CN102530234B - 使用多功能顶端的机身及其制造方法 - Google Patents
使用多功能顶端的机身及其制造方法 Download PDFInfo
- Publication number
- CN102530234B CN102530234B CN201110365139.2A CN201110365139A CN102530234B CN 102530234 B CN102530234 B CN 102530234B CN 201110365139 A CN201110365139 A CN 201110365139A CN 102530234 B CN102530234 B CN 102530234B
- Authority
- CN
- China
- Prior art keywords
- frame component
- fuselage
- main body
- upswept frame
- upswept
- 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
- 238000004519 manufacturing process Methods 0.000 title claims description 30
- 238000009432 framing Methods 0.000 claims description 51
- 239000002131 composite material Substances 0.000 claims description 39
- 238000000034 method Methods 0.000 claims description 28
- 150000001875 compounds Chemical class 0.000 claims description 21
- 238000009826 distribution Methods 0.000 claims description 16
- 238000004891 communication Methods 0.000 claims description 10
- 239000004616 structural foam Substances 0.000 claims description 9
- 230000007613 environmental effect Effects 0.000 claims description 8
- 239000000463 material Substances 0.000 claims description 8
- 238000005728 strengthening Methods 0.000 claims description 6
- 241001468684 Diplocardia Species 0.000 claims description 4
- 230000003292 diminished effect Effects 0.000 claims description 2
- 239000003351 stiffener Substances 0.000 description 12
- 238000012544 monitoring process Methods 0.000 description 6
- 239000000835 fiber Substances 0.000 description 5
- 239000010410 layer Substances 0.000 description 5
- 238000005516 engineering process Methods 0.000 description 4
- 239000007787 solid Substances 0.000 description 4
- 238000007711 solidification Methods 0.000 description 4
- 230000008023 solidification Effects 0.000 description 4
- 239000000758 substrate Substances 0.000 description 4
- 230000005540 biological transmission Effects 0.000 description 3
- 238000013461 design Methods 0.000 description 3
- 238000010586 diagram Methods 0.000 description 3
- 238000003825 pressing Methods 0.000 description 3
- 230000000712 assembly Effects 0.000 description 2
- 238000000429 assembly Methods 0.000 description 2
- 238000010276 construction Methods 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 230000006872 improvement Effects 0.000 description 2
- 238000012423 maintenance Methods 0.000 description 2
- 229920005989 resin Polymers 0.000 description 2
- 239000011347 resin Substances 0.000 description 2
- 239000002356 single layer Substances 0.000 description 2
- 238000004458 analytical method Methods 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 230000001413 cellular effect Effects 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- 239000003822 epoxy resin Substances 0.000 description 1
- 238000011156 evaluation Methods 0.000 description 1
- 239000006260 foam Substances 0.000 description 1
- 230000010354 integration Effects 0.000 description 1
- 238000005304 joining Methods 0.000 description 1
- 230000013011 mating Effects 0.000 description 1
- 230000007246 mechanism Effects 0.000 description 1
- 230000008520 organization Effects 0.000 description 1
- 230000010412 perfusion Effects 0.000 description 1
- 239000011120 plywood Substances 0.000 description 1
- 229920000647 polyepoxide Polymers 0.000 description 1
- 230000008569 process Effects 0.000 description 1
- 238000012545 processing Methods 0.000 description 1
- 230000002787 reinforcement Effects 0.000 description 1
- 230000003014 reinforcing effect Effects 0.000 description 1
- 238000009418 renovation Methods 0.000 description 1
- 238000007493 shaping process Methods 0.000 description 1
- 238000012546 transfer Methods 0.000 description 1
- 238000009461 vacuum packaging Methods 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
- B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
- B29C70/28—Shaping operations therefor
- B29C70/30—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
- B64C1/068—Fuselage sections
-
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
- B29L2031/00—Other particular articles
- B29L2031/30—Vehicles, e.g. ships or aircraft, or body parts thereof
- B29L2031/3076—Aircrafts
- B29L2031/3082—Fuselages
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C2001/0054—Fuselage structures substantially made from particular materials
- B64C2001/0072—Fuselage structures substantially made from particular materials from composite materials
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/40—Weight reduction
Landscapes
- Engineering & Computer Science (AREA)
- Manufacturing & Machinery (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Transportation (AREA)
- Chemical & Material Sciences (AREA)
- Composite Materials (AREA)
- Moulding By Coating Moulds (AREA)
- Tents Or Canopies (AREA)
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US12/944,113 | 2010-11-11 | ||
| US12/944,113 US8752791B2 (en) | 2010-11-11 | 2010-11-11 | Fuselage employing multifunctional crown and method of making the same |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN102530234A CN102530234A (zh) | 2012-07-04 |
| CN102530234B true CN102530234B (zh) | 2015-04-29 |
Family
ID=44905700
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201110365139.2A Active CN102530234B (zh) | 2010-11-11 | 2011-11-11 | 使用多功能顶端的机身及其制造方法 |
Country Status (4)
| Country | Link |
|---|---|
| US (1) | US8752791B2 (enExample) |
| EP (1) | EP2452872B1 (enExample) |
| JP (1) | JP6039175B2 (enExample) |
| CN (1) | CN102530234B (enExample) |
Families Citing this family (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE102007050422B4 (de) * | 2007-10-22 | 2012-03-08 | Airbus Operations Gmbh | Flugzeugkomponentenmontagesystem |
| USD732459S1 (en) * | 2013-05-21 | 2015-06-23 | Airbus Corporate Jet Centre | Aircraft cabin |
| PL2979975T3 (pl) * | 2014-07-30 | 2018-01-31 | Airbus Helicopters Deutschland GmbH | Statek powietrzny ze strukturą ramową, która zawiera co najmniej jedną pustą ramę |
| EP3508430A1 (en) * | 2015-03-23 | 2019-07-10 | Bombardier Inc. | Simulation of loads on aerostructures during aircraft assembly |
| WO2018061281A1 (ja) | 2016-09-29 | 2018-04-05 | 株式会社Ｓｕｂａｒｕ | 複合材構造体及び複合材構造体の製造方法 |
| CN106596003B (zh) * | 2016-11-29 | 2019-04-23 | 中国航空工业集团公司沈阳飞机设计研究所 | 一种复合材料飞机机身段充压试验方法 |
| DE102017112594A1 (de) * | 2017-06-08 | 2018-12-13 | Airbus Operations Gmbh | Luftverteilungssystem für eine Flugzeugkabine |
| US11220353B2 (en) * | 2019-04-18 | 2022-01-11 | The Boeing Company | Method of fabricating a composite structure |
| US11866200B2 (en) * | 2020-11-18 | 2024-01-09 | The Boeing Company | Pulsed line fabrication for a fuselage using work stations |
| US11872780B2 (en) | 2022-06-02 | 2024-01-16 | The Boeing Company | Methods and tool for cutting an uncured composite material |
| DE102022133280A1 (de) * | 2022-12-14 | 2024-06-20 | Airbus Operations Gmbh | Bauteil mit Hohlleiter, Datenübertragungssystem und Luftfahrzeug |
Citations (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| USD539210S1 (en) * | 2005-04-28 | 2007-03-27 | The Boeing Company | Modular archway for an aircraft |
| CN101631715A (zh) * | 2007-01-23 | 2010-01-20 | 空中客车德国有限公司 | 具有金属框架的crp/金属复合结构的飞机或飞船机身 |
Family Cites Families (23)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH04329125A (ja) * | 1991-04-30 | 1992-11-17 | Mitsubishi Heavy Ind Ltd | 複合材料一体成形方法 |
| JPH1016085A (ja) * | 1996-07-04 | 1998-01-20 | Mitsubishi Heavy Ind Ltd | 航空機の胴体外板の製造方法 |
| JP4318381B2 (ja) * | 2000-04-27 | 2009-08-19 | 本田技研工業株式会社 | 繊維強化複合材からなる胴体構造体の製造方法、及びそれにより製造される胴体構造体 |
| DE10154063B4 (de) * | 2001-11-02 | 2013-11-28 | Airbus Operations Gmbh | Doppelwandiger Kernverbund, vorzugsweise Faserverbund |
| US7380752B2 (en) * | 2003-10-17 | 2008-06-03 | The Boeing Company | Aircraft interior architecture |
| US7252267B2 (en) * | 2003-10-17 | 2007-08-07 | The Boeing Company | Aircraft archway architecture |
| US7228611B2 (en) * | 2003-11-18 | 2007-06-12 | The Boeing Company | Method of transferring large uncured composite laminates |
| US7166251B2 (en) * | 2004-12-01 | 2007-01-23 | The Boeing Company | Segmented flexible barrel lay-up mandrel |
| JP4800672B2 (ja) * | 2005-06-09 | 2011-10-26 | 株式会社竹中工務店 | 経路構造 |
| DE102005043898A1 (de) * | 2005-09-14 | 2007-03-22 | Airbus Deutschland Gmbh | Fenster-Anordnung zum Einrichten größerer Flugzeugfenster |
| US9359061B2 (en) * | 2005-10-31 | 2016-06-07 | The Boeing Company | Compliant stiffener for aircraft fuselage |
| DE102005054869A1 (de) * | 2005-11-17 | 2007-05-31 | Airbus Deutschland Gmbh | Verfahren zur Herstellung einer Rumpfzelle eines Luftfahrzeugs |
| DE102006002248B4 (de) * | 2006-01-17 | 2008-01-03 | Airbus Deutschland Gmbh | Strukturgebende Konstruktion für einen Flugzeugrumpf |
| JP2008028549A (ja) * | 2006-07-19 | 2008-02-07 | Taisei Corp | 通信波搬送導波管 |
| DE102006039292B4 (de) * | 2006-08-22 | 2010-07-22 | Airbus Deutschland Gmbh | Rahmenelement, Flugzeugklimatisierungssystem sowie Verfahren zur Montage eines Rahmenelements in einem Flugzeug |
| US7861970B2 (en) | 2006-11-02 | 2011-01-04 | The Boeing Company | Fuselage structure including an integrated fuselage stanchion |
| US7735779B2 (en) * | 2006-11-02 | 2010-06-15 | The Boeing Company | Optimized fuselage structure |
| DE102007049926A1 (de) * | 2007-10-18 | 2009-04-23 | Airbus Deutschland Gmbh | System und Verfahren zur Klimatisierung zumindest eines Teilbereichs eines Flugzeugs |
| US7879276B2 (en) * | 2007-11-08 | 2011-02-01 | The Boeing Company | Foam stiffened hollow composite stringer |
| US8040243B2 (en) | 2008-11-18 | 2011-10-18 | The Boeing Company | RFID-based corrosion and moisture detection |
| US8421692B2 (en) * | 2009-02-25 | 2013-04-16 | The Boeing Company | Transmitting power and data |
| US8500066B2 (en) * | 2009-06-12 | 2013-08-06 | The Boeing Company | Method and apparatus for wireless aircraft communications and power system using fuselage stringers |
| US8570152B2 (en) * | 2009-07-23 | 2013-10-29 | The Boeing Company | Method and apparatus for wireless sensing with power harvesting of a wireless signal |
-
2010
- 2010-11-11 US US12/944,113 patent/US8752791B2/en active Active
-
2011
- 2011-11-04 EP EP11187923.5A patent/EP2452872B1/en active Active
- 2011-11-09 JP JP2011245427A patent/JP6039175B2/ja active Active
- 2011-11-11 CN CN201110365139.2A patent/CN102530234B/zh active Active
Patent Citations (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| USD539210S1 (en) * | 2005-04-28 | 2007-03-27 | The Boeing Company | Modular archway for an aircraft |
| CN101631715A (zh) * | 2007-01-23 | 2010-01-20 | 空中客车德国有限公司 | 具有金属框架的crp/金属复合结构的飞机或飞船机身 |
Also Published As
| Publication number | Publication date |
|---|---|
| US8752791B2 (en) | 2014-06-17 |
| EP2452872B1 (en) | 2019-08-28 |
| CN102530234A (zh) | 2012-07-04 |
| JP6039175B2 (ja) | 2016-12-07 |
| JP2012101787A (ja) | 2012-05-31 |
| US20120119028A1 (en) | 2012-05-17 |
| EP2452872A3 (en) | 2017-10-04 |
| EP2452872A2 (en) | 2012-05-16 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN102530234B (zh) | 使用多功能顶端的机身及其制造方法 | |
| JP5548192B2 (ja) | 強化補強材を作製する方法 | |
| RU2466905C2 (ru) | Элемент обшивки как часть фюзеляжа самолета | |
| KR101837217B1 (ko) | 일체화된 보강부재를 갖는 복합 구조물 그 제조 방법 | |
| KR102067291B1 (ko) | 접착식 복합 에어포일 및 이의 제작 방법 | |
| EP2605902B1 (en) | Composite structures having composite-to-metal joints and method for making the same | |
| RU2602100C2 (ru) | Структура самолета для обеспечения высокой устойчивости к оттягиванию композитного стрингера | |
| US7597953B2 (en) | Composite fiber component produced by braiding | |
| AU2016201021B2 (en) | Conformal composite antenna assembly | |
| US8939406B2 (en) | Joining composite fuselage sections along window belts | |
| CN213832083U (zh) | 一种共固化复合材料无人机机身 | |
| CN102514708B (zh) | 一种整体式复合材料中央翼盒 | |
| KR101484203B1 (ko) | 섬유 강화 수지 차체 구조체 및 그 제조방법 | |
| KR20150053222A (ko) | 기하학적 형상의 필러 소재를 가지는 라미네이트 복합체 방사상의 필러 및 그의 형성 방법 | |
| US20160368586A1 (en) | Production method for producing a load-bearing fuselage panel and fuselage panel producible therewith | |
| US20110217510A1 (en) | Reinforced aircraft fuselage panel and method of manufacture | |
| US8973870B2 (en) | Wall component for an aircraft | |
| CN206765397U (zh) | 一种纤维增强复合舱板 | |
| CN116280272B (zh) | 一体化纤维复合材料姿控舱 | |
| CN219487727U (zh) | 一体化纤维复合材料姿控舱 | |
| CN206889425U (zh) | 蜂窝夹层结构等强度连接结构 | |
| US11267584B2 (en) | Method for manufacturing a rear section of an aircraft and aircraft rear section | |
| CN114193990A (zh) | 机臂以及飞行汽车 | |
| CN113524808A (zh) | 飞行汽车地板及其制备方法和飞行汽车 | |
| US20030057603A1 (en) | Supporting arm of a passenger door of an aircraft |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant |