GB577790A - Improvements relating to the manufacture of light non-metallic structural material or components - Google Patents

Improvements relating to the manufacture of light non-metallic structural material or components

Info

Publication number
GB577790A
GB577790A GB25297/38A GB2529738A GB577790A GB 577790 A GB577790 A GB 577790A GB 25297/38 A GB25297/38 A GB 25297/38A GB 2529738 A GB2529738 A GB 2529738A GB 577790 A GB577790 A GB 577790A
Authority
GB
United Kingdom
Prior art keywords
cores
resin
cellular
pack
skin
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
GB25297/38A
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.)
AERO RES Ltd
De Havilland Aircraft Co Ltd
Original Assignee
AERO RES Ltd
De Havilland Aircraft Co Ltd
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 AERO RES Ltd, De Havilland Aircraft Co Ltd filed Critical AERO RES Ltd
Priority to GB25297/38A priority Critical patent/GB577790A/en
Publication of GB577790A publication Critical patent/GB577790A/en
Expired legal-status Critical Current

Links

Classifications

    • 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
    • B29C66/00—General aspects of processes or apparatus for joining preformed parts
    • B29C66/70—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
    • B29C66/72—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the structure of the material of the parts to be joined
    • B29C66/721—Fibre-reinforced materials
    • 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
    • B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
    • B29C65/02—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure
    • 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
    • B29C66/00—General aspects of processes or apparatus for joining preformed parts
    • B29C66/01—General aspects dealing with the joint area or with the area to be joined
    • B29C66/05—Particular design of joint configurations
    • B29C66/10—Particular design of joint configurations particular design of the joint cross-sections
    • B29C66/11—Joint cross-sections comprising a single joint-segment, i.e. one of the parts to be joined comprising a single joint-segment in the joint cross-section
    • B29C66/112—Single lapped joints
    • 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
    • B29C66/00—General aspects of processes or apparatus for joining preformed parts
    • B29C66/01—General aspects dealing with the joint area or with the area to be joined
    • B29C66/05—Particular design of joint configurations
    • B29C66/10—Particular design of joint configurations particular design of the joint cross-sections
    • B29C66/11—Joint cross-sections comprising a single joint-segment, i.e. one of the parts to be joined comprising a single joint-segment in the joint cross-section
    • B29C66/114—Single butt joints
    • 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
    • B29C66/00—General aspects of processes or apparatus for joining preformed parts
    • B29C66/40—General aspects of joining substantially flat articles, e.g. plates, sheets or web-like materials; Making flat seams in tubular or hollow articles; Joining single elements to substantially flat surfaces
    • B29C66/41—Joining substantially flat articles ; Making flat seams in tubular or hollow articles
    • B29C66/43—Joining a relatively small portion of the surface of said articles
    • B29C66/438—Joining sheets for making hollow-walled, channelled structures or multi-tubular articles
    • 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
    • B29C66/00—General aspects of processes or apparatus for joining preformed parts
    • B29C66/70—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
    • B29C66/72—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the structure of the material of the parts to be joined
    • B29C66/729—Textile or other fibrous material made from plastics
    • B29C66/7292—Textile or other fibrous material made from plastics coated
    • 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
    • B29C70/28—Shaping operations therefor
    • B29C70/30—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core
    • B29C70/34—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core and shaping or impregnating by compression, i.e. combined with compressing after the lay-up operation
    • B29C70/345—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core and shaping or impregnating by compression, i.e. combined with compressing after the lay-up operation using matched moulds
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • 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
    • 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
    • B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
    • B29C65/02—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure
    • B29C65/18—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using heated tools
    • 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
    • B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
    • B29C65/02—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure
    • B29C65/18—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using heated tools
    • B29C65/24—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using heated tools characterised by the means for heating the tool
    • B29C65/30—Electrical means
    • 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
    • B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
    • B29C65/48—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding
    • B29C65/4805—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding characterised by the type of adhesives
    • B29C65/483—Reactive adhesives, e.g. chemically curing adhesives
    • 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
    • B29C66/00—General aspects of processes or apparatus for joining preformed parts
    • B29C66/70—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
    • B29C66/72—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the structure of the material of the parts to be joined
    • B29C66/721—Fibre-reinforced materials
    • B29C66/7214—Fibre-reinforced materials characterised by the length of the fibres
    • B29C66/72141—Fibres of continuous length
    • 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
    • B29C66/00—General aspects of processes or apparatus for joining preformed parts
    • B29C66/70—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
    • B29C66/73—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset
    • B29C66/739—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the material of the parts to be joined being a thermoplastic or a thermoset
    • B29C66/7394—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the material of at least one of the parts being a thermoset
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
    • B29K2105/00—Condition, form or state of moulded material or of the material to be shaped
    • B29K2105/24—Condition, form or state of moulded material or of the material to be shaped crosslinked or vulcanised
    • B29K2105/246—Uncured, e.g. green
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
    • B29L2024/00—Articles with hollow walls
    • B29L2024/006—Articles with hollow walls multi-channelled
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
    • B29L2031/00—Other particular articles
    • B29L2031/30—Vehicles, e.g. ships or aircraft, or body parts thereof
    • B29L2031/3076—Aircrafts
    • B29L2031/3085—Wings
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
    • B29L2031/00—Other particular articles
    • B29L2031/60—Multitubular or multicompartmented articles, e.g. honeycomb
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
    • B29L2031/00—Other particular articles
    • B29L2031/60—Multitubular or multicompartmented articles, e.g. honeycomb
    • B29L2031/608—Honeycomb structures
    • 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
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/40—Weight reduction

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Architecture (AREA)
  • Chemical & Material Sciences (AREA)
  • Composite Materials (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Civil Engineering (AREA)
  • Structural Engineering (AREA)
  • Textile Engineering (AREA)
  • Laminated Bodies (AREA)

Abstract

577,790. Compound sheet materials. BRUYNE, N. A. De, AERO RESEARCH, Ltd., and DE HAVILLAND AIRCRAFT CO., Ltd. Aug. 29, 1938, Nos. 25297 and 31468. [Class 140] [Also in Groups V and XXXIII] A method of manufacturing light reinforced synthetic - resin structures in cellular form, applicable to the construction of aircraft &c. comprises laying or wrapping an unset resinimpregnated fibrous or filar reinforcement material, such as textile fabric, rove, sliver, &c, over or around a series of cores so that these cores, which are packed together substantially parallel, are each surrounded and continuously separated by the material, applying heat to the pack, applying pressure to the pack transversely to the cores, and withdrawing the cores endwise from the material, whereby a set cellular structure of reinforced resin is left. To produce a structure having hexagonal cells or passages, a mould bed 1, Fig. 1, is provided with ribs and grooves, and over it is applied a first layer 2 of resin-impregnated fabric, a series of hexagonal cores 3, a second layer 4 of impregnated fabric, a second series 5 of cores, and so on, the pack being completed by a platen 8 and then heated and compressed, after which the cores are withdrawn endwise. Alternatively, the cells may be of triangular, square, circular &c. crosssection. The outer surfaces of the cellular material may be covered by a sheet or skin of resin-impregnated or adhesive-treated material, such as laminated material or wood veneer, which may be applied prior to the application of heat and pressure to the pack. The set material, e.g., in the form of a plank or board, may have the cellular cross-section either transverse to the board &c. or in the plane thereof, the latter form being applicable to a tailplane &c. structure provided with a stressed skin. Such a skin may be formed by applying over the ends of the cell walls 36, Fig. 9, a layer of impregnated fabric 37, which is pressed down to form shallow pockets and is secured by stitching or stringing 38' at each side of the walls 36. The pockets are filled with unset resin 38, over which is laid a skin 39 of impregnated veneer, fabric, metal &c. the whole being set by heat and pressure. The cellular structure may be curved in cross-section. The cells may taper lengthwise.
GB25297/38A 1938-08-29 1938-08-29 Improvements relating to the manufacture of light non-metallic structural material or components Expired GB577790A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB25297/38A GB577790A (en) 1938-08-29 1938-08-29 Improvements relating to the manufacture of light non-metallic structural material or components

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB25297/38A GB577790A (en) 1938-08-29 1938-08-29 Improvements relating to the manufacture of light non-metallic structural material or components

Publications (1)

Publication Number Publication Date
GB577790A true GB577790A (en) 1946-05-31

Family

ID=10225404

Family Applications (1)

Application Number Title Priority Date Filing Date
GB25297/38A Expired GB577790A (en) 1938-08-29 1938-08-29 Improvements relating to the manufacture of light non-metallic structural material or components

Country Status (1)

Country Link
GB (1) GB577790A (en)

Cited By (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2639248A (en) * 1949-07-27 1953-05-19 Us Plywood Corp Dielectric material
US2700634A (en) * 1949-09-09 1955-01-25 Northrop Aircraft Inc Method of laminating a cellular core sandwich
US2744042A (en) * 1951-06-21 1956-05-01 Goodyear Tire & Rubber Laminated panels
US2793972A (en) * 1954-05-24 1957-05-28 Goodyear Aircraft Corp Method of making metal-faced laminates
US2816298A (en) * 1954-11-12 1957-12-17 Joseph F Foster Boat construction
US3139369A (en) * 1960-08-03 1964-06-30 Lockheed Aircraft Corp Apparatus for making laminated building panels of cellular structure
US3339326A (en) * 1964-07-06 1967-09-05 Midland Ross Corp Panel with triangular cross-section foam core elements
FR2545037A1 (en) * 1983-04-27 1984-11-02 Messerschmitt Boelkow Blohm CONSTRUCTION-SANDWICH ELEMENT IN FIBROUS COMPOSITE MATERIAL
FR2559422A1 (en) * 1984-02-13 1985-08-16 Gen Electric COMPOSITE HOLLOW BLADE PROFILE ELEMENT WITH CORRUGATED INTERNAL SUPPORT STRUCTURE AND MANUFACTURING METHOD THEREOF
GB2188281A (en) * 1986-03-25 1987-09-30 Tidd Strongbox Ltd Structural panel
GB2225282A (en) * 1988-09-30 1990-05-30 Michael Sean Barron Fibre reinforced foam structural components
GB2225742A (en) * 1988-12-09 1990-06-13 Westland Helicopters Moulding a fibre reinforced composite, into a hollow structure comprising outer and inner skins connected by ribs
US5399221A (en) * 1990-05-04 1995-03-21 Northrop Grumman Corporation Continuous process for forming fiber-reinforced high temperature thermoplastic resin honeycomb structures
US8057623B2 (en) 2006-07-14 2011-11-15 Airbus Operations Limited Composite manufacturing method
WO2016085336A1 (en) * 2014-11-27 2016-06-02 Fibercore Ip B.V. Method for forming of a tubular semi-finished product from fibre-reinforced plastic material
US9481115B2 (en) 2006-08-14 2016-11-01 Airbus Operations Limited Moulding tool and method of manufacturing a part
CN109720011A (en) * 2018-12-18 2019-05-07 天长市天翔集团有限公司 A kind of corrugated board forming processing device
US11046420B2 (en) * 2019-10-23 2021-06-29 The Boeing Company Trailing edge flap having a waffle grid interior structure

Cited By (27)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2639248A (en) * 1949-07-27 1953-05-19 Us Plywood Corp Dielectric material
US2700634A (en) * 1949-09-09 1955-01-25 Northrop Aircraft Inc Method of laminating a cellular core sandwich
US2744042A (en) * 1951-06-21 1956-05-01 Goodyear Tire & Rubber Laminated panels
US2793972A (en) * 1954-05-24 1957-05-28 Goodyear Aircraft Corp Method of making metal-faced laminates
US2816298A (en) * 1954-11-12 1957-12-17 Joseph F Foster Boat construction
US3139369A (en) * 1960-08-03 1964-06-30 Lockheed Aircraft Corp Apparatus for making laminated building panels of cellular structure
US3339326A (en) * 1964-07-06 1967-09-05 Midland Ross Corp Panel with triangular cross-section foam core elements
FR2545037A1 (en) * 1983-04-27 1984-11-02 Messerschmitt Boelkow Blohm CONSTRUCTION-SANDWICH ELEMENT IN FIBROUS COMPOSITE MATERIAL
FR2559422A1 (en) * 1984-02-13 1985-08-16 Gen Electric COMPOSITE HOLLOW BLADE PROFILE ELEMENT WITH CORRUGATED INTERNAL SUPPORT STRUCTURE AND MANUFACTURING METHOD THEREOF
GB2154286A (en) * 1984-02-13 1985-09-04 Gen Electric Hollow laminated airfoil
GB2188281A (en) * 1986-03-25 1987-09-30 Tidd Strongbox Ltd Structural panel
GB2188281B (en) * 1986-03-25 1989-11-15 Tidd Strongbox Ltd Structural panel
GB2225282A (en) * 1988-09-30 1990-05-30 Michael Sean Barron Fibre reinforced foam structural components
GB2225282B (en) * 1988-09-30 1992-07-15 Michael Sean Barron Fibre reinforced foam structural components.
GB2225742A (en) * 1988-12-09 1990-06-13 Westland Helicopters Moulding a fibre reinforced composite, into a hollow structure comprising outer and inner skins connected by ribs
US5399221A (en) * 1990-05-04 1995-03-21 Northrop Grumman Corporation Continuous process for forming fiber-reinforced high temperature thermoplastic resin honeycomb structures
US8057623B2 (en) 2006-07-14 2011-11-15 Airbus Operations Limited Composite manufacturing method
US9764518B2 (en) 2006-07-14 2017-09-19 Airbus Operations Limited Composite manufacturing method
US9481115B2 (en) 2006-08-14 2016-11-01 Airbus Operations Limited Moulding tool and method of manufacturing a part
NL2013887A (en) * 2014-11-27 2016-09-20 Fibercore Ip Bv Method for forming a tubular semi-finished product from fiber-reinforced plastic material.
CN107000337A (en) * 2014-11-27 2017-08-01 光纤芯Ip有限公司 Tubular semifinished method is formed by fiber reinforced plastic materials
WO2016085336A1 (en) * 2014-11-27 2016-06-02 Fibercore Ip B.V. Method for forming of a tubular semi-finished product from fibre-reinforced plastic material
US10336012B2 (en) * 2014-11-27 2019-07-02 Fibercore Ip B.V. Method for forming of a tubular semi-finished product from fibre-reinforced plastic material
CN107000337B (en) * 2014-11-27 2019-09-24 光纤芯Ip有限公司 Tubular semifinished method is formed by fiber reinforced plastic materials
CN109720011A (en) * 2018-12-18 2019-05-07 天长市天翔集团有限公司 A kind of corrugated board forming processing device
CN109720011B (en) * 2018-12-18 2020-10-30 天长市天翔集团有限公司 Corrugated container board forming device
US11046420B2 (en) * 2019-10-23 2021-06-29 The Boeing Company Trailing edge flap having a waffle grid interior structure

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