GB201313636D0 - Aircraft Structure - Google Patents
Aircraft StructureInfo
- Publication number
- GB201313636D0 GB201313636D0 GBGB1313636.1A GB201313636A GB201313636D0 GB 201313636 D0 GB201313636 D0 GB 201313636D0 GB 201313636 A GB201313636 A GB 201313636A GB 201313636 D0 GB201313636 D0 GB 201313636D0
- Authority
- GB
- United Kingdom
- Prior art keywords
- aircraft structure
- aircraft
- 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.)
- Withdrawn
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/18—Spars; Ribs; Stringers
- B64C3/187—Ribs
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/18—Spars; Ribs; Stringers
- B64C3/182—Stringers, longerons
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Laminated Bodies (AREA)
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1313636.1A GB2516830A (en) | 2013-07-31 | 2013-07-31 | Aircraft Structure |
PCT/GB2014/052008 WO2015015152A1 (en) | 2013-07-31 | 2014-07-02 | Aircraft structure |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1313636.1A GB2516830A (en) | 2013-07-31 | 2013-07-31 | Aircraft Structure |
Publications (2)
Publication Number | Publication Date |
---|---|
GB201313636D0 true GB201313636D0 (en) | 2013-09-11 |
GB2516830A GB2516830A (en) | 2015-02-11 |
Family
ID=49167211
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1313636.1A Withdrawn GB2516830A (en) | 2013-07-31 | 2013-07-31 | Aircraft Structure |
Country Status (2)
Country | Link |
---|---|
GB (1) | GB2516830A (en) |
WO (1) | WO2015015152A1 (en) |
Families Citing this family (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2528080A (en) | 2014-07-08 | 2016-01-13 | Airbus Operations Ltd | Structure |
GB2528076B (en) | 2014-07-08 | 2020-07-29 | Airbus Operations Ltd | Rib foot |
GB2528078B (en) | 2014-07-08 | 2020-07-29 | Airbus Operations Ltd | Structure |
US11180238B2 (en) * | 2018-11-19 | 2021-11-23 | The Boeing Company | Shear ties for aircraft wing |
GB2583940A (en) * | 2019-05-14 | 2020-11-18 | Airbus Operations Ltd | Aircraft panel assembly |
EP3894168B1 (en) | 2019-05-14 | 2023-10-11 | Airbus Operations Limited | Aircraft wing assembly |
CN110406657B (en) * | 2019-07-31 | 2021-06-01 | 中国商用飞机有限责任公司北京民用飞机技术研究中心 | Civil aircraft wing upper wall plate root connecting corner box, connecting structure and wing |
CN112193432B (en) * | 2020-08-21 | 2022-04-12 | 浙江大学 | Method for installing aircraft wall panel and method for calculating assembly clearance between aircraft wall panel and framework |
CN113428378B (en) * | 2021-08-12 | 2023-10-20 | 中航西安飞机工业集团股份有限公司 | Wing rib positioning and checking method |
GB2612958B (en) * | 2021-11-08 | 2023-12-20 | Airbus Operations Ltd | Panel assembly |
Family Cites Families (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5242523A (en) * | 1992-05-14 | 1993-09-07 | The Boeing Company | Caul and method for bonding and curing intricate composite structures |
JP4416900B2 (en) * | 2000-03-10 | 2010-02-17 | 富士重工業株式会社 | Composite panel and method for manufacturing the same |
US6386481B1 (en) * | 2001-01-08 | 2002-05-14 | Patria Finavicomp Oy | Arrangement for fastening stringers to aircraft wing ribs |
US7159822B2 (en) * | 2004-04-06 | 2007-01-09 | The Boeing Company | Structural panels for use in aircraft fuselages and other structures |
US7635106B2 (en) * | 2006-11-30 | 2009-12-22 | The Boeing Company | Composite shear tie |
FR2923800B1 (en) * | 2007-11-16 | 2010-05-21 | Airbus France | DEVICE FOR CONNECTING AN INTERNAL STRUCTURE PART OF AN AIRCRAFT AND THE FUSELAGE THEREOF |
DE102007055233A1 (en) * | 2007-11-20 | 2009-05-28 | Airbus Deutschland Gmbh | Coupling device for joining fuselage sections, combination of a coupling device and at least one fuselage section and method for producing the coupling device |
FR2970463B1 (en) * | 2011-01-17 | 2013-02-15 | Airbus Operations Sas | LIGHTING DEVICE WITH IMPROVED MECHANICAL STRENGTH. |
FR2970942B1 (en) * | 2011-01-28 | 2013-02-22 | Airbus Operations Sas | CONNECTING STIFF FRAMES BETWEEN AN AIRCRAFT FUSELAGE AND A VESSEL HOUSING |
-
2013
- 2013-07-31 GB GB1313636.1A patent/GB2516830A/en not_active Withdrawn
-
2014
- 2014-07-02 WO PCT/GB2014/052008 patent/WO2015015152A1/en active Application Filing
Also Published As
Publication number | Publication date |
---|---|
GB2516830A (en) | 2015-02-11 |
WO2015015152A1 (en) | 2015-02-05 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
WAP | Application withdrawn, taken to be withdrawn or refused ** after publication under section 16(1) |