BRPI0923172A2 - estrutura da zona de introdução de carga na extremidade traseira de uma aeronave - Google Patents
estrutura da zona de introdução de carga na extremidade traseira de uma aeronaveInfo
- Publication number
- BRPI0923172A2 BRPI0923172A2 BRPI0923172A BRPI0923172A BRPI0923172A2 BR PI0923172 A2 BRPI0923172 A2 BR PI0923172A2 BR PI0923172 A BRPI0923172 A BR PI0923172A BR PI0923172 A BRPI0923172 A BR PI0923172A BR PI0923172 A2 BRPI0923172 A2 BR PI0923172A2
- Authority
- BR
- Brazil
- Prior art keywords
- aircraft
- rear end
- zone structure
- introduction zone
- cargo
- 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
- B64C1/26—Attaching the wing or tail units or stabilising surfaces
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Body Structure For Vehicles (AREA)
- Connection Of Plates (AREA)
- Heterocyclic Carbon Compounds Containing A Hetero Ring Having Oxygen Or Sulfur (AREA)
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| ES200803604A ES2385993B1 (es) | 2008-12-18 | 2008-12-18 | Fuselaje trasero de una aeronave con una zona de introducción de carga de un estabilizador horizontal de cola y de un estabilizador vertical de cola que comprende elementos receptores de las cargas de dichos estabilizadores unidos a elementos estructurales del fuselaje. |
| PCT/ES2009/070608 WO2010070184A1 (es) | 2008-12-18 | 2009-12-18 | Estructura de la zona de introducción de cargas en el fuselaje trasero de una aeronave |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| BRPI0923172A2 true BRPI0923172A2 (pt) | 2016-02-16 |
Family
ID=42109917
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| BRPI0923172A BRPI0923172A2 (pt) | 2008-12-18 | 2009-12-18 | estrutura da zona de introdução de carga na extremidade traseira de uma aeronave |
Country Status (8)
| Country | Link |
|---|---|
| US (1) | US8267352B2 (pt) |
| EP (1) | EP2371704B1 (pt) |
| CN (1) | CN102307782B (pt) |
| BR (1) | BRPI0923172A2 (pt) |
| CA (1) | CA2747690C (pt) |
| ES (1) | ES2385993B1 (pt) |
| RU (1) | RU2514301C2 (pt) |
| WO (1) | WO2010070184A1 (pt) |
Families Citing this family (31)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE102006026169B4 (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 |
| DE102006026170B4 (de) * | 2006-06-06 | 2012-06-21 | Airbus Operations Gmbh | Flugzeugrumpfstruktur und Verfahren zu deren Herstellung |
| US8167249B1 (en) | 2009-03-25 | 2012-05-01 | The Boeing Company | Controllable upper surface blown nozzle |
| US8403256B1 (en) | 2009-03-25 | 2013-03-26 | The Boeing Company | Swept-wing powered-lift aircraft |
| US8322655B1 (en) | 2009-03-25 | 2012-12-04 | The Boeing Company | Twin-boom empennage |
| US8353478B1 (en) | 2009-03-25 | 2013-01-15 | The Boeing Company | Blended wing aircraft |
| US8061655B1 (en) * | 2009-03-25 | 2011-11-22 | The Boeing Company | Aircraft configuration utilizing fuselage, wing, empennage, and exhaust flow control devices |
| ES2378702B1 (es) * | 2009-04-21 | 2013-02-28 | Airbus Operations, S.L. | Herrajes para la cogida del estabilizador vertical de cola de una aeronave. |
| US8382045B2 (en) | 2009-07-21 | 2013-02-26 | The Boeing Company | Shape-changing control surface |
| ES2400769B1 (es) | 2010-10-19 | 2014-02-12 | Airbus Operations, S.L. | Herraje estanco para la cogida del estabilizador vertical de cola de una aeronave. |
| EP2599711B1 (en) * | 2011-12-01 | 2017-07-26 | Airbus Operations S.L. | Highly loaded frame of an aircraft fuselage with a lattice structured web |
| EP2634086A1 (en) | 2012-02-28 | 2013-09-04 | Airbus Operations S.L. | Reinforcing structure integrated in the internal structure of an aircraft of composite material |
| IL223443A (en) * | 2012-12-04 | 2014-06-30 | Elbit Systems Cyclone Ltd | Buildings from composite materials with integral composite connectors and manufacturing methods |
| CN103625631A (zh) * | 2013-08-23 | 2014-03-12 | 中国航空工业集团公司西安飞机设计研究所 | 一种垂尾对接结构设计方法 |
| CN103434636B (zh) * | 2013-09-03 | 2016-08-17 | 中国商用飞机有限责任公司 | 连接飞机垂尾的机身对接结构及包括机身对接结构的飞机 |
| CN106184697B (zh) * | 2016-09-14 | 2019-02-05 | 北京航空航天大学 | 一种直线贯穿构架式复合材料机身结构 |
| DE102017117314A1 (de) | 2017-07-31 | 2019-01-31 | Airbus Operations Gmbh | Befestigungseinheit zum beweglichen Befestigen einer Luftfahrzeugkomponente an einer Tragstruktur eines Luftfahrzeugs |
| EP3626607A1 (en) * | 2018-09-18 | 2020-03-25 | Airbus Operations GmbH | An aircraft component |
| CN109720544A (zh) * | 2018-11-12 | 2019-05-07 | 中航通飞研究院有限公司 | 一种大型水上飞机机身垂尾对接结构 |
| EP3653490B1 (en) * | 2018-11-16 | 2024-01-03 | Airbus Operations, S.L.U. | Frame assembly for a rear section of an aircraft and rear section of an aircraft comprising said frame assembly |
| CN111237083B (zh) * | 2018-11-28 | 2022-01-11 | 海鹰航空通用装备有限责任公司 | 组合喷管结构及具有其的飞机 |
| CN110203373B (zh) * | 2019-05-24 | 2022-04-08 | 成都飞机工业（集团）有限责任公司 | 一种无人机垂平尾拆卸结构 |
| CN110920867B (zh) * | 2019-12-09 | 2023-04-14 | 中航沈飞民用飞机有限责任公司 | 一种民用客机平尾侧向惯性载荷承载铰链接头 |
| US11511846B2 (en) * | 2020-05-27 | 2022-11-29 | The Boeing Company | Aircraft with multi spar box connection to fuselage |
| US11370523B2 (en) * | 2020-05-27 | 2022-06-28 | The Boeing Company | Aircraft with multi spar box connection to fuselage |
| US12404003B2 (en) | 2020-08-12 | 2025-09-02 | The Boeing Company | CFRP fuselage frame with securement to vertical tail fin |
| US11932398B2 (en) | 2020-08-24 | 2024-03-19 | The Boeing Company | Horizontal stabilizer assembly for an aircraft |
| CN112141360B (zh) * | 2020-10-14 | 2024-08-20 | 中国商用飞机有限责任公司北京民用飞机技术研究中心 | 一种垂尾盒段试验支撑假件及试验设备 |
| CN113955080B (zh) * | 2021-11-29 | 2023-10-20 | 中国商用飞机有限责任公司 | 配平式的平尾连接结构 |
| US12404004B1 (en) * | 2024-02-29 | 2025-09-02 | Pipistrel D.O.O. | Wing-fuselage joint |
Family Cites Families (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2212456A (en) * | 1937-09-16 | 1940-08-20 | Arado Fiugzeugwerke Gmbh | Shell or fuselage for aircraft |
| FR2632604B1 (fr) * | 1988-06-08 | 1991-07-12 | Aerospatiale | Cadre en materiau composite notamment pour fuselage d'aeronef, et son procede de fabrication |
| SU1762750A3 (ru) * | 1990-06-11 | 1992-09-15 | Акционерное Общество "Авиатика" (Su) | Аэродинамический руль самолета |
| JP4318381B2 (ja) * | 2000-04-27 | 2009-08-19 | 本田技研工業株式会社 | 繊維強化複合材からなる胴体構造体の製造方法、及びそれにより製造される胴体構造体 |
| RU2207299C1 (ru) * | 2002-03-29 | 2003-06-27 | Акционерное общество открытого типа "ОКБ Сухого" | Цельноповоротное горизонтальное оперение |
| RU2270783C1 (ru) * | 2004-09-07 | 2006-02-27 | Открытое акционерное общество Таганрогский авиационный научно-технический комплекс им. Г.М. Бериева | Хвостовая часть транспортного самолета |
| DE102005003297B4 (de) * | 2005-01-24 | 2007-03-29 | Eads Deutschland Gmbh | Flugzeug mit einer Rumpfhecksektion zur Anbindung von Höhen- und Seitenleitwerken |
| DE102005003296B4 (de) * | 2005-01-24 | 2007-03-29 | Eads Deutschland Gmbh | Rumpfhecksektion eines Flugzeugs |
| CN100509560C (zh) * | 2006-05-29 | 2009-07-08 | 空中客车德国有限公司 | 机翼调节 |
| ES2315109B1 (es) * | 2006-06-30 | 2010-01-12 | Airbus España, S.L. | Herraje con cajon de torsion, de material plastico reforzado con fibras de carbono, para acoplar un conjunto motor de accionamiento / husillo para el trimado de un estabilizador horizontal de una aeronave. |
| WO2008092970A1 (es) | 2007-01-29 | 2008-08-07 | Airbus España, S.L. | Cuaderna de carga de aeronave en material compuesto |
-
2008
- 2008-12-18 ES ES200803604A patent/ES2385993B1/es not_active Expired - Fee Related
-
2009
- 2009-02-19 US US12/388,750 patent/US8267352B2/en not_active Expired - Fee Related
- 2009-12-18 EP EP09808939A patent/EP2371704B1/en not_active Not-in-force
- 2009-12-18 CA CA2747690A patent/CA2747690C/en not_active Expired - Fee Related
- 2009-12-18 BR BRPI0923172A patent/BRPI0923172A2/pt not_active Application Discontinuation
- 2009-12-18 RU RU2011129629/11A patent/RU2514301C2/ru not_active IP Right Cessation
- 2009-12-18 CN CN200980155891.5A patent/CN102307782B/zh not_active Expired - Fee Related
- 2009-12-18 WO PCT/ES2009/070608 patent/WO2010070184A1/es not_active Ceased
Also Published As
| Publication number | Publication date |
|---|---|
| CA2747690A1 (en) | 2010-06-24 |
| RU2514301C2 (ru) | 2014-04-27 |
| RU2011129629A (ru) | 2013-01-27 |
| EP2371704B1 (en) | 2012-09-26 |
| CN102307782A (zh) | 2012-01-04 |
| ES2385993A1 (es) | 2012-08-06 |
| CN102307782B (zh) | 2014-04-09 |
| ES2385993B1 (es) | 2013-06-17 |
| EP2371704A1 (en) | 2011-10-05 |
| US20100155532A1 (en) | 2010-06-24 |
| US8267352B2 (en) | 2012-09-18 |
| WO2010070184A1 (es) | 2010-06-24 |
| CA2747690C (en) | 2017-02-21 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| B11A | Dismissal acc. art.33 of ipl - examination not requested within 36 months of filing | ||
| B11Y | Definitive dismissal - extension of time limit for request of examination expired [chapter 11.1.1 patent gazette] |