US2428979A - Structural element made from paper and like sheets - Google Patents

Structural element made from paper and like sheets Download PDF

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Publication number
US2428979A
US2428979A US622454A US62245445A US2428979A US 2428979 A US2428979 A US 2428979A US 622454 A US622454 A US 622454A US 62245445 A US62245445 A US 62245445A US 2428979 A US2428979 A US 2428979A
Authority
US
United States
Prior art keywords
sheets
lines
adhesive
sheet
paper
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
US622454A
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English (en)
Inventor
May George
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.)
Dufay Chromex Ltd
Original Assignee
Dufay Chromex 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 Dufay Chromex Ltd filed Critical Dufay Chromex Ltd
Priority to FR930670D priority Critical patent/FR930670A/fr
Priority to US772746A priority patent/US2527752A/en
Application granted granted Critical
Publication of US2428979A publication Critical patent/US2428979A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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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
    • E04C2/365—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 by honeycomb structures
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B31—MAKING ARTICLES OF PAPER, CARDBOARD OR MATERIAL WORKED IN A MANNER ANALOGOUS TO PAPER; WORKING PAPER, CARDBOARD OR MATERIAL WORKED IN A MANNER ANALOGOUS TO PAPER
    • B31D—MAKING ARTICLES OF PAPER, CARDBOARD OR MATERIAL WORKED IN A MANNER ANALOGOUS TO PAPER, NOT PROVIDED FOR IN SUBCLASSES B31B OR B31C
    • B31D3/00—Making articles of cellular structure, e.g. insulating board
    • B31D3/02—Making articles of cellular structure, e.g. insulating board honeycombed structures, i.e. the cells having an essentially hexagonal section
    • 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
    • Y10T156/00—Adhesive bonding and miscellaneous chemical manufacture
    • Y10T156/10—Methods of surface bonding and/or assembly therefor
    • Y10T156/1002—Methods of surface bonding and/or assembly therefor with permanent bending or reshaping or surface deformation of self sustaining lamina
    • Y10T156/1003—Methods of surface bonding and/or assembly therefor with permanent bending or reshaping or surface deformation of self sustaining lamina by separating laminae between spaced secured areas [e.g., honeycomb expanding]
    • 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
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49616—Structural member making
    • Y10T29/4962—Grille making
    • 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

Definitions

  • This invention consists of improvements in structural elements made from paper and like sheets and includes a method of building up such elements and for producing double-skin structures with intermediate spacing.
  • the elements may be fiat or curved panels or may have double curvature or stream-line form, and may form doors, walls, partitions or parts or fittings for aircraft such as stream-line tanks or nacelles.
  • the present invention relates to the same general type of structural elements.
  • the objects of this invention are to provide economic methods of making efiective structural elements particularly those of stream-line form.
  • a method of making a'cellular filling for a double-skin structural element includes the steps of applying to a sheet of paper (or to a film of cellulose .ester or like plastic) lines (or rows of dots) of adhesive e. g.
  • the preferred method of ,applying the'lines of adhesive is that known as the silk screen process in which a flat screen of silk associated with a stencil is hinged along one edge so that the screen and stencil may be raised for theinsertion of-a.
  • the silk screen itself nay be painted or otherwisecoated with a resist such as a varnish which prevents glue from aassing through the screen and a series of parallel lines on the screen are left without resist to tllOW the glue to pass through.
  • the :uccessive sheets are not removed from the silk :creen apparatus but are left to accumulate in I. pile in the apparatus.
  • the silk screen device where paper sheets of a uniform size and shape are used, there may be two hinged screens and. stencils (for treating alternate sheets) so that the staggering of the adhesive lines in alternate sheets of a pile can be most economically effected.
  • An alternative economic method is to dispose the lines so that the outermost line at one side is closer to the edge than the outermost line at the other side (closer by one-quarter the distance separating adjacent lines) so that when through 180", the staggering of the adhesive lines will be automatically produced.
  • the lines of adhesive applied through the stencil may be in short sections and may be inclined to one another. I
  • the setting of the adhesive may be hastened by well-known means '(e. g. heat and/or pressure).
  • the cutting of the assembled pile of adheringsheetsinto narrow widths can be done before or after opening out the sheets to the honeycomb or lattice form but preferably before opening out.
  • the expansion may be assisted by the use of air 'currents..
  • the filling i. e. the expanded honeycomb or lattice
  • the filling may be strengthened by dipping in a solution or suspension of an artificial resin or a solution of a cellulose ester plastic or other suitable setting plastic in liquid form.
  • the lattice or honeycomb when opened out may be'metallised, i. e. may be coated by dip- .with cellulose acetate solution or a synthetic resin or plastomer.
  • An alternative method of applying the lines of adhesive to the sheets of paper or the like is by a printing machine such as a Wharfedale printing machine or a platen printing machine and in order that contiguous sheets may have the adhesive lines staggered, the sheet delivery of the printing machine or the sheet feed of the printing machine may be so arranged as to provide for this alternate staggering of the printed lines of adhesive on successive sheets.
  • the filling above described is secured on both sides by adhesive to boards such as plywood, fibre board or plastic wood sheets or to sheets of paper or the like which sheets lie in contact with the edges of the open honeycomb or lattice.
  • boards such as plywood, fibre board or plastic wood sheets or to sheets of paper or the like which sheets lie in contact with the edges of the open honeycomb or lattice.
  • the inner surface may first be built up on a mandrel or mould of appropriate shape say by sticking two layers or three layers of paper together over said mandrel.
  • the first sheet to be applied to the mandrel or mould is built up from laminations of paper or of thin fabric or of both.
  • the paper or fabric maybe of odd lengths and pieces or may be cut up into comparatively small squares and each piece is laid in position and secured by an adhesive.
  • a chemical setting adhesive can be employed, for example a mixture of a urea formaldehyde glue with a hardening agent or of casein and a paste made from starch.
  • the pieces will overlap and may be rubbed down.
  • the layer as a whole may on an average comprise two or three laminations.
  • the filling (in'pieces of suitable size) is applied and secured by adhesive to the inner skin thus formed, the walls of the filling being of course'at right-angles to the inner skin 4 I: and showing in transverse. chain lines the position of the guillotine cuts,
  • Figure 8 is a plan view of 2. opened out
  • Figure 9 is a plan view partly broken away.
  • Figure 101 s a side end view
  • I Figure 11 a bottom end view of a structural element in which the cellular filling is covered on each side with plywood.
  • the base l2 of the silk screen apparatus has a rectangular upstanding frame 13 about a quarcellular filling ter of an inch high with finger recesses H on the frame l3) and the first operation is to attach at each point. 'Then the outer skin is again built up over the filling in the same way as the inner skin was built up.
  • Figure Us a plan of the silk screen apparatus ready for squeegeeing the first lines of glue
  • Figure 2 is a similar plan with the lid open, and with one set of lines of glue applied to a bottom sheet of cardboard or paper board.
  • Figure 3 is a plan similar to Figure 2 showing
  • the base l2 at the back has upstanding pins l9 on which can slide vertically a, transom 20 to which is hinged the lid 2
  • This book or pile is cut in a guillotine along the chain lines 25 at right-angles to the lines of adhesive i8, and each slice can be opened out as indicated in Figure 8 to form a filling having a honeycomb or lattice structure as indicated at 25.
  • l0 and 11 plywood boards 21 are shown stuck to each side of the filling.
  • the peripheral spaces between the plywood sheet may be cleared away for a short depth and filled up with a setting filler such as plastic Wood.
  • This filler may be of thermoplastic material and may be applied manually by a little trowel or equivalent. In place of plywood, glass fibre cloth may be used. As explained above, the filler may be treated with a metallised varnish to render it proof against moisture or water vapour.
  • Iclaim 1. A method ofv making a cellular filling for a double-skin structural element which includes the steps of applying to a cellulosic sheet lines of adhesive, superimposing a number of such sheets into a stack with the adhesive lines alternately staggered, cutting the stack of sheetsai right-angles to said adhesive lines into slices oi the width desired for the thickness of said cellular filling and opening out the non-adhering walls to form a lattice.
  • a method of making a cellular filling for a double-skin structural element which includes the steps of stencilling on to a cellulosic sheei lines alternately staggered, cutting the stack of sheets at right-angles to said adhesive lines into slices of the width desired for the thickness of said cellular filling and opening out the nonadhering walls to form a lattice.
  • a method of making a cellular filling for a double-skin structural element which includes the steps of applying to a sheet of paper by the silk screen process a number or parallel lines of adhesive, then applying to a second sheet of paper parallel lines of adhesive uniformly staggered in relation to the lines of the first sheet, treating a third sheet in the same way as the first sheet, superimposing a large number of such sheets into a stack with the adhesive lines alternatelystaggered so that the contiguous sheets cohere along the adhesive lines, cutting the stack of sheets at right-angles to said adhesive lines into slices of the width desired for the thickness of said cellular filling and opening out the non-adhering walls to form a lattice.
  • a method of making a double-skin structural element which includes the steps of applying to a cellulosic sheet parallel lines, of adhesive, superimposing a number of such sheets into a stack with the adhesive lines alternately staggered, cutting the stack. of sheets at right-angles to said adhesive lines into slices of the width desired for the thickness of said cellular filling, opening out thenon-adhering walls to form a lattice and securing on each side of saidlattice a covering plate.
  • a method of making a double-skin structural element which includes the steps of applying to a cellulosic sheet parallel lines of adhesive,
  • a method of making a double-skin structural element which includes the steps of applying to a cellulosic sheet parallel lines of adhesive, superimposing a number of such sheets into a stack with the adhesive lines alternately staggered, cutting the stack of sheets-at right-angles to said adhesive lines into slices of the width desired for the thickness of said cellular filling,

Landscapes

  • Engineering & Computer Science (AREA)
  • Architecture (AREA)
  • Civil Engineering (AREA)
  • Structural Engineering (AREA)
  • Laminated Bodies (AREA)
US622454A 1944-05-25 1945-10-15 Structural element made from paper and like sheets Expired - Lifetime US2428979A (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
FR930670D FR930670A (fr) 1944-05-25 1946-07-16 Garnissage cellulaire en papier ou feuilles analogues
US772746A US2527752A (en) 1944-05-25 1947-09-08 Apparatus for building up structural elements from paper sheets

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB2428979X 1944-05-25

Publications (1)

Publication Number Publication Date
US2428979A true US2428979A (en) 1947-10-14

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BE (1) BE466619A (en))
GB (1) GB591772A (en))

Cited By (42)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2514801A (en) * 1948-09-13 1950-07-11 Gerald G Sapp Paper crimper and stacker
US2518164A (en) * 1946-07-02 1950-08-08 Leonard S Meyer Apparatus for producing composite sheet material
US2527752A (en) * 1944-05-25 1950-10-31 Dufay Chromex Ltd Apparatus for building up structural elements from paper sheets
US2553054A (en) * 1948-01-02 1951-05-15 Lincoln Machine and method for producing a continuous honeycomb structure
US2556011A (en) * 1947-05-05 1951-06-05 Chrysler Corp Method of making a cellular structural panel and product
US2556470A (en) * 1947-11-22 1951-06-12 Douglas Aircraft Co Inc Heat insulating structural panel
US2581421A (en) * 1948-04-27 1952-01-08 Douglas Aircraft Co Inc Method and apparatus for making structural elements
US2608500A (en) * 1947-12-06 1952-08-26 Douglas Aircraft Co Inc Structural element
US2608502A (en) * 1947-02-15 1952-08-26 Glenn L Martin Co Honeycomb structure and method of making same
US2609068A (en) * 1949-03-11 1952-09-02 Glenn L Martin Co Metal foil honeycomb core
US2622999A (en) * 1947-08-02 1952-12-23 Roddis Plywood Corp Method for making honeycomb core doors
US2636540A (en) * 1949-08-06 1953-04-28 John D Lincoln Honeycomb core fabricating machine
US2648371A (en) * 1948-03-27 1953-08-11 Goodwin Method and machine for producing a continuous honeycomb structure
US2649131A (en) * 1948-03-27 1953-08-18 John D Lincoln Machine and method for producing continuous honeycomb structures
US2670314A (en) * 1948-03-18 1954-02-23 Douglas Aircraft Co Inc Method for making honeycomb cores for sandwich type structures
US2700634A (en) * 1949-09-09 1955-01-25 Northrop Aircraft Inc Method of laminating a cellular core sandwich
US2720948A (en) * 1950-03-04 1955-10-18 Glenn L Martin Co Honeycomb panel constructed for bolting or riveting to framework or another panel
US2731379A (en) * 1953-04-21 1956-01-17 Union Bag & Paper Corp Method of making honeycomb material
US2734842A (en) * 1949-02-23 1956-02-14 Process of manufacturing spaced plate arc extinguishers
US2784134A (en) * 1952-10-30 1957-03-05 Ionia Mfg Company Method of manufacturing composite panels
US2793718A (en) * 1950-01-25 1957-05-28 Glenn L Martin Co Honeycomb panel and method of making same
US2848132A (en) * 1950-01-26 1958-08-19 Davous Leon Packing means
US2885772A (en) * 1954-09-14 1959-05-12 Northrop Aircraft Inc Pre-contouring honeycomb cores before expansion of the honeycomb
US2910396A (en) * 1952-11-12 1959-10-27 Bettinger Corp Structural reticulated webs or honeycombs and curtain wall panels made from same
US2936021A (en) * 1956-05-29 1960-05-10 Hexcel Products Inc Honeycomb expanding means and method
US2983640A (en) * 1957-06-24 1961-05-09 Hexcel Products Inc Method of making honeycomb
US3006798A (en) * 1959-03-23 1961-10-31 Hexcel Products Inc Method of making honeycomb
US3016315A (en) * 1958-10-08 1962-01-09 Carl D Hall Jr Honeycomb structure and method
US3032458A (en) * 1956-03-08 1962-05-01 Dufaylite Dev Ltd Cellular structures made from sheet materials
US3074839A (en) * 1956-09-17 1963-01-22 Messrs Dufaylite Developments Method of making honeycomb material
US3106503A (en) * 1955-03-31 1963-10-08 Boardman M Randall Method of making honeycomb structural panels
DE1192508B (de) * 1956-09-17 1965-05-06 Dufaylite Dev Ltd Verfahren zur Herstellung von Flachmateriallagenriegeln
US3201138A (en) * 1962-09-10 1965-08-17 Jr Culver S Brown Laminated ski with a honeycomb core
US3257253A (en) * 1962-03-22 1966-06-21 Weyerhaeuser Co Laminated cellular panel
US3276784A (en) * 1965-05-12 1966-10-04 Jr Henry M Anderson Laminated ski having a foam filled honeycomb core
US3428515A (en) * 1960-05-27 1969-02-18 Lorentzen Hans L Structural board having open cells extending at an angle to the surfaces of the board
US3513529A (en) * 1966-06-28 1970-05-26 Aaron L Hitchens Method of producing cellular structures
USB481737I5 (en)) * 1974-06-21 1976-01-13
US4957577A (en) * 1988-04-04 1990-09-18 Plascore, Inc. Method for making welded honeycomb core
US4981744A (en) * 1990-04-24 1991-01-01 Swank Michael W Non-planar expandable honeycomb structure
WO2004014643A1 (en) * 2002-08-08 2004-02-19 Alethea Rosalind Melanie Hall Method of manufacturing a framework having a honeycomb structure
US20100307677A1 (en) * 2007-12-21 2010-12-09 Carsten Buhlmann Method for producing a decorative laminate

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
BE792836A (fr) * 1971-12-17 1973-06-15 Ciba Geigy Uk Ltd Perfectionnements apportes a la fabrication de produits alveolaires
GB1596848A (en) * 1977-12-08 1981-09-03 Dufaylite Dev Ltd Structural cellular materials
GB2173447A (en) * 1985-03-28 1986-10-15 Dufaylite Dev Ltd Panel material
DE19540261C2 (de) * 1995-10-28 1998-07-02 Steinhoff Laminat Gmbh Verfahren zur Herstellung von Formteilen

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1552478A (en) * 1924-08-23 1925-09-08 Arthur B Fosseen Tile-making machinery
US2385352A (en) * 1942-06-12 1945-09-25 Mengel Company Method of making hollow panels

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1552478A (en) * 1924-08-23 1925-09-08 Arthur B Fosseen Tile-making machinery
US2385352A (en) * 1942-06-12 1945-09-25 Mengel Company Method of making hollow panels

Cited By (45)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2527752A (en) * 1944-05-25 1950-10-31 Dufay Chromex Ltd Apparatus for building up structural elements from paper sheets
US2518164A (en) * 1946-07-02 1950-08-08 Leonard S Meyer Apparatus for producing composite sheet material
US2608502A (en) * 1947-02-15 1952-08-26 Glenn L Martin Co Honeycomb structure and method of making same
US2556011A (en) * 1947-05-05 1951-06-05 Chrysler Corp Method of making a cellular structural panel and product
US2622999A (en) * 1947-08-02 1952-12-23 Roddis Plywood Corp Method for making honeycomb core doors
US2556470A (en) * 1947-11-22 1951-06-12 Douglas Aircraft Co Inc Heat insulating structural panel
US2608500A (en) * 1947-12-06 1952-08-26 Douglas Aircraft Co Inc Structural element
US2553054A (en) * 1948-01-02 1951-05-15 Lincoln Machine and method for producing a continuous honeycomb structure
US2670314A (en) * 1948-03-18 1954-02-23 Douglas Aircraft Co Inc Method for making honeycomb cores for sandwich type structures
US2649131A (en) * 1948-03-27 1953-08-18 John D Lincoln Machine and method for producing continuous honeycomb structures
US2648371A (en) * 1948-03-27 1953-08-11 Goodwin Method and machine for producing a continuous honeycomb structure
US2581421A (en) * 1948-04-27 1952-01-08 Douglas Aircraft Co Inc Method and apparatus for making structural elements
US2514801A (en) * 1948-09-13 1950-07-11 Gerald G Sapp Paper crimper and stacker
US2734842A (en) * 1949-02-23 1956-02-14 Process of manufacturing spaced plate arc extinguishers
US2609068A (en) * 1949-03-11 1952-09-02 Glenn L Martin Co Metal foil honeycomb core
US2636540A (en) * 1949-08-06 1953-04-28 John D Lincoln Honeycomb core fabricating machine
US2700634A (en) * 1949-09-09 1955-01-25 Northrop Aircraft Inc Method of laminating a cellular core sandwich
US2793718A (en) * 1950-01-25 1957-05-28 Glenn L Martin Co Honeycomb panel and method of making same
US2848132A (en) * 1950-01-26 1958-08-19 Davous Leon Packing means
US2720948A (en) * 1950-03-04 1955-10-18 Glenn L Martin Co Honeycomb panel constructed for bolting or riveting to framework or another panel
US2784134A (en) * 1952-10-30 1957-03-05 Ionia Mfg Company Method of manufacturing composite panels
US2910396A (en) * 1952-11-12 1959-10-27 Bettinger Corp Structural reticulated webs or honeycombs and curtain wall panels made from same
US2731379A (en) * 1953-04-21 1956-01-17 Union Bag & Paper Corp Method of making honeycomb material
US2885772A (en) * 1954-09-14 1959-05-12 Northrop Aircraft Inc Pre-contouring honeycomb cores before expansion of the honeycomb
US3106503A (en) * 1955-03-31 1963-10-08 Boardman M Randall Method of making honeycomb structural panels
US3032458A (en) * 1956-03-08 1962-05-01 Dufaylite Dev Ltd Cellular structures made from sheet materials
US2936021A (en) * 1956-05-29 1960-05-10 Hexcel Products Inc Honeycomb expanding means and method
US3074839A (en) * 1956-09-17 1963-01-22 Messrs Dufaylite Developments Method of making honeycomb material
DE1192508B (de) * 1956-09-17 1965-05-06 Dufaylite Dev Ltd Verfahren zur Herstellung von Flachmateriallagenriegeln
US2983640A (en) * 1957-06-24 1961-05-09 Hexcel Products Inc Method of making honeycomb
US3016315A (en) * 1958-10-08 1962-01-09 Carl D Hall Jr Honeycomb structure and method
US3006798A (en) * 1959-03-23 1961-10-31 Hexcel Products Inc Method of making honeycomb
US3428515A (en) * 1960-05-27 1969-02-18 Lorentzen Hans L Structural board having open cells extending at an angle to the surfaces of the board
US3257253A (en) * 1962-03-22 1966-06-21 Weyerhaeuser Co Laminated cellular panel
US3201138A (en) * 1962-09-10 1965-08-17 Jr Culver S Brown Laminated ski with a honeycomb core
US3276784A (en) * 1965-05-12 1966-10-04 Jr Henry M Anderson Laminated ski having a foam filled honeycomb core
US3513529A (en) * 1966-06-28 1970-05-26 Aaron L Hitchens Method of producing cellular structures
USB481737I5 (en)) * 1974-06-21 1976-01-13
US3982057A (en) * 1974-06-21 1976-09-21 The United States Of America As Represented By The Secretary Of The Army Paper honeycomb cushioning pad
US4957577A (en) * 1988-04-04 1990-09-18 Plascore, Inc. Method for making welded honeycomb core
US4981744A (en) * 1990-04-24 1991-01-01 Swank Michael W Non-planar expandable honeycomb structure
WO2004014643A1 (en) * 2002-08-08 2004-02-19 Alethea Rosalind Melanie Hall Method of manufacturing a framework having a honeycomb structure
US20050269019A1 (en) * 2002-08-08 2005-12-08 Hall Alethea R M Method of manufacturing a framework having a honeycomb structure
US20100307677A1 (en) * 2007-12-21 2010-12-09 Carsten Buhlmann Method for producing a decorative laminate
US9174423B2 (en) * 2007-12-21 2015-11-03 Surface Technologies Gmbh & Co. Kg Method for producing a decorative laminate

Also Published As

Publication number Publication date
GB591772A (en) 1947-08-28
BE466619A (en))

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