ES2608817T3 - Método de fabricación de largueros conformados de material compuesto - Google Patents
Método de fabricación de largueros conformados de material compuesto Download PDFInfo
- Publication number
- ES2608817T3 ES2608817T3 ES08827299.2T ES08827299T ES2608817T3 ES 2608817 T3 ES2608817 T3 ES 2608817T3 ES 08827299 T ES08827299 T ES 08827299T ES 2608817 T3 ES2608817 T3 ES 2608817T3
- Authority
- ES
- Spain
- Prior art keywords
- stringers
- composite panel
- stringer
- composite
- crossbar
- 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 54
- 238000004519 manufacturing process Methods 0.000 title description 13
- 238000000034 method Methods 0.000 claims abstract description 27
- 238000000576 coating method Methods 0.000 claims abstract description 8
- 239000011248 coating agent Substances 0.000 claims abstract description 7
- 238000000926 separation method Methods 0.000 claims abstract description 7
- 239000000463 material Substances 0.000 claims description 7
- 239000006260 foam Substances 0.000 claims description 3
- 239000010410 layer Substances 0.000 description 17
- 229920005989 resin Polymers 0.000 description 14
- 239000011347 resin Substances 0.000 description 14
- 239000002344 surface layer Substances 0.000 description 10
- 230000007704 transition Effects 0.000 description 8
- 239000002184 metal Substances 0.000 description 7
- 239000011159 matrix material Substances 0.000 description 5
- 239000000835 fiber Substances 0.000 description 4
- 230000001154 acute effect Effects 0.000 description 3
- 238000007596 consolidation process Methods 0.000 description 3
- 239000003822 epoxy resin Substances 0.000 description 3
- 239000004744 fabric Substances 0.000 description 3
- 229920000647 polyepoxide Polymers 0.000 description 3
- 238000007493 shaping process Methods 0.000 description 3
- 238000009825 accumulation Methods 0.000 description 2
- 230000015572 biosynthetic process Effects 0.000 description 2
- 239000011152 fibreglass Substances 0.000 description 2
- 230000003014 reinforcing effect Effects 0.000 description 2
- 229920000049 Carbon (fiber) Polymers 0.000 description 1
- 239000004593 Epoxy Substances 0.000 description 1
- 239000004917 carbon fiber Substances 0.000 description 1
- 238000005056 compaction Methods 0.000 description 1
- -1 delamination Substances 0.000 description 1
- 230000032798 delamination Effects 0.000 description 1
- 238000013461 design Methods 0.000 description 1
- 239000013013 elastic material Substances 0.000 description 1
- 230000002349 favourable effect Effects 0.000 description 1
- 239000000945 filler Substances 0.000 description 1
- LNEPOXFFQSENCJ-UHFFFAOYSA-N haloperidol Chemical compound C1CC(O)(C=2C=CC(Cl)=CC=2)CCN1CCCC(=O)C1=CC=C(F)C=C1 LNEPOXFFQSENCJ-UHFFFAOYSA-N 0.000 description 1
- 238000003475 lamination Methods 0.000 description 1
- 239000004620 low density foam Substances 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
- 239000007769 metal material Substances 0.000 description 1
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 239000002245 particle Substances 0.000 description 1
- 230000000704 physical effect Effects 0.000 description 1
- 239000000843 powder Substances 0.000 description 1
- 238000003825 pressing Methods 0.000 description 1
- 230000002787 reinforcement Effects 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 239000013585 weight reducing agent Substances 0.000 description 1
- 239000002759 woven fabric Substances 0.000 description 1
- 230000037303 wrinkles Effects 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
- B29C43/00—Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor
- B29C43/02—Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor of articles of definite length, i.e. discrete articles
- B29C43/10—Isostatic pressing, i.e. using non-rigid pressure-exerting members against rigid parts or dies
-
- 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
- B29C70/34—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 and shaping or impregnating by compression, i.e. combined with compressing after the lay-up operation
- B29C70/342—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 and shaping or impregnating by compression, i.e. combined with compressing after the lay-up operation using isostatic pressure
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29D—PRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCES IN A PLASTIC STATE
- B29D99/00—Subject matter not provided for in other groups of this subclass
- B29D99/001—Producing wall or panel-like structures, e.g. for hulls, fuselages, or buildings
- B29D99/0014—Producing wall or panel-like structures, e.g. for hulls, fuselages, or buildings provided with ridges or ribs, e.g. joined ribs
-
- 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
- B64C1/064—Stringers; Longerons
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/18—Spars; Ribs; Stringers
- B64C3/182—Stringers, longerons
-
- 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
- B29C43/00—Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor
- B29C43/32—Component parts, details or accessories; Auxiliary operations
- B29C43/36—Moulds for making articles of definite length, i.e. discrete articles
- B29C43/3642—Bags, bleeder sheets or cauls for isostatic pressing
- B29C2043/3649—Inflatable bladders using gas or fluid and related details
-
- 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
- B29L2022/00—Hollow articles
-
- 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
- B29L2031/54—Balls
-
- 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
-
- 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T156/00—Adhesive bonding and miscellaneous chemical manufacture
- Y10T156/10—Methods of surface bonding and/or assembly therefor
- Y10T156/1002—Methods of surface bonding and/or assembly therefor with permanent bending or reshaping or surface deformation of self sustaining lamina
- Y10T156/1028—Methods of surface bonding and/or assembly therefor with permanent bending or reshaping or surface deformation of self sustaining lamina by bending, drawing or stretch forming sheet to assume shape of configured lamina while in contact therewith
-
- 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/31504—Composite [nonstructural laminate]
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Composite Materials (AREA)
- Architecture (AREA)
- Civil Engineering (AREA)
- Structural Engineering (AREA)
- Moulding By Coating Moulds (AREA)
- Casting Or Compression Moulding Of Plastics Or The Like (AREA)
- Laminated Bodies (AREA)
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US753482 | 2007-05-24 | ||
| US11/753,482 US7861969B2 (en) | 2007-05-24 | 2007-05-24 | Shaped composite stringers and methods of making |
| PCT/US2008/064427 WO2009023346A2 (en) | 2007-05-24 | 2008-05-21 | Shaped composite stringers and methods of making |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| ES2608817T3 true ES2608817T3 (es) | 2017-04-17 |
Family
ID=40071512
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| ES08827299.2T Active ES2608817T3 (es) | 2007-05-24 | 2008-05-21 | Método de fabricación de largueros conformados de material compuesto |
Country Status (6)
| Country | Link |
|---|---|
| US (2) | US7861969B2 (cg-RX-API-DMAC7.html) |
| EP (1) | EP2152574B1 (cg-RX-API-DMAC7.html) |
| JP (1) | JP2010527836A (cg-RX-API-DMAC7.html) |
| CN (1) | CN101678890B (cg-RX-API-DMAC7.html) |
| ES (1) | ES2608817T3 (cg-RX-API-DMAC7.html) |
| WO (1) | WO2009023346A2 (cg-RX-API-DMAC7.html) |
Families Citing this family (104)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2888816B1 (fr) * | 2005-07-20 | 2007-08-31 | Airbus France Sas | Panneau auto-raidi monolithique |
| DE102006002248B4 (de) * | 2006-01-17 | 2008-01-03 | Airbus Deutschland Gmbh | Strukturgebende Konstruktion für einen Flugzeugrumpf |
| GB0611875D0 (en) * | 2006-06-15 | 2006-07-26 | Airbus Uk Ltd | A stringer for an aircraft wing and a method of forming thereof |
| US7861969B2 (en) | 2007-05-24 | 2011-01-04 | The Boeing Company | Shaped composite stringers and methods of making |
| US20080302912A1 (en) * | 2007-06-08 | 2008-12-11 | The Boeing Company | Bladderless Mold Line Conformal Hat Stringer |
| US8043554B2 (en) * | 2007-06-08 | 2011-10-25 | The Boeing Company | Manufacturing process using bladderless mold line conformal hat stringer |
| US7879276B2 (en) | 2007-11-08 | 2011-02-01 | The Boeing Company | Foam stiffened hollow composite stringer |
| US8100361B2 (en) * | 2007-12-20 | 2012-01-24 | Airbus Deutschland Gmbh | Hull structure |
| US20110186580A1 (en) * | 2008-03-03 | 2011-08-04 | Samsung Heavy Ind. Co., Ltd. | Reinforcing member for corrugated membrane of lng cargo tank, membrane assembly having the reinforcing member and method for constructing the same |
| ES2352941B1 (es) * | 2008-05-16 | 2012-01-25 | Airbus Operations, S.L. | Estructura integrada de aeronave en material compuesto |
| DE102008002117B4 (de) * | 2008-05-30 | 2013-10-31 | Airbus Operations Gmbh | Verbund und Struktur |
| US9327467B2 (en) * | 2008-07-10 | 2016-05-03 | The Boeing Company | Composite mandrel for autoclave curing applications |
| US9238335B2 (en) * | 2008-07-10 | 2016-01-19 | The Boeing Company | Mandrel for autoclave curing applications |
| GB0813584D0 (en) * | 2008-07-25 | 2008-09-03 | Airbus Uk Ltd | Method of stiffening a rib |
| US8540921B2 (en) | 2008-11-25 | 2013-09-24 | The Boeing Company | Method of forming a reinforced foam-filled composite stringer |
| FR2940176B1 (fr) * | 2008-12-22 | 2011-02-11 | Aircelle Sa | Procede de fabrication d'un panneau d'attenuation acoustique, notamment pour l'aeronautique |
| US9352533B2 (en) * | 2009-01-29 | 2016-05-31 | The Boeing Company | Elastomeric riblets |
| US8678316B2 (en) * | 2009-01-29 | 2014-03-25 | The Boeing Company | Amorphous metal riblets |
| US8668166B2 (en) * | 2009-01-29 | 2014-03-11 | The Boeing Company | Shape memory riblets |
| US8684310B2 (en) * | 2009-01-29 | 2014-04-01 | The Boeing Company | Rigid tipped riblets |
| US8074694B2 (en) | 2009-05-28 | 2011-12-13 | The Boeing Company | Stringer transition method |
| 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 |
| US8617687B2 (en) * | 2009-08-03 | 2013-12-31 | The Boeing Company | Multi-functional aircraft structures |
| CN102019592B (zh) * | 2009-09-10 | 2012-07-04 | 中国航空工业集团公司北京航空制造工程研究所 | 一种大尺寸复合材料加筋壁板成形的定位装置 |
| US8413928B2 (en) * | 2009-09-25 | 2013-04-09 | The Boeing Company | Structurally designed aerodynamic riblets |
| US8733702B1 (en) * | 2009-12-02 | 2014-05-27 | The Boeing Company | Reduced solar absorptivity applique |
| US8714485B2 (en) | 2009-12-15 | 2014-05-06 | The Boeing Company | Method of fabricating a hat stringer |
| US9010689B1 (en) | 2010-01-04 | 2015-04-21 | The Boeing Company | Fluid dynamic vent dam |
| CN101791821B (zh) * | 2010-04-08 | 2011-09-14 | 中国航空工业集团公司北京航空制造工程研究所 | 一种大尺寸复合材料长桁的成形装置 |
| DE102010018726B4 (de) * | 2010-04-29 | 2013-08-14 | Premium Aerotec Gmbh | Verfahren zur Herstellung eines mit zumindest einem Hohlprofil versehenen Bauteils |
| US8408493B2 (en) * | 2010-05-19 | 2013-04-02 | The Boeing Company | Composite stringer end trim |
| US9682762B1 (en) * | 2010-05-20 | 2017-06-20 | The Boeing Company | Stiffener with shaped end termination |
| US20120012242A1 (en) * | 2010-07-14 | 2012-01-19 | Spirit Aerosystems, Inc. | Method and system for material placement over radiused edges |
| FR2963272B1 (fr) * | 2010-07-29 | 2012-08-17 | Airbus Operations Sas | Procede de fabrication d'un panneau raidi en materiau composite |
| US8795567B2 (en) * | 2010-09-23 | 2014-08-05 | The Boeing Company | Method for fabricating highly contoured composite stiffeners with reduced wrinkling |
| CN102139533A (zh) * | 2011-03-14 | 2011-08-03 | 沈阳飞机工业(集团)有限公司 | 复合材料ω长桁与壁板共固化组合工装 |
| WO2012137310A1 (ja) | 2011-04-05 | 2012-10-11 | 三菱重工業株式会社 | 再生エネルギー型発電装置及び油圧ポンプの取付け方法 |
| DE102011017460A1 (de) | 2011-04-20 | 2012-10-25 | Airbus Operations Gmbh | Faserverbundbauteil, Flügelspitzenverlängerung und Flugzeug mit einem Faserverbundteil |
| US8651419B2 (en) * | 2011-07-18 | 2014-02-18 | The Boeing Company | Flexible truss frame and method of making the same |
| US9931807B2 (en) | 2011-08-08 | 2018-04-03 | The Boeing Company | Flexible compactor with reinforcing spine |
| US8997642B2 (en) | 2011-08-08 | 2015-04-07 | The Boeing Company | Method for transporting, placing and compacting composite stiffeners |
| FR2985213B1 (fr) * | 2011-12-28 | 2016-12-30 | Airbus Operations Sas | Panneau composite auto-raidi et procede de realisation |
| US8703269B2 (en) | 2012-02-14 | 2014-04-22 | Gulfstream Aerospace Corporation | Reinforced composite structures for aircrafts and methods for making the same |
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| US20130299073A1 (en) * | 2012-05-08 | 2013-11-14 | Lockheed Martin Corporation | Contour caul with expansion region |
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| FR2991228B1 (fr) | 2012-05-29 | 2015-03-06 | Airbus Operations Sas | Procede et dispositif de realisation d'un panneau composite auto-raidi |
| GB201217245D0 (en) * | 2012-09-27 | 2012-11-07 | Airbus Operations Ltd | A cure tool |
| US9333713B2 (en) | 2012-10-04 | 2016-05-10 | The Boeing Company | Method for co-curing composite skins and stiffeners in an autoclave |
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| US9162396B2 (en) * | 2012-10-12 | 2015-10-20 | The Boeing Company | Method for forming fuselage stringers |
| FR2999970B1 (fr) | 2012-12-20 | 2015-06-19 | Airbus Operations Sas | Procede de realisation d'une preforme textile a fibres continues par circulation d'un flux de gaz chaud a travers un ensemble fibreux |
| 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 |
| US8906179B2 (en) | 2013-02-21 | 2014-12-09 | The Boeing Company | Systems, tools, and methods for forming composite tubular stringers and stiffened composite structures having composite tubular stringers |
| US9272767B2 (en) | 2013-04-19 | 2016-03-01 | The Boeing Company | Compacting uncured composite members on contoured mandrel surfaces |
| US9395339B2 (en) * | 2013-08-26 | 2016-07-19 | The Boeing Comapany | Apparatus for non-destructive inspection of stringers |
| US9475569B2 (en) | 2013-10-29 | 2016-10-25 | Gulfstream Aerospace Corporation | Methods for manufacturing an i-stringer of an aircraft and devices for use in such methods |
| FR3015433B1 (fr) | 2013-12-23 | 2016-02-12 | Airbus Operations Sas | Ensemble pour aeronef comprenant un mat d'accrochage integre a la nacelle et agence en partie arriere du fuselage |
| EP2889211B1 (en) * | 2013-12-31 | 2018-10-24 | Airbus Operations S.L. | Aircraft structure made of composite material |
| EP3113936A1 (en) | 2014-03-04 | 2017-01-11 | Bombardier Inc. | Method and apparatus for forming a composite laminate stack using a breathable polyethylene vacuum film |
| US9828164B2 (en) | 2014-05-22 | 2017-11-28 | Fontaine Engineered Products, Inc. | Intermodal container and method of constructing same |
| CN104029397B (zh) * | 2014-06-09 | 2016-08-17 | 中航复合材料有限责任公司 | 一种飞机复合材料机身壁板的制备装置及制备方法 |
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| JP6444157B2 (ja) * | 2014-12-15 | 2018-12-26 | 三菱重工業株式会社 | 複合構造体の成形方法 |
| US9919791B2 (en) * | 2015-04-15 | 2018-03-20 | Gulfstream Aerospace Corporation | Stiffening structures, wing structures, and methods for manufacturing stiffening structures |
| US10456960B2 (en) | 2015-07-24 | 2019-10-29 | The Boeing Company | Systems and methods for incrementally forming a composite part |
| US9809297B2 (en) * | 2015-08-26 | 2017-11-07 | The Boeing Company | Structures containing stiffeners having transition portions |
| US11426971B2 (en) | 2015-10-13 | 2022-08-30 | The Boeing Company | Composite structure and method for barely visible impact damage detection |
| US10427778B2 (en) * | 2016-03-14 | 2019-10-01 | The Boeing Company | Heat shield assembly and method |
| US10105940B2 (en) * | 2016-04-18 | 2018-10-23 | The Boeing Company | Formation of composite laminates having one or more divergent flanges |
| US10259176B2 (en) * | 2016-08-03 | 2019-04-16 | The Boeing Company | System and method associated with drape forming |
| ES2887428T3 (es) * | 2016-11-16 | 2021-12-22 | Airbus Operations Gmbh | Componente de estructura de aeronave para un flujo laminar |
| CN106769533B (zh) * | 2016-11-29 | 2019-08-23 | 中国航空工业集团公司沈阳飞机设计研究所 | 一种复合材料隔框结构四点弯曲试验方法 |
| EP3378788B1 (en) * | 2017-03-22 | 2021-04-28 | AIRBUS HELICOPTERS DEUTSCHLAND GmbH | An aircraft with a fuselage that comprises at least one hollow beam element |
| CN110891752A (zh) * | 2017-07-25 | 2020-03-17 | 株式会社斯巴鲁 | 复合材料成形夹具及复合材料成形方法 |
| US10875625B2 (en) * | 2017-08-23 | 2020-12-29 | The Boeing Company | Co-cured spar and stringer center wing box |
| US11034431B2 (en) * | 2017-09-25 | 2021-06-15 | The Boeing Company | Composite article with fly-away bag carrier |
| US11014644B2 (en) | 2017-10-25 | 2021-05-25 | The Boeing Company | Stiffened-cavity for modular wrap ply assembly for hat stringer |
| FR3076261B1 (fr) * | 2018-01-02 | 2021-04-23 | Stelia Aerospace | Coque de siege autoraidie et methode de realisation |
| US10669005B2 (en) * | 2018-02-27 | 2020-06-02 | The Boeing Company | Solid laminate stringer |
| GB2575102A (en) * | 2018-06-29 | 2020-01-01 | Airbus Operations Ltd | Duct stringer with bulkhead |
| US11180238B2 (en) * | 2018-11-19 | 2021-11-23 | The Boeing Company | Shear ties for aircraft wing |
| JP7161399B2 (ja) * | 2018-12-28 | 2022-10-26 | 株式会社Subaru | 樹脂含浸測定装置 |
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| JP2010527836A (ja) | 2010-08-19 |
| WO2009023346A2 (en) | 2009-02-19 |
| CN101678890B (zh) | 2013-01-16 |
| US7861969B2 (en) | 2011-01-04 |
| CN101678890A (zh) | 2010-03-24 |
| EP2152574B1 (en) | 2016-12-07 |
| EP2152574A2 (en) | 2010-02-17 |
| US8377247B2 (en) | 2013-02-19 |
| US20110088833A1 (en) | 2011-04-21 |
| US20080290214A1 (en) | 2008-11-27 |
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