EP1664453A4 - Dispositif d'ouverture anvick et procede de formation et d'utilisation - Google Patents

Dispositif d'ouverture anvick et procede de formation et d'utilisation

Info

Publication number
EP1664453A4
EP1664453A4 EP03814653A EP03814653A EP1664453A4 EP 1664453 A4 EP1664453 A4 EP 1664453A4 EP 03814653 A EP03814653 A EP 03814653A EP 03814653 A EP03814653 A EP 03814653A EP 1664453 A4 EP1664453 A4 EP 1664453A4
Authority
EP
European Patent Office
Prior art keywords
reinforcement
elements
trusses
truss
aperture device
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Withdrawn
Application number
EP03814653A
Other languages
German (de)
English (en)
Other versions
EP1664453A2 (fr
Inventor
Theodore E Anvick
Forrest Ryan Chadwick
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.)
COMPOSITE INSULATED PANEL SYSTEMS Corp
COMPOSITE INSULATED PANEL SYST
Original Assignee
COMPOSITE INSULATED PANEL SYSTEMS Corp
COMPOSITE INSULATED PANEL SYST
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 COMPOSITE INSULATED PANEL SYSTEMS Corp, COMPOSITE INSULATED PANEL SYST filed Critical COMPOSITE INSULATED PANEL SYSTEMS Corp
Publication of EP1664453A2 publication Critical patent/EP1664453A2/fr
Publication of EP1664453A4 publication Critical patent/EP1664453A4/fr
Withdrawn legal-status Critical Current

Links

Classifications

    • EFIXED CONSTRUCTIONS
    • E04BUILDING
    • E04CSTRUCTURAL ELEMENTS; BUILDING MATERIALS
    • E04C5/00Reinforcing elements, e.g. for concrete; Auxiliary elements therefor
    • E04C5/16Auxiliary parts for reinforcements, e.g. connectors, spacers, stirrups
    • E04C5/162Connectors or means for connecting parts for reinforcements
    • E04C5/163Connectors or means for connecting parts for reinforcements the reinforcements running in one single direction
    • EFIXED CONSTRUCTIONS
    • E04BUILDING
    • E04CSTRUCTURAL ELEMENTS; BUILDING MATERIALS
    • E04C5/00Reinforcing elements, e.g. for concrete; Auxiliary elements therefor
    • E04C5/01Reinforcing elements of metal, e.g. with non-structural coatings
    • E04C5/02Reinforcing elements of metal, e.g. with non-structural coatings of low bending resistance
    • E04C5/04Mats
    • EFIXED CONSTRUCTIONS
    • E04BUILDING
    • E04CSTRUCTURAL ELEMENTS; BUILDING MATERIALS
    • E04C5/00Reinforcing elements, e.g. for concrete; Auxiliary elements therefor
    • E04C5/01Reinforcing elements of metal, e.g. with non-structural coatings
    • E04C5/06Reinforcing elements of metal, e.g. with non-structural coatings of high bending resistance, i.e. of essentially three-dimensional extent, e.g. lattice girders
    • E04C5/0636Three-dimensional reinforcing mats composed of reinforcing elements laying in two or more parallel planes and connected by separate reinforcing parts
    • EFIXED CONSTRUCTIONS
    • E04BUILDING
    • E04CSTRUCTURAL ELEMENTS; BUILDING MATERIALS
    • E04C5/00Reinforcing elements, e.g. for concrete; Auxiliary elements therefor
    • E04C5/01Reinforcing elements of metal, e.g. with non-structural coatings
    • E04C5/06Reinforcing elements of metal, e.g. with non-structural coatings of high bending resistance, i.e. of essentially three-dimensional extent, e.g. lattice girders
    • E04C5/0636Three-dimensional reinforcing mats composed of reinforcing elements laying in two or more parallel planes and connected by separate reinforcing parts
    • E04C5/064Three-dimensional reinforcing mats composed of reinforcing elements laying in two or more parallel planes and connected by separate reinforcing parts the reinforcing elements in each plane being formed by, or forming a, mat of longitunal and transverse bars
    • EFIXED CONSTRUCTIONS
    • E04BUILDING
    • E04CSTRUCTURAL ELEMENTS; BUILDING MATERIALS
    • E04C5/00Reinforcing elements, e.g. for concrete; Auxiliary elements therefor
    • E04C5/01Reinforcing elements of metal, e.g. with non-structural coatings
    • E04C5/06Reinforcing elements of metal, e.g. with non-structural coatings of high bending resistance, i.e. of essentially three-dimensional extent, e.g. lattice girders
    • E04C5/065Light-weight girders, e.g. with precast parts
    • EFIXED CONSTRUCTIONS
    • E04BUILDING
    • E04CSTRUCTURAL ELEMENTS; BUILDING MATERIALS
    • E04C5/00Reinforcing elements, e.g. for concrete; Auxiliary elements therefor
    • E04C5/16Auxiliary parts for reinforcements, e.g. connectors, spacers, stirrups
    • E04C5/162Connectors or means for connecting parts for reinforcements
    • E04C5/166Connectors or means for connecting parts for reinforcements the reinforcements running in different directions
    • E04C5/167Connection by means of clips or other resilient elements

Definitions

  • This invention relates to the design of framework for the reinforcement of structures, including reinforcement for cementations, more particularly, the invention relates to an aperture reinforcement device that girds and cinctures other reinforcement in order to enhance composite and ductile properties of reinforcement arrays.
  • Such panels have also been designed to provide insulation, weather-tight sealing, and to be connected to adjacent panels, roof systems, and to footers.
  • the panels have typically been connected to roof trusses or rafters using conventional brackets, which are nailed to the wooden rafters or trusses and to wooden headers.
  • Fig. 1D shows one pair of intersecting trusses 12b in an array to form a panel assemblage.
  • Fig. 2A shows truss aperture formation by weaving of the web element over the cord.
  • Fig. 2B shows lateral reinforcement cinctured by apertures formed by alternating wed vertices.
  • Fig. 2D is a longitudinal cross section of a woven web aperture cincturing cords and a lateral.
  • Fig. 3C shows reinforcement cinctured at a right angel by the aperture shown in figures 3A and 3B.
  • Fig. 3G, 3H show cro9ssing and lapping cinctured by an independent aperture device.
  • Fig. 5A shows a foundation conection, truss, core, and cementation design alternative.
  • Fig. 50 is a truss core array with intersecting truss planes and aperture connections.
  • An array of reinforcement comprised of a plurality of trusses 12 are integrated into a space frame shown in (Fig 1) of predetermined length, width, and thickness by the insertion and attachment of lateral reinforcement 8c,d of predetermined size through aligned apertures 11 of spaced trusses.
  • truss 12 is disposed in spatial relationships with its neighbor by elements of an insulative core shown m ⁇ Fig ⁇ 31), whose grooved transverse faces ⁇ lheT central web area of trusses 11.
  • Space frame (Fi ⁇ 1D) is built up from interspersed truss 12 and insulative core elements 15. The predetermined dimensions of core elements 15 dispose and establish truss 1 spacing and truss 12 in turn positions core elements 15 in relation to space frame ( Fig 1E ) reinforcement attachments to allow required embedment in the event cementations (20) are applied.
  • each truss 12 In a given plurality is spaced, positioned and rotated equally and in opposite directions from its neighbors around a longitudinal axis so that the angled vertices 6 (Fig 1D) of neighboring trusses 12b lie flush with each other, sandwiched between two cords 8a,b. (Planes folded plate) Paired apertures 11
  • Perpendicular ductile truss connections 13 in which ⁇ pettums 11 (Figs 1 ⁇ and 1 H) formed by two connected web elements of a truss are overlapped in the area of truss interinterconnection such that lateral reinforcement 8c, 8d passes through apertures of both trusses at interconnection points 13a and 13B.
  • Apertures 11 are formed by the bending, weaving, sewing, or tying of web 7.
  • FIG. 11 formed by continuous web 7.
  • the manner of using the aperture device 11 is adaptable to structural requirements of any given form or disposition and can be erected as follows: panels can be fabricated and erected as framework reinforcement at site as follows: a preferred embodiment an element of said core 15 panels are placed on a horizontal surface with an edge 16 facing upward which has been grooved 14 to fit and position a truss 12. In this example, two opposite edges 16 of core panel 15 element are grooved 14. An adhesive is applied to said edge 16 and an element of an Anvick aperture (11) composite truss 12a-z configuration is fitted within the preformed grooves 14 which accept half of the girth of the wehhinp element 7 and position said element with respect to said core paneHS.
  • a corresponding grooved core paneHS element is fitted on top of the first element and completes the embedment of the first truss 12 configuration.
  • the positioning Is such that there Is sufficient clearance between the truss 12 and reinforcement attachment points 8a,b,c,d for required embedment in cementations 20.
  • This process is repeated, the core panel elements 15 aligned flush with each other and positioning the truss 12 array, until the desired panel width is assembled.
  • Once said adhesive has set the panel can be set in place on an arrangement of reinforcement protruding at predetermined spatial relation from a previously formed foundation structure 18.
  • independently locatable aperture cincturing devices 13a-z attach the foundation reinforcement 18 to either the lateral 8c,d or longitudinal 8a, b reinforcement elements when the aperture connecting, lateral reinforcement 8c,d are inserted through the apertures 11.
  • Welded wire fabric 19 can be installed, if called for, prior to the ad dition of said lateral reinforcement 8c,d. which then serves to cincture 13f, said fabric when installed overlt.
  • ⁇ yster ⁇ components alternatively may be fabricated off site.
  • each truss 12b in a given plurality is spaced, aligned, and then rotated in an opposite direction from adjacent trusses 12b so that they intersect at their corresponding apertures 11.
  • Said apertures 11 of said adjacent trusses 12 are bent at an angle to the web 7 so that they lie flush with one another.
  • Cords 8a and 8b of said trusses 12 sandwich the attached, paired, flush positioned vertices 6a forming paired apertures 11.
  • Reinforcement 8c,d is then inserted and communicated through and girded within said apertures 11 to complete an embodiments basic array.
  • the resulting array is a folded plate structure with multidirectional truss 12 behavior.
  • Said curvilinear and or wave form webbing 7 effect provides for a real three dimensional structural action once connecting reinforcement 8,c,d ,and 18, and cementations 20 are installed.
  • a truss 12b structure is elaborated by assembling said trusses 12 edge to edge in planes which intersect at longitudinal lines of vertices 6a which alternate from side to side of the resulting three dimensional space frame, along a transverse axis perpendicular to a longitudinal axis.
  • This transverse axis in cross section consequently resembles a longitudinal cross section, consisting of alternating substantially equilateral triangles, neighboring triangles inverted, between parallel lines, bases of said triangular cross section composed of cords 8c,d which pass through cincturing vertices 6a along the intersecting planes of longitudinal trusses 12.
  • Vertices 6a in this embodiment are bet ⁇ : at Sri angkf and al a location as to allow therrf to lie flush Wit each other, to be sandwiched between the double cords of a longitudinal truss, and to protrude beyond said cords sufficiently to allow a connecting transverse cords Sc.d to be threaded through the cincturing girdle formed between said dual cords and protruding vertex.
  • Said cords 12 form alternating lines from side to side of a so comprised space frame along said space frames longitudinal axis at the alternating vertices 6a of the continuous web 7 element initially described. Alternating intersecting planes of trusses 12 in both longitudinal and transverse sfr ⁇ cTures.
  • Each cinctXired verieYlSa of a frame is one comer of the square base of one or more said structures, depending upon location at an edge, corner, or in the field of a panel of this configuration of space frame, as well as summit vertex 6a of an inverted neighboring one, the alternate square bases forming a substantially planar opposite surface lattices of a space frame.
  • Independently locatable apertures can be shaped in a variety of shapes. When placed onto the array locatable apertures require cross reinforcement to by communicated into and held disposed within said aperture to effect installation of said aperture.
  • Trusses so equipped with aperture devices are positioned to space, align, and support reinforcement extending through and between foundation cementations and connecting structures. Use of trusses with apertures aligns such reinforcement to coincide with reinforcement of the supported reinforcement array. Similarly such use is appropriate and desirable for bond beam construction.
  • the Anvick composite aperture connection of this invention can be used in structural cementations and other hybrid material structures
  • the walls can be pre assembled, or p re-formed, offsite according to the required size dimensions and then transported to the job site.

Landscapes

  • Engineering & Computer Science (AREA)
  • Architecture (AREA)
  • Civil Engineering (AREA)
  • Structural Engineering (AREA)
  • Rod-Shaped Construction Members (AREA)
  • Woven Fabrics (AREA)

Abstract

L'invention concerne une ouverture constituée par un ou plusieurs éléments d'un support, utilisés pour former des connexions malléables avec d'autres éléments de renfort. Ladite ouverture peut être constituée par le positionnement, le recourbement, l'entrecroisement ou l'embranchement d'un ou plusieurs de ces éléments. Les supports peuvent être disposés en parallèle ou selon des plans d'intersection et reliés par l'utilisation des ouvertures sur l'emplacement ou fabriqués hors site. Ils peuvent être assemblés dans des structures ou dans des panneaux modulaires, ou faits sur commande, avec lesquels ces structures peuvent être établies, et inclus dans des injections de ciment. L'isolation et d'autres systèmes mécaniques peuvent être incorporés à ces renforts et systèmes de panneaux avant imbrication dans des injections de ciment. Les renforts formant des ouvertures peuvent également être employés pour incorporer des structures de la technique antérieure avec des propriétés améliorées. Les systèmes interconnectés résultants d'ouvertures, de renforts, d'isolation et d'autres systèmes sont généralement sont inclus dans les injections de ciment afin de donner des structures avec des interconnexions de ductilité supérieure et un comportement composite amélioré.
EP03814653A 2002-12-19 2003-12-05 Dispositif d'ouverture anvick et procede de formation et d'utilisation Withdrawn EP1664453A4 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US42097602P 2002-12-19 2002-12-19
PCT/US2003/038715 WO2004061247A2 (fr) 2002-12-19 2003-12-05 Dispositif d'ouverture anvick et procede de formation et d'utilisation

Publications (2)

Publication Number Publication Date
EP1664453A2 EP1664453A2 (fr) 2006-06-07
EP1664453A4 true EP1664453A4 (fr) 2009-08-05

Family

ID=32712947

Family Applications (1)

Application Number Title Priority Date Filing Date
EP03814653A Withdrawn EP1664453A4 (fr) 2002-12-19 2003-12-05 Dispositif d'ouverture anvick et procede de formation et d'utilisation

Country Status (5)

Country Link
US (1) US20060137282A1 (fr)
EP (1) EP1664453A4 (fr)
AU (1) AU2003297678A1 (fr)
CA (1) CA2543405A1 (fr)
WO (1) WO2004061247A2 (fr)

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US7140158B2 (en) * 2004-07-06 2006-11-28 William Steadman Composite beam
CA2574722C (fr) * 2007-01-22 2009-12-01 Ideas Without Borders Inc. Systeme de renforcement d'un element structural de batiment
US8852490B2 (en) * 2009-04-09 2014-10-07 Pat Halton Fore, III Systems and methods of concrete apparatus with incorporated lifter
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US20140059967A1 (en) * 2010-12-03 2014-03-06 Richard P. Martter Reinforcing assembly having working members with non-planar tips
US9121170B2 (en) * 2011-04-29 2015-09-01 Geo-Hidrol, S.A. Framework for structural use
US20130255667A1 (en) * 2012-04-02 2013-10-03 Colorado School Of Mines Solid particle thermal energy storage design for a fluidized-bed concentrating solar power plant
WO2013165235A1 (fr) * 2012-05-01 2013-11-07 Mesh Construction Technology (Mct) Panneau sandwich, procédé de construction d'un tel panneau sandwich, âme d'un tel panneau sandwich, et bâtiment construit d'une pluralité de tels panneaux sandwich
US9702348B2 (en) 2013-04-03 2017-07-11 Alliance For Sustainable Energy, Llc Chemical looping fluidized-bed concentrating solar power system and method
WO2015073098A2 (fr) * 2013-08-27 2015-05-21 University Of Virginia Patent Foundation Structures spatiales tridimensionnelles assemblées à partir de pièces de composants et leurs procédés de fabrication
US10119276B2 (en) 2016-07-15 2018-11-06 Richard P. Martter Reinforcing assemblies having downwardly-extending working members on structurally reinforcing bars for concrete slabs or other structures
US11220822B2 (en) 2016-07-15 2022-01-11 Conbar Systems Llc Reinforcing assemblies having downwardly-extending working members on structurally reinforcing bars for concrete slabs or other structures
US11242689B2 (en) * 2018-03-29 2022-02-08 Bailey Metal Products Limited Floor panel system
PT3556960T (pt) * 2018-04-20 2021-07-21 Solidian Gmbh Montagem de armadura e procedimento para fabrico de um corpo de material de construção mediante utilização da montagem de armadura
RU2680156C1 (ru) * 2018-05-30 2019-02-18 Александр Николаевич Чуйков Конструкционная панель и соединительный элемент для указанной панели
RU184157U1 (ru) * 2018-08-03 2018-10-17 Александр Николаевич Чуйков Арматурный каркас
US11092010B2 (en) 2019-02-20 2021-08-17 Dsi Tunneling Llc Underground support system and method
RU2744597C1 (ru) * 2020-06-30 2021-03-11 Александр Григорьевич Бекренёв Пространственный арматурный модуль

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GB117915A (en) * 1917-06-08 1918-08-08 Joah Haigh Walker Improvements in and relating to Metal Reinforcement for Concrete.
GB240018A (en) * 1924-10-27 1925-09-24 George William Stokes Improvements in or connected with metal re-inforcements for concrete and like work
FR2033467A5 (fr) * 1969-02-25 1970-12-04 Matreno
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AU7519481A (en) * 1980-09-10 1982-03-18 Wallen, R.L. Space frame
GB2164367A (en) * 1984-09-10 1986-03-19 Partek Ab A concrete building unit of a sandwich structure
FR2800112A1 (fr) * 1999-10-22 2001-04-27 Philippe Durand Armature pour paroi en beton

Also Published As

Publication number Publication date
US20060137282A1 (en) 2006-06-29
WO2004061247A2 (fr) 2004-07-22
EP1664453A2 (fr) 2006-06-07
AU2003297678A1 (en) 2004-07-29
AU2003297678A8 (en) 2004-07-29
WO2004061247A3 (fr) 2005-03-10
CA2543405A1 (fr) 2004-07-22

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