JP2015227151A5 - - Google Patents
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- Publication number
- JP2015227151A5 JP2015227151A5 JP2014125201A JP2014125201A JP2015227151A5 JP 2015227151 A5 JP2015227151 A5 JP 2015227151A5 JP 2014125201 A JP2014125201 A JP 2014125201A JP 2014125201 A JP2014125201 A JP 2014125201A JP 2015227151 A5 JP2015227151 A5 JP 2015227151A5
- Authority
- JP
- Japan
- Prior art keywords
- web
- rib structure
- notch
- symmetrical
- symmetrical rib
- 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
- 239000003351 stiffener Substances 0.000 claims 2
- 230000003796 beauty Effects 0.000 claims 1
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US13/923,841 US9296466B2 (en) | 2013-06-21 | 2013-06-21 | Symmetric wing rib with center plane fastened shear ties |
| US13/923,841 | 2013-06-21 |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| JP2015227151A JP2015227151A (ja) | 2015-12-17 |
| JP2015227151A5 true JP2015227151A5 (enExample) | 2017-08-03 |
| JP6494186B2 JP6494186B2 (ja) | 2019-04-03 |
Family
ID=50980176
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP2014125201A Active JP6494186B2 (ja) | 2013-06-21 | 2014-06-18 | 中心面が固定されたシアタイを有する対称翼リブ |
Country Status (9)
| Country | Link |
|---|---|
| US (1) | US9296466B2 (enExample) |
| EP (1) | EP2815961B1 (enExample) |
| JP (1) | JP6494186B2 (enExample) |
| KR (1) | KR102153756B1 (enExample) |
| CN (1) | CN104229121B (enExample) |
| AU (1) | AU2014201864B2 (enExample) |
| CA (1) | CA2847635C (enExample) |
| ES (1) | ES2616729T3 (enExample) |
| RU (1) | RU2661411C2 (enExample) |
Families Citing this family (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP2910365B1 (en) * | 2014-02-21 | 2017-04-26 | Airbus Operations GmbH | Composite structural element and torsion box |
| US10479474B2 (en) | 2016-07-14 | 2019-11-19 | The Boeing Company | Friction stir welded wingtip torque box |
| US10745103B2 (en) * | 2017-05-31 | 2020-08-18 | The Boeing Company | Aircraft, aircraft wings and associated shear ties |
| CN108082474B (zh) * | 2017-10-31 | 2022-11-18 | 中航通飞华南飞机工业有限公司 | 一种水上飞机断阶框结构 |
| US11319051B2 (en) * | 2020-01-03 | 2022-05-03 | The Boeing Company | Stiffened composite ribs |
Family Cites Families (14)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB157310A (en) | 1919-02-27 | 1922-06-08 | John William Rapp | Improvements in airplane ribs |
| FR1396979A (fr) | 1964-06-01 | 1965-04-23 | Kirk Wing Company | Structure de profil d'aile et son procédé de fabrication |
| US4557440A (en) | 1983-08-18 | 1985-12-10 | The Boeing Company | Movable panel with compound curvature and method of making same |
| GB2409443A (en) | 2003-12-23 | 2005-06-29 | Airbus Uk Ltd | Rib for an aircraft and the manufacture thereof |
| GB0606079D0 (en) * | 2006-03-27 | 2006-05-03 | Airbus Uk Ltd | Aircraft component |
| FR2901243B1 (fr) * | 2006-05-16 | 2008-06-27 | Airbus France Sas | Dispositif d'accrochage d'un moteur d'aeronef |
| GB0619512D0 (en) * | 2006-10-03 | 2006-11-15 | Airbus Uk Ltd | Fitting |
| US7721995B2 (en) * | 2006-12-13 | 2010-05-25 | The Boeing Company | Rib support for wing panels |
| US7686251B2 (en) * | 2006-12-13 | 2010-03-30 | The Boeing Company | Rib support for wing panels |
| FR2948099B1 (fr) * | 2009-07-16 | 2012-05-11 | Airbus Operations Sas | Procede de fabrication d'un aeronef a voilure fixe |
| US8714485B2 (en) | 2009-12-15 | 2014-05-06 | The Boeing Company | Method of fabricating a hat stringer |
| EP2463291B1 (en) * | 2010-12-09 | 2016-05-04 | Shin-Etsu Chemical Co., Ltd. | Hydrosilylation method, method for producing organosilicon compound, and organosilicon compound. |
| US8679616B2 (en) | 2010-12-14 | 2014-03-25 | The Boeing Company | Skew-angle radius filler |
| JP6093192B2 (ja) * | 2013-01-25 | 2017-03-08 | 三菱航空機株式会社 | 航空機の機体用パネル、航空機の翼 |
-
2013
- 2013-06-21 US US13/923,841 patent/US9296466B2/en active Active
-
2014
- 2014-03-27 CA CA2847635A patent/CA2847635C/en active Active
- 2014-04-01 AU AU2014201864A patent/AU2014201864B2/en active Active
- 2014-04-21 KR KR1020140047710A patent/KR102153756B1/ko active Active
- 2014-06-17 RU RU2014124529A patent/RU2661411C2/ru active
- 2014-06-17 CN CN201410270297.3A patent/CN104229121B/zh active Active
- 2014-06-18 JP JP2014125201A patent/JP6494186B2/ja active Active
- 2014-06-19 ES ES14173180.2T patent/ES2616729T3/es active Active
- 2014-06-19 EP EP14173180.2A patent/EP2815961B1/en active Active
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