ES2418858T5 - Soporte costal para paneles de alas - Google Patents
Soporte costal para paneles de alas Download PDFInfo
- Publication number
- ES2418858T5 ES2418858T5 ES07024235.9T ES07024235T ES2418858T5 ES 2418858 T5 ES2418858 T5 ES 2418858T5 ES 07024235 T ES07024235 T ES 07024235T ES 2418858 T5 ES2418858 T5 ES 2418858T5
- Authority
- ES
- Spain
- Prior art keywords
- metal
- stringer
- flange
- stringers
- 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.)
- Active
Links
- QTCANKDTWWSCMR-UHFFFAOYSA-N costic aldehyde Natural products C1CCC(=C)C2CC(C(=C)C=O)CCC21C QTCANKDTWWSCMR-UHFFFAOYSA-N 0.000 title description 2
- ISTFUJWTQAMRGA-UHFFFAOYSA-N iso-beta-costal Natural products C1C(C(=C)C=O)CCC2(C)CCCC(C)=C21 ISTFUJWTQAMRGA-UHFFFAOYSA-N 0.000 title description 2
- 229910052751 metal Inorganic materials 0.000 claims description 73
- 239000002184 metal Substances 0.000 claims description 73
- 238000005253 cladding Methods 0.000 claims description 42
- 238000000034 method Methods 0.000 claims description 37
- 238000004519 manufacturing process Methods 0.000 claims description 15
- 239000011248 coating agent Substances 0.000 claims description 14
- 238000000576 coating method Methods 0.000 claims description 14
- 238000005304 joining Methods 0.000 claims description 11
- 210000000720 eyelash Anatomy 0.000 claims description 3
- 239000003381 stabilizer Substances 0.000 claims description 3
- 230000008569 process Effects 0.000 description 12
- 239000003351 stiffener Substances 0.000 description 9
- 238000005553 drilling Methods 0.000 description 8
- 239000002131 composite material Substances 0.000 description 6
- 238000000926 separation method Methods 0.000 description 6
- 238000013461 design Methods 0.000 description 5
- 239000000463 material Substances 0.000 description 5
- 230000008901 benefit Effects 0.000 description 4
- 230000006835 compression Effects 0.000 description 4
- 238000007906 compression Methods 0.000 description 4
- 230000002787 reinforcement Effects 0.000 description 4
- 150000001875 compounds Chemical class 0.000 description 3
- 230000007246 mechanism Effects 0.000 description 3
- 230000004048 modification Effects 0.000 description 3
- 238000012986 modification Methods 0.000 description 3
- 229910052782 aluminium Inorganic materials 0.000 description 2
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 2
- 238000005452 bending Methods 0.000 description 2
- 230000015572 biosynthetic process Effects 0.000 description 2
- 238000009434 installation Methods 0.000 description 2
- 238000012423 maintenance Methods 0.000 description 2
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 1
- 229920000271 Kevlar® Polymers 0.000 description 1
- 238000000429 assembly Methods 0.000 description 1
- 239000011230 binding agent Substances 0.000 description 1
- 238000005266 casting Methods 0.000 description 1
- 239000004020 conductor Substances 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000007613 environmental effect Effects 0.000 description 1
- 239000011888 foil Substances 0.000 description 1
- 238000005242 forging Methods 0.000 description 1
- 239000003365 glass fiber Substances 0.000 description 1
- 229910002804 graphite Inorganic materials 0.000 description 1
- 239000010439 graphite Substances 0.000 description 1
- 230000010354 integration Effects 0.000 description 1
- 239000004761 kevlar Substances 0.000 description 1
- 230000008520 organization Effects 0.000 description 1
- 230000009467 reduction Effects 0.000 description 1
- 239000011347 resin Substances 0.000 description 1
- 229920005989 resin Polymers 0.000 description 1
- 238000010008 shearing Methods 0.000 description 1
- 238000012546 transfer Methods 0.000 description 1
- 230000007306 turnover Effects 0.000 description 1
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
- B64C3/26—Construction, shape, or attachment of separate skins, e.g. panels
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Connection Of Plates (AREA)
Applications Claiming Priority (4)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US610444 | 2006-12-13 | ||
| US11/610,444 US7721995B2 (en) | 2006-12-13 | 2006-12-13 | Rib support for wing panels |
| US11/867,158 US7686251B2 (en) | 2006-12-13 | 2007-10-04 | Rib support for wing panels |
| US867158 | 2007-10-04 |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| ES2418858T3 ES2418858T3 (es) | 2013-08-16 |
| ES2418858T5 true ES2418858T5 (es) | 2017-05-19 |
Family
ID=39133792
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| ES07024235.9T Active ES2418858T5 (es) | 2006-12-13 | 2007-12-13 | Soporte costal para paneles de alas |
Country Status (4)
| Country | Link |
|---|---|
| US (1) | US7686251B2 (enExample) |
| EP (1) | EP1942052B2 (enExample) |
| JP (1) | JP5156356B2 (enExample) |
| ES (1) | ES2418858T5 (enExample) |
Families Citing this family (26)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB0606079D0 (en) * | 2006-03-27 | 2006-05-03 | Airbus Uk Ltd | Aircraft component |
| GB0709118D0 (en) * | 2007-05-14 | 2007-06-20 | Airbus Uk Ltd | Reinforced panel |
| KR101711226B1 (ko) * | 2009-04-17 | 2017-02-28 | 쓰리엠 이노베이티브 프로퍼티즈 컴파니 | 패턴화된 전도체를 갖는 낙뢰 보호 시트 |
| US8167245B1 (en) * | 2009-11-03 | 2012-05-01 | The Boeing Company | Fuel barrier |
| ES2402463B1 (es) * | 2010-11-30 | 2014-03-13 | Airbus Operations, S.L. | Un revestimiento de una superficie sustentadora de una aeronave. |
| US8684311B2 (en) | 2012-03-07 | 2014-04-01 | The Boeing Company | Bonded splice joint |
| US9943937B2 (en) | 2012-09-28 | 2018-04-17 | The Boeing Company | System and method for manufacturing a wing panel |
| GB201220937D0 (en) * | 2012-11-21 | 2013-01-02 | Airbus Uk Ltd | Modular structural assembly |
| US9296466B2 (en) * | 2013-06-21 | 2016-03-29 | The Boeing Company | Symmetric wing rib with center plane fastened shear ties |
| US9156538B1 (en) * | 2013-07-22 | 2015-10-13 | The Boeing Company | Aircraft skin attachment system |
| GB2528076B (en) | 2014-07-08 | 2020-07-29 | Airbus Operations Ltd | Rib foot |
| EP3040268A1 (en) * | 2014-12-30 | 2016-07-06 | Airbus Operations, S.L. | Stringer stiffened aircraft composite structures |
| US10040537B2 (en) * | 2015-01-15 | 2018-08-07 | The Boeing Company | Laminate composite wing structures |
| US9849967B2 (en) * | 2015-04-01 | 2017-12-26 | The Boeing Company | Composite rib for an aircraft |
| US10196126B2 (en) * | 2015-04-07 | 2019-02-05 | The Boeing Company | Rib structure and method of forming thereof |
| CN105253291A (zh) * | 2015-10-14 | 2016-01-20 | 哈尔滨飞机工业集团有限责任公司 | 一种带梳状接头的机翼整体机加壁板及应用 |
| US10696373B2 (en) * | 2016-09-13 | 2020-06-30 | The Boeing Company | Aircraft wings and aircraft including such aircraft wings |
| US20180328371A1 (en) * | 2017-05-09 | 2018-11-15 | Borgwarner Inc. | Backplate and method of making and using the same |
| US10745103B2 (en) | 2017-05-31 | 2020-08-18 | The Boeing Company | Aircraft, aircraft wings and associated shear ties |
| GB2566920A (en) * | 2017-07-12 | 2019-04-03 | Safran Nacelles Ltd | Fitting for a stiffened panel |
| US11136107B2 (en) * | 2018-10-05 | 2021-10-05 | The Boeing Company | Method and apparatus for attaching a fuselage frame to a wing box |
| US11180238B2 (en) * | 2018-11-19 | 2021-11-23 | The Boeing Company | Shear ties for aircraft wing |
| US11038334B2 (en) * | 2019-01-14 | 2021-06-15 | The Boeing Company | Aircraft wing composite ribs having electrical grounding paths |
| US10913548B2 (en) | 2019-01-14 | 2021-02-09 | The Boeing Company | Metallic fittings for coupling composite ribs to skin panels of aircraft wings |
| US11548607B2 (en) * | 2019-12-16 | 2023-01-10 | The Boeing Company | Longitudinal beam joint for a pressure deck assembly |
| CN111159943B (zh) * | 2019-12-25 | 2023-07-21 | 中国航空工业集团公司西安飞机设计研究所 | 一种动翼面封严结构的屈曲处理方法 |
Family Cites Families (17)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2367750A (en) | 1941-01-17 | 1945-01-23 | Central Aircraft Corp | Aircraft construction |
| US3034608A (en) † | 1959-03-03 | 1962-05-15 | Budd Co | Sheet stiffening stringer |
| US4310132A (en) | 1978-02-16 | 1982-01-12 | Nasa | Fuselage structure using advanced technology fiber reinforced composites |
| GB2072579B (en) † | 1980-04-01 | 1984-06-06 | British Aerospace | Stiffened panel of fibre reinforced plastics materials |
| GB2312483B (en) * | 1996-04-24 | 2000-02-23 | British Aerospace | Joint assemblies |
| US6766984B1 (en) | 1998-07-16 | 2004-07-27 | Icom Engineering Corporation | Stiffeners for aircraft structural panels |
| JP4416900B2 (ja) * | 2000-03-10 | 2010-02-17 | 富士重工業株式会社 | 複合材パネルおよびその製造方法 |
| CA2402848C (en) * | 2000-04-05 | 2009-06-16 | Kenneth Earl Nunn | K-spar configuration for bonded wing construction |
| JP4425424B2 (ja) * | 2000-05-01 | 2010-03-03 | 本田技研工業株式会社 | 繊維強化複合材からなるジョグル付き半硬化物品の製造方法、及びそれを用いた予備成形構造体の製造方法 |
| US6386481B1 (en) | 2001-01-08 | 2002-05-14 | Patria Finavicomp Oy | Arrangement for fastening stringers to aircraft wing ribs |
| JP3600179B2 (ja) * | 2001-03-30 | 2004-12-08 | 川崎重工業株式会社 | 翼の内部圧力開放構造 |
| JP4545339B2 (ja) * | 2001-04-05 | 2010-09-15 | 富士重工業株式会社 | 複合材翼およびその製造方法 |
| US7159822B2 (en) | 2004-04-06 | 2007-01-09 | The Boeing Company | Structural panels for use in aircraft fuselages and other structures |
| US8444087B2 (en) † | 2005-04-28 | 2013-05-21 | The Boeing Company | Composite skin and stringer structure and method for forming the same |
| US7410352B2 (en) | 2005-04-13 | 2008-08-12 | The Boeing Company | Multi-ring system for fuselage barrel formation |
| US8715560B2 (en) | 2005-11-10 | 2014-05-06 | The Boeing Company | Method to control thickness in composite parts cured on closed angle tool |
| US7635106B2 (en) † | 2006-11-30 | 2009-12-22 | The Boeing Company | Composite shear tie |
-
2007
- 2007-10-04 US US11/867,158 patent/US7686251B2/en active Active
- 2007-12-12 JP JP2007320940A patent/JP5156356B2/ja active Active
- 2007-12-13 EP EP07024235.9A patent/EP1942052B2/en active Active
- 2007-12-13 ES ES07024235.9T patent/ES2418858T5/es active Active
Also Published As
| Publication number | Publication date |
|---|---|
| US20080173757A1 (en) | 2008-07-24 |
| EP1942052B2 (en) | 2016-11-02 |
| JP2008174223A (ja) | 2008-07-31 |
| EP1942052B1 (en) | 2013-04-10 |
| ES2418858T3 (es) | 2013-08-16 |
| JP5156356B2 (ja) | 2013-03-06 |
| US7686251B2 (en) | 2010-03-30 |
| EP1942052A1 (en) | 2008-07-09 |
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