CN105438438B - 复合材料的机翼边缘附接及方法 - Google Patents
复合材料的机翼边缘附接及方法 Download PDFInfo
- Publication number
- CN105438438B CN105438438B CN201510595950.8A CN201510595950A CN105438438B CN 105438438 B CN105438438 B CN 105438438B CN 201510595950 A CN201510595950 A CN 201510595950A CN 105438438 B CN105438438 B CN 105438438B
- Authority
- CN
- China
- Prior art keywords
- composite
- edge
- wing
- skin panel
- thickness
- 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
- 239000002131 composite material Substances 0.000 title claims abstract description 226
- 238000000034 method Methods 0.000 title claims abstract description 40
- 238000003754 machining Methods 0.000 claims description 13
- 238000010276 construction Methods 0.000 description 9
- 238000004519 manufacturing process Methods 0.000 description 9
- 239000000463 material Substances 0.000 description 9
- 239000000945 filler Substances 0.000 description 6
- 230000007704 transition Effects 0.000 description 5
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 4
- 238000012423 maintenance Methods 0.000 description 4
- 229910052751 metal Inorganic materials 0.000 description 4
- 239000002184 metal Substances 0.000 description 4
- 230000004048 modification Effects 0.000 description 4
- 238000012986 modification Methods 0.000 description 4
- 239000010936 titanium Substances 0.000 description 4
- 229910000851 Alloy steel Inorganic materials 0.000 description 3
- 229910000831 Steel Inorganic materials 0.000 description 3
- 229910052782 aluminium Inorganic materials 0.000 description 3
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 3
- 238000013461 design Methods 0.000 description 3
- 239000010959 steel Substances 0.000 description 3
- 229910001069 Ti alloy Inorganic materials 0.000 description 2
- 239000004918 carbon fiber reinforced polymer Substances 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 238000005304 joining Methods 0.000 description 2
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical class C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 description 2
- 238000012545 processing Methods 0.000 description 2
- 230000000284 resting effect Effects 0.000 description 2
- 239000000565 sealant Substances 0.000 description 2
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 1
- 239000004593 Epoxy Substances 0.000 description 1
- 229910001200 Ferrotitanium Inorganic materials 0.000 description 1
- 241001264313 Semioptera wallacii Species 0.000 description 1
- 239000000853 adhesive Substances 0.000 description 1
- 230000001070 adhesive effect Effects 0.000 description 1
- 229910045601 alloy Inorganic materials 0.000 description 1
- 239000000956 alloy Substances 0.000 description 1
- 238000013459 approach Methods 0.000 description 1
- 238000005452 bending Methods 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000007613 environmental effect Effects 0.000 description 1
- 238000007667 floating Methods 0.000 description 1
- 229910002804 graphite Inorganic materials 0.000 description 1
- 239000010439 graphite Substances 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 230000010354 integration Effects 0.000 description 1
- 238000003475 lamination Methods 0.000 description 1
- 230000007246 mechanism Effects 0.000 description 1
- 239000007769 metal material Substances 0.000 description 1
- 150000002739 metals Chemical class 0.000 description 1
- 230000008569 process Effects 0.000 description 1
- 238000003672 processing method Methods 0.000 description 1
- 230000009467 reduction Effects 0.000 description 1
- 238000009419 refurbishment Methods 0.000 description 1
- 230000000717 retained effect Effects 0.000 description 1
- 238000007493 shaping process Methods 0.000 description 1
- 239000000758 substrate Substances 0.000 description 1
- 229910052719 titanium Inorganic materials 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/28—Leading or trailing edges attached to primary structures, e.g. forming fixed slots
-
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F5/00—Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
- B64F5/10—Manufacturing or assembling aircraft, e.g. jigs therefor
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Manufacturing & Machinery (AREA)
- Transportation (AREA)
- Moulding By Coating Moulds (AREA)
- Laminated Bodies (AREA)
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US14/488,987 | 2014-09-17 | ||
| US14/488,987 US10329009B2 (en) | 2014-09-17 | 2014-09-17 | Composite wing edge attachment and method |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN105438438A CN105438438A (zh) | 2016-03-30 |
| CN105438438B true CN105438438B (zh) | 2019-12-27 |
Family
ID=54012041
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201510595950.8A Active CN105438438B (zh) | 2014-09-17 | 2015-09-17 | 复合材料的机翼边缘附接及方法 |
Country Status (4)
| Country | Link |
|---|---|
| US (2) | US10329009B2 (https=) |
| EP (1) | EP3000719B1 (https=) |
| JP (1) | JP6644481B2 (https=) |
| CN (1) | CN105438438B (https=) |
Families Citing this family (34)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US9896190B1 (en) * | 2014-05-07 | 2018-02-20 | The Boeing Company | Wing leading edge architecture suitable for laminar flow |
| DE102015105298B4 (de) * | 2015-04-08 | 2021-12-23 | Deutsches Zentrum für Luft- und Raumfahrt e.V. | Flügelstruktur für Flugobjekte und Verfahren zum Austausch einer Flügelvorderkante bei einer Flügelstruktur |
| US20170259521A1 (en) * | 2016-02-08 | 2017-09-14 | Bell Helicopter Textron Inc. | Large Cell Core Stiffened Panels with Solid Inserts |
| EP3243744B1 (en) * | 2016-05-11 | 2019-05-01 | Airbus Operations Limited | Aircraft joint |
| EP3243743B1 (en) * | 2016-05-11 | 2021-05-05 | Airbus Operations Limited | Aircraft joint |
| US10179640B2 (en) | 2016-08-24 | 2019-01-15 | The Boeing Company | Wing and method of manufacturing |
| EP3330174B1 (en) * | 2016-12-02 | 2019-10-30 | Airbus Operations, S.L. | Aircraft stabilizer leading edge integration with torsion box and fuselage |
| NL2018263B1 (nl) * | 2017-01-31 | 2018-08-16 | Fibercore Ip Bv | Aerodynamisch of hydrodynamisch blad uit gelaagd materiaal |
| EP3421352B1 (en) * | 2017-06-28 | 2022-10-26 | Airbus Operations S.L. | Modular lifting surface and method for manufacturing thereof |
| GB201710385D0 (en) * | 2017-06-29 | 2017-08-16 | Airbus Operations Gmbh | Aerofoil structure and method of assembly |
| US10773789B2 (en) * | 2017-07-07 | 2020-09-15 | The Boeing Company | Skin-panel interface of an aircraft |
| US10828851B2 (en) * | 2017-07-28 | 2020-11-10 | The Boeing Company | Slip sheet with compensation surface |
| CN108032988B (zh) * | 2017-10-25 | 2020-06-16 | 北京航空航天大学 | 一种纤维增强复合材料飞行器舱段连接结构及其制备方法 |
| CN108100218B (zh) * | 2017-11-16 | 2021-04-16 | 中国航空工业集团公司西安飞机设计研究所 | 一种带翼型的可拆卸雷达罩支撑结构 |
| GB201719790D0 (en) | 2017-11-28 | 2018-01-10 | Airbus Operations Gmbh | Aircraft joint with a curable composite bushing |
| EP3521162B1 (en) | 2018-02-02 | 2022-06-22 | AIRBUS HELICOPTERS DEUTSCHLAND GmbH | A helicopter with a fuselage and a tail boom which are connected via a shear connection |
| US11047308B2 (en) * | 2018-06-29 | 2021-06-29 | The Boeing Company | Acoustic panel for thrust reversers |
| GB2577936A (en) * | 2018-10-12 | 2020-04-15 | Airbus Operations Ltd | Aircraft assembly |
| CN109649675B (zh) * | 2018-11-30 | 2021-10-29 | 中国商用飞机有限责任公司北京民用飞机技术研究中心 | 一种机翼下壁板对接区的密封优化方法 |
| CN109572996B (zh) * | 2018-12-04 | 2022-04-19 | 中国航空工业集团公司西安飞机设计研究所 | 一种考虑温度变化的尾翼抗鸟撞附加蒙皮前缘结构 |
| CN109815528A (zh) * | 2018-12-13 | 2019-05-28 | 航天神舟飞行器有限公司 | 一种基于大型复合翼气的飞行器参数优化的方法 |
| CN110065620A (zh) * | 2019-04-12 | 2019-07-30 | 西安飞机工业（集团）有限责任公司 | 一种复合材料壁板连接结构 |
| CN110145678B (zh) * | 2019-05-13 | 2022-06-17 | 湖北三江航天红阳机电有限公司 | 一种大尺寸复杂蜂窝夹层结构复合壳片以及整体成型方法 |
| US11383820B2 (en) * | 2019-06-11 | 2022-07-12 | The Boeing Company | Aerodynamic surface lap splice |
| US11352124B2 (en) * | 2019-11-01 | 2022-06-07 | The Boeing Company | Continuous skin leading edge slats |
| US11572152B2 (en) | 2020-05-21 | 2023-02-07 | The Boeing Company | Structural composite airfoils with a single spar, and related methods |
| US11554848B2 (en) * | 2020-05-21 | 2023-01-17 | The Boeing Company | Structural composite airfoils with a single spar, and related methods |
| US11401026B2 (en) | 2020-05-21 | 2022-08-02 | The Boeing Company | Structural composite airfoils with a single spar, and related methods |
| US11453476B2 (en) | 2020-05-21 | 2022-09-27 | The Boeing Company | Structural composite airfoils with an improved leading edge, and related methods |
| CN114771802A (zh) | 2021-01-22 | 2022-07-22 | 波音公司 | 空气动力学结构以及形成空气动力学结构的方法 |
| GB2611298A (en) * | 2021-09-27 | 2023-04-05 | Airbus Operations Ltd | A kit of parts for forming an aerofoil assembly |
| EP4186783B1 (en) * | 2021-11-24 | 2025-01-08 | Airbus Operations, S.L.U. | Manufacturing method of a control surface of an aircraft |
| FR3136506B1 (fr) * | 2022-06-10 | 2025-05-02 | Safran Nacelles | Procédé de réalisation d’un assemblage de pièces pour un ensemble propulsif d’aéronef |
| CN115871956B (zh) * | 2022-11-27 | 2025-12-02 | 中国特种飞行器研究所 | 一种基于等效腔体的漂浮特性试验模型 |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US7909290B2 (en) * | 2005-12-20 | 2011-03-22 | Airbus Operations Limited | Joint for use in aircraft construction |
| CN102007035A (zh) * | 2008-03-25 | 2011-04-06 | 空中客车操作有限公司 | 复合飞行器接头 |
| EP2457822A1 (en) * | 2010-11-30 | 2012-05-30 | Airbus Operations S.L. | Interface arrangement between two components of an aircraft lifting surface using an intermediate part |
| US8444091B2 (en) * | 2008-12-18 | 2013-05-21 | Airbus Operations S.L. | Aircraft stabilizer surface trailing edge |
| EP2334546B1 (fr) * | 2008-09-30 | 2013-05-22 | Airbus Operations | Assemblage de panneaux pour fuselage d'aeronef |
Family Cites Families (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5340280A (en) * | 1991-09-30 | 1994-08-23 | General Electric Company | Dovetail attachment for composite blade and method for making |
| FR2905739B1 (fr) * | 2006-09-08 | 2008-11-07 | Airbus France Sas | Assemblage de panneaux et procede de montage d'un assemblage de panneaux |
| JP4657194B2 (ja) * | 2006-11-20 | 2011-03-23 | 本田技研工業株式会社 | 前縁スキンの段差調整構造および前縁スキンの組付方法 |
| GB0712549D0 (en) * | 2007-06-29 | 2007-08-08 | Airbus Uk Ltd | Improvements in elongate composite structural members |
| GB0712553D0 (en) * | 2007-06-29 | 2007-08-08 | Airbus Uk Ltd | Composite panel stiffener |
| GB0901640D0 (en) * | 2009-02-03 | 2009-03-11 | Airbus Uk Ltd | Joint |
| GB0910938D0 (en) * | 2009-06-25 | 2009-08-05 | Airbus Operations Ltd | Method of manufacturing a structure |
| GB0918750D0 (en) * | 2009-10-27 | 2009-12-09 | Airbus Uk Ltd | Cover trailing edge profile |
| ES2396881B1 (es) * | 2010-11-30 | 2014-01-29 | Airbus Operations, S.L. | Disposición de interfaz entre dos componentes de una estructura de una aeronave usando una pieza de sellado. |
| GB201200912D0 (en) * | 2012-01-19 | 2012-02-29 | Airbus Operations Ltd | Fastener receptacle strip |
-
2014
- 2014-09-17 US US14/488,987 patent/US10329009B2/en active Active
-
2015
- 2015-06-11 JP JP2015118307A patent/JP6644481B2/ja active Active
- 2015-08-25 EP EP15182386.1A patent/EP3000719B1/en active Active
- 2015-09-17 CN CN201510595950.8A patent/CN105438438B/zh active Active
-
2018
- 2018-11-07 US US16/183,243 patent/US10933972B2/en active Active
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US7909290B2 (en) * | 2005-12-20 | 2011-03-22 | Airbus Operations Limited | Joint for use in aircraft construction |
| CN102007035A (zh) * | 2008-03-25 | 2011-04-06 | 空中客车操作有限公司 | 复合飞行器接头 |
| EP2334546B1 (fr) * | 2008-09-30 | 2013-05-22 | Airbus Operations | Assemblage de panneaux pour fuselage d'aeronef |
| US8444091B2 (en) * | 2008-12-18 | 2013-05-21 | Airbus Operations S.L. | Aircraft stabilizer surface trailing edge |
| EP2457822A1 (en) * | 2010-11-30 | 2012-05-30 | Airbus Operations S.L. | Interface arrangement between two components of an aircraft lifting surface using an intermediate part |
Also Published As
| Publication number | Publication date |
|---|---|
| EP3000719A1 (en) | 2016-03-30 |
| JP6644481B2 (ja) | 2020-02-12 |
| US20190071165A1 (en) | 2019-03-07 |
| JP2016175631A (ja) | 2016-10-06 |
| US20160244143A1 (en) | 2016-08-25 |
| US10933972B2 (en) | 2021-03-02 |
| EP3000719B1 (en) | 2020-08-19 |
| CN105438438A (zh) | 2016-03-30 |
| US10329009B2 (en) | 2019-06-25 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| GR01 | Patent grant | ||
| GR01 | Patent grant |