CN1863668A - 在包括局部加强件的层压板中的接合结构 - Google Patents
在包括局部加强件的层压板中的接合结构 Download PDFInfo
- Publication number
- CN1863668A CN1863668A CNA2004800292288A CN200480029228A CN1863668A CN 1863668 A CN1863668 A CN 1863668A CN A2004800292288 A CNA2004800292288 A CN A2004800292288A CN 200480029228 A CN200480029228 A CN 200480029228A CN 1863668 A CN1863668 A CN 1863668A
- Authority
- CN
- China
- Prior art keywords
- layer part
- metal
- wrong
- edge
- folding
- 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.)
- Granted
Links
- 230000002787 reinforcement Effects 0.000 title description 7
- 239000002184 metal Substances 0.000 claims abstract description 103
- 239000010410 layer Substances 0.000 abstract description 90
- 239000012790 adhesive layer Substances 0.000 abstract description 4
- 230000003014 reinforcing effect Effects 0.000 abstract 3
- 238000010276 construction Methods 0.000 abstract 1
- 239000000463 material Substances 0.000 description 7
- 229920002430 Fibre-reinforced plastic Polymers 0.000 description 3
- 239000000853 adhesive Substances 0.000 description 3
- 230000001070 adhesive effect Effects 0.000 description 3
- 239000011151 fibre-reinforced plastic Substances 0.000 description 3
- 238000005728 strengthening Methods 0.000 description 3
- 238000001465 metallisation Methods 0.000 description 2
- 238000005096 rolling process Methods 0.000 description 2
- 239000002344 surface layer Substances 0.000 description 2
- 235000003140 Panax quinquefolius Nutrition 0.000 description 1
- 240000005373 Panax quinquefolius Species 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000003825 pressing Methods 0.000 description 1
- 230000035945 sensitivity Effects 0.000 description 1
- 230000008719 thickening Effects 0.000 description 1
Images
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 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
- B29C70/88—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts characterised primarily by possessing specific properties, e.g. electrically conductive or locally reinforced
- B29C70/882—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts characterised primarily by possessing specific properties, e.g. electrically conductive or locally reinforced partly or totally electrically conductive, e.g. for EMI shielding
- B29C70/885—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts characterised primarily by possessing specific properties, e.g. electrically conductive or locally reinforced partly or totally electrically conductive, e.g. for EMI shielding with incorporated metallic wires, nets, films or plates
-
- 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
- B32B15/08—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 of synthetic resin
-
- 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
- B32B15/14—Layered products comprising a layer of metal next to 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
- 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
- B32B3/02—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 features of form at particular places, e.g. in edge regions
- B32B3/08—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 features of form at particular places, e.g. in edge regions characterised by added members at particular parts
-
- 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
-
- 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
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/40—Weight reduction
-
- 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
- Y10T428/12—All metal or with adjacent metals
- Y10T428/12493—Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.]
- Y10T428/12535—Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.] with additional, spatially distinct nonmetal component
- Y10T428/12556—Organic component
-
- 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
- Y10T428/19—Sheets or webs edge spliced or joined
-
- 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.]
- Y10T428/24777—Edge feature
Abstract
Description
Claims (9)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
NL1024479A NL1024479C2 (nl) | 2003-10-07 | 2003-10-07 | Verbindingsconstructie in een laminaat met een plaatselijke versterking. |
NL1024479 | 2003-10-07 |
Publications (2)
Publication Number | Publication Date |
---|---|
CN1863668A true CN1863668A (zh) | 2006-11-15 |
CN100540280C CN100540280C (zh) | 2009-09-16 |
Family
ID=34420822
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CNB2004800292288A Active CN100540280C (zh) | 2003-10-07 | 2004-10-05 | 在包括局部加强件的层压板中的接合结构 |
Country Status (10)
Country | Link |
---|---|
US (1) | US7560152B2 (zh) |
EP (1) | EP1670633B1 (zh) |
JP (1) | JP4938455B2 (zh) |
CN (1) | CN100540280C (zh) |
BR (1) | BRPI0415086B1 (zh) |
CA (1) | CA2541820C (zh) |
DE (1) | DE602004027060D1 (zh) |
NL (1) | NL1024479C2 (zh) |
RU (1) | RU2358877C2 (zh) |
WO (1) | WO2005032805A1 (zh) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN101711212A (zh) * | 2007-04-26 | 2010-05-19 | 空中客车运营有限公司 | 纤维金属叠层面板 |
CN101873965A (zh) * | 2007-10-18 | 2010-10-27 | 空中客车运营简易股份公司 | 飞机机身环周接合部处的ω形加固件的拼接 |
CN106457703A (zh) * | 2014-03-17 | 2017-02-22 | Gtm先进产品有限公司 | 金属片和相互结合的粘合剂层的叠层及获得此叠层的方法 |
CN106470830A (zh) * | 2014-04-25 | 2017-03-01 | 福克飞机结构公司 | 由层压件制成的面板及其制造方法 |
Families Citing this family (17)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102006031436B4 (de) | 2006-07-07 | 2012-12-06 | Airbus Operations Gmbh | Strukturelement, Verfahren zur Herstellung eines derartigen Strukturelements und Flugzeug mit einem derartigen Strukturelement |
DE102008010228A1 (de) * | 2008-02-21 | 2009-09-03 | Airbus Deutschland Gmbh | Verfahren und Vorrichtung zur Herstellung faserverstärkter Kunststoffprofilteile |
US8220745B2 (en) * | 2008-04-14 | 2012-07-17 | Airbus Deutschland Gmbh | Connection arrangement for connecting a first and second reinforcing element for an aircraft or spacecraft, and a shell component |
US8857128B2 (en) * | 2009-05-18 | 2014-10-14 | Apple Inc. | Reinforced device housing |
US8372495B2 (en) | 2010-05-26 | 2013-02-12 | Apple Inc. | Electronic device enclosure using sandwich construction |
US9120272B2 (en) | 2010-07-22 | 2015-09-01 | Apple Inc. | Smooth composite structure |
US8333345B2 (en) * | 2010-08-26 | 2012-12-18 | The Boeing Company | Composite aircraft joint |
US9011623B2 (en) | 2011-03-03 | 2015-04-21 | Apple Inc. | Composite enclosure |
DE102011108167B4 (de) * | 2011-07-20 | 2014-02-13 | Airbus Operations Gmbh | Fenstertrichter sowie Fensterbereich für ein Flugzeug |
US10407955B2 (en) | 2013-03-13 | 2019-09-10 | Apple Inc. | Stiff fabric |
CN204608330U (zh) | 2013-12-20 | 2015-09-02 | 苹果公司 | 编织纤维带 |
EP2907654A1 (en) | 2014-02-13 | 2015-08-19 | Airbus Operations GmbH | Joints in fibre metal laminates |
NL2015437B1 (en) | 2015-09-15 | 2017-04-03 | Gtm-Advanced Products B V | Laminate of mutually bonded adhesive layers and metal sheets, and method to obtain such laminate. |
GB2545655A (en) * | 2015-12-18 | 2017-06-28 | Airbus Operations Ltd | A structure formed from composite material |
NL2017850B1 (en) * | 2016-11-23 | 2018-05-28 | Gtm Advanced Products B V | Laminate of mutually bonded adhesive layers and spliced metal sheets |
US10864686B2 (en) | 2017-09-25 | 2020-12-15 | Apple Inc. | Continuous carbon fiber winding for thin structural ribs |
JP2020064488A (ja) * | 2018-10-18 | 2020-04-23 | レノボ・シンガポール・プライベート・リミテッド | 筐体用部材及び電子機器 |
Family Cites Families (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE69808903T2 (de) * | 1997-05-28 | 2003-08-07 | Structural Laminates Co | Verfahren zur herstellung eines mehrschichtwerkstoffes und ein mehrschichtwerkstoff der mit diesem verfahren herzustellen ist |
NL1015141C2 (nl) * | 2000-05-09 | 2001-11-13 | Fokker Aerostructures Bv | Verbindingsconstructie in een laminaat uit metalen en kunststof lagen. |
NL1023854C2 (nl) * | 2003-07-08 | 2005-01-11 | Stork Fokker Aesp Bv | Laminaat met vullaag. |
-
2003
- 2003-10-07 NL NL1024479A patent/NL1024479C2/nl not_active IP Right Cessation
-
2004
- 2004-10-05 EP EP04774997A patent/EP1670633B1/en active Active
- 2004-10-05 DE DE602004027060T patent/DE602004027060D1/de active Active
- 2004-10-05 BR BRPI0415086-4A patent/BRPI0415086B1/pt not_active IP Right Cessation
- 2004-10-05 CA CA2541820A patent/CA2541820C/en active Active
- 2004-10-05 JP JP2006532145A patent/JP4938455B2/ja not_active Expired - Fee Related
- 2004-10-05 CN CNB2004800292288A patent/CN100540280C/zh active Active
- 2004-10-05 RU RU2006115617/02A patent/RU2358877C2/ru not_active IP Right Cessation
- 2004-10-05 US US10/575,016 patent/US7560152B2/en active Active
- 2004-10-05 WO PCT/NL2004/000700 patent/WO2005032805A1/en active Application Filing
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN101711212A (zh) * | 2007-04-26 | 2010-05-19 | 空中客车运营有限公司 | 纤维金属叠层面板 |
CN101873965A (zh) * | 2007-10-18 | 2010-10-27 | 空中客车运营简易股份公司 | 飞机机身环周接合部处的ω形加固件的拼接 |
CN101873965B (zh) * | 2007-10-18 | 2013-10-23 | 空中客车运营简易股份公司 | 飞机机身环周接合部处的ω形加固件的拼接 |
CN106457703A (zh) * | 2014-03-17 | 2017-02-22 | Gtm先进产品有限公司 | 金属片和相互结合的粘合剂层的叠层及获得此叠层的方法 |
CN106457703B (zh) * | 2014-03-17 | 2019-04-19 | Gtm先进产品有限公司 | 金属片和相互结合的粘合剂层的叠层及获得此叠层的方法 |
CN106470830A (zh) * | 2014-04-25 | 2017-03-01 | 福克飞机结构公司 | 由层压件制成的面板及其制造方法 |
CN106470830B (zh) * | 2014-04-25 | 2018-11-09 | 福克飞机结构公司 | 由层压件制成的面板及其制造方法 |
Also Published As
Publication number | Publication date |
---|---|
CA2541820A1 (en) | 2005-04-14 |
EP1670633B1 (en) | 2010-05-05 |
DE602004027060D1 (de) | 2010-06-17 |
NL1024479C2 (nl) | 2005-04-08 |
WO2005032805A1 (en) | 2005-04-14 |
BRPI0415086B1 (pt) | 2014-06-17 |
CA2541820C (en) | 2012-12-04 |
US7560152B2 (en) | 2009-07-14 |
RU2358877C2 (ru) | 2009-06-20 |
CN100540280C (zh) | 2009-09-16 |
RU2006115617A (ru) | 2007-11-20 |
US20070042214A1 (en) | 2007-02-22 |
BRPI0415086A (pt) | 2006-12-26 |
JP4938455B2 (ja) | 2012-05-23 |
JP2007507373A (ja) | 2007-03-29 |
EP1670633A1 (en) | 2006-06-21 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
C06 | Publication | ||
PB01 | Publication | ||
C10 | Entry into substantive examination | ||
SE01 | Entry into force of request for substantive examination | ||
C14 | Grant of patent or utility model | ||
GR01 | Patent grant | ||
C56 | Change in the name or address of the patentee |
Owner name: FOKKER AEROSTRUCTURES B.V. Free format text: FORMER NAME: STORK FOKKER AESP BV |
|
CP01 | Change in the name or title of a patent holder |
Address after: Holland Pa Bond Ray Hurt Co-patentee after: Airbus GmbH Patentee after: Fokker Aerostructures B.V. Address before: Holland Pa Bond Ray Hurt Co-patentee before: Airbus GmbH Patentee before: Stork Focke AESP N. V. |
|
C56 | Change in the name or address of the patentee | ||
CP01 | Change in the name or title of a patent holder |
Address after: Holland Pa Bond Ray Hurt Co-patentee after: Airbus GmbH Patentee after: Fokker Aerostructures B.V. Address before: Holland Pa Bond Ray Hurt Co-patentee before: Airbus GmbH Patentee before: Fokker Aerostructures B.V. |