FR2953193B1 - Aeronef comportant une cloison interne - Google Patents
Aeronef comportant une cloison interneInfo
- Publication number
- FR2953193B1 FR2953193B1 FR0958505A FR0958505A FR2953193B1 FR 2953193 B1 FR2953193 B1 FR 2953193B1 FR 0958505 A FR0958505 A FR 0958505A FR 0958505 A FR0958505 A FR 0958505A FR 2953193 B1 FR2953193 B1 FR 2953193B1
- Authority
- FR
- France
- Prior art keywords
- aircraft
- roofing
- internal
- internal roofing
- 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
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
- B64C1/10—Bulkheads
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Casting Or Compression Moulding Of Plastics Or The Like (AREA)
- Diaphragms And Bellows (AREA)
- Tires In General (AREA)
Priority Applications (5)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0958505A FR2953193B1 (fr) | 2009-11-30 | 2009-11-30 | Aeronef comportant une cloison interne |
CN201080062447.1A CN102741118B (zh) | 2009-11-30 | 2010-11-30 | 包括内部隔墙的航空器 |
PCT/FR2010/052577 WO2011064519A2 (fr) | 2009-11-30 | 2010-11-30 | Aeronef comportant une cloison interne |
US13/511,853 US8777160B2 (en) | 2009-11-30 | 2010-11-30 | Aircraft including an internal partition |
CA2781777A CA2781777C (fr) | 2009-11-30 | 2010-11-30 | Aeronef comportant une cloison interne |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0958505A FR2953193B1 (fr) | 2009-11-30 | 2009-11-30 | Aeronef comportant une cloison interne |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2953193A1 FR2953193A1 (fr) | 2011-06-03 |
FR2953193B1 true FR2953193B1 (fr) | 2012-03-16 |
Family
ID=42271928
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR0958505A Expired - Fee Related FR2953193B1 (fr) | 2009-11-30 | 2009-11-30 | Aeronef comportant une cloison interne |
Country Status (5)
Country | Link |
---|---|
US (1) | US8777160B2 (fr) |
CN (1) | CN102741118B (fr) |
CA (1) | CA2781777C (fr) |
FR (1) | FR2953193B1 (fr) |
WO (1) | WO2011064519A2 (fr) |
Families Citing this family (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2953193B1 (fr) * | 2009-11-30 | 2012-03-16 | Airbus Operations Sas | Aeronef comportant une cloison interne |
GB201110973D0 (en) * | 2011-06-28 | 2011-08-10 | Airbus Operations Ltd | Bracket |
FR2983826B1 (fr) * | 2011-12-12 | 2013-12-20 | Airbus Operations Sas | Structure avant d'avion perfectionnee a compartiment pour train d'atterrissage. |
DE102012022713B3 (de) * | 2012-11-21 | 2014-02-13 | Diehl Aircabin Gmbh | Paneel und Verfahren zur Herstellung eines Paneels |
DE102015111160B4 (de) * | 2015-07-09 | 2018-09-06 | Airbus Operations Gmbh | Rumpfstruktur und Verfahren zum Herstellen einer Rumpfstruktur |
ES2733055T3 (es) * | 2015-12-03 | 2019-11-27 | Airbus Operations Sl | Mamparo de presión |
FR3049927B1 (fr) * | 2016-04-07 | 2018-04-20 | Airbus Operations | Troncon d'aeronef comprenant une cloison de pressurisation |
US10173765B2 (en) * | 2016-04-07 | 2019-01-08 | The Boeing Company | Pressure bulkhead apparatus |
US10988231B2 (en) | 2016-07-21 | 2021-04-27 | The Boeing Company | Space frame fuselage with pressure membrane |
EP3375706B1 (fr) * | 2017-03-15 | 2022-05-18 | Airbus Operations S.L. | Fuselage résistant aux chocs |
DE102017211764B4 (de) * | 2017-07-10 | 2021-05-12 | Siemens Healthcare Gmbh | C-Bogen für eine medizinische Untersuchungs- oder Behandlungseinrichtung |
EP4035993A1 (fr) | 2021-01-27 | 2022-08-03 | The Boeing Company | Connecteur pour connecter un caisson de voilure central à une cloison d'un aéronef |
CN114802698A (zh) | 2021-01-27 | 2022-07-29 | 波音公司 | 在飞机中用于连接中央翼盒和隔舱的接头 |
Family Cites Families (21)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB581142A (en) * | 1942-11-18 | 1946-10-02 | Vickers Armstrongs Ltd | Improvements in or connected with pressure cabins for aircraft |
US2519393A (en) * | 1947-03-14 | 1950-08-22 | Noyes Howard | Bladder type tank or cell |
GB626443A (en) * | 1947-08-28 | 1949-07-14 | Fireproof Tanks Ltd | Improvements relating to the support of flexible liquid containers |
US2840259A (en) * | 1955-09-06 | 1958-06-24 | Boeing Co | Fabric slosh bulkhead |
GB857616A (en) * | 1958-04-03 | 1961-01-04 | Marston Excelsior Ltd | Flexible articles |
DE2659401A1 (de) | 1975-12-31 | 1977-08-04 | Lightspeed Usa Inc | Luftschiff |
DE3844080C2 (de) * | 1988-12-28 | 1993-12-23 | Deutsche Aerospace Airbus | Druckwand für einen Flugzeugrumpf |
US5451015A (en) * | 1993-05-18 | 1995-09-19 | Bell Helicopter Textron Inc. | Crashworthy composite aircraft structure with integral fuel tank |
US5788184A (en) * | 1997-01-04 | 1998-08-04 | Eddy; Robert G. | Aircraft passenger safety enhanced fuselage insulation blanket |
US5899412A (en) * | 1997-12-19 | 1999-05-04 | Northrop Grumman Corporation | Aircraft pressure containment assembly module |
US7083147B2 (en) * | 2004-03-11 | 2006-08-01 | The Boeing Company | Modularized insulation, systems, apparatus, and methods |
ES2310059B1 (es) * | 2004-12-31 | 2009-11-11 | Airbus España, S.L. | Dispositivo de sellado para la ranura de paso del arbol de accionamiento de un flap en la carena ventral de un avion. |
FR2894561B1 (fr) | 2005-12-14 | 2008-02-15 | Eurocopter France | Reservoir aerotransportable de stockage d'un produit a larguer en vol |
US7766277B2 (en) * | 2006-01-19 | 2010-08-03 | The Boeing Company | Deformable forward pressure bulkhead for an aircraft |
FR2901240B1 (fr) * | 2006-05-17 | 2009-01-09 | Airbus France Sas | Poutre interne composite pour renforcer la structure d'un aeronef |
DE102007046479B4 (de) * | 2006-12-13 | 2015-08-27 | Airbus Operations Gmbh | Brandschutzvorrichtung für ein Luft- oder Raumfahrzeug |
DE102007044388B4 (de) * | 2007-09-18 | 2012-08-02 | Airbus Operations Gmbh | Druckschott und Verfahren zum Unterteilen eines Luft- oder Raumfahrzeugs |
DE102007052140B4 (de) * | 2007-10-31 | 2012-10-25 | Airbus Operations Gmbh | Struktur, insbesondere Rumpfstruktur eines Luft- oder Raumfahrzeugs |
FR2933375B1 (fr) * | 2008-07-01 | 2011-04-15 | Airbus France | Agencement de fuselage d'avion |
US8476564B2 (en) * | 2008-07-02 | 2013-07-02 | The Boeing Company | Thermally activated variable stiffness composites for aircraft seals |
FR2953193B1 (fr) * | 2009-11-30 | 2012-03-16 | Airbus Operations Sas | Aeronef comportant une cloison interne |
-
2009
- 2009-11-30 FR FR0958505A patent/FR2953193B1/fr not_active Expired - Fee Related
-
2010
- 2010-11-30 CA CA2781777A patent/CA2781777C/fr not_active Expired - Fee Related
- 2010-11-30 WO PCT/FR2010/052577 patent/WO2011064519A2/fr active Application Filing
- 2010-11-30 CN CN201080062447.1A patent/CN102741118B/zh not_active Expired - Fee Related
- 2010-11-30 US US13/511,853 patent/US8777160B2/en active Active
Also Published As
Publication number | Publication date |
---|---|
CA2781777C (fr) | 2018-10-30 |
FR2953193A1 (fr) | 2011-06-03 |
CA2781777A1 (fr) | 2011-06-03 |
WO2011064519A2 (fr) | 2011-06-03 |
CN102741118A (zh) | 2012-10-17 |
CN102741118B (zh) | 2015-04-08 |
US20120267478A1 (en) | 2012-10-25 |
WO2011064519A3 (fr) | 2011-08-11 |
US8777160B2 (en) | 2014-07-15 |
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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 |
|
PLFP | Fee payment |
Year of fee payment: 11 |
|
PLFP | Fee payment |
Year of fee payment: 12 |
|
ST | Notification of lapse |
Effective date: 20220705 |