WO2011073573A3 - Procédé de fabrication d'un panneau composite de bord de fuite pour un élément d ' aéronef - Google Patents
Procédé de fabrication d'un panneau composite de bord de fuite pour un élément d ' aéronef Download PDFInfo
- Publication number
- WO2011073573A3 WO2011073573A3 PCT/FR2010/052729 FR2010052729W WO2011073573A3 WO 2011073573 A3 WO2011073573 A3 WO 2011073573A3 FR 2010052729 W FR2010052729 W FR 2010052729W WO 2011073573 A3 WO2011073573 A3 WO 2011073573A3
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- trailing edge
- production
- edge panel
- aircraft element
- composite trailing
- Prior art date
Links
Classifications
-
- 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
- B29D99/0025—Producing blades or the like, e.g. blades for turbines, propellers, or wings
- B29D99/0028—Producing blades or the like, e.g. blades for turbines, propellers, or wings hollow blades
-
- 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
- B29C70/302—Details of the edges of fibre composites, e.g. edge finishing or means to avoid delamination
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/18—Spars; Ribs; Stringers
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/20—Integral or sandwich constructions
-
- 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
- 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
- B29L2031/3085—Wings
-
- 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
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49616—Structural member making
- Y10T29/49622—Vehicular structural member making
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Composite Materials (AREA)
- Moulding By Coating Moulds (AREA)
- Laminated Bodies (AREA)
- Casting Or Compression Moulding Of Plastics Or The Like (AREA)
Abstract
Priority Applications (6)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
BR112012011517A BR112012011517A2 (pt) | 2009-12-18 | 2010-12-14 | método para a produção de um painel de borda lateral de compósito para um elemento de aeronaves |
RU2012129704/11A RU2012129704A (ru) | 2009-12-18 | 2010-12-14 | Способ изготовления композитной панели задней кромки элемента летательного аппарата |
CN2010800576976A CN102656085A (zh) | 2009-12-18 | 2010-12-14 | 用于生产飞行器元件的复合后缘板的方法 |
US13/516,770 US20120267479A1 (en) | 2009-12-18 | 2010-12-14 | Method for the production of a composite trailing edge panel for an aircraft element |
CA2782708A CA2782708A1 (fr) | 2009-12-18 | 2010-12-14 | Panneau structurant composite de bord de fuite pour un element d'un aeronef |
EP10805808A EP2512915A2 (fr) | 2009-12-18 | 2010-12-14 | Procédé de fabrication d'un panneau de composite de bord de fuite pour un élément d'aéronef |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0906157A FR2954269B1 (fr) | 2009-12-18 | 2009-12-18 | Pannneau structurant composite de bord de fuite pour element d'aeronef |
FR09/06157 | 2009-12-18 |
Publications (2)
Publication Number | Publication Date |
---|---|
WO2011073573A2 WO2011073573A2 (fr) | 2011-06-23 |
WO2011073573A3 true WO2011073573A3 (fr) | 2011-08-11 |
Family
ID=42352157
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/FR2010/052729 WO2011073573A2 (fr) | 2009-12-18 | 2010-12-14 | Panneau structurant composite de bord de fuite pour un élément d'un aéronef |
Country Status (8)
Country | Link |
---|---|
US (1) | US20120267479A1 (fr) |
EP (1) | EP2512915A2 (fr) |
CN (1) | CN102656085A (fr) |
BR (1) | BR112012011517A2 (fr) |
CA (1) | CA2782708A1 (fr) |
FR (1) | FR2954269B1 (fr) |
RU (1) | RU2012129704A (fr) |
WO (1) | WO2011073573A2 (fr) |
Families Citing this family (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB201120707D0 (en) | 2011-12-01 | 2012-01-11 | Airbus Operations Ltd | Leading edge structure |
CN110667821B (zh) * | 2019-10-25 | 2023-10-20 | 中航西飞民用飞机有限责任公司 | 一种飞机机翼后缘复合材料隔框结构及其制作方法 |
EP3835038B1 (fr) | 2019-12-11 | 2023-05-10 | Airbus Operations, S.L.U. | Bord de fuite pour une surface de levage intégrée multilongerons composite et procédé de fabrication dudit bord de fuite |
CN114919210A (zh) * | 2022-04-22 | 2022-08-19 | 南京聚隆复合材料技术有限公司 | 一种复合材料机翼骨架的成型方法 |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3219123A (en) * | 1963-03-29 | 1965-11-23 | Bolkow Gmbh | Airfoil construction and method of making an airfoil |
DE1275279B (de) * | 1965-10-06 | 1968-08-14 | Boelkow Gmbh | Verfahren zum Herstellen eines Verbundbauteils aus glasfaserverstaerktem Kunststoff |
US5332178A (en) * | 1992-06-05 | 1994-07-26 | Williams International Corporation | Composite wing and manufacturing process thereof |
US20010017336A1 (en) * | 1998-07-30 | 2001-08-30 | Makoto Hirahara | Composite airfoil structures and their forming methods |
DE102008013759A1 (de) * | 2008-03-12 | 2009-09-17 | Airbus Deutschland Gmbh | Verfahren zur Herstellung eines integralen Faserverbundbauteils sowie Kernform zur Durchführung des Verfahrens |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR902579A (fr) | 1943-03-17 | 1945-09-04 | Licentia Gmbh | Amplificateur à quatre fils pour systèmes à fréquences porteuses |
US7681835B2 (en) * | 1999-11-18 | 2010-03-23 | Rocky Mountain Composites, Inc. | Single piece co-cure composite wing |
US6889937B2 (en) * | 1999-11-18 | 2005-05-10 | Rocky Mountain Composites, Inc. | Single piece co-cure composite wing |
EP1764307A1 (fr) * | 2005-09-14 | 2007-03-21 | EADS Construcciones Aeronauticas, S.A. | Procédé de fabrication d'un bord d'attaque monolithique |
-
2009
- 2009-12-18 FR FR0906157A patent/FR2954269B1/fr active Active
-
2010
- 2010-12-14 BR BR112012011517A patent/BR112012011517A2/pt not_active Application Discontinuation
- 2010-12-14 CN CN2010800576976A patent/CN102656085A/zh active Pending
- 2010-12-14 RU RU2012129704/11A patent/RU2012129704A/ru not_active Application Discontinuation
- 2010-12-14 WO PCT/FR2010/052729 patent/WO2011073573A2/fr active Application Filing
- 2010-12-14 EP EP10805808A patent/EP2512915A2/fr not_active Withdrawn
- 2010-12-14 CA CA2782708A patent/CA2782708A1/fr not_active Abandoned
- 2010-12-14 US US13/516,770 patent/US20120267479A1/en not_active Abandoned
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3219123A (en) * | 1963-03-29 | 1965-11-23 | Bolkow Gmbh | Airfoil construction and method of making an airfoil |
DE1275279B (de) * | 1965-10-06 | 1968-08-14 | Boelkow Gmbh | Verfahren zum Herstellen eines Verbundbauteils aus glasfaserverstaerktem Kunststoff |
US5332178A (en) * | 1992-06-05 | 1994-07-26 | Williams International Corporation | Composite wing and manufacturing process thereof |
US20010017336A1 (en) * | 1998-07-30 | 2001-08-30 | Makoto Hirahara | Composite airfoil structures and their forming methods |
DE102008013759A1 (de) * | 2008-03-12 | 2009-09-17 | Airbus Deutschland Gmbh | Verfahren zur Herstellung eines integralen Faserverbundbauteils sowie Kernform zur Durchführung des Verfahrens |
Also Published As
Publication number | Publication date |
---|---|
CA2782708A1 (fr) | 2011-06-23 |
EP2512915A2 (fr) | 2012-10-24 |
US20120267479A1 (en) | 2012-10-25 |
FR2954269A1 (fr) | 2011-06-24 |
CN102656085A (zh) | 2012-09-05 |
WO2011073573A2 (fr) | 2011-06-23 |
BR112012011517A2 (pt) | 2016-06-07 |
RU2012129704A (ru) | 2014-01-27 |
FR2954269B1 (fr) | 2012-12-28 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
WO2010070181A3 (fr) | Ferrure de nervure | |
WO2009156549A3 (fr) | Structure de surface de support d'aéronef | |
WO2009156105A3 (fr) | Procédé et moule de fabrication pour la production de pale de rotor d'éolienne | |
BRPI0814998A2 (pt) | Processo para a produção de um componente bem como componente de termoplástico reforçado com fibras | |
WO2011069899A3 (fr) | Procédé pour rattacher un élément composite renforcé par des fibres à un élément de structure d'un aéronef et d'un véhicule spatial et un dispositif correspondant | |
WO2013158182A3 (fr) | Procédé de fabrication de panneau sandwich | |
EP2153979A4 (fr) | Caisson de torsion multi-longerons intégré en matériau composite | |
WO2013118030A3 (fr) | Panneau de sol destiné à former un revêtement de sol, revêtement de sol formé à partir de tels panneaux de sol et procédé permettant de fabriquer de tels panneaux de sol | |
WO2014096004A3 (fr) | Procédé de fabrication d'élément d'enveloppe aérodynamique pour pale de turbine éolienne | |
WO2008154066A3 (fr) | Procédés et appareil pour aéronef | |
WO2010118448A3 (fr) | Membrure et procédé de fabrication d'une telle membrure | |
WO2012028467A8 (fr) | Composant de fuselage de véhicule à aspiration d'air, procédé de production d'un composant de fuselage de véhicule à aspiration d'air et véhicule, en particulier aéronef, pourvu d'un composant de fuselage de véhicule à aspiration d'air | |
WO2012001207A3 (fr) | Fuselage d'aéronef en matériau composite et procédés pour sa fabrication | |
WO2011073573A3 (fr) | Procédé de fabrication d'un panneau composite de bord de fuite pour un élément d ' aéronef | |
WO2014158295A3 (fr) | Structure de soutien de fuselage pour avion à aile haute | |
WO2009147341A3 (fr) | Mat d'accrochage de moteur comprenant des moyens de fixation des longerons et des panneaux agences en dehors de l'espace interieur de caisson | |
WO2011003844A3 (fr) | Lisse | |
WO2010072675A3 (fr) | Procédé de production de minces couches libres de matériaux semi-conducteurs avec des surfaces structurées | |
EP2128017A4 (fr) | Structure de matière composée pour le fuselage d'un aéronef et son procédé de fabrication | |
WO2009083262A3 (fr) | Composant structurel aile-fuselage permettant de relier deux ailes portantes et une section de fuselage à un avion | |
WO2008132171A3 (fr) | Élément structurel de fuselage d'avion | |
WO2011010155A3 (fr) | Direction de véhicules par commande de profils aérodynamiques | |
WO2010036406A3 (fr) | Procédé pour produire des structures composites résistant aux balles et à l'arme blanche | |
WO2010130687A3 (fr) | Procédé de fabrication d'un fuselage d'avion et fuselage d'avion | |
WO2011106733A3 (fr) | Conception de pale et d'aile aérodynamique et structurelle évoluée |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
WWE | Wipo information: entry into national phase |
Ref document number: 201080057697.6 Country of ref document: CN |
|
121 | Ep: the epo has been informed by wipo that ep was designated in this application |
Ref document number: 10805808 Country of ref document: EP Kind code of ref document: A1 |
|
ENP | Entry into the national phase |
Ref document number: 2782708 Country of ref document: CA |
|
WWE | Wipo information: entry into national phase |
Ref document number: 2010805808 Country of ref document: EP |
|
NENP | Non-entry into the national phase |
Ref country code: DE |
|
WWE | Wipo information: entry into national phase |
Ref document number: 13516770 Country of ref document: US |
|
WWE | Wipo information: entry into national phase |
Ref document number: 2012129704 Country of ref document: RU |
|
REG | Reference to national code |
Ref country code: BR Ref legal event code: B01A Ref document number: 112012011517 Country of ref document: BR |
|
ENP | Entry into the national phase |
Ref document number: 112012011517 Country of ref document: BR Kind code of ref document: A2 Effective date: 20120515 |