FR2954544B1 - Procede de conception de kits de reparation standardises pour fuselage d'aeronef - Google Patents
Procede de conception de kits de reparation standardises pour fuselage d'aeronefInfo
- Publication number
- FR2954544B1 FR2954544B1 FR0959118A FR0959118A FR2954544B1 FR 2954544 B1 FR2954544 B1 FR 2954544B1 FR 0959118 A FR0959118 A FR 0959118A FR 0959118 A FR0959118 A FR 0959118A FR 2954544 B1 FR2954544 B1 FR 2954544B1
- Authority
- FR
- France
- Prior art keywords
- repair kits
- aircraft fuselage
- designing
- external
- area
- 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.)
- Expired - Fee Related
Links
Classifications
-
- 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
- B64F5/40—Maintaining or repairing aircraft
-
- G—PHYSICS
- G06—COMPUTING; CALCULATING OR COUNTING
- G06F—ELECTRIC DIGITAL DATA PROCESSING
- G06F30/00—Computer-aided design [CAD]
- G06F30/10—Geometric CAD
- G06F30/15—Vehicle, aircraft or watercraft design
-
- 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
- B29C73/00—Repairing of articles made from plastics or substances in a plastic state, e.g. of articles shaped or produced by using techniques covered by this subclass or subclass B29D
- B29C73/04—Repairing of articles made from plastics or substances in a plastic state, e.g. of articles shaped or produced by using techniques covered by this subclass or subclass B29D using preformed elements
-
- G—PHYSICS
- G06—COMPUTING; CALCULATING OR COUNTING
- G06F—ELECTRIC DIGITAL DATA PROCESSING
- G06F2113/00—Details relating to the application field
- G06F2113/28—Fuselage, exterior or interior
Landscapes
- Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Geometry (AREA)
- General Physics & Mathematics (AREA)
- Aviation & Aerospace Engineering (AREA)
- Theoretical Computer Science (AREA)
- Mathematical Optimization (AREA)
- Computational Mathematics (AREA)
- Manufacturing & Machinery (AREA)
- Mathematical Analysis (AREA)
- Transportation (AREA)
- Pure & Applied Mathematics (AREA)
- Computer Hardware Design (AREA)
- Evolutionary Computation (AREA)
- General Engineering & Computer Science (AREA)
- Automation & Control Theory (AREA)
- Management, Administration, Business Operations System, And Electronic Commerce (AREA)
Priority Applications (5)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0959118A FR2954544B1 (fr) | 2009-12-17 | 2009-12-17 | Procede de conception de kits de reparation standardises pour fuselage d'aeronef |
PCT/FR2010/052712 WO2011073566A1 (fr) | 2009-12-17 | 2010-12-14 | Procédé de conception de kits de réparation standardisés pour fuselage d'aéronef |
EP10809008A EP2513823A1 (fr) | 2009-12-17 | 2010-12-14 | Procédé de conception de kits de réparation standardisés pour fuselage d'aéronef |
CN201080062809.7A CN102741846B (zh) | 2009-12-17 | 2010-12-14 | 航空器机身用的标准化修理包的设计方法 |
US13/516,394 US20130024165A1 (en) | 2009-12-17 | 2010-12-14 | Method for designing standardised repair kits for an aircraft fuselage |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0959118A FR2954544B1 (fr) | 2009-12-17 | 2009-12-17 | Procede de conception de kits de reparation standardises pour fuselage d'aeronef |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2954544A1 FR2954544A1 (fr) | 2011-06-24 |
FR2954544B1 true FR2954544B1 (fr) | 2013-11-22 |
Family
ID=41819701
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR0959118A Expired - Fee Related FR2954544B1 (fr) | 2009-12-17 | 2009-12-17 | Procede de conception de kits de reparation standardises pour fuselage d'aeronef |
Country Status (5)
Country | Link |
---|---|
US (1) | US20130024165A1 (fr) |
EP (1) | EP2513823A1 (fr) |
CN (1) | CN102741846B (fr) |
FR (1) | FR2954544B1 (fr) |
WO (1) | WO2011073566A1 (fr) |
Families Citing this family (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2953812B1 (fr) * | 2009-12-11 | 2012-09-07 | Airbus Operations Sas | Procede de reparation d'un fuselage d'aeronef |
FR3016963B1 (fr) * | 2014-01-27 | 2016-01-22 | Airbus | Dispositif et procede de localisation d'impacts sur une surface externe d'un corps |
US9646431B2 (en) * | 2014-10-22 | 2017-05-09 | The Boeing Company | Augmented reality system for assessing an affected area of an aircraft |
CN104386263A (zh) * | 2014-11-12 | 2015-03-04 | 沈阳航空航天大学 | 一种飞机上z型长桁的拼接修理方法 |
CN106275499B (zh) * | 2016-08-22 | 2018-07-13 | 中国航空工业集团公司西安飞机设计研究所 | 一种飞机结构死角处防腐蚀设计方法 |
US11865647B2 (en) * | 2020-03-13 | 2024-01-09 | The Boeing Company | Utilization of CNC machining in composite part rework |
Family Cites Families (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6219930B1 (en) * | 1998-02-27 | 2001-04-24 | Randall M. McPherson | Apparatus and method of use for calculating an estimate of damaged surface repair cost |
US7707058B2 (en) * | 2001-08-31 | 2010-04-27 | Hewlett-Packard Development Company, L.P. | Predicting parts needed for an onsite repair using expected waste derived from repair history |
CN1361039A (zh) * | 2002-01-29 | 2002-07-31 | 许陆文 | 飞行器结构损伤复合材料快速修复技术与设备 |
US6876950B2 (en) * | 2002-04-26 | 2005-04-05 | The Boeing Company | System and method for damage evaluation |
US20070095457A1 (en) * | 2005-11-02 | 2007-05-03 | The Boeing Company | Fast line maintenance repair method and system for composite structures |
US8560376B2 (en) * | 2007-05-31 | 2013-10-15 | Airbus Operations S.A.S. | Method, system, and computer program product for a maintenance optimization model |
US20090234616A1 (en) * | 2008-02-21 | 2009-09-17 | Syncretek Llc | Automatic Repair Planning and Part Archival System (ARPPAS) |
US8209838B2 (en) * | 2008-12-19 | 2012-07-03 | The Boeing Company | Repairing composite structures |
US8977528B2 (en) * | 2009-04-27 | 2015-03-10 | The Boeing Company | Bonded rework simulation tool |
-
2009
- 2009-12-17 FR FR0959118A patent/FR2954544B1/fr not_active Expired - Fee Related
-
2010
- 2010-12-14 US US13/516,394 patent/US20130024165A1/en not_active Abandoned
- 2010-12-14 CN CN201080062809.7A patent/CN102741846B/zh not_active Expired - Fee Related
- 2010-12-14 EP EP10809008A patent/EP2513823A1/fr not_active Withdrawn
- 2010-12-14 WO PCT/FR2010/052712 patent/WO2011073566A1/fr active Application Filing
Also Published As
Publication number | Publication date |
---|---|
FR2954544A1 (fr) | 2011-06-24 |
CN102741846B (zh) | 2015-09-16 |
US20130024165A1 (en) | 2013-01-24 |
CN102741846A (zh) | 2012-10-17 |
EP2513823A1 (fr) | 2012-10-24 |
WO2011073566A1 (fr) | 2011-06-23 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
FR2954544B1 (fr) | Procede de conception de kits de reparation standardises pour fuselage d'aeronef | |
EP2264825A4 (fr) | Batterie auxiliaire à air et procédé de fabrication associé | |
PL400393A1 (pl) | Komórka paliwowa z kolnierzem i elementem ustalajacym dla narzedzia spalinowego | |
WO2011008762A3 (fr) | Refroidissement de système de test de dispositif de stockage | |
EP2672549A4 (fr) | Pièce pour batterie secondaire, procédé permettant de la fabriquer, et batterie secondaire et système à plusieurs batteries fabriqués grâce à cette pièce | |
EP3016147B8 (fr) | Module de cellule solaire et procédé et dispositif de réparation de celui-ci | |
FR2944623B1 (fr) | Procede et outil de simulation du comportement aerodynamique d'un aeronef en vol au voisinage du sol | |
FR2953812B1 (fr) | Procede de reparation d'un fuselage d'aeronef | |
WO2014028169A3 (fr) | Éléments composites de transport de déchets et d'eaux usées et leurs procédés de fabrication pour leur utilisation à bord d'un avion | |
BR112017018885A2 (pt) | método de cultura celular para células-tronco mesenquimais | |
BR112013016487A2 (pt) | sistema de célula de solda com comunicação | |
BRPI0918937A2 (pt) | sistema de gerenciamento de iluminação, método para implementar o sistema de gerenciamento de iluminação e módulo executivo para o uso em um sistema de gerenciamento de iluminação | |
EA025172B9 (ru) | Способ оценки способности достижения одним или более эмбрионами человека стадии бластоцисты | |
ATE555983T1 (de) | Vorrichtung zur anbringung eines tragwerks an einem flugzeugrumpf | |
PL3565035T3 (pl) | Litowy akumulator wielokrotnego ładowania i sposób wytwarzania litowego akumulatora wielokrotnego ładowania | |
EP3092476A4 (fr) | Structure et procédé pour indiquer des constituants indésirables dans un système de pile à combustible | |
EP3340333A4 (fr) | Pile courbe à faible déformation structurale et son procédé de fabrication | |
EP3416856A4 (fr) | Système d'économie de carburant par arrêt-démarrage à fonctionnalité étendue pour véhicules professionnels | |
FR2970238B1 (fr) | Piece et procede de reparation d'une structure endommagee, en particulier de peau d'aeronef, ainsi qu'un kit de reparation de mise en oeuvre | |
EP2574726A3 (fr) | Trou décalé de refroidissement d'aube de turbine | |
FR2966371B1 (fr) | Procede et installation d'usinage avec refroidissement cryogenique | |
WO2014176437A3 (fr) | Plaque pour trou de trépan rétractable et procédé associé | |
EP3000781A4 (fr) | Pile à combustible et son procédé de fabrication | |
BR112015004682A2 (pt) | método para gerenciar o carregamento de um conjunto de baterias com base em um sistema de carregamento e sistema de carregamento de um conjunto de baterias. | |
EP3474361A4 (fr) | Module de piles à combustible, dispositif de piles à combustible et procédé de fabrication de module de piles à combustible |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PLFP | Fee payment |
Year of fee payment: 7 |
|
PLFP | Fee payment |
Year of fee payment: 8 |
|
PLFP | Fee payment |
Year of fee payment: 9 |
|
ST | Notification of lapse |
Effective date: 20190905 |