US3391511A - Lightweight structure having a honeycomb interior - Google Patents

Lightweight structure having a honeycomb interior Download PDF

Info

Publication number
US3391511A
US3391511A US378168A US37816864A US3391511A US 3391511 A US3391511 A US 3391511A US 378168 A US378168 A US 378168A US 37816864 A US37816864 A US 37816864A US 3391511 A US3391511 A US 3391511A
Authority
US
United States
Prior art keywords
wall
cell units
sheets
cell
sheet
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 - Lifetime
Application number
US378168A
Other languages
English (en)
Inventor
Harris Leighton Richard
Davey Alan Edwin
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.)
Rolls Royce Composite Materials Ltd
Original Assignee
Bristol Aeroplane Plastics 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 Bristol Aeroplane Plastics Ltd filed Critical Bristol Aeroplane Plastics Ltd
Application granted granted Critical
Publication of US3391511A publication Critical patent/US3391511A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

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
    • E04C2/34—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
    • E04C2/36—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 spaced apart by transversely-placed strip material, e.g. honeycomb panels
    • 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
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B27/00—Layered products comprising a layer of synthetic resin
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • 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
    • Y10T428/24165—Hexagonally shaped cavities

Definitions

  • a structure according to this disclosure consists of two skins of sheet material, and a system of interconnected webs extending through the structure from one skin to the other, the webs being constituted by the walls of a plurality of cell units, each cell unit having a wall which forms a closed perimeter and which is perpendicular to the sheets or nearly so, the wall of each cell unit being substantially in contact with, and secured to, the walls of neighbouring cell units, and the ends of the walls of the cell units being secured to the skins, the securing between each cell unit and each skin being distributed over an area several times greater than the cross sectional area of the wall of that cell unit intersected by an imaginary plane lying between the sheets.
  • This invention concerns structures having a thickness dimension of a lesser order than their other two dimensions.
  • the invention has been developed for such purposes as the making of hulls of boats, and domed structures, but it is of wide potential use.
  • a method of making a structure according to this invention comprises assembling a plurality of substantially rigid cell units between two sheets, each cell unit having a wall which forms a closed perimeter and which is perpendicular to the sheets or nearly so, the wall of each cell unit being substantially in contact with the walls of the neighbouring cell units, and the ends of the cell units being substantially in contact with the sheets; and securing the cell units to one another and to the sheets at those surfaces which are substantially in contact, the securing between each cell unit and each sheet being distributed over an area several times greater than the cross sectional area of the wall of that cell unit intersected by an imaginary plane lying between the sheets; the walls of the cell units collectively becoming a system of interconnected webs extending through the final structure from one sheet to the other.
  • FIGURE 1 is a perspective view of a structure in course of assembly, using cell units with corrugated walls;
  • FIGURES 2 and 3 show alternative shapes of cell unit
  • FIGURES 4 to 6 show alternative constructions of cell unit
  • FIGURE 7 illustrates the use of tapered cell units to make a curved structure
  • FIGURE 8 is a view similar to FIGURE 1, showing cell units with tongues and grooves on their walls;
  • FIGURES 9 to 11 illustrate the formation of structures of single or double curvature, using cell units as shown in FIGURE 8;
  • FIGURE 12 is a perspective view of a larger cell unit.
  • FIGURE 13 shows one way of completing the edge of a structure.
  • each unit includes an outer component 2 and an inner component 14. These are rigid mouldings of resin-impregnated glass fibre.
  • the perimeter of the outer component formed by a wall 4, is square, and each face of the wall has corrugations, with flat crests 6, extending from end to end of the cell unit.
  • One end of the outer component (the upper end in FIGURE 1) is open, and the other end is closed by an end wall 10, which is integral with the wall 4.
  • the open end is encircled by an intermittent flange 12.
  • an inverted inner component 14 which is generally similar to the outer component 2, but with a perimeter wall 13 which is plain and sufficiently smaller to fit inside the outer component.
  • the wall 13 of the inner component 14 is coated with a synthetic resin adhesive, preferably an epoxy resin, for example by dipping, brushing, or spraying.
  • a synthetic resin adhesive preferably an epoxy resin
  • this adhesive forms a layer in contact with the walls 4, 13 of both components. This gradually cures at atmospheric temperature, or curing may be assisted by heating.
  • a support 16 is made ready, with a top surface 17 having the contour required for one face of the structure, in this case fiat.
  • the support 16 may be of concrete.
  • a sheet 13 of felted glass fibres is soaked in epoxy resin, and is then laid on the support.
  • a plurality of the cell units 15 are coated with epoxy resin and are then assembled on the sheet into close relationship, with the corrugation crests 6 of each cell unit abutting respective crests on neighbouring cell units.
  • a second sheet 20 of felted glass fibre soaked in epoxy resin is laid upon the assembly, and is pressed down by a roller (not shown). Then the components are left while the resin cures, either at atmospheric temperature, or with the application of heat.
  • the resin forms bonds between all those surfaces which are substantially in contact, namely between the lower end walls 10 and the sheet 18, between the upper ends 19 of the components 14 and the sheet 20, between the flanges 12 and the sheet 20, and between the abutting corrugation crests 6.
  • the cell units 15 become bonded to the sheets and to one another, and the walls 4 and 13 collectively become a system of interconnected webs, which irnpart stability to the structure in all directions and which are themselves stiffened by the corrugations.
  • the resin in the sheets 18 and 20 may act as the bonding agent between the sheets and the cell units 15, so that it may only be necessary to coat the crests 6 of the corrugations on the cell units before assembly.
  • a principal feature of the invention is that the area of bonded surfaces between each cell unit 15 and each sheet 18 or 20 is several times greater than the cross sectional area of the wall of that cell unit which is intersected by an imaginary plane lying between the sheets.
  • FIGURE 1 where part of the wall 4 of one outer component 2 is shown broken away to the plane A-A, to reveal the cross section 22.
  • the cross section of the wall 13 of the inner component 14 requires to be added to this, and is indicated in chain lines at 24. In this way, an optimum relationship may be Obtained between the weight of the structure as a whole, and the strengths of the webs and of the bonded joints.
  • each cell unit and each sheet is at least 10 times the cross sectional area of the wall of that cell intersected by an imaginary plane lying between the sheets.
  • FIGURE 8 shows how the inner component 14 may be replaced by a lid 26, with a depending skirt 28 which fits inside the wall 4 and is bonded to it.
  • FIGURE 12 shows a rectangular perimeter
  • FIGURES 2 and 3 show examples of regular polygonal perimeters; hexagonal in FIGURE 2 and triangular in FIGURE 3.
  • Preferably all the cell units have the same polygonal perimeter.
  • an assortment of cell unit shapes and sizes may be used.
  • the walls 30 of the outer components 32 are flat, like those of the inner components 34.
  • FIGURE 4 shows a cell wall 36 with upper and lower open ends, closed by lids 38, 40, which have skirts 42, 44 which fit within the wall 36 and are bonded to it.
  • the area of the flat face 46 of each lid is preferably at least times the cross section of the wall 36.
  • Each lid has a flange 48 which projects as far as the plane of the corrugation crests 58, but no further.
  • the cell wall 36 may be formed by cutting lengths from a tube, preferably one produced by extrusion.
  • a flange 12 as shown in FIGURE 1 may provide the sole connection, the inner component 14 of FIGURE 1 being omitted. Furthermore, this flange 12 may be repeated at the other end of the cell unit, in place of an integral end wall 10. Such flanges may be moulded integral with the wall 4, as shown in FIGURE 1. Alternatively they may be separate components, similar to the lids 38, 40 in FIGURE 4, but with the parts within the skirts 42, 44 omitted.
  • the interiors of the cell units may simply contain air, or other gas, or they may be filled with lightweight matcrial, e.g. polyvinyl chloride foam. If the cell units are open-ended, such material will help to keep the sheets 13 and smooth until they have cured.
  • lightweight matcrial e.g. polyvinyl chloride foam.
  • FIGURES 5 and 6 illustrate other forms of cell unit construction, in both of which the cell unit is a hollow block.
  • the wall 52 and ends 54 are all parts of an integral moulding formed around a core 55, which may be of lightweight material and be left in place, or may be of low melting point material which is removed through a small hole by heating after curing.
  • the wall 57 is built up of components secured together, and is also secured to end members 5?. This construction is particularly convenient if the cell unit is of metal.
  • the parts of the cell unit may be welded or riveted together, or may be bonded, either by a suitable adhesive, or by a low melting point metal, i.e. by soldering or brazing.
  • the cell units may be tapered from one end to the other, as shown at 55 in FIGURE 7. By placing the cell units alternately opposite ways up, it is possible to produce flat areas of structure using these same tapered cell units.
  • FIGURES 8 to ll A more versatile means of producing curved structures is shown in FIGURES 8 to ll.
  • the outsides of the walls 58 of the cell units have tongues 60 and grooves 62, defined between pairs of ribs 64. These tongues and grooves extend from end to end of the cell unit, and are brought into cooperating engagement with grooves and tongues of neighbouring cell units, and a bonding agent is provided between the engaging tongues and grooves.
  • FIGURES 9 and 10 it is possible to tilt adjacent units relatively to one another while still retaining a substantial area of bonding between tongues and grooves.
  • the grooves 62 are somewhat wider than the tongues 6i), and in addition the grooves and tongues may be somewhat tapered as shown. This enables adjacent cell units to be twisted somewhat relatively to one another, as indicated by the outline 65 in FIGURE 9. In this way, curved structures, for example as complex as that shown in FIGURE 11, may be made.
  • the Wall may be moulded, or may be extruded in the manner described with reference to FIGURE 4.
  • the tongues 69 and ribs 64 form parts of the system of interconnected webs in the completed structure. In fact, the remainder of the walls of neighbouring cell units need not come close together.
  • the cell walls may be cylindrical, with tongues and grooves alternately at intervals of around their peripheries.
  • Another way of making curved structures is by using cell units with corrugated walls as shown in FIGURE 1, but arranged so that the crests on any one unit enter the valleys in adjacent units, and vice versa.
  • the sheets should either be formed to a correct rigid curved shape between being placed in position, or should be of flexible material. If these are substantial double curvature, the sheets should either again be formed to curved shape beforehand, or they should be of material which will stretch. A fibrous material is particularly suitable.
  • the cell units are of larger area, as may be the case in flat structures, they may have internal partitions, as shown at 66 in FIGURE 12.
  • the spacing of the walls (and partitions if any) in the cell units should be selected in accordance with the rigidity of the skins in relation to the rigidity of the structure as a whole, and can be chosen to produce an optimum ratio of strength and rigidity to weight of structure. Moreover, the spacing can be made non-uniform, to deal with localised points of high loading of the structure.
  • fillers 68 of a curable resin/ fibre dough may be used, to produce a required outline while using cell units of a uniform shape, and this outline may be closed in by a cover strip 70.
  • the layers of sheet material are each 0.3 inch thick, of glass fibre reinforced plastic material, and the cell units are as shown in FIG- URE 1, measuring 5 inches square and 3 inches deep.
  • the inner and outer components making up each cell unit are made as pressure mouldings from a glass fibre dough, and have wall thicknesses of 0.1 inch.
  • a wide variety of materials may be used for the cell units and for the sheets, and a wide variety of means may be used for securing the cell units to one another and to the sheets.
  • materials may be used for the cell units and for the sheets, and a wide variety of means may be used for securing the cell units to one another and to the sheets.
  • means may be used for securing the cell units to one another and to the sheets.
  • the sheets may be of: fibrous material impregnated with synthetic resin, the fibrous material being of glass, asbestos, sisal, or wire, and being in the form of woven sheet, parallel threads or rovings, felt, or mat; continuous sheets of polyvinyl chloride, nylon, or polythene; or metal, in particular stainless steel.
  • the cell units may be of materials similar to those of the sheets.
  • the securing may be by means of an epoxy, polyester, phenol, or rubber based adhesive; welding synthetic resinous materials by a solvent; soldering, brazing, spot welding or puddle welding of metals; or riveting. If an adhesive, a solvent, or a low melting point metal is used, the
  • securing may be by bonding over the entire area of those surfaces which are substantially in contact. If the securing is by spot welding, puddle welding (i.e. local fushion initiated from one outer face only of two thin components to be joined), or riveting, the securing is at a plurality of points distributed over the area. In all cases, the areas are made sufficiently great to enable the securing of the webs to the sheet to be of the same order of strength as the webs themselves.
  • a structure according to the invention may be formed from more than one sandwich; for exmple it could comprise three layers of sheet material, two outer and one central, and two intermediate layers of cell units.
  • a lightweight sandwich structure and having a honeycomb interior comprising a first sheet, a plurality of adjacent, individual and substantially rigid cell units of plastic material which are each covered on one side thereof by, and bonded to the said first sheet, and a second sheet which covers, and is bonded to, sides of the said adjacent cell units opposite each said one side; each cell unit comprising a continuous peripheral wall which lies transversely to both said first and second sheets, first and second sheet engaging portions which are substantially wider than the thickness of said peripheral wall and extend substantially perpendicular to said peripheral wall and from opposite ends thereof, said first and second sheets being respectively bonded to said first and second portions; said peripheral wall having at least first and second pairs of surfaces, said first pair of surfaces being adhesively fastened to a complementary pair of surfaces on a first adjacent cell unit, said second pair of surfaces being adhesively fastened to a complementary pair of surfaces on a second adjacent cell unit, the two surfaces in each of the said pairs of surfaces lying substantially parallel to each other but facing in opposite directions, the planes of all the said surfaces intersecting said first
  • one of the said pairs of surfaces is constituted by the opposite sides of a rib member and the complementary pair of surfaces on the adjacent cell unit is constituted by the two sides of a groove.
  • peripheral wall is polygonal with substantially straight sides and the first and second pairs of surfaces are each positioned intermediate the lengths of the sides and are perpendicular thereto.
  • each cell unit is constituted by a lid member which is applied to close one end of the space within the cell unit.
  • each cell unit includes an outer and an inner component, each component comprising a peripheral wall and an end wall, the peripheral wall of the inner component lying within the peripheral wall of the outer component and being secured to it, the inner component being in an inverted attitude relatively to the outer component, so that the end walls constitute the first and second sheet engaging portions, respectively.
  • each cell unit has a flange at one end constituting the first sheet engaging portion, and a closed end at its other end constituting the second sheet engaging portion
  • each of the four faces of the peripheral wall has two ribs, each of which ribs presents one of said adhesively fastened surfaces, and each of the said four faces presents two further pairs of closely spaced ribs, the mutually facing surfaces of each pair also constituting two of the said adhesively fastened surfaces.
  • each said cell unit is tilted with respect to at least some adjacent cell unit and said sheets are curved.

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Architecture (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Civil Engineering (AREA)
  • Structural Engineering (AREA)
  • Laminated Bodies (AREA)
  • Artificial Filaments (AREA)
US378168A 1963-06-28 1964-06-26 Lightweight structure having a honeycomb interior Expired - Lifetime US3391511A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB25838/63A GB1070927A (en) 1963-06-28 1963-06-28 Improvements in laminated cellular structures

Publications (1)

Publication Number Publication Date
US3391511A true US3391511A (en) 1968-07-09

Family

ID=10234175

Family Applications (1)

Application Number Title Priority Date Filing Date
US378168A Expired - Lifetime US3391511A (en) 1963-06-28 1964-06-26 Lightweight structure having a honeycomb interior

Country Status (7)

Country Link
US (1) US3391511A (nl)
CH (1) CH432784A (nl)
DE (1) DE1484135B1 (nl)
GB (1) GB1070927A (nl)
NL (1) NL140593B (nl)
NO (1) NO124324B (nl)
SE (1) SE340057B (nl)

Cited By (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3663346A (en) * 1970-07-22 1972-05-16 Nasa Honeycomb core structures of minimal surface tubule sections
US3849237A (en) * 1971-04-08 1974-11-19 L Zetlin Structural member of sheet material
US3906571A (en) * 1971-04-08 1975-09-23 Lev Zetlin Structural member of sheet material
US3914486A (en) * 1973-03-27 1975-10-21 Skapti Josef Borgford Shear form structures
US4001474A (en) * 1974-08-26 1977-01-04 Wilkins & Associates, Inc. Honeycomb panel cellular structure having triangular cells
US4399641A (en) * 1979-09-01 1983-08-23 Firma Gerhardi & Cie Synthetic resin glass insulating pane
US4400927A (en) * 1980-07-14 1983-08-30 Iowa State Research Foundation, Inc. Method of forming a skeletal dome structure in situ
US4524556A (en) * 1980-01-31 1985-06-25 Messerschmitt-Boelkow-Blohm Gesellschaft Mit Beschrankter Haftung Surface type structural component, especially for aircraft
EP0223053A2 (de) * 1985-11-14 1987-05-27 Messerschmitt-Bölkow-Blohm Gesellschaft mit beschränkter Haftung Sandwichbauteil
WO1988006970A1 (en) * 1987-03-16 1988-09-22 Hexcel Corporation Formable honeycomb panel
US5052188A (en) * 1990-10-24 1991-10-01 Gas Research Institute Desiccant materials for use in gas fired cooling and dehumidification equipment
FR2668526A1 (fr) * 1990-10-31 1992-04-30 Harnois Georges Bassin formant piscine dispose a l'interieur d'un local d'habitation.
US5354394A (en) * 1992-11-10 1994-10-11 Seeton Technologies Apparatus and method for forming honeycomb core
US5817269A (en) * 1996-10-25 1998-10-06 The Boeing Company Composite fabrication method and tooling to improve part consolidation
US6217000B1 (en) 1996-10-25 2001-04-17 The Boeing Company Composite fabrication method and tooling to improve part consolidation
GR1005771B (el) * 2007-01-23 2008-01-16 Παυλος Νικολαου Μιχελης Πολυστρωτη, κυψελωτη πλακα απο συνθετο υλικο με συνεχη τρισδιαστατη ενισχυση
CN103661918A (zh) * 2012-08-28 2014-03-26 波音公司 粘接的复合材料飞机机翼
EP2743065A1 (en) * 2012-12-14 2014-06-18 AIRBUS HELICOPTERS DEUTSCHLAND GmbH Grid type fibre composite structure and method of manufacturing such grid type structure
CN108000894A (zh) * 2017-11-08 2018-05-08 江西洪都航空工业集团有限责任公司 一种整体成型复合材料正交筋连续承力结构

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2577120A (en) * 1946-04-06 1951-12-04 Western Electric Co Honeycomb structure
FR998428A (fr) * 1945-09-27 1952-01-18 Perfectionnements apportés aux articles ou objets en caoutchouc aéré ou autres matières élastiques analogues
US2668327A (en) * 1950-04-21 1954-02-09 California Reinforced Plastics Method of making a curved honeycomb product
US2959257A (en) * 1957-03-18 1960-11-08 James R Campbell Honeycomb core and panel utilizing same
US3103460A (en) * 1963-09-10 Picket
US3193434A (en) * 1961-07-12 1965-07-06 Alexander C H Weiss Decorative architectural panels and method of producing same

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE802186C (de) * 1948-10-02 1951-02-05 Albert Fezer Aus einem Rahmen, einer oberen und einer unteren Deckplatte bestehendes ebenes Gebilde, insbesondere fuer Tueren o. dgl.
DE880931C (de) * 1947-02-13 1953-06-25 Folke Roland Werner Werneskog Bauelement, insbesondere Bauplatte, und Verfahren zu ihrer Herstellung
DE1132886B (de) * 1958-03-12 1962-07-12 Contraves Ag Verfahren zum Herstellen von Zellstrukturbaukoerpern

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3103460A (en) * 1963-09-10 Picket
FR998428A (fr) * 1945-09-27 1952-01-18 Perfectionnements apportés aux articles ou objets en caoutchouc aéré ou autres matières élastiques analogues
US2577120A (en) * 1946-04-06 1951-12-04 Western Electric Co Honeycomb structure
US2668327A (en) * 1950-04-21 1954-02-09 California Reinforced Plastics Method of making a curved honeycomb product
US2959257A (en) * 1957-03-18 1960-11-08 James R Campbell Honeycomb core and panel utilizing same
US3193434A (en) * 1961-07-12 1965-07-06 Alexander C H Weiss Decorative architectural panels and method of producing same

Cited By (25)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3663346A (en) * 1970-07-22 1972-05-16 Nasa Honeycomb core structures of minimal surface tubule sections
US3849237A (en) * 1971-04-08 1974-11-19 L Zetlin Structural member of sheet material
US3906571A (en) * 1971-04-08 1975-09-23 Lev Zetlin Structural member of sheet material
US3914486A (en) * 1973-03-27 1975-10-21 Skapti Josef Borgford Shear form structures
US4001474A (en) * 1974-08-26 1977-01-04 Wilkins & Associates, Inc. Honeycomb panel cellular structure having triangular cells
US4399641A (en) * 1979-09-01 1983-08-23 Firma Gerhardi & Cie Synthetic resin glass insulating pane
US4524556A (en) * 1980-01-31 1985-06-25 Messerschmitt-Boelkow-Blohm Gesellschaft Mit Beschrankter Haftung Surface type structural component, especially for aircraft
US4400927A (en) * 1980-07-14 1983-08-30 Iowa State Research Foundation, Inc. Method of forming a skeletal dome structure in situ
EP0223053A2 (de) * 1985-11-14 1987-05-27 Messerschmitt-Bölkow-Blohm Gesellschaft mit beschränkter Haftung Sandwichbauteil
EP0223053A3 (en) * 1985-11-14 1987-12-16 Messerschmitt-Bolkow-Blohm Gesellschaft Mit Beschrankter Haftung Sandwich building element
WO1988006970A1 (en) * 1987-03-16 1988-09-22 Hexcel Corporation Formable honeycomb panel
US4859517A (en) * 1987-03-16 1989-08-22 Hexcel Corporation Formable honeycomb panel
US5052188A (en) * 1990-10-24 1991-10-01 Gas Research Institute Desiccant materials for use in gas fired cooling and dehumidification equipment
FR2668526A1 (fr) * 1990-10-31 1992-04-30 Harnois Georges Bassin formant piscine dispose a l'interieur d'un local d'habitation.
US5354394A (en) * 1992-11-10 1994-10-11 Seeton Technologies Apparatus and method for forming honeycomb core
US5817269A (en) * 1996-10-25 1998-10-06 The Boeing Company Composite fabrication method and tooling to improve part consolidation
US6217000B1 (en) 1996-10-25 2001-04-17 The Boeing Company Composite fabrication method and tooling to improve part consolidation
GR1005771B (el) * 2007-01-23 2008-01-16 Παυλος Νικολαου Μιχελης Πολυστρωτη, κυψελωτη πλακα απο συνθετο υλικο με συνεχη τρισδιαστατη ενισχυση
EP1950034A1 (en) * 2007-01-23 2008-07-30 Michelis Pavlos Multilayered honeycomb panel from compopsite material with continuous three-dimensinal reinforcement
CN103661918A (zh) * 2012-08-28 2014-03-26 波音公司 粘接的复合材料飞机机翼
EP2743065A1 (en) * 2012-12-14 2014-06-18 AIRBUS HELICOPTERS DEUTSCHLAND GmbH Grid type fibre composite structure and method of manufacturing such grid type structure
US20140170372A1 (en) * 2012-12-14 2014-06-19 Eurocopter Deutschland Gmbh Grid type fiber composite structure and method of manufacturing such grid type structure
RU2553303C1 (ru) * 2012-12-14 2015-06-10 Эйрбас Хеликоптерс Дойчланд Гмбх Решетчатая волокнистая композиционная конструкция и способ производства такой решетчатой конструкции
US9266303B2 (en) * 2012-12-14 2016-02-23 Airbus Helicopters Deutschland GmbH Grid type fiber composite structure and method of manufacturing such grid type structure
CN108000894A (zh) * 2017-11-08 2018-05-08 江西洪都航空工业集团有限责任公司 一种整体成型复合材料正交筋连续承力结构

Also Published As

Publication number Publication date
NL140593B (nl) 1973-12-17
DE1484135B1 (de) 1970-04-30
GB1070927A (en) 1967-06-07
NO124324B (nl) 1972-04-04
NL6407261A (nl) 1964-12-29
CH432784A (fr) 1967-03-31
SE340057B (nl) 1971-11-01

Similar Documents

Publication Publication Date Title
US3391511A (en) Lightweight structure having a honeycomb interior
US6155450A (en) Composite shell shaped as a body of revolution
US4223053A (en) Truss core panels
EP0030129B1 (en) Reinforcement board
US4084029A (en) Sine wave beam web and method of manufacture
US20040105960A1 (en) Structural sandwich members
US2644777A (en) Composite structural material
US4453357A (en) Wall structure, wall element for use in the wall structure and method for making the same
NO153786B (no) System for overfoering av informasjon.
US9266303B2 (en) Grid type fiber composite structure and method of manufacturing such grid type structure
JP2004506554A (ja) 正弦波形ウエブ付き複合材支持構造物とその製作法
US3461632A (en) Lightweight cellular structural material
US3640798A (en) Composite structural core assembly
EP1379379B1 (en) Improved structural sandwich members
RU2081267C1 (ru) Способ изготовления сотовых заполнителей
US7028441B2 (en) Structural member and a method of manufacturing said member
EP0690784B1 (en) Former for core sandwich in composite reinforced plastics
US2880473A (en) Fibrous glass laminations
WO2020039338A1 (en) Structural honeycomb
KR101319937B1 (ko) 마그네슘 샌드위치 구조체 및 그 제작방법
GB2193465A (en) Improvements relating to reinforced bodies
JPH106418A (ja) 繊維強化プラスチック製のハニカムコア
JPS6010840Y2 (ja) 複合材料製抗張構造体
JP2594016Y2 (ja) 異形ハニカムパネル
JP3019595U (ja) 断熱積層板