WO2005028138A1 - A method of producing honeycomb structure - Google Patents

A method of producing honeycomb structure Download PDF

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Publication number
WO2005028138A1
WO2005028138A1 PCT/KR2004/002325 KR2004002325W WO2005028138A1 WO 2005028138 A1 WO2005028138 A1 WO 2005028138A1 KR 2004002325 W KR2004002325 W KR 2004002325W WO 2005028138 A1 WO2005028138 A1 WO 2005028138A1
Authority
WO
WIPO (PCT)
Prior art keywords
honeycomb structure
hexagonal
pegs
press
metal plates
Prior art date
Application number
PCT/KR2004/002325
Other languages
French (fr)
Inventor
Kiho Park
Original Assignee
Yang, Hoejung
Lee, Bongwoo
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 Yang, Hoejung, Lee, Bongwoo filed Critical Yang, Hoejung
Priority to AU2004274348A priority Critical patent/AU2004274348B2/en
Priority to JP2006527907A priority patent/JP2007506557A/en
Priority to US10/573,532 priority patent/US7721404B2/en
Priority to BRPI0414747-2A priority patent/BRPI0414747A/en
Priority to CA002538762A priority patent/CA2538762A1/en
Priority to EP04774584A priority patent/EP1667802A4/en
Publication of WO2005028138A1 publication Critical patent/WO2005028138A1/en

Links

Classifications

    • 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
    • B32B3/00—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form
    • B32B3/10—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by a discontinuous layer, i.e. formed of separate pieces of material
    • B32B3/12—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by a discontinuous layer, i.e. formed of separate pieces of material characterised by a layer of regularly- arranged cells, e.g. a honeycomb structure
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21D—WORKING OR PROCESSING OF SHEET METAL OR METAL TUBES, RODS OR PROFILES WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21D47/00—Making rigid structural elements or units, e.g. honeycomb structures
    • 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
    • B32B15/00—Layered products comprising a layer of metal
    • B32B15/04—Layered products comprising a layer of metal comprising metal as the main or only constituent of a layer, which is next to another layer of the same or of a different material
    • 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
    • B32B3/00—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form
    • B32B3/26—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by a particular shape of the outline of the cross-section of a continuous layer; characterised by a layer with cavities or internal voids ; characterised by an apertured layer
    • B32B3/30—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by a particular shape of the outline of the cross-section of a continuous layer; characterised by a layer with cavities or internal voids ; characterised by an apertured layer characterised by a layer formed with recesses or projections, e.g. hollows, grooves, protuberances, ribs
    • 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
    • B32B7/00—Layered products characterised by the relation between layers; Layered products characterised by the relative orientation of features between layers, or by the relative values of a measurable parameter between layers, i.e. products comprising layers having different physical, chemical or physicochemical properties; Layered products characterised by the interconnection of layers
    • B32B7/04—Interconnection of layers
    • B32B7/12—Interconnection of layers using interposed adhesives or interposed materials with bonding properties
    • 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
    • E04C2/326—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 with corrugations, incisions or reliefs in more than one direction of the element
    • 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
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2305/00—Condition, form or state of the layers or laminate
    • B32B2305/02—Cellular or porous
    • B32B2305/024—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
    • B32B2311/00—Metals, their alloys or their compounds
    • 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
    • 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
    • Y10T29/49826—Assembling or joining
    • Y10T29/49885—Assembling or joining with coating before or during assembling
    • 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
    • Y10T29/49826—Assembling or joining
    • Y10T29/49893—Peripheral joining of opposed mirror image parts to form a hollow body

Definitions

  • the present invention relates to a honeycomb structure that is formed using a press with a die to make two metal plates(2, 6) which have hexagonal pegs positioned at a certain distance from each other, and these plates are joined together into a complete honeycomb structure.
  • FIG 1 is the position of hexagonal cells on the metal plate A;
  • FIG 2 is the position of hexagonal cells on the metal plate B;
  • FIG 3 shows position of hexagonal cells on both metal plate A and B when one plate is overlapping the other;
  • FIG 4 is the metal plate A with hexagonal pegs formed by a press
  • FIG 5 is the metal plate B with hexagonal pegs formed by a press
  • FIG 6 is the honeycomb structured block in which metal formed plates are joined together.
  • FIG 7 is showing a method of extending the total size of the core block by joining the honeycomb blocks in a zigzag manner.
  • FIG 8 is showing a method of making honeycomb sandwich panel attaching non- woven fabric and face sheets on a core. ⁇ Description of the numbers on drawing> 2.
  • the present invention is using a press to form a honeycomb structure out of many different types of metal plate.
  • a press it seems it is very difficult or impossible to form a honeycomb structure with a single process using a press, because the hexagonal cells within the structure are placed right next to each other sharing the very thin cell-walls among them.
  • a die is needed to be built for the making of hexagonal cells of the honeycomb structure.
  • Honeycomb structure consists of many hexagonal cells lined up continuously but because the cell walls are so thin, it is nearly impossible to form the structure with a press and a single die in one step.
  • a die is designed and the hexagonal cells on the die are placed at a certain distance from each other, as shown in FIG 1 and FIG 2, so that when the cell positions from those two FIGs are overlapping, the result is a perfect honeycomb shape as shown in FIG 3.
  • This die and a press are used to change the shape of two thin metal plates(2, 6), shown in FIG 1 and FIG 2, into two formed metal plates which have hexagonal pegs(14) protruding out as shown in FIG 4 and FIG 5. And then, in order to make a shape of honeycomb structure, these two formed metal plates are joined together into a block, like in FIG 6, by facing the protruding sides to each other and inserting one plate's pegs (14) into the spaces among the other plate's pegs (14). In order to have physical properties of honeycomb structure from the block described above, the hexagonal pegs (14) have to be bonded to each other strongly.
  • FIG 7 shows the method of extending the size of the block by joining the honeycomb blocks (20, 22) in a zigzag manner
  • FIG 8 shows the making of a honeycomb sandwich panel. Face sheets (26) and adhesive are added to the top and bottom of the block. The face sheets can be made out of many different materials. Non-woven fabric (24) can be used with the adhesive to create a better bond between the sheets (26) and the block.
  • a press and a die are used to make the process of producing honeycomb structure simpler.
  • honeycomb structure can be formed using many different types of metal that have high tensile, compression, and bending strength.

Landscapes

  • Engineering & Computer Science (AREA)
  • Architecture (AREA)
  • Civil Engineering (AREA)
  • Structural Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Laminated Bodies (AREA)
  • Panels For Use In Building Construction (AREA)
  • Press-Shaping Or Shaping Using Conveyers (AREA)

Abstract

A method of producing honeycomb structure using a press and a die to form two metal plates that have hexagonal pegs protruding out on one side and applying welding material or some adhesive onto the hexagonal pegs and then joining the two formed metal plates by facing the protruding sides to each other. The process can produce a high-quality honeycomb structure rapidly at a low cost with many different types of metal.

Description

Description
A METHOD OF PRODUCING HONEYCOMB STRUCTURE
Technical Field The present invention relates to a honeycomb structure that is formed using a press with a die to make two metal plates(2, 6) which have hexagonal pegs positioned at a certain distance from each other, and these plates are joined together into a complete honeycomb structure.
Description of Drawings FIG 1 is the position of hexagonal cells on the metal plate A; FIG 2 is the position of hexagonal cells on the metal plate B; FIG 3 shows position of hexagonal cells on both metal plate A and B when one plate is overlapping the other; FIG 4 is the metal plate A with hexagonal pegs formed by a press FIG 5 is the metal plate B with hexagonal pegs formed by a press FIG 6 is the honeycomb structured block in which metal formed plates are joined together. FIG 7 is showing a method of extending the total size of the core block by joining the honeycomb blocks in a zigzag manner. FIG 8 is showing a method of making honeycomb sandwich panel attaching non- woven fabric and face sheets on a core. <Description of the numbers on drawing> 2. Metal plate A 4. Position of the hexagonal cells on metal plate A 6. Metal plate B 8. Position of the hexagonal cells on metal plate B 10 Metal plate A + B 12 Position of the hexagonal cells that are made automatically 14 Hexagonal peg 16 Hexagonal cell 18 Hexagonal cells that are made automatically 20 Honeycomb block A 22 Honeycomb block B 24 Non-woven fabric 26 Face sheet
Technical Problems Unlike the existing methods, the present invention is using a press to form a honeycomb structure out of many different types of metal plate. However, it seems it is very difficult or impossible to form a honeycomb structure with a single process using a press, because the hexagonal cells within the structure are placed right next to each other sharing the very thin cell-walls among them.
Technical Solutions In the present invention, a die is needed to be built for the making of hexagonal cells of the honeycomb structure. Honeycomb structure consists of many hexagonal cells lined up continuously but because the cell walls are so thin, it is nearly impossible to form the structure with a press and a single die in one step. In the present' invention, however, a die is designed and the hexagonal cells on the die are placed at a certain distance from each other, as shown in FIG 1 and FIG 2, so that when the cell positions from those two FIGs are overlapping, the result is a perfect honeycomb shape as shown in FIG 3. This die and a press are used to change the shape of two thin metal plates(2, 6), shown in FIG 1 and FIG 2, into two formed metal plates which have hexagonal pegs(14) protruding out as shown in FIG 4 and FIG 5. And then, in order to make a shape of honeycomb structure, these two formed metal plates are joined together into a block, like in FIG 6, by facing the protruding sides to each other and inserting one plate's pegs (14) into the spaces among the other plate's pegs (14). In order to have physical properties of honeycomb structure from the block described above, the hexagonal pegs (14) have to be bonded to each other strongly. So, before joining the two formed metal plates together from the previous process, some adhesives or welding materials are inserted or applied on the outer surface of the pegs (14). FIG 7 shows the method of extending the size of the block by joining the honeycomb blocks (20, 22) in a zigzag manner FIG 8 shows the making of a honeycomb sandwich panel. Face sheets (26) and adhesive are added to the top and bottom of the block. The face sheets can be made out of many different materials. Non-woven fabric (24) can be used with the adhesive to create a better bond between the sheets (26) and the block. Advantageous Effects In the present invention, a press and a die are used to make the process of producing honeycomb structure simpler. Also, honeycomb structure can be formed using many different types of metal that have high tensile, compression, and bending strength.

Claims

Claims 1. A method of producing honeycomb structure using a press and a die to form two metal plates that have hexagonal pegs protruding out on one side and applying welding material or some adhesive onto the hexagonal pegs and then joining the two formed metal plates by facing the protruding sides to each other.
2. The method of claim 1, wherein the pegs have different polygonal shapes such as triangular, square, and octagonal or even circular.
PCT/KR2004/002325 2003-09-24 2004-09-14 A method of producing honeycomb structure WO2005028138A1 (en)

Priority Applications (6)

Application Number Priority Date Filing Date Title
AU2004274348A AU2004274348B2 (en) 2003-09-24 2004-09-14 A method of producing honeycomb structure
JP2006527907A JP2007506557A (en) 2003-09-24 2004-09-14 Manufacturing method of honeycomb structure
US10/573,532 US7721404B2 (en) 2003-09-24 2004-09-14 Method of producing honeycomb structure
BRPI0414747-2A BRPI0414747A (en) 2003-09-24 2004-09-14 a method for producing a honeycomb structure
CA002538762A CA2538762A1 (en) 2003-09-24 2004-09-14 A method of producing honeycomb structure
EP04774584A EP1667802A4 (en) 2003-09-24 2004-09-14 A method of producing honeycomb structure

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
KR20-2003-0030237 2003-09-24
KR20-2003-0030237U KR200350066Y1 (en) 2003-09-24 2003-09-24 A method of producing honeycomb structure

Publications (1)

Publication Number Publication Date
WO2005028138A1 true WO2005028138A1 (en) 2005-03-31

Family

ID=36168997

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/KR2004/002325 WO2005028138A1 (en) 2003-09-24 2004-09-14 A method of producing honeycomb structure

Country Status (10)

Country Link
US (1) US7721404B2 (en)
EP (1) EP1667802A4 (en)
JP (1) JP2007506557A (en)
KR (1) KR200350066Y1 (en)
CN (1) CN1905963A (en)
AU (1) AU2004274348B2 (en)
BR (1) BRPI0414747A (en)
CA (1) CA2538762A1 (en)
RU (1) RU2342211C2 (en)
WO (1) WO2005028138A1 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9579866B2 (en) 2009-09-15 2017-02-28 Rep Ip Ag Honeycomb structure element

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR100628654B1 (en) 2004-12-13 2006-09-26 박기호 A method of producing honeycomb structural material with hexagonal cups having a fringe
JP2013052581A (en) * 2011-09-03 2013-03-21 Awa Paper Mfg Co Ltd Honeycomb structure
WO2017107922A1 (en) * 2015-12-21 2017-06-29 张跃 Cellular column, cellular beam, cellular floor slab and cellular board building
KR102184163B1 (en) * 2016-10-31 2020-11-30 위에 장 Metal plate clamping a kind of hollow tube
CN110977341B (en) * 2019-11-28 2022-04-12 中国航发沈阳黎明航空发动机有限责任公司 Process method for improving machining quality of honeycomb annular part

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JPH05212477A (en) * 1992-02-04 1993-08-24 Sky Alum Co Ltd High rigidity structural member
JPH0910871A (en) * 1995-06-28 1997-01-14 Sankyo Manitetsuku:Kk Hollow structural material and honeycomb structural material
JPH10244518A (en) * 1997-03-06 1998-09-14 Tokitsugu Ishikawa Extrusion molding die for honeycomb structure

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Publication number Priority date Publication date Assignee Title
US3617416A (en) * 1967-06-23 1971-11-02 Aerojet General Co Honeycomb structures
WO1988003086A1 (en) * 1986-10-24 1988-05-05 Patterson Fred R Variable geometry core structure
DE10101612C1 (en) * 2001-01-16 2002-10-31 Bohmann Dirk Braced plate construction made of flat molded components
KR100680383B1 (en) * 2005-10-13 2007-02-08 현대자동차주식회사 Mold producing method for catalytic honeycomb

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH05212477A (en) * 1992-02-04 1993-08-24 Sky Alum Co Ltd High rigidity structural member
JPH0910871A (en) * 1995-06-28 1997-01-14 Sankyo Manitetsuku:Kk Hollow structural material and honeycomb structural material
JPH10244518A (en) * 1997-03-06 1998-09-14 Tokitsugu Ishikawa Extrusion molding die for honeycomb structure

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
See also references of EP1667802A4 *

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9579866B2 (en) 2009-09-15 2017-02-28 Rep Ip Ag Honeycomb structure element
US9770882B2 (en) 2009-09-15 2017-09-26 Rep Ip Ag Honeycomb structure element

Also Published As

Publication number Publication date
EP1667802A4 (en) 2008-04-23
RU2006112822A (en) 2007-11-10
JP2007506557A (en) 2007-03-22
US20070033794A1 (en) 2007-02-15
EP1667802A1 (en) 2006-06-14
CN1905963A (en) 2007-01-31
AU2004274348B2 (en) 2008-03-20
AU2004274348A1 (en) 2005-03-31
RU2342211C2 (en) 2008-12-27
CA2538762A1 (en) 2005-03-31
BRPI0414747A (en) 2006-11-21
KR200350066Y1 (en) 2004-05-14
US7721404B2 (en) 2010-05-25

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