ATE548256T1 - Verfahren zur befestigung eines bodenmoduls eines flugzeuges - Google Patents
Verfahren zur befestigung eines bodenmoduls eines flugzeugesInfo
- Publication number
- ATE548256T1 ATE548256T1 AT09745912T AT09745912T ATE548256T1 AT E548256 T1 ATE548256 T1 AT E548256T1 AT 09745912 T AT09745912 T AT 09745912T AT 09745912 T AT09745912 T AT 09745912T AT E548256 T1 ATE548256 T1 AT E548256T1
- Authority
- AT
- Austria
- Prior art keywords
- aircraft
- floor module
- fixing
- board structure
- floor
- Prior art date
Links
Classifications
-
- 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
- B64C1/18—Floors
-
- 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)
- Manufacturing & Machinery (AREA)
- Mechanical Engineering (AREA)
- Transportation (AREA)
- Body Structure For Vehicles (AREA)
- Connection Of Plates (AREA)
- Automatic Assembly (AREA)
- Lining Or Joining Of Plastics Or The Like (AREA)
- Automobile Manufacture Line, Endless Track Vehicle, Trailer (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0852896A FR2930521B1 (fr) | 2008-04-29 | 2008-04-29 | Module de plancher d'aeronef, structure et procede de fixation d'un tel module, aeronef comprenant ceux-ci |
PCT/FR2009/000508 WO2009138593A2 (fr) | 2008-04-29 | 2009-04-29 | Module de plancher d'aéronef, structure et procédé de fixation d'un tel module, aéronef comprenant ceux-ci |
Publications (1)
Publication Number | Publication Date |
---|---|
ATE548256T1 true ATE548256T1 (de) | 2012-03-15 |
Family
ID=40289195
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
AT09745912T ATE548256T1 (de) | 2008-04-29 | 2009-04-29 | Verfahren zur befestigung eines bodenmoduls eines flugzeuges |
Country Status (6)
Country | Link |
---|---|
US (1) | US20110036946A1 (de) |
EP (1) | EP2280865B1 (de) |
CN (1) | CN102015442A (de) |
AT (1) | ATE548256T1 (de) |
FR (1) | FR2930521B1 (de) |
WO (1) | WO2009138593A2 (de) |
Families Citing this family (17)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2933065B1 (fr) * | 2008-06-30 | 2011-08-26 | Airbus France | Procede d'assemblage d'un plancher dans une structure de coque prealablement constituee d'un troncon de fuselage d'aeronef |
FR2947525B1 (fr) * | 2009-07-02 | 2011-09-02 | Airbus Operations Sas | Plancher d'aeronef a encombrement optimise |
FR2947524B1 (fr) * | 2009-07-02 | 2011-12-30 | Airbus Operations Sas | Procede de fabrication d'un aeronef comprenant un plancher |
FR2977566B1 (fr) | 2011-07-05 | 2014-05-02 | Airbus Operations Sas | Structure intermediaire de support pour poste de pilotage d'un aeronef |
US9199715B2 (en) | 2013-10-10 | 2015-12-01 | The Boeing Company | Self-aligning fitting assemblies and systems and methods including the same |
FR3018267B1 (fr) * | 2014-03-07 | 2017-12-22 | Airbus Operations Sas | Dispositif de positionnement relatif de deux pieces telles qu'une traverse et un cadre de fuselage |
EP3161566B1 (de) * | 2014-06-27 | 2021-03-24 | Airbus Canada Limited Partnership | Umformung von verformten komponenten zur montage |
US10001158B2 (en) * | 2015-08-14 | 2018-06-19 | The Boeing Company | Anti-rotation for eccentric bushings |
DE102015116591A1 (de) | 2015-09-30 | 2017-03-30 | Airbus Operations Gmbh | Profil zum Verbinden einer Fußbodenstruktur und Dichtungssystem für eine Fußbodenstruktur |
FR3048227B1 (fr) * | 2016-02-25 | 2019-06-28 | Airbus Operations | Plancher unitaire et pointe avant d’aeronef comportant un tel plancher et procede d’integration d’une telle pointe avant |
FR3059302B1 (fr) * | 2016-11-30 | 2019-05-17 | Airbus Operations | Ensemble pour aeronef comprenant un panneau auto-raidi assemble a un element structurel au moyen d'une alternance de nervures terminales et de languettes terminales |
FR3059980B1 (fr) * | 2016-12-09 | 2019-01-25 | Stelia Aerospace | Plancher de cabine pour aeronef et procede de montage d'un tel plancher |
DE102017220378A1 (de) | 2017-11-15 | 2019-05-16 | Airbus Operations Gmbh | Bodenbaugruppe mit monolithischem Bodenelement sowie Luftfahrzeugbereich und Luftfahrzeug mit einer Bodenbaugruppe |
CN108423192B (zh) * | 2018-04-16 | 2023-06-23 | 西安飞机工业(集团)有限责任公司 | 一种飞机工艺地板的固定结构及安装方法 |
US20200023936A1 (en) * | 2018-07-19 | 2020-01-23 | Airbus Americas, Inc. | Modular cabin floor installation method |
US11281236B2 (en) * | 2019-01-25 | 2022-03-22 | Textron Innovations Inc. | Alternative yaw control |
FR3130763A1 (fr) * | 2021-12-16 | 2023-06-23 | Airbus Operations | Procédé d’assemblage d’un tronçon de fuselage d’un aéronef utilisant un module de plancher comme conformateur de forme. |
Family Cites Families (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2263919A (en) * | 1939-10-21 | 1941-11-25 | Lockheed Aircraft Corp | Sound and vibration insulation for aircraft cabins |
DE3141869C2 (de) * | 1981-10-22 | 1984-02-02 | Messerschmitt-Bölkow-Blohm GmbH, 8000 München | Fußbodenkonstruktion für den oberen Laderaum eines Luftfahrzeuges |
US4989809A (en) * | 1988-03-14 | 1991-02-05 | The Boeing Company | Removable aircraft floor structure-reinforcing strongback |
US5560102A (en) * | 1992-10-13 | 1996-10-01 | The Boeing Company | Panel and fuselage assembly |
FR2745260B1 (fr) * | 1996-02-28 | 1998-04-03 | Airbus Ind | Systeme et procede de conversion rapide et reversible d'un avion entre une configuration passagers et une configuration fret |
DE10319503B4 (de) * | 2003-04-30 | 2009-07-30 | Telair International Gmbh | Frachtdeck für ein Flugzeug |
EP1646558B1 (de) * | 2003-07-18 | 2006-11-15 | Telair International GmbH | Frachtraumboden für ein flugzeug und verfahren zu dessen montage |
FR2872780B1 (fr) * | 2004-07-08 | 2006-11-17 | Airbus France Sas | Plancher pour aeronef |
FR2872782B1 (fr) * | 2004-07-08 | 2007-10-05 | Airbus France Sas | Plancher pour aeronef |
FR2872781B1 (fr) * | 2004-07-08 | 2007-10-05 | Airbus France Sas | Plancher pour aeronef |
US7182291B2 (en) * | 2005-03-23 | 2007-02-27 | The Boeing Company | Integrated aircraft structural floor |
US7721992B2 (en) * | 2007-03-07 | 2010-05-25 | The Boeing Company | Aircraft floor to fuselage attachment |
US7967251B2 (en) * | 2008-03-18 | 2011-06-28 | The Boeing Company | Truss network for aircraft floor attachment |
FR2947525B1 (fr) * | 2009-07-02 | 2011-09-02 | Airbus Operations Sas | Plancher d'aeronef a encombrement optimise |
FR2947524B1 (fr) * | 2009-07-02 | 2011-12-30 | Airbus Operations Sas | Procede de fabrication d'un aeronef comprenant un plancher |
-
2008
- 2008-04-29 FR FR0852896A patent/FR2930521B1/fr not_active Expired - Fee Related
-
2009
- 2009-04-29 EP EP09745912A patent/EP2280865B1/de not_active Not-in-force
- 2009-04-29 WO PCT/FR2009/000508 patent/WO2009138593A2/fr active Application Filing
- 2009-04-29 US US12/989,965 patent/US20110036946A1/en not_active Abandoned
- 2009-04-29 CN CN2009801154339A patent/CN102015442A/zh active Pending
- 2009-04-29 AT AT09745912T patent/ATE548256T1/de active
Also Published As
Publication number | Publication date |
---|---|
FR2930521B1 (fr) | 2010-09-03 |
US20110036946A1 (en) | 2011-02-17 |
EP2280865A2 (de) | 2011-02-09 |
WO2009138593A4 (fr) | 2010-02-25 |
WO2009138593A3 (fr) | 2010-01-07 |
FR2930521A1 (fr) | 2009-10-30 |
CN102015442A (zh) | 2011-04-13 |
WO2009138593A2 (fr) | 2009-11-19 |
EP2280865B1 (de) | 2012-03-07 |
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