GB1351813A - Quasi-isotropic sandwich core filament winding method and apparatus for same - Google Patents

Quasi-isotropic sandwich core filament winding method and apparatus for same

Info

Publication number
GB1351813A
GB1351813A GB1529271A GB1529271A GB1351813A GB 1351813 A GB1351813 A GB 1351813A GB 1529271 A GB1529271 A GB 1529271A GB 1529271 A GB1529271 A GB 1529271A GB 1351813 A GB1351813 A GB 1351813A
Authority
GB
United Kingdom
Prior art keywords
jig
sheet
resin
series
mandrel
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.)
Expired
Application number
GB1529271A
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.)
FIGGE I E
Original Assignee
FIGGE I E
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 FIGGE I E filed Critical FIGGE I E
Publication of GB1351813A publication Critical patent/GB1351813A/en
Expired legal-status Critical Current

Links

Classifications

    • 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
    • E04C2/30—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by the shape or structure
    • E04C2/32—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by the shape or structure formed of corrugated or otherwise indented sheet-like material; composed of such layers with or without layers of flat sheet-like material
    • 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
    • B29C53/583—Winding and joining, e.g. winding spirally helically for making tubular articles with particular features
    • B29C53/587—Winding and joining, e.g. winding spirally helically for making tubular articles with particular features having a non-uniform wall-structure, e.g. with inserts, perforations, locally concentrated reinforcements
    • 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
    • B29C53/82—Cores or mandrels
    • B29C53/821—Mandrels especially adapted for winding and joining
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29D—PRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCES IN A PLASTIC STATE
    • B29D24/00—Producing articles with hollow walls
    • B29D24/002—Producing articles with hollow walls formed with structures, e.g. cores placed between two plates or sheets, e.g. partially filled
    • B29D24/005—Producing articles with hollow walls formed with structures, e.g. cores placed between two plates or sheets, e.g. partially filled the structure having joined ribs, e.g. honeycomb
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29D—PRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCES IN A PLASTIC STATE
    • B29D28/00—Producing nets or the like, e.g. meshes, lattices
    • B29D28/005—Reticulated structure comprising reinforcements of substantial or continuous length
    • 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
    • E04C2/30—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by the shape or structure
    • E04C2/34—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by the shape or structure composed of two or more spaced sheet-like parts
    • 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
    • Y10S52/00—Static structures, e.g. buildings
    • Y10S52/10—Polyhedron
    • 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
    • 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.]
    • Y10T428/24273—Structurally defined web or sheet [e.g., overall dimension, etc.] including aperture
    • Y10T428/24298—Noncircular aperture [e.g., slit, diamond, rectangular, etc.]
    • 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
    • Y10T428/29—Coated or structually defined flake, particle, cell, strand, strand portion, rod, filament, macroscopic fiber or mass thereof
    • Y10T428/2913—Rod, strand, filament or fiber
    • Y10T428/2933—Coated or with bond, impregnation or core
    • Y10T428/2964—Artificial fiber or filament
    • Y10T428/2967—Synthetic resin or polymer
    • Y10T428/2969—Polyamide, polyimide or polyester
    • 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
    • Y10T428/31504—Composite [nonstructural laminate]
    • Y10T428/31511—Of epoxy ether

Landscapes

  • Engineering & Computer Science (AREA)
  • Architecture (AREA)
  • Mechanical Engineering (AREA)
  • Civil Engineering (AREA)
  • Structural Engineering (AREA)
  • Moulding By Coating Moulds (AREA)

Abstract

1351813 Moulding resin-fibre elements I E FIGGE 17 May 1971 [20 May 1970] 15292/71 Heading B5A [Also in Divisions D1 and F2] A unitary resin-fibre structural element comprises alternate layers of mutually crossing filaments 6 disposed one above the other and defining a series of tetrahedrons 9 arranged in longitudinal rows, those in one row pointing upwards and those in adjacent rows pointing downwards and being in an offset sequential relation to adjacent rows. The fibres are laid in a series of parallel longitudinal planes and in two series of parallel planes that traverse the structure at opposite angles to the longitudinal axis. As shown all three planes are inclined to the minor axis (the vertical axis). The embodiment of Fig. 2 is prepared by winding one continuous filament back and forth across jig 1, impregnating the winding with epoxy resin, curing the resin, cutting any overhanging filament and removing the product from the jig. In the production of a cylindrical structure the jig comprises a cylindrical mandrel 10 upon which is helically wrapped a sheet 11 of fibreglass having upstanding knobs 12 of tetrahedral shape, the sheet being held in place by pins 5a driven into the mandrel in a helical path. Epoxy resin is applied and cured, the pins removed, any overhanging filament cut, the sheet 11 and the product removed from the mandrel 10 and the sheet removed from inside the product which may be used as a shaft. In a third embodiment the jig has the shape of an aerofoil.
GB1529271A 1970-05-20 1971-05-17 Quasi-isotropic sandwich core filament winding method and apparatus for same Expired GB1351813A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US3959770A 1970-05-20 1970-05-20

Publications (1)

Publication Number Publication Date
GB1351813A true GB1351813A (en) 1974-05-01

Family

ID=21906328

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1529271A Expired GB1351813A (en) 1970-05-20 1971-05-17 Quasi-isotropic sandwich core filament winding method and apparatus for same

Country Status (4)

Country Link
US (1) US3645833A (en)
JP (1) JPS5539658B1 (en)
DE (1) DE2124614A1 (en)
GB (1) GB1351813A (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2527867A1 (en) * 1974-07-05 1976-02-05 Europ Propulsion THREE-DIMENSIONAL STRUCTURE FOR REINFORCEMENT AND PROCEDURE FOR ITS IMPLEMENTATION
DE2912463A1 (en) * 1978-03-29 1979-11-15 Europ Propulsion THREE-DIMENSIONAL RING-SHAPED TEXTURE, USED IN PARTICULAR AS A REINFORCEMENT
GB2149061A (en) * 1983-10-26 1985-06-05 Agusta Aeronaut Costr Propeller shafts
GB2158471A (en) * 1984-05-04 1985-11-13 Budd Co Fiberous armor material
GB2309928A (en) * 1996-02-06 1997-08-13 Deutsche Forsch Luft Raumfahrt Production of a curved fibre-resin composite element

Families Citing this family (34)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3849237A (en) * 1971-04-08 1974-11-19 L Zetlin Structural member of sheet material
US3772126A (en) * 1971-10-21 1973-11-13 M & M Intern Plastics Inc Apparatus and method for making fiberglass grating
US3983281A (en) * 1973-07-16 1976-09-28 Wakeman Alfred W Tape structures
US4020205A (en) * 1975-06-13 1977-04-26 The United States Of America As Represented By The Secretary Of The Army Structural cores
US4241117A (en) * 1979-06-14 1980-12-23 The United States Of America As Represented By The Secretary Of The Army Structural cores and their fabrication
US4348442A (en) * 1979-08-17 1982-09-07 Figge Irving E Structural panel
DE2935198C2 (en) * 1979-08-31 1981-12-24 Heraeus Quarzschmelze Gmbh, 6450 Hanau Process for the tool-free production of porous shaped bodies from quartz glass and the use of these shaped bodies
US4376669A (en) * 1980-08-15 1983-03-15 The British Petroleum Company Limited Method of fabricating energy absorbing structure
US4357292A (en) * 1981-08-27 1982-11-02 International Grating, Inc. Method of molding in solid floor plate to a fiberglass reinforced molded resin grating
US4715560A (en) * 1983-03-14 1987-12-29 Lear Fan Limited Composite cruciform structure for joining intersecting structural members of an airframe and the like
US4600619A (en) * 1984-12-31 1986-07-15 The Boeing Company Continuously wound filament structure for use in noise attenuation element
US4741943A (en) * 1985-12-30 1988-05-03 The Boeing Company Aerodynamic structures of composite construction
US4719726A (en) * 1986-04-14 1988-01-19 Helmut Bergman Continuous spherical truss construction
US4857125A (en) * 1986-12-22 1989-08-15 General Electric Company Method for reinforcing conical shaped object
US5593395A (en) * 1987-08-07 1997-01-14 Martz; Joel D. Vapor permeable dressing
US5061258A (en) * 1987-08-07 1991-10-29 Martz Joel D Vapor permeable dressing with releasable medication
GB8808280D0 (en) * 1988-04-08 1988-05-11 Lk Tool Co Ltd Machine structure
US5070673A (en) * 1988-11-02 1991-12-10 Tetrahex, Inc. Tetrahexagonal truss structure
US5040966A (en) * 1988-11-02 1991-08-20 Tetrahex, Inc. Die for making a tetrahexagonal truss structure
US4923544A (en) * 1988-11-02 1990-05-08 Tetrahex, Inc. Method of manufacturing a tetrahexaconal truss structure
US4974275A (en) * 1989-12-04 1990-12-04 Backes James G Method of manufacture of snowshoes
CA2058025C (en) * 1990-12-21 2003-01-21 George Daniel Forsythe Process for multiple yarn winding in ordered fashion and resulting product
US5215615A (en) * 1990-12-21 1993-06-01 E. I. Du Pont De Nemours And Company Process for multiple yarn winding in ordered fashion and resulting product
US5435869A (en) * 1993-08-27 1995-07-25 Christensen; Roland Method for manufacturing a composite crank arm
US5913994A (en) * 1996-08-30 1999-06-22 Norton Company Method for fabricating abrasive discs
US6007894A (en) * 1997-07-10 1999-12-28 Mcdonnell Dougal Corporation Quasi-isotropic composite isogrid structure and method of making same
US6641897B2 (en) * 1998-02-13 2003-11-04 The Milwaukee School Of Engineering Three dimensional object
US6655633B1 (en) * 2000-01-21 2003-12-02 W. Cullen Chapman, Jr. Tubular members integrated to form a structure
US20040037979A1 (en) * 2002-08-21 2004-02-26 Monson Robert James Pressurized elastomer mount
US20030146346A1 (en) * 2002-12-09 2003-08-07 Chapman Jr W. Cullen Tubular members integrated to form a structure
WO2010019802A1 (en) * 2008-08-15 2010-02-18 Gesturetek, Inc. Enhanced multi-touch detection
US8444900B2 (en) * 2008-08-15 2013-05-21 Sigma-Tek, Llc Method and system for forming composite geometric support structures
US9126374B2 (en) 2010-09-28 2015-09-08 Russell B. Hanson Iso-grid composite component
CA3045029C (en) 2017-04-24 2023-12-05 Rigidcore Group Llc Sheet material, mold, and methods of making and using the sheet material and mold

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3047191A (en) * 1957-11-26 1962-07-31 Hercules Powder Co Ltd Filament wound vessels and methods for forming same
US3086576A (en) * 1959-12-14 1963-04-23 Herbert V Thaden Apparatus for forming products from resin-impregnated long fiber filaments
US3436038A (en) * 1967-04-11 1969-04-01 Aerojet General Co Structures
US3425884A (en) * 1967-11-06 1969-02-04 Crompton & Knowles Corp Method of making an open mesh,rigid,glass fiber reinforced resin structure

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2527867A1 (en) * 1974-07-05 1976-02-05 Europ Propulsion THREE-DIMENSIONAL STRUCTURE FOR REINFORCEMENT AND PROCEDURE FOR ITS IMPLEMENTATION
DE2912463A1 (en) * 1978-03-29 1979-11-15 Europ Propulsion THREE-DIMENSIONAL RING-SHAPED TEXTURE, USED IN PARTICULAR AS A REINFORCEMENT
GB2149061A (en) * 1983-10-26 1985-06-05 Agusta Aeronaut Costr Propeller shafts
GB2158471A (en) * 1984-05-04 1985-11-13 Budd Co Fiberous armor material
GB2309928A (en) * 1996-02-06 1997-08-13 Deutsche Forsch Luft Raumfahrt Production of a curved fibre-resin composite element
GB2309928B (en) * 1996-02-06 1999-08-18 Deutsche Forsch Luft Raumfahrt Process for the production of a structural element

Also Published As

Publication number Publication date
JPS5539658B1 (en) 1980-10-13
DE2124614A1 (en) 1973-06-14
US3645833A (en) 1972-02-29

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Legal Events

Date Code Title Description
PS Patent sealed [section 19, patents act 1949]
PCNP Patent ceased through non-payment of renewal fee