GB876220A - Structural honeycomb materials - Google Patents

Structural honeycomb materials

Info

Publication number
GB876220A
GB876220A GB2842156A GB2842156A GB876220A GB 876220 A GB876220 A GB 876220A GB 2842156 A GB2842156 A GB 2842156A GB 2842156 A GB2842156 A GB 2842156A GB 876220 A GB876220 A GB 876220A
Authority
GB
United Kingdom
Prior art keywords
adhesive
sheet material
stack
platen
machine direction
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
GB2842156A
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to GB2842156A priority Critical patent/GB876220A/en
Priority to ES0237569A priority patent/ES237569A1/en
Priority to US683810A priority patent/US3074839A/en
Priority to FR1182857D priority patent/FR1182857A/en
Priority to CH5062857A priority patent/CH364182A/en
Priority to DED26463A priority patent/DE1192508B/en
Publication of GB876220A publication Critical patent/GB876220A/en
Priority to BE616749A priority patent/BE616749A/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
    • E04C2/34—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

Landscapes

  • Engineering & Computer Science (AREA)
  • Architecture (AREA)
  • Civil Engineering (AREA)
  • Structural Engineering (AREA)
  • Laminated Bodies (AREA)

Abstract

876,220. Laminates; honeycomb paper. MAY, G., and GORELL, J. H. Sept. 12, 1957 [Sept. 17, 1956], No. 28421/56. Classes 96 and 140. [Also in Group XXII] A structural honeycomb material is produced by securing together layers of sheet material having a machine direction to form a stack by means of an adhesive distributed in parallel elongated securing zones which cross, and are spaced apart in, the machine direction of the sheet material and are so positioned that the securing zones at one face of a layer are staggered with reference to the securing zones at the other face thereof and forming the stack into a plurality of expandable packs of strips of the sheet material by cutting it in the machine direction. The machine direction is the direction in which the sheet material has passed in web form through machinery (e.g. a paper mill, loom or rolling mill) in the course of its manufacture. Sheet materials referred to are paper, glass cloth and metal foil; the adhesive may be a curable resin. The adhesive zones may extend fully or only part way across the strips. The adhesive may be applied to each layer immediately after it is added to the stack, and before adding the next layer, or it may be applied to the layers before they are brought together. The material may be produced by folding a continuous web upon itself, or by superposing sheets, each of which is folded at at least one end to provide a part of the next layer of the stack. These methods produce a honeycomb material having closed cells at the edges, and portions may therefore be fitted together side by side, as shown in Fig. 7, and facing skins adhesively secured to the slices to close the cells. As shown in Fig. 2, a stack of layers of sheet material 12 from a roll 13 is produced by folding upon a platen 14 slidably mounted on table 15. The table has an upstanding rib 16 which has a sliding fit in a complementary groove in the underside of the platen, to prevent the platen from turning. After each layer has been applied, lines 7 of adhesive are applied by e.g. a printing roller or a silk screen device. The platen is then moved along the table, the sheet material pulled down to cover the adhesive lines, and the next set of adhesive lines applied in staggered relation to the first. Specification 591,772 is referred to.
GB2842156A 1956-09-17 1956-09-17 Structural honeycomb materials Expired GB876220A (en)

Priority Applications (7)

Application Number Priority Date Filing Date Title
GB2842156A GB876220A (en) 1956-09-17 1956-09-17 Structural honeycomb materials
ES0237569A ES237569A1 (en) 1956-09-17 1957-09-12 Structural honeycomb materials
US683810A US3074839A (en) 1956-09-17 1957-09-13 Method of making honeycomb material
FR1182857D FR1182857A (en) 1956-09-17 1957-09-17 Honeycomb material and its manufacturing process
CH5062857A CH364182A (en) 1956-09-17 1957-09-17 Component, method for its production and use of the component
DED26463A DE1192508B (en) 1956-09-17 1957-09-17 Process for the production of flat material layer bars
BE616749A BE616749A (en) 1956-09-17 1962-04-20 Honeycomb material and its manufacturing process

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB2842156A GB876220A (en) 1956-09-17 1956-09-17 Structural honeycomb materials

Publications (1)

Publication Number Publication Date
GB876220A true GB876220A (en) 1961-08-30

Family

ID=10275358

Family Applications (1)

Application Number Title Priority Date Filing Date
GB2842156A Expired GB876220A (en) 1956-09-17 1956-09-17 Structural honeycomb materials

Country Status (2)

Country Link
ES (1) ES237569A1 (en)
GB (1) GB876220A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2001098075A1 (en) * 2000-06-16 2001-12-27 E.I. Du Pont De Nemours And Company Honeycomb structure

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2001098075A1 (en) * 2000-06-16 2001-12-27 E.I. Du Pont De Nemours And Company Honeycomb structure
US6592963B1 (en) 2000-06-16 2003-07-15 E. I. Du Pont De Nemours And Company Honeycomb structure

Also Published As

Publication number Publication date
ES237569A1 (en) 1958-02-01

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