FR2984845B1 - Element de structure de fuselage d'aeronef anti deversement - Google Patents
Element de structure de fuselage d'aeronef anti deversementInfo
- Publication number
- FR2984845B1 FR2984845B1 FR1162138A FR1162138A FR2984845B1 FR 2984845 B1 FR2984845 B1 FR 2984845B1 FR 1162138 A FR1162138 A FR 1162138A FR 1162138 A FR1162138 A FR 1162138A FR 2984845 B1 FR2984845 B1 FR 2984845B1
- Authority
- FR
- France
- Prior art keywords
- structure element
- aircraft fuselage
- fuselage structure
- speed aircraft
- speed
- 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
- B64C1/061—Frames
-
- 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
-
- 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
- B64C1/40—Sound or heat insulation, e.g. using insulation blankets
- B64C1/403—Arrangement of fasteners specially adapted therefor, e.g. of clips
- B64C1/406—Arrangement of fasteners specially adapted therefor, e.g. of clips in combination with supports for lines, e.g. for pipes or cables
-
- 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
- B64C2001/0054—Fuselage structures substantially made from particular materials
- B64C2001/0081—Fuselage structures substantially made from particular materials from metallic materials
-
- 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
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/13—Hollow or container type article [e.g., tube, vase, etc.]
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1162138A FR2984845B1 (fr) | 2011-12-21 | 2011-12-21 | Element de structure de fuselage d'aeronef anti deversement |
US13/716,903 US8967540B2 (en) | 2011-12-21 | 2012-12-17 | Anti lateral-torsional buckling structural member of an aircraft fuselage |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1162138A FR2984845B1 (fr) | 2011-12-21 | 2011-12-21 | Element de structure de fuselage d'aeronef anti deversement |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2984845A1 FR2984845A1 (fr) | 2013-06-28 |
FR2984845B1 true FR2984845B1 (fr) | 2014-07-11 |
Family
ID=45815761
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1162138A Expired - Fee Related FR2984845B1 (fr) | 2011-12-21 | 2011-12-21 | Element de structure de fuselage d'aeronef anti deversement |
Country Status (2)
Country | Link |
---|---|
US (1) | US8967540B2 (fr) |
FR (1) | FR2984845B1 (fr) |
Families Citing this family (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US9394056B2 (en) * | 2013-03-16 | 2016-07-19 | The Beoing Company | Air duct assembly and method of installing the same |
EP3083395B1 (fr) * | 2013-12-20 | 2021-09-08 | Saab Ab | Élément de raidissement et structure renforcée |
US9856008B2 (en) * | 2014-05-19 | 2018-01-02 | The Boeing Company | Composite structure and methods of forming thereof |
US9862122B2 (en) | 2014-08-14 | 2018-01-09 | The Boeing Company | Reinforced bladder |
FR3044291B1 (fr) * | 2015-11-27 | 2020-02-28 | Airbus Operations (S.A.S.) | Raidisseur d'aeronef a tete raidie |
FR3048311B1 (fr) * | 2016-02-26 | 2019-12-13 | Airbus Helicopters | Dispositif de protection de cable pour aeronef et aeronef |
US10144497B2 (en) * | 2016-04-18 | 2018-12-04 | The Boeing Company | Hat section door frame with integral gussets |
CN106626434B (zh) * | 2016-11-29 | 2019-03-08 | 中国航空工业集团公司沈阳飞机设计研究所 | 一种飞机复合材料隔框结构制造及设计方法 |
EP4036014A1 (fr) | 2018-03-28 | 2022-08-03 | Airbus Operations GmbH | Ensemble fuselage pour aéronef |
DE102018207763A1 (de) * | 2018-05-17 | 2019-11-21 | Airbus Operations Gmbh | Rumpfstruktur für ein Luftfahrzeug |
CA3131095A1 (fr) * | 2019-04-12 | 2020-10-15 | Ihi Aerospace Co., Ltd. | Dispositif de joint et procede d'assemblage pour ce dernier |
Family Cites Families (27)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1922371A (en) * | 1930-07-17 | 1933-08-15 | Russell G Jones | Aircraft |
US1907002A (en) * | 1931-10-05 | 1933-05-02 | Budd Edward G Mfg Co | Sheet metal airplane structure |
US2755216A (en) * | 1952-08-16 | 1956-07-17 | Douglas Aircraft Co Inc | Process for forming a multi-ducted shell |
US2941760A (en) * | 1954-12-14 | 1960-06-21 | Rolls Royce | Aircraft structure |
US4671470A (en) * | 1985-07-15 | 1987-06-09 | Beech Aircraft Corporation | Method for fastening aircraft frame elements to sandwich skin panels covering same using woven fiber connectors |
US7051978B2 (en) * | 2004-03-29 | 2006-05-30 | The Boeing Company | Adaptable payload processes |
US7261256B2 (en) * | 2004-03-29 | 2007-08-28 | The Boeing Company | Variable-duct support assembly |
US7837147B2 (en) * | 2005-03-18 | 2010-11-23 | The Boeing Company | Systems and methods for reducing noise in aircraft fuselages and other structures |
DE102006002248B4 (de) * | 2006-01-17 | 2008-01-03 | Airbus Deutschland Gmbh | Strukturgebende Konstruktion für einen Flugzeugrumpf |
US8910908B2 (en) * | 2006-10-31 | 2014-12-16 | Airbus Operations Gmbh | Two-piece stiffening element |
US7871040B2 (en) * | 2006-11-10 | 2011-01-18 | The Boeing Company | Composite aircraft structures with hat stiffeners |
US8523110B2 (en) * | 2007-03-28 | 2013-09-03 | Airbus Operations Gmbh | Door frame component of cast titanium and structural fuselage part |
US8082667B2 (en) * | 2007-05-31 | 2011-12-27 | The Boeing Company | Apparatus and methods for securing a first structural member and a second structural member to one another |
DE102007030026A1 (de) * | 2007-06-29 | 2009-01-02 | Airbus Deutschland Gmbh | Strukturbauteil mit Spant- und Querträgerelement |
DE102007032233B4 (de) * | 2007-07-11 | 2014-07-10 | Airbus Operations Gmbh | Installationssystem für ein Flugzeug |
DE102007044389A1 (de) * | 2007-09-18 | 2009-04-02 | Airbus Deutschland Gmbh | Strukturbauteil und Rumpf eines Luft- oder Raumfahrzeugs |
FR2921898B1 (fr) * | 2007-10-08 | 2009-12-11 | Airbus France | Structure de fuselage pour fuselage d'aeronef en materiau composite et aeronef equipe d'une telle structure de fuselage |
FR2922518B1 (fr) * | 2007-10-18 | 2010-04-23 | Airbus France | Structure d'avion comportant des jonctions d'arrets de raidisseurs |
FR2928577B1 (fr) * | 2008-03-14 | 2011-11-25 | Airbus France | Procede de realisation d'un raidisseur evide en forme de omega et noyau pour la realisation d'un raidisseur evide en forme de omega |
FR2931720B1 (fr) * | 2008-06-02 | 2010-12-17 | Airbus France | Procede d'assemblage orbital de troncons d'aeronef en materiau composite |
US8336820B2 (en) * | 2008-10-27 | 2012-12-25 | Embraer S.A. | Aircraft cabin floor structures, systems and methods |
ES2382765B1 (es) * | 2009-06-29 | 2013-05-03 | Airbus Operations, S.L. | Diseño de cuadernas de aeronave |
FR2947241B1 (fr) * | 2009-06-29 | 2012-12-07 | Airbus France | Encadrement d'une ouverture menagee dans un fuselage d'aeronef |
ES2383986B1 (es) * | 2009-12-30 | 2013-05-16 | Airbus Operations, S.L. | Cuaderna de fuselaje de aeronave en material compuesto con alma estabilizada. |
ES2384349B1 (es) * | 2009-12-30 | 2013-05-16 | Airbus Operations, S.L. | Cuaderna de fuselaje de aeronave en material compuesto con costillas estabilizadoras. |
CN103261021B (zh) * | 2010-12-28 | 2016-01-20 | 贝尔直升机泰克斯特龙公司 | 多向负载连接系统 |
US8651419B2 (en) * | 2011-07-18 | 2014-02-18 | The Boeing Company | Flexible truss frame and method of making the same |
-
2011
- 2011-12-21 FR FR1162138A patent/FR2984845B1/fr not_active Expired - Fee Related
-
2012
- 2012-12-17 US US13/716,903 patent/US8967540B2/en not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
US8967540B2 (en) | 2015-03-03 |
FR2984845A1 (fr) | 2013-06-28 |
US20130164465A1 (en) | 2013-06-27 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PLFP | Fee payment |
Year of fee payment: 5 |
|
PLFP | Fee payment |
Year of fee payment: 6 |
|
PLFP | Fee payment |
Year of fee payment: 7 |
|
PLFP | Fee payment |
Year of fee payment: 9 |
|
ST | Notification of lapse |
Effective date: 20210805 |