DE602007006510D1 - Flügelummantelungsplattenanordnung und flügelummantelungsplatte für einen flugzeugflügel und herstellungsverfahren dafür - Google Patents
Flügelummantelungsplattenanordnung und flügelummantelungsplatte für einen flugzeugflügel und herstellungsverfahren dafürInfo
- Publication number
- DE602007006510D1 DE602007006510D1 DE602007006510T DE602007006510T DE602007006510D1 DE 602007006510 D1 DE602007006510 D1 DE 602007006510D1 DE 602007006510 T DE602007006510 T DE 602007006510T DE 602007006510 T DE602007006510 T DE 602007006510T DE 602007006510 D1 DE602007006510 D1 DE 602007006510D1
- Authority
- DE
- Germany
- Prior art keywords
- wing
- mounting plate
- manufacturing
- method therefor
- plane
- 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.)
- Active
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/18—Spars; Ribs; Stringers
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/26—Construction, shape, or attachment of separate skins, e.g. panels
-
- 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
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GBGB0613949.7A GB0613949D0 (en) | 2006-07-13 | 2006-07-13 | A wing cover panel assembly and wing cover panel for an aircraft wing and a method of forming thereof |
PCT/GB2007/050382 WO2008007135A2 (en) | 2006-07-13 | 2007-07-05 | A wing cover panel assembly and wing cover panel for an aircraft wing and a method of forming thereof |
Publications (1)
Publication Number | Publication Date |
---|---|
DE602007006510D1 true DE602007006510D1 (de) | 2010-06-24 |
Family
ID=36955605
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE602007006510T Active DE602007006510D1 (de) | 2006-07-13 | 2007-07-05 | Flügelummantelungsplattenanordnung und flügelummantelungsplatte für einen flugzeugflügel und herstellungsverfahren dafür |
Country Status (11)
Country | Link |
---|---|
US (1) | US8398024B2 (de) |
EP (1) | EP2054297B1 (de) |
JP (1) | JP2009542524A (de) |
CN (1) | CN101432191B (de) |
AT (1) | ATE467554T1 (de) |
BR (1) | BRPI0712214A2 (de) |
CA (1) | CA2644269C (de) |
DE (1) | DE602007006510D1 (de) |
GB (1) | GB0613949D0 (de) |
RU (1) | RU2438925C2 (de) |
WO (1) | WO2008007135A2 (de) |
Families Citing this family (28)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US8100316B2 (en) * | 2008-05-29 | 2012-01-24 | Airbus Operations Gmbh | Method for joining aircraft fuselage elements by friction stir welding (fsw) |
US7857191B2 (en) * | 2008-06-16 | 2010-12-28 | Embraer-Empresa Brasileira De Aeronautica S.A. | Friction stir welding (FSW) methods and systems and friction stir welded components made thereby |
KR101649376B1 (ko) * | 2008-10-13 | 2016-08-31 | 한국전자통신연구원 | Mdct 기반 음성/오디오 통합 부호화기의 lpc 잔차신호 부호화/복호화 장치 |
GB201000878D0 (en) * | 2010-01-20 | 2010-03-10 | Airbus Operations Ltd | Sandwich panel |
GB201018185D0 (en) | 2010-10-28 | 2010-12-08 | Airbus Operations Ltd | Wing tip device attachment apparatus and method |
ES2402463B1 (es) * | 2010-11-30 | 2014-03-13 | Airbus Operations, S.L. | Un revestimiento de una superficie sustentadora de una aeronave. |
CN102139759A (zh) * | 2011-02-17 | 2011-08-03 | 中国航空工业集团公司西安飞机设计研究所 | 一种大尺寸复合材料整体壁板补强方法 |
US9168998B2 (en) * | 2011-11-23 | 2015-10-27 | The Boeing Company | Composite propeller spar |
CN102806617B (zh) * | 2012-06-04 | 2014-11-05 | 中航复合材料有限责任公司 | 一种整体成型“工”型加筋复合材料壁板的模具 |
CN102848498B (zh) * | 2012-06-04 | 2014-08-13 | 中航复合材料有限责任公司 | 一种整体成型“j”型加筋复合材料壁板的模具 |
FR2995237B1 (fr) | 2012-09-07 | 2015-05-01 | Airbus Operations Sas | Systeme ameliore de soudage par friction malaxage comprenant un contre-appui mobile. |
FR2995236B1 (fr) * | 2012-09-07 | 2015-05-01 | Airbus Operations Sas | Procede et systeme ameliores de soudage par friction malaxage d'un raidisseur sur un panneau d'aeronef. |
GB201220937D0 (en) * | 2012-11-21 | 2013-01-02 | Airbus Uk Ltd | Modular structural assembly |
JP5840161B2 (ja) * | 2013-03-04 | 2016-01-06 | 本田技研工業株式会社 | 異種材接合体の接合方法 |
US9341207B2 (en) | 2013-07-30 | 2016-05-17 | Gulfstream Aerospace Corporation | Web component and method of making a web component |
US9676549B2 (en) | 2014-12-02 | 2017-06-13 | Fontaine Commercial Trailer, Inc. | Floor assembly for transportable refrigerated container |
CN105235237A (zh) * | 2015-11-18 | 2016-01-13 | 江西洪都航空工业集团有限责任公司 | 一种复合材料j型加筋壁板成型工艺及成型工装 |
CN105346102B (zh) * | 2015-11-27 | 2018-02-23 | 沈阳飞机工业(集团)有限公司 | 复合材料j型纵墙定位整体成型工装及其成型方法 |
US10696373B2 (en) * | 2016-09-13 | 2020-06-30 | The Boeing Company | Aircraft wings and aircraft including such aircraft wings |
CN108100230A (zh) * | 2017-12-01 | 2018-06-01 | 中国直升机设计研究所 | 一种直升机平尾翼盒 |
JP2019131071A (ja) * | 2018-01-31 | 2019-08-08 | 三菱重工業株式会社 | 航空機 |
CN110550187A (zh) * | 2018-06-01 | 2019-12-10 | 空中客车德国运营有限责任公司 | 用于飞行器的机翼装置和飞行器 |
CN108688793B (zh) * | 2018-07-27 | 2023-11-24 | 中国工程物理研究院总体工程研究所 | 筒式发射无人机机翼折叠展开机构 |
FR3089442B1 (fr) * | 2018-12-05 | 2020-12-18 | Airbus Operations Sas | Procédé d’assemblage d’au moins deux pièces par soudage par transparence, procédé d’assemblage d’une structure primaire d’un mât d’aéronef par soudage par transparence, structure primaire d’un mât d’aéronef ainsi obtenue et aéronef comprenant ladite structure primaire |
CN109624355A (zh) * | 2018-12-10 | 2019-04-16 | 西安航空职业技术学院 | 高性能vari工艺成型复合材料的出胶结构及方法 |
NL2023459B1 (en) * | 2019-07-08 | 2021-02-02 | Kok & Van Engelen Composite Structures B V | Fuselage structure of an aircraft and method for manufacturing the same |
US11701737B2 (en) * | 2019-09-10 | 2023-07-18 | Qingdao Cimc Reefer Trailer Co., Ltd. | Friction-stir-welded sheet-and-post sidewall |
US11498656B1 (en) * | 2021-04-26 | 2022-11-15 | Rohr, Inc. | Airfoil system with embedded electric device |
Family Cites Families (20)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
BE428581A (de) * | ||||
US1331150A (en) * | 1917-10-09 | 1920-02-17 | Harris G Hooper | Aeroplane construction |
US1372478A (en) * | 1919-10-15 | 1921-03-22 | Bradley Parker Richardson | Method of fireproofing aircraft parts |
US1796654A (en) * | 1927-11-07 | 1931-03-17 | Hermann Otto | Metallic aeroplane wing |
US2396625A (en) * | 1941-03-26 | 1946-03-12 | Budd Edward G Mfg Co | Aircraft structure |
US2473728A (en) | 1944-04-20 | 1949-06-21 | Curtiss Wright Corp | Structural joint |
US3185267A (en) * | 1952-07-26 | 1965-05-25 | Pavlecka John | Interlocked panel structure |
US2955415A (en) | 1957-11-27 | 1960-10-11 | Theodore M Long | Cooled combustion chamber liner and nozzle supported in buckling modes |
US3093219A (en) * | 1961-04-06 | 1963-06-11 | Monte Copter Inc | Plural-section airfoils |
GB1128331A (en) | 1965-01-27 | 1968-09-25 | Handley Page Ltd | Improvements in or relating to aircraft wings, fuselages and the like and their manufacture |
JPS5014319Y1 (de) * | 1967-08-29 | 1975-05-02 | ||
US3827661A (en) | 1972-07-26 | 1974-08-06 | Ryson Aviat Corp | Aircraft wing structure and method of assembly |
CA1010002A (en) | 1973-04-25 | 1977-05-10 | Minnesota Mining And Manufacturing Company | Guide roller biasing shim liner |
US3920206A (en) * | 1974-08-05 | 1975-11-18 | Us Air Force | Non-penetrating rib-to-surface structural clip connector assembly |
SU1826409A1 (ru) | 1989-10-05 | 1995-12-27 | Московский машиностроительный завод им.С.В.Ильюшина | Силовой отсек кессона крыла в зоне крепления пилона двигателя |
GB2312483B (en) | 1996-04-24 | 2000-02-23 | British Aerospace | Joint assemblies |
US5887828A (en) | 1997-11-13 | 1999-03-30 | Northrop Grumman Corporation | Seamless mission adaptive control surface |
JP4397466B2 (ja) | 1999-07-06 | 2010-01-13 | 東芝三菱電機産業システム株式会社 | 永久磁石式回転電機 |
US20050247756A1 (en) * | 2004-03-31 | 2005-11-10 | Frazer James T | Connection mechanism and method |
DE102004018579A1 (de) * | 2004-04-16 | 2005-11-03 | Airbus Deutschland Gmbh | Verkleidung für eine Struktur eines Flugzeugs |
-
2006
- 2006-07-13 GB GBGB0613949.7A patent/GB0613949D0/en not_active Ceased
-
2007
- 2007-07-05 EP EP07733803A patent/EP2054297B1/de not_active Not-in-force
- 2007-07-05 CN CN200780015574.4A patent/CN101432191B/zh not_active Expired - Fee Related
- 2007-07-05 AT AT07733803T patent/ATE467554T1/de not_active IP Right Cessation
- 2007-07-05 US US12/302,862 patent/US8398024B2/en not_active Expired - Fee Related
- 2007-07-05 CA CA2644269A patent/CA2644269C/en not_active Expired - Fee Related
- 2007-07-05 BR BRPI0712214-4A patent/BRPI0712214A2/pt not_active IP Right Cessation
- 2007-07-05 DE DE602007006510T patent/DE602007006510D1/de active Active
- 2007-07-05 WO PCT/GB2007/050382 patent/WO2008007135A2/en active Application Filing
- 2007-07-05 RU RU2008149090/11A patent/RU2438925C2/ru not_active IP Right Cessation
- 2007-07-05 JP JP2009518973A patent/JP2009542524A/ja active Pending
Also Published As
Publication number | Publication date |
---|---|
BRPI0712214A2 (pt) | 2012-03-13 |
CA2644269A1 (en) | 2008-01-17 |
GB0613949D0 (en) | 2006-08-23 |
ATE467554T1 (de) | 2010-05-15 |
WO2008007135A3 (en) | 2008-05-22 |
CN101432191A (zh) | 2009-05-13 |
RU2438925C2 (ru) | 2012-01-10 |
WO2008007135A2 (en) | 2008-01-17 |
RU2008149090A (ru) | 2010-08-20 |
EP2054297B1 (de) | 2010-05-12 |
CA2644269C (en) | 2015-03-24 |
CN101432191B (zh) | 2012-03-07 |
US8398024B2 (en) | 2013-03-19 |
EP2054297A2 (de) | 2009-05-06 |
US20090200423A1 (en) | 2009-08-13 |
JP2009542524A (ja) | 2009-12-03 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
8364 | No opposition during term of opposition |