JP2008519730A5 - - Google Patents
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- Publication number
- JP2008519730A5 JP2008519730A5 JP2007540690A JP2007540690A JP2008519730A5 JP 2008519730 A5 JP2008519730 A5 JP 2008519730A5 JP 2007540690 A JP2007540690 A JP 2007540690A JP 2007540690 A JP2007540690 A JP 2007540690A JP 2008519730 A5 JP2008519730 A5 JP 2008519730A5
- Authority
- JP
- Japan
- Prior art keywords
- lower arch
- fuselage
- frame according
- structure frame
- fuselage structure
- 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.)
- Granted
Links
- 239000002131 composite material Substances 0.000 claims 2
- 239000003365 glass fiber Substances 0.000 claims 1
- 239000002184 metal Substances 0.000 claims 1
- 239000002905 metal composite material Substances 0.000 claims 1
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR0452622A FR2877916B1 (fr) | 2004-11-15 | 2004-11-15 | Cadre de structure de fuselage d'aeronef |
| PCT/FR2005/050932 WO2006051235A1 (fr) | 2004-11-15 | 2005-11-07 | Cadre de structure de fuselage d'aéronef |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| JP2008519730A JP2008519730A (ja) | 2008-06-12 |
| JP2008519730A5 true JP2008519730A5 (enExample) | 2010-03-11 |
| JP4524313B2 JP4524313B2 (ja) | 2010-08-18 |
Family
ID=34951041
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP2007540690A Expired - Fee Related JP4524313B2 (ja) | 2004-11-15 | 2005-11-07 | 航空機胴体構造フレーム |
Country Status (11)
| Country | Link |
|---|---|
| US (1) | US7874516B2 (enExample) |
| EP (1) | EP1812288B1 (enExample) |
| JP (1) | JP4524313B2 (enExample) |
| CN (1) | CN100546872C (enExample) |
| AT (1) | ATE403598T1 (enExample) |
| BR (1) | BRPI0517861A (enExample) |
| CA (1) | CA2585869C (enExample) |
| DE (1) | DE602005008765D1 (enExample) |
| FR (1) | FR2877916B1 (enExample) |
| RU (1) | RU2357892C2 (enExample) |
| WO (1) | WO2006051235A1 (enExample) |
Families Citing this family (41)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE102006019123B4 (de) * | 2006-04-25 | 2012-08-02 | Airbus Operations Gmbh | Bodenstruktur für einen Rumpf |
| DE102006026169B4 (de) * | 2006-06-06 | 2012-06-21 | Airbus Operations Gmbh | Flugzeugrumpfstruktur und Verfahren zu deren Herstellung |
| DE102006026170B4 (de) * | 2006-06-06 | 2012-06-21 | Airbus Operations Gmbh | Flugzeugrumpfstruktur und Verfahren zu deren Herstellung |
| DE102006026168A1 (de) * | 2006-06-06 | 2008-01-31 | Airbus Deutschland Gmbh | Flugzeugrumpfstruktur und Verfahren zu deren Herstellung |
| DE102006029231B4 (de) * | 2006-06-26 | 2013-09-26 | Airbus Operations Gmbh | Druckschott für einen Rumpf für die Luft- und Raumfahrt |
| US9611029B2 (en) * | 2006-10-11 | 2017-04-04 | The Boeing Company | Floor beam support assembly, system, and associated method |
| GB2477882B (en) * | 2006-12-08 | 2011-10-19 | Boeing Co | Energy absorbing structure for aircraft |
| US8376275B2 (en) * | 2006-12-08 | 2013-02-19 | The Boeing Company | Energy absorbing structure for aircraft |
| US7954760B2 (en) * | 2007-06-11 | 2011-06-07 | The Boeing Company | Cargo floor, system, and method |
| DE102007030026A1 (de) * | 2007-06-29 | 2009-01-02 | Airbus Deutschland Gmbh | Strukturbauteil mit Spant- und Querträgerelement |
| DE102008007838B4 (de) * | 2008-02-07 | 2013-07-18 | Airbus Operations Gmbh | Fußbodensystem für eine Rumpfzelle eines Flugzeugs |
| DE102008010197B4 (de) * | 2008-02-20 | 2012-03-22 | Airbus Operations Gmbh | Verfahren zum Verbinden von zwei Rumpfsektionen unter Schaffung eines Querstoßes sowie Querstoßverbindung |
| 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 |
| DE102008038806A1 (de) | 2008-08-13 | 2010-02-25 | Airbus Deutschland Gmbh | Vormontage und Integration von Flugzeugkabinen |
| DE102008042036A1 (de) * | 2008-09-12 | 2010-03-25 | Airbus Deutschland Gmbh | Stange zur Abstützung von Bauteilen innerhalb einer Rumpfzellenstruktur eines Flugzeugs |
| US8336820B2 (en) * | 2008-10-27 | 2012-12-25 | Embraer S.A. | Aircraft cabin floor structures, systems and methods |
| DE102009012424B4 (de) | 2009-03-10 | 2014-03-20 | Telair International Gmbh | Frachtraumboden für einen Frachtraum eines Flugzeugs sowie Verfahren zur Montage eines solchen |
| FR2947524B1 (fr) * | 2009-07-02 | 2011-12-30 | Airbus Operations Sas | Procede de fabrication d'un aeronef comprenant un plancher |
| DE102009049007A1 (de) * | 2009-10-09 | 2011-04-21 | Airbus Operations Gmbh | Druckrumpf eines Flugzeuges mit heckseitiger Druckkalotte |
| DE102010014302B4 (de) * | 2010-04-09 | 2014-12-04 | Premium Aerotec Gmbh | Luftfahrzeug und Befestigungsanordnung für eine Fußbodenstruktur in einem Luftfahrzeug |
| DE102010014638B4 (de) | 2010-04-12 | 2019-08-01 | Airbus Defence and Space GmbH | Luftfahrzeug mit einer integrierten energieaufnehmenden Verformungsstruktur und Luftfahrzeug mit einem derartigen Rumpf |
| DE102010045588B4 (de) | 2010-09-16 | 2017-04-06 | Airbus Operations Gmbh | Rumpfsegment für ein Luftfahrzeug |
| DE102010062018B4 (de) | 2010-11-26 | 2015-05-13 | Airbus Operations Gmbh | Stützstab zur Stützung einer Fussbodenstruktur eines Flugzeugs |
| US8776375B2 (en) * | 2011-05-19 | 2014-07-15 | The Boeing Company | Aircraft structure for high capacity pull off |
| ES2401517B1 (es) * | 2011-05-31 | 2014-06-18 | Airbus Operations S.L. | Cuaderna de aeronave en material compuesto. |
| FR2979896A1 (fr) * | 2011-09-08 | 2013-03-15 | Airbus Operations Sas | Element de cadre de fuselage d'aeronef |
| ES2645628T3 (es) * | 2011-12-01 | 2017-12-07 | Airbus Operations S.L. | Cuaderna altamente cargada de un fuselaje de aeronave con un alma con estructura de celosía |
| DE102012005353A1 (de) * | 2012-03-16 | 2013-09-19 | Airbus Operations Gmbh | Flugzeugrumpfstruktur mit Querprofilen und Fachwerkstruktur |
| RU2519301C1 (ru) * | 2013-02-18 | 2014-06-10 | Иван Сергеевич Рыбкин | Шпангоут переменной жесткости |
| US9505354B2 (en) * | 2013-09-16 | 2016-11-29 | The Boeing Company | Carbon fiber reinforced polymer cargo beam with integrated cargo stanchions and c-splices |
| EP2876042B1 (en) * | 2013-11-20 | 2018-01-03 | AIRBUS HELICOPTERS DEUTSCHLAND GmbH | Helicopter airframe |
| PL2905228T3 (pl) * | 2014-02-06 | 2018-05-30 | Airbus Helicopters Deutschland GmbH | Płatowiec kadłubowy i zbiornik |
| EP2907743A1 (en) * | 2014-02-13 | 2015-08-19 | Airbus Operations GmbH | Stiffening element, method for coupling the same, and shell component for an aircraft or spacecraft |
| FR3021624B1 (fr) * | 2014-05-30 | 2017-12-22 | Airbus Operations Sas | Liaison coulissante entre la structure plancher et la structure de coque d'un aeronef. |
| US10625844B2 (en) * | 2014-11-10 | 2020-04-21 | The Boeing Company | Fuselage with structural and non-structural stanchions |
| FR3035070B1 (fr) * | 2015-04-20 | 2017-05-05 | Airbus Operations Sas | Aeronef a section courante simplifiee |
| US10745098B2 (en) * | 2017-09-05 | 2020-08-18 | The Boeing Company | Energy-absorbing under-floor airframe |
| US11383817B2 (en) * | 2019-07-19 | 2022-07-12 | The Boeing Company | Modular fuselage assemblies for aircraft, aircraft including modular fuselage assemblies, and MEl'hods of assembling modular fuselage assemblies |
| FR3124487A1 (fr) * | 2021-06-29 | 2022-12-30 | Airbus Operations | Élément de liaison entre un premier et un deuxième élément structurel de fuselage d’un aéronef permettant une dissipation améliorée des efforts. |
| FR3128938A1 (fr) * | 2021-11-10 | 2023-05-12 | Airbus Operations | Ensemble structurel pour un aéronef |
| US20250368312A1 (en) * | 2024-05-29 | 2025-12-04 | The Boeing Company | Stanchion for aircraft structure |
Family Cites Families (17)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US1803494A (en) * | 1928-12-20 | 1931-05-05 | Emboutissage Et De Const Mecan | Hollow-frame assembly |
| US1963416A (en) * | 1932-03-07 | 1934-06-19 | Boeing Co | Airplane structural elements |
| US2412778A (en) * | 1944-12-18 | 1946-12-17 | Cons Vultee Aircraft Corp | Suspension type flooring for aircraft |
| SU708102A1 (ru) * | 1977-08-02 | 1980-01-05 | Предприятие П/Я А-3611 | Соединение оболочек из композиционных материалов |
| US4308703A (en) * | 1980-01-18 | 1982-01-05 | James Knowles | Metal connector struts for truss-type beams |
| DE3141869C2 (de) * | 1981-10-22 | 1984-02-02 | Messerschmitt-Bölkow-Blohm GmbH, 8000 München | Fußbodenkonstruktion für den oberen Laderaum eines Luftfahrzeuges |
| US5171510A (en) * | 1988-06-08 | 1992-12-15 | Aerospatiale Societe Nationale Industrielle | Method of producing a frame made of a composite material, especially for the fuselage of an aircraft |
| DE4017978C2 (de) * | 1990-06-05 | 1993-09-30 | Dornier Luftfahrt | Herstellung profilierter Stringer |
| US5072895A (en) * | 1990-07-05 | 1991-12-17 | Mark Camus | Cargo platform assembly mounted to a helicopter |
| SU1726691A1 (ru) * | 1990-08-29 | 1992-04-15 | Центральный научно-исследовательский институт специального машиностроения | Опорный шпангоут из композиционного материала |
| US5560102A (en) * | 1992-10-13 | 1996-10-01 | The Boeing Company | Panel and fuselage assembly |
| CN1153500A (zh) * | 1994-04-06 | 1997-07-02 | 波音公司 | 半刚性、轻型玻璃纤维/聚酰亚胺泡沫夹层绝缘层片 |
| DE4416506C2 (de) * | 1994-05-10 | 1999-12-02 | Daimler Chrysler Aerospace | Passagierflugzeug |
| DE19929471C1 (de) * | 1999-06-26 | 2001-01-18 | Eads Airbus Gmbh | Verfahren und Vorrichtung zur Herstellung eines dreidimensionalen Großbauteiles |
| GB0113916D0 (en) * | 2001-06-07 | 2001-08-01 | Bae Systems Plc | Adding glass to composite bonding surfaces |
| CN2507779Y (zh) * | 2001-07-30 | 2002-08-28 | 罗专予 | 半圆形飞机水密封舱 |
| DE10145276B4 (de) * | 2001-09-14 | 2008-04-10 | Deutsches Zentrum für Luft- und Raumfahrt e.V. | Flugzeug, insbesondere Passagierflugzeug, mit einem Rumpf, der eine tragende Primärstruktur und einen Frachtraum umfasst |
-
2004
- 2004-11-15 FR FR0452622A patent/FR2877916B1/fr not_active Expired - Fee Related
-
2005
- 2005-11-07 US US11/718,845 patent/US7874516B2/en not_active Expired - Fee Related
- 2005-11-07 CN CNB2005800390001A patent/CN100546872C/zh not_active Expired - Fee Related
- 2005-11-07 BR BRPI0517861-4A patent/BRPI0517861A/pt not_active Application Discontinuation
- 2005-11-07 EP EP05819334A patent/EP1812288B1/fr not_active Expired - Lifetime
- 2005-11-07 DE DE602005008765T patent/DE602005008765D1/de not_active Expired - Lifetime
- 2005-11-07 AT AT05819334T patent/ATE403598T1/de not_active IP Right Cessation
- 2005-11-07 RU RU2007122393/11A patent/RU2357892C2/ru not_active IP Right Cessation
- 2005-11-07 CA CA2585869A patent/CA2585869C/fr not_active Expired - Fee Related
- 2005-11-07 WO PCT/FR2005/050932 patent/WO2006051235A1/fr not_active Ceased
- 2005-11-07 JP JP2007540690A patent/JP4524313B2/ja not_active Expired - Fee Related
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