to a component based on velor fabric with at least a first and a second layer and intermediate webs connecting these layers.
  • resin-hardened fiber composites has found a wide range of applications, be it in the form of load-bearing structural elements or for the fulfillment of insulation tasks. With the greatest possible rigidity and compressive strength, the lowest possible weight is also sought for special cases, such as flight technology.
  • types of weave such as weft velvet and warp velvet are known.
  • double velvet is created, in which the connecting webs do a double shedding between the layer-creating velor threads.
  • the length of the floating threads is adjustable so that longer or shorter web lengths are achieved.
  • the center threads of the pile threads are then cut on a cutting bench.
  • the present invention has set itself the task of creating a light, yet stable, multi-layer, practically sandwich-like component with means simple to manufacture and even using existing machines, which optimally embodies the properties mentioned .
  • the intermediate webs are given a more or less steep oblique position, it proving advantageous in a further development that the intermediate webs run obliquely in a controlled manner.
  • a load flowing over the wide area is still converted into a rectified layer displacement component.
  • This is particularly advantageous for partial high loads, since the entire body is then included in the resistance to deformation.
  • the corresponding regulation, ie rectification of the webs also makes the evasive movement determinable. It has proven to be favorable that the intermediate webs enclose an angle of approximately 65 ° with a horizontal. Depending on the purpose of the component, a steeper position can be useful. In this case, the intermediate webs enclose an angle of approx.
  • an intermediate web consists of two weakly twisted individual webs.
  • the intermediate web consist of 8-shaped twisted individual webs.
  • the component 1 shown is produced on a velor weaving machine.
  • the corresponding velor fabric or Raschel plush fabric is multi-ply, in the embodiment two-ply.
  • a first, upper layer bears the reference number 2; a second, lower layer is denoted by 3.
  • Co-woven support threads which form intermediate webs 4, hold the two layers 2, 3 together at a distance from one another the. There is the uncleaved structure of a double velvet integration.
  • the number of support threads results from the weft density of the layers 2 and 3, also the number of support threads, measured over the weaving width and finally from the repeat size of the weave. With, for example, 2000 threads per 1 m weaving width, 12 picks / cm in the upper layer and the lower layer and 3/6 weft weave, there are 800,000 intermediate webs 4 between the two layers 2, 3.
  • intermediate webs 4 By changing the number of web threads and weft density as well as binding, intermediate webs 4, which are several times higher or lower, can be woven in.
  • the required strength of the upper layer 2 and the lower layer 3 and bending strength are achieved by appropriate use of material from the warp and weft in the top layers.
  • the web height is variable and can be individually adjusted to the desired height.
  • the support threads forming the intermediate webs 4 endeavor to straighten up after the weaving or to reset in a load-free state. This leads to a parallel spacing of the layers 2 and 3.
  • the clear distance x between the two layers 2 and 3 corresponds to a multiple of a layer thickness.
  • the intermediate webs 4 which are comparable to the pile threads of a velor double velvet weave, are stiffened like the entire component body by hardening resin, so that the intermediate webs 4 form rigid spacing elements between the first layer 2 and the second layer 3. Deferring the intermediate ge 4 in its end position shown in Fig. 1 happens even after the complete compression of the weave structure. Accordingly, no damage occurs during the weaving process due to the necessary deflections, which fact can be used advantageously in the manufacture of such components.
  • the average length of the intermediate webs 4 is greater than the clear distance x between the layers 2, 3.
  • the free support thread sections forming them therefore do not change in the shortest possible way between the two adjacent layers 2, 3. Rather, as can be seen from FIG. 1, there is a slight inclination, seen from the viewing direction A in FIG. 1.
  • an oblique bevel is used so that one can speak of a regulated bevel course.
  • the corresponding helix angle alpha is, according to FIG. 3, approximately 65 °, based on the horizontal support base of component 1, that is to say a horizontal.
  • the variant Fig. 8 embodies a solution in that the intermediate webs 4 are arranged with alternating large and small distances. The larger distance corresponds to approximately twice the small distance between the parallel webs. 8, these intermediate webs are designed in an angular position to the horizontal as in FIG. 6.
  • intermediate webs 8 which run crosswise to one another, are provided between two intermediate webs 4 are.
  • the latter are located in the larger distance between two intermediate webs 4.
  • the crossing angle beta is 50 ° to the horizontal.
  • the pile threads of the fabric forming the intermediate webs 8 are rooted at a distance from the adjacent row of intermediate webs which corresponds to approximately one fifth of the length of an intermediate web 8.
  • the viewing direction B in FIG. 1 results in a vertical orientation (compare FIG. 4) to the base mentioned in all cases.
  • intermediate length is chosen because the intermediate webs 4 each consist of weakly twisted individual webs 4 ', 4 ⁇ , the real length turns out to be greater.
  • the weakly helical rise results from the perspective illustration, FIG. 1.
  • the intermediate web 4 is thus drilled into an eight (comparable to an oval ring rotated by 180 degrees about its longitudinal axis), the individual webs 4 ', 4' being connected to one another in their crossover area 5.
  • Such intersection-like crossover areas 5 are achieved by touching the loop sections of the intermediate webs 4 forming the eight.
  • the intermediate webs 4, 8 In the layer-side exit area and, of course, also in the entry area, the intermediate webs 4, 8 have socle-like transition areas 6, comparable to above-ground roots of trees etc. This leads to a practically frustoconical transition between the inside of the layers and the spacing elements.
  • the Kebelstumpfbasis corresponds to several times the cross section of a single web 4 'or 4 ⁇ .
  • the circular fields recognizable on the top in FIG. 1 are intended to represent the layer entry area of the intermediate symbolize ribs 4. It is based on a W integration.
  • the intermediate web 4 designed as an eight creates after binding in the crossover area 5 two teardrop-shaped or chain link-like sections, the cavity of which is denoted by a, b, and which, depending on the vicinity of the individual webs 4 ', 4', can also be completely or partially filled with resin .
  • Partial loads on the wide surfaces of component 1 also involve the intermediate webs located in the wider area, since, due to the slight inclination position, which is also the same, an opposing displacement movement (arrows z, z 'in FIG. 1) of layers 2 and 3 occurs.
  • the described shape of the intermediate webs 4 also has a force-consuming effect.
  • a constant parallelism of the layers 2 and 3 is obtained by striking the weft thread 9 of the upper and lower fabric layer by means of a serrated blade 10 (see FIG. 7).
  • the reed bars of the serrated sheet 10 have notches 11 on the goods side, the bottom of which defines the center distance y of the layers 2 and 3, that is to say the upper and lower goods.
  • the distance can be 8 mm, for example.
  • the serrated blade also allows the weft threads 9 to be struck exactly in terms of height.
  • the warp threads are designated 12 throughout and form the intermediate webs 4, 8.
  • the uneven distribution of the intermediate webs leads to relatively large spaces. This reduces resin absorption.
  • the parts are lighter in weight.
  • the cross-shaped blocking of the rooms also increases the strength.
  • FIGS. 10 to 12 show, based on the exemplary embodiment in FIG. 10, a corner configuration in which the upper layer 2 folds into the inner corner of the angularly shaped component.
  • This constellation can be blocked by an additional layer 13 placed on the inside.
  • the additional layer 13 takes an essentially parallel curve to the apex zone 14 of the profile.
  • FIGS. 11 and 12 Component laminates are shown in FIGS. 11 and 12. These are bordered.
  • the edge zone 15 is reduced to a minimum of the total thickness. This is done by bundling the layers 2, 3 of each component 1.
  • Another advantage is the opposite inclined alignment of the individual components 1. This leads to an internal blockage and a very high strength of the overall component.
  • the fabric structure explained is soaked with marker-containing resin plus hardener.
  • the excess amount of resin is squeezed or rolled out, so that the inner structure is resin-free except for the wetted, web-forming support threads and the two impregnated fabric layers.
  • Sufficient resin is dragged along so that the crossover areas 5 are well saturated with resin; reference is made to FIG. 2, from which such a resin accumulation zone can be seen.
  • the corresponding evacuation to resin takes place to such an extent that the restoring force of the intermediate webs 4 is released until, as already indicated, they reach their basic or final position.
  • After the drying process emerge hardened components of high rigidity and compressive strength.
  • the good deformability of the velor fabric or Raschel plush fabric also allows the production of slightly spherically curved components.
  • the realized sandwich-like structure counteracts any delamination tendency, for example in the sense of a layer peeling off, due to a single coherent structure.
  • such a component 1 is composed of a plurality of fabric sections 1 ', 1''.
  • a velor fabric section 1 ' is split in the connection area to the other velor fabric section 1''.
  • the gap is designated 7 there and is generated by a center cut in accordance with the desired depth of overlap.
  • the corresponding edge zone of the subsequent tissue section 1 '' is inserted into the opening thus created.
  • the edge layers near the connection area are pressed together in the direction of the spacing space. This is followed by the described soaking with resin and squeezing. The tissue resets in the manner described.
  • connection area V The corresponding provision can be limited by back support in the connection area V, so that the thickness of the component 1 is the same throughout.
  • the more flattened edge zone disappears in the existing space.
  • the brush-like web stubble freestanding by gap cut bury itself anchoring in the outside of the overlapped edge of the fabric section 1 ''. The latter leads to an intimate, durable bond.

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  • Engineering & Computer Science (AREA)
  • Textile Engineering (AREA)
  • Architecture (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Wood Science & Technology (AREA)
  • Civil Engineering (AREA)
  • Structural Engineering (AREA)
  • Woven Fabrics (AREA)
  • Laminated Bodies (AREA)
  • Treatments For Attaching Organic Compounds To Fibrous Goods (AREA)
  • Yarns And Mechanical Finishing Of Yarns Or Ropes (AREA)
  • Professional, Industrial, Or Sporting Protective Garments (AREA)
  • Treatment Of Fiber Materials (AREA)
  • Finishing Walls (AREA)
  • Panels For Use In Building Construction (AREA)
  • Manufacturing Of Multi-Layer Textile Fabrics (AREA)
  • Details Of Garments (AREA)
  • Chemical Or Physical Treatment Of Fibers (AREA)
  • Air Bags (AREA)
EP88110601A 1987-07-17 1988-07-02 Elément de construction à base d'un tissu de velours et procédé de fabrication Expired - Lifetime EP0299308B1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
AT88110601T ATE72471T1 (de) 1987-07-17 1988-07-02 Bauteil auf velours-gewebebasis und verfahren zu seiner herstellung.

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE3723681 1987-07-17
DE19873723681 DE3723681A1 (de) 1987-07-17 1987-07-17 Bauteil auf velours-gewebebasis und verfahren zu seiner herstellung

Publications (3)

Publication Number Publication Date
EP0299308A2 true EP0299308A2 (fr) 1989-01-18
EP0299308A3 EP0299308A3 (en) 1989-05-31
EP0299308B1 EP0299308B1 (fr) 1992-02-05

Family

ID=6331791

Family Applications (1)

Application Number Title Priority Date Filing Date
EP88110601A Expired - Lifetime EP0299308B1 (fr) 1987-07-17 1988-07-02 Elément de construction à base d'un tissu de velours et procédé de fabrication

Country Status (12)

Country Link
US (2) US4840828A (fr)
EP (1) EP0299308B1 (fr)
JP (1) JP2590214B2 (fr)
AT (1) ATE72471T1 (fr)
BR (1) BR8803585A (fr)
CA (1) CA1323288C (fr)
DD (1) DD285386A5 (fr)
DE (2) DE3723681A1 (fr)
ES (1) ES2030116T3 (fr)
GR (1) GR3003861T3 (fr)
HK (1) HK138593A (fr)
IL (1) IL87120A (fr)

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0495163A1 (fr) 1991-01-12 1992-07-22 Vorwerk & Co. Interholding GmbH Elément de construction à base d'un tissu "face-à-face"
WO1992017661A1 (fr) * 1991-04-05 1992-10-15 Vorwerk & Co. Interholding Gmbh Composant en tissu resinifie a couches espacees et procede de fabrication d'un revetement
WO1993003235A2 (fr) * 1991-07-30 1993-02-18 Metalleido S.R.L. Module sectionnel d'habitation
EP0586873A1 (fr) * 1992-08-31 1994-03-16 Vorwerk & Co. Interholding GmbH Tissu "face-à-face"
DE4300481A1 (de) * 1993-01-11 1994-07-14 Kunert Heinz Rahmenlose Isolierverglasung und Verfahren zu deren Herstellung
WO1995023251A1 (fr) * 1994-02-23 1995-08-31 Vorwerk & Co. Interholding Gmbh Tissu a deux couches espacees
WO2014121787A3 (fr) * 2013-02-07 2014-11-27 Technische Universität Dresden Structure en tissu à constitution cellulaire

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NL187076C (nl) * 1986-12-08 1991-05-16 Parabeam Bv Werkwijze voor het vervaardigen van een dubbelweefsel alsmede weefgetouw voor een dubbelweefsel voor het uitvoeren van die werkwijze.
DE3903216A1 (de) * 1989-02-03 1990-08-09 Parabeam Bv Airbag
FR2645881B1 (fr) * 1989-04-14 1992-06-12 Hexcel Genin Sa Etoffe thermo-plastique
DE69101397T2 (de) * 1990-05-31 1994-06-23 United Technologies Corp Verbundartikel hergestellt aus faserverstärktem Glas-Bindemittel und Glas-keramischem Bindemittel.
US5534318A (en) * 1991-03-18 1996-07-09 Parabeam Industrie-En Handelsonderneming B.V. Hollow fiber-reinforced plastic body
US5699796A (en) * 1993-01-29 1997-12-23 Cardima, Inc. High resolution intravascular signal detection
DE4202589C1 (en) * 1992-01-30 1993-04-22 Deutsche Aerospace Ag, 8000 Muenchen, De Prodn. of integral sandwich structure from preformed textile - comprises impregnating core yarns with hardenable plastic and placing between rigid baseplate and covering plate
DE4215662A1 (de) * 1992-05-13 1993-11-18 Akzo Nv Textiles Anti-Vandalismus Flächengebilde
DE4300480A1 (de) * 1993-01-11 1994-07-14 Kunert Heinz Sicherheitsglaselement mit Wärmedämmeigenschaften
DE4327022C2 (de) * 1993-08-12 1995-05-24 Daimler Benz Ag Element zur Absorption von Aufprallenergie, insbesondere für Fahrzeuge
ATE278075T1 (de) * 1995-01-25 2004-10-15 Kunert Heinz Hochwärmedämmend ausgerüsteter boden-, decken- oder wandaufbau
DE19502238A1 (de) * 1995-01-25 1996-08-01 Kunert Heinz Hochwärmedämmend ausgerüsteter Boden-, Decken- oder Wandaufbau
DE29504458U1 (de) * 1995-03-16 1995-05-11 Gebrüder Friedrich GmbH, 38229 Salzgitter Matte
US7051489B1 (en) 1999-08-12 2006-05-30 Hunter Douglas Inc. Ceiling system with replacement panels
KR20010081471A (ko) * 2000-02-15 2001-08-29 조문수 샌드위치 패널
US7377084B2 (en) * 2000-04-24 2008-05-27 Hunter Douglas Inc. Compressible structural panel
US7060156B2 (en) * 2001-07-23 2006-06-13 Vrac, Llc Three-dimensional spacer fabric resin interlaminar infusion media process and vacuum-induced reinforcing composite laminate structures
US7048985B2 (en) * 2001-07-23 2006-05-23 Vrac, Llc Three-dimensional spacer fabric resin infusion media and reinforcing composite lamina
US6688338B2 (en) * 2001-12-26 2004-02-10 Paul Meli Secondary containment system for pipelines
US7303641B2 (en) * 2002-12-03 2007-12-04 Hunter Douglas Inc. Method for fabricating cellular structural panels
US20070022672A1 (en) * 2005-07-11 2007-02-01 Bachynski Michael R Hurricane protection harness
DE202005010964U1 (de) 2005-07-12 2006-11-23 Jacob Composite Gmbh Hybrid-Verbindungselement
JP5318432B2 (ja) * 2008-02-12 2013-10-16 東レ・デュポン株式会社 防御用パイル織物
ES2758718T3 (es) * 2013-03-11 2020-05-06 Parabeam Bv Material de relleno para tapicería para un recubrimiento elástico, aislante o acolchado de objetos o piezas de construcción
DE102013217990A1 (de) 2013-09-09 2015-03-12 hollomet GmbH Dämpfungskörper
CN110863482B (zh) * 2019-12-06 2022-07-05 湖南易兴建筑有限公司 纤维陶瓷建筑的施工方法

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Publication number Priority date Publication date Assignee Title
US3090406A (en) * 1961-02-23 1963-05-21 Raymond Dev Ind Inc Woven panel and method of making same
FR1393269A (fr) * 1963-09-24 1965-03-26 Lister & Company Ltd Perfectionnements aux matières textiles
US3481427A (en) * 1968-11-29 1969-12-02 Mc Donnell Douglas Corp Acoustical panel structure

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0495163A1 (fr) 1991-01-12 1992-07-22 Vorwerk & Co. Interholding GmbH Elément de construction à base d'un tissu "face-à-face"
WO1992017661A1 (fr) * 1991-04-05 1992-10-15 Vorwerk & Co. Interholding Gmbh Composant en tissu resinifie a couches espacees et procede de fabrication d'un revetement
US5387455A (en) * 1991-04-05 1995-02-07 Vorwerk & Co. Interholding Gmbh Component made of resinified space-layer fabric, and a method of producing a lagging
WO1993003235A2 (fr) * 1991-07-30 1993-02-18 Metalleido S.R.L. Module sectionnel d'habitation
WO1993003235A3 (fr) * 1991-07-30 1993-04-01 Metalleido Srl Module sectionnel d'habitation
EP0586873A1 (fr) * 1992-08-31 1994-03-16 Vorwerk & Co. Interholding GmbH Tissu "face-à-face"
DE4300481A1 (de) * 1993-01-11 1994-07-14 Kunert Heinz Rahmenlose Isolierverglasung und Verfahren zu deren Herstellung
WO1995023251A1 (fr) * 1994-02-23 1995-08-31 Vorwerk & Co. Interholding Gmbh Tissu a deux couches espacees
US6037035A (en) * 1994-02-23 2000-03-14 Vorwerk & Co. Interholding Gmbh Spacer fabric
WO2014121787A3 (fr) * 2013-02-07 2014-11-27 Technische Universität Dresden Structure en tissu à constitution cellulaire
US9562306B2 (en) 2013-02-07 2017-02-07 Technische Universität Dresden Fabric structure with cellular construction

Also Published As

Publication number Publication date
US4840828A (en) 1989-06-20
HK138593A (en) 1993-12-24
ATE72471T1 (de) 1992-02-15
USRE33923E (en) 1992-05-12
DE3868297D1 (de) 1992-03-19
EP0299308B1 (fr) 1992-02-05
IL87120A0 (en) 1988-12-30
EP0299308A3 (en) 1989-05-31
CA1323288C (fr) 1993-10-19
BR8803585A (pt) 1989-02-08
DE3723681A1 (de) 1989-01-26
DD285386A5 (de) 1990-12-12
IL87120A (en) 1992-05-25
ES2030116T3 (es) 1992-10-16
JP2590214B2 (ja) 1997-03-12
JPH0197273A (ja) 1989-04-14
GR3003861T3 (fr) 1993-03-16

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