JP2018070141A5 - - Google Patents
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- Publication number
- JP2018070141A5 JP2018070141A5 JP2017152114A JP2017152114A JP2018070141A5 JP 2018070141 A5 JP2018070141 A5 JP 2018070141A5 JP 2017152114 A JP2017152114 A JP 2017152114A JP 2017152114 A JP2017152114 A JP 2017152114A JP 2018070141 A5 JP2018070141 A5 JP 2018070141A5
- Authority
- JP
- Japan
- Prior art keywords
- fuselage barrel
- butt joint
- section
- stringer
- main section
- 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
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US15/258,919 US10308342B2 (en) | 2016-09-07 | 2016-09-07 | Method of repairing damage to fuselage barrel and associated apparatus and system |
| US15/258,919 | 2016-09-07 |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| JP2018070141A JP2018070141A (ja) | 2018-05-10 |
| JP2018070141A5 true JP2018070141A5 (enExample) | 2020-09-17 |
| JP7012483B2 JP7012483B2 (ja) | 2022-01-28 |
Family
ID=59315470
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP2017152114A Active JP7012483B2 (ja) | 2016-09-07 | 2017-08-07 | 胴体バレルに対する損傷を修理する方法並びに関連装置及びシステム |
Country Status (5)
| Country | Link |
|---|---|
| US (2) | US10308342B2 (enExample) |
| EP (1) | EP3293105B1 (enExample) |
| JP (1) | JP7012483B2 (enExample) |
| CN (1) | CN107792390B (enExample) |
| CA (1) | CA2974245C (enExample) |
Families Citing this family (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US7325771B2 (en) * | 2004-09-23 | 2008-02-05 | The Boeing Company | Splice joints for composite aircraft fuselages and other structures |
| FR3089946B1 (fr) * | 2018-12-18 | 2021-01-08 | Airbus Operations Sas | structure d’un FUSELAGE D’UN aeronef présentant un panneau renforcé par un treillis |
| US11427351B2 (en) | 2019-12-06 | 2022-08-30 | The Boeing Company | Carrier and operational frame system and methods of assembling a structure |
| EP3978358B1 (en) * | 2020-09-30 | 2024-11-06 | The Boeing Company | Aircraft fuselage longitudinal splice for joining half barrel fuselage sections and other spliced fuselage sections |
| NL2027402B1 (en) * | 2021-01-26 | 2022-08-19 | Boeing Co | Aircraft assembly formed of mating half barrel sections and the method of assembling the same |
| JP2022081436A (ja) * | 2020-11-18 | 2022-05-31 | ザ・ボーイング・カンパニー | 機体の移動ライン組立 |
| US11801576B2 (en) | 2020-11-18 | 2023-10-31 | The Boeing Company | Aircraft assembly formed of mating half barrel sections and the method of assembling the same |
| US11919617B2 (en) | 2020-12-17 | 2024-03-05 | The Boeing Company | Circumferential lap splices for sections of fuselage |
| US12420954B2 (en) * | 2023-04-12 | 2025-09-23 | The Boeing Company | Composite repair components with customizable shims |
| CN119525315B (zh) * | 2024-11-14 | 2025-10-28 | 中航西安飞机工业集团股份有限公司 | 一种弱刚性结构飞机钣金框缘偏移修复工装及方法 |
Family Cites Families (21)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5518208A (en) * | 1993-12-28 | 1996-05-21 | The Boeing Company | Optimum aircraft body frame to body skin shear tie installation pattern for body skin/stringer circumferential splices |
| US6849150B1 (en) * | 2001-01-16 | 2005-02-01 | Lockheed Martin Corporation | System and method of forming structural assemblies with 3-D woven joint pre-forms |
| US7325771B2 (en) * | 2004-09-23 | 2008-02-05 | The Boeing Company | Splice joints for composite aircraft fuselages and other structures |
| FR2901246B1 (fr) * | 2006-05-19 | 2008-06-20 | Airbus France Sas | Procede de reparation d'une zone endommagee d'un fuselage d'aeronef |
| US7871040B2 (en) | 2006-11-10 | 2011-01-18 | The Boeing Company | Composite aircraft structures with hat stiffeners |
| US8047469B2 (en) * | 2008-03-01 | 2011-11-01 | The Boeing Company | Airframe attachment fitting |
| US7967250B2 (en) * | 2008-05-12 | 2011-06-28 | EMBRAER—Empresa Brasileira de Aeronáutica | Hybrid aircraft fuselage structural components and methods of making same |
| DE102009009491A1 (de) | 2009-02-18 | 2010-09-09 | Airbus Deutschland Gmbh | Verfahren zum Herstellen eines Schalenkörpers |
| FR2953812B1 (fr) * | 2009-12-11 | 2012-09-07 | Airbus Operations Sas | Procede de reparation d'un fuselage d'aeronef |
| ES2395604B1 (es) | 2010-10-29 | 2013-12-26 | Airbus Operations, S.L. | Reparación interior doblada. |
| US8567722B2 (en) * | 2010-12-15 | 2013-10-29 | The Boeing Company | Splice and associated method for joining fuselage sections |
| US8616500B2 (en) | 2011-03-04 | 2013-12-31 | The Boeing Company | Diamond shaped window for composite and/or metallic airframe |
| US8844108B2 (en) * | 2011-07-12 | 2014-09-30 | The Boeing Company | Large area repair of composite aircraft |
| US8914979B2 (en) * | 2011-07-21 | 2014-12-23 | Spirit AcroSystems, Inc. | System and method for assembling aircraft components |
| US8684311B2 (en) * | 2012-03-07 | 2014-04-01 | The Boeing Company | Bonded splice joint |
| US8939406B2 (en) * | 2012-07-02 | 2015-01-27 | The Boeing Company | Joining composite fuselage sections along window belts |
| US8985512B1 (en) * | 2012-09-21 | 2015-03-24 | The Boeing Company | Aircraft, fuselages, and associated methods |
| US8960606B2 (en) | 2012-10-31 | 2015-02-24 | The Boeing Company | Circumference splice for joining shell structures |
| GB2517954B (en) | 2013-09-05 | 2018-07-04 | Airbus Operations Ltd | Repair of a damaged composite aircraft wing |
| EP2873620B1 (en) | 2013-11-14 | 2018-05-16 | Airbus Operations GmbH | Repair method for fuselage components of aircraft or spacecraft |
| FR3037558B1 (fr) * | 2015-06-19 | 2017-05-26 | Airbus Operations Sas | Procede de fabrication d'un panneau de fuselage par surmoulage et panneau de fuselage ainsi obtenu |
-
2016
- 2016-09-07 US US15/258,919 patent/US10308342B2/en active Active
-
2017
- 2017-07-11 EP EP17180646.6A patent/EP3293105B1/en active Active
- 2017-07-19 CA CA2974245A patent/CA2974245C/en active Active
- 2017-08-07 JP JP2017152114A patent/JP7012483B2/ja active Active
- 2017-09-06 CN CN201710795168.XA patent/CN107792390B/zh active Active
-
2019
- 2019-04-24 US US16/393,716 patent/US11104412B2/en active Active
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