WO2009153248A3 - Adhesive connection of folded honeycomb cores in sandwich structures - Google Patents
Adhesive connection of folded honeycomb cores in sandwich structures Download PDFInfo
- Publication number
- WO2009153248A3 WO2009153248A3 PCT/EP2009/057415 EP2009057415W WO2009153248A3 WO 2009153248 A3 WO2009153248 A3 WO 2009153248A3 EP 2009057415 W EP2009057415 W EP 2009057415W WO 2009153248 A3 WO2009153248 A3 WO 2009153248A3
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- folded honeycomb
- adhesive connection
- sandwich structures
- honeycomb cores
- adhesive
- Prior art date
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
- B32B37/00—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding
- B32B37/14—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by the properties of the layers
- B32B37/146—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by the properties of the layers whereby one or more of the layers is a honeycomb structure
-
- 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
- B32B3/00—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar form; Layered products 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 form; Layered products 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 form; Layered products 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
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B37/00—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding
- B32B37/12—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by using adhesives
- B32B37/1284—Application of adhesive
- B32B37/1292—Application of adhesive selectively, e.g. in stripes, in patterns
-
- 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
- B32B5/00—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
- B32B5/22—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed
- B32B5/24—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer
-
- 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
-
- 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
- B32B7/14—Interconnection of layers using interposed adhesives or interposed materials with bonding properties applied in spaced arrangements, e.g. in stripes
-
- 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
- B32B2250/00—Layers arrangement
- B32B2250/40—Symmetrical or sandwich layers, e.g. ABA, ABCBA, ABCCBA
-
- 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
- B32B2260/00—Layered product comprising an impregnated, embedded, or bonded layer wherein the layer comprises an impregnation, embedding, or binder 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
- B32B2262/00—Composition or structural features of fibres which form a fibrous or filamentary layer or are present as additives
- B32B2262/02—Synthetic macromolecular fibres
- B32B2262/0261—Polyamide fibres
- B32B2262/0269—Aromatic polyamide fibres
-
- 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
- B32B2264/00—Composition or properties of particles which form a particulate layer or are present as additives
- B32B2264/10—Inorganic particles
- B32B2264/105—Metal
-
- 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
- B32B2307/00—Properties of the layers or laminate
- B32B2307/20—Properties of the layers or laminate having particular electrical or magnetic properties, e.g. piezoelectric
- B32B2307/208—Magnetic, paramagnetic
-
- 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
- B32B2605/00—Vehicles
- B32B2605/18—Aircraft
Abstract
According to an embodiment of the invention, a sandwich structure (200) having a folded honeycomb core (201) is produced by applying an adhesive to the honeycomb webs (301, 304) of the folded honeycomb core (201) and then positioning it in a targeted manner so that the adhesive in a first area (302) is reduced and is supplied to a second area (309) where it is collected. The positioning of the adhesive is for example brought about by magnetic forces or hot air.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE102008028864A DE102008028864B4 (en) | 2008-06-19 | 2008-06-19 | Adhesive bonding of folded honeycomb cores in sandwich structures, device and use |
DE102008028864.0 | 2008-06-19 |
Publications (2)
Publication Number | Publication Date |
---|---|
WO2009153248A2 WO2009153248A2 (en) | 2009-12-23 |
WO2009153248A3 true WO2009153248A3 (en) | 2010-06-24 |
Family
ID=41111386
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/EP2009/057415 WO2009153248A2 (en) | 2008-06-19 | 2009-06-16 | Adhesive connection of folded honeycomb cores in sandwich structures |
Country Status (2)
Country | Link |
---|---|
DE (1) | DE102008028864B4 (en) |
WO (1) | WO2009153248A2 (en) |
Families Citing this family (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102012018158A1 (en) | 2012-09-14 | 2014-04-10 | Eads Deutschland Gmbh | Structural component e.g. aircraft component for aircraft, has integrated energy storage element which stores electrical energy |
DE102014007510A1 (en) | 2014-05-23 | 2015-11-26 | Airbus Defence and Space GmbH | Sandwich component and method for producing a sandwich component |
DE102014007511A1 (en) | 2014-05-23 | 2015-11-26 | Airbus Defence and Space GmbH | Sandwich component and method for producing a sandwich component |
DE102016117113B3 (en) * | 2016-09-12 | 2018-02-01 | Johann Kreuter | Structural mat, structured mat composite, sandwich structure and method and apparatus for producing a structural mat |
DE102017006714A1 (en) | 2017-07-14 | 2018-02-08 | Daimler Ag | Method for producing a reinforced component |
DE102019124642A1 (en) * | 2019-09-13 | 2021-03-18 | Dr. Ing. H.C. F. Porsche Aktiengesellschaft | Trim component for a motor vehicle and method for producing a trim component and sandwich material for a trim component |
Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0527109A1 (en) * | 1991-08-05 | 1993-02-10 | Alusuisse-Lonza Services Ag | Process for the manufacture of a composite panel with a cellular core and at least one outer layer |
US5944935A (en) * | 1996-07-24 | 1999-08-31 | Zukas; Florian J. | Preparation of adhesively bonded sandwich structures |
US20040020595A1 (en) * | 1999-10-26 | 2004-02-05 | Nalge Nunc International | Method of making a multi-well test plate having adhesively secured transparent bottom panel |
US20040026034A1 (en) * | 2001-05-02 | 2004-02-12 | Bernark Colin | Method and device for depositing adhesive on an alveolar surface |
US20040060652A1 (en) * | 2002-09-26 | 2004-04-01 | Mcneely John L. | Method and apparatus for applying a film adhesive to a perforated panel |
US20050274454A1 (en) * | 2004-06-09 | 2005-12-15 | Extrand Charles W | Magneto-active adhesive systems |
Family Cites Families (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1273771A (en) * | 1969-02-28 | 1972-05-10 | Ciba Geigy Uk Ltd | Improvements in or relating to cellular core structures |
FR2839075B1 (en) * | 2002-04-25 | 2006-05-19 | Airbus France | PERFORATED ADHESIVE FILM AND METHOD FOR MANUFACTURING THE SAME |
-
2008
- 2008-06-19 DE DE102008028864A patent/DE102008028864B4/en active Active
-
2009
- 2009-06-16 WO PCT/EP2009/057415 patent/WO2009153248A2/en active Application Filing
Patent Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0527109A1 (en) * | 1991-08-05 | 1993-02-10 | Alusuisse-Lonza Services Ag | Process for the manufacture of a composite panel with a cellular core and at least one outer layer |
US5944935A (en) * | 1996-07-24 | 1999-08-31 | Zukas; Florian J. | Preparation of adhesively bonded sandwich structures |
US20040020595A1 (en) * | 1999-10-26 | 2004-02-05 | Nalge Nunc International | Method of making a multi-well test plate having adhesively secured transparent bottom panel |
US20040026034A1 (en) * | 2001-05-02 | 2004-02-12 | Bernark Colin | Method and device for depositing adhesive on an alveolar surface |
US20040060652A1 (en) * | 2002-09-26 | 2004-04-01 | Mcneely John L. | Method and apparatus for applying a film adhesive to a perforated panel |
US20050274454A1 (en) * | 2004-06-09 | 2005-12-15 | Extrand Charles W | Magneto-active adhesive systems |
Also Published As
Publication number | Publication date |
---|---|
DE102008028864A1 (en) | 2009-12-31 |
WO2009153248A2 (en) | 2009-12-23 |
DE102008028864B4 (en) | 2013-04-25 |
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