BRPI0816864A2 - caverna de pressão e método para subdivisão de uma aeronave ou espaçonave. - Google Patents
caverna de pressão e método para subdivisão de uma aeronave ou espaçonave.Info
- Publication number
- BRPI0816864A2 BRPI0816864A2 BRPI0816864A BRPI0816864A BRPI0816864A2 BR PI0816864 A2 BRPI0816864 A2 BR PI0816864A2 BR PI0816864 A BRPI0816864 A BR PI0816864A BR PI0816864 A BRPI0816864 A BR PI0816864A BR PI0816864 A2 BRPI0816864 A2 BR PI0816864A2
- Authority
- BR
- Brazil
- Prior art keywords
- aircraft
- inner contour
- subdivision
- edge
- spacecraft
- 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
- B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
- B64C1/10—Bulkheads
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Connection Of Plates (AREA)
- Gasket Seals (AREA)
- Pressure Vessels And Lids Thereof (AREA)
- Compositions Of Oxide Ceramics (AREA)
- Physical Vapour Deposition (AREA)
- Superstructure Of Vehicle (AREA)
- Laminated Bodies (AREA)
- Tires In General (AREA)
- Printing Plates And Materials Therefor (AREA)
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US97328607P | 2007-09-18 | 2007-09-18 | |
| DE102007044388A DE102007044388B4 (de) | 2007-09-18 | 2007-09-18 | Druckschott und Verfahren zum Unterteilen eines Luft- oder Raumfahrzeugs |
| PCT/EP2008/057700 WO2009037008A1 (de) | 2007-09-18 | 2008-06-18 | Druckschott und verfahren zum unterteilen eines luft- oder raumfahrzeugs |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| BRPI0816864A2 true BRPI0816864A2 (pt) | 2017-05-16 |
Family
ID=40384067
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| BRPI0816864A BRPI0816864A2 (pt) | 2007-09-18 | 2008-06-18 | caverna de pressão e método para subdivisão de uma aeronave ou espaçonave. |
Country Status (10)
| Country | Link |
|---|---|
| US (1) | US8444089B2 (pt) |
| EP (1) | EP2190734B1 (pt) |
| JP (1) | JP2010538892A (pt) |
| CN (1) | CN101801783B (pt) |
| AT (1) | ATE502846T1 (pt) |
| BR (1) | BRPI0816864A2 (pt) |
| CA (1) | CA2698422A1 (pt) |
| DE (2) | DE102007044388B4 (pt) |
| RU (1) | RU2471672C2 (pt) |
| WO (1) | WO2009037008A1 (pt) |
Families Citing this family (36)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE102006027707A1 (de) * | 2006-06-14 | 2007-12-20 | Airbus Deutschland Gmbh | Heckstruktur 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 |
| ES2347122B1 (es) * | 2009-03-31 | 2011-08-11 | Airbus Operations, S.L. | Estructura de ensamblaje del mamparo de presion de una aeronave. |
| US8759356B2 (en) * | 2009-05-19 | 2014-06-24 | Dow Agrosciences, Llc. | Compounds and methods for controlling fungi |
| FR2953193B1 (fr) * | 2009-11-30 | 2012-03-16 | Airbus Operations Sas | Aeronef comportant une cloison interne |
| FR2979897B1 (fr) * | 2011-09-13 | 2014-08-22 | Airbus Operations Sas | Dispositif de liaison entre une lisse et un cadre d'une structure d'un aeronef |
| DE102012005451A1 (de) * | 2012-03-20 | 2013-09-26 | Airbus Operations Gmbh | Druckrumpf eines Luftfahrzeuges, mit einer Rumpfschale und einem hierin angeordneten Druckschott |
| DE102012011027A1 (de) * | 2012-06-05 | 2013-12-05 | Airbus Operations Gmbh | Druckrumpf eines Luftfahrzeugs, mit einer Rumpfstruktur und einem hierin speziell befestigten Druckschott |
| DE102012016553A1 (de) * | 2012-08-22 | 2014-02-27 | Airbus Operations Gmbh | Druckrumpf eines Flugzeugs, der ein Druckschott umfasst |
| FR2998548B1 (fr) * | 2012-11-23 | 2015-01-30 | Airbus Operations Sas | Nacelle d'aeronef comprenant une liaison renforcee entre une entree d'air et une motorisation |
| FR3005936B1 (fr) * | 2013-05-24 | 2016-08-19 | Airbus Operations Sas | Plaque de support pour le passage de systemes entre deux zones a pressurisations differentes d'un aeronef. |
| US10189578B2 (en) * | 2013-06-12 | 2019-01-29 | The Boeing Company | Self-balancing pressure bulkhead |
| DE102013114391A1 (de) * | 2013-12-18 | 2015-06-18 | Airbus Operations Gmbh | Druckrumpf eines Flugzeuges, umfassend ein bewegbar relativ zur Rumpfstruktur befestigtes Druckschott |
| EP3064429A1 (en) * | 2015-03-06 | 2016-09-07 | Airbus Operations GmbH | Pressure bulkhead adapted to non-circular fuselage section |
| ES2709346T3 (es) * | 2015-03-06 | 2019-04-16 | Airbus Operations Gmbh | Mamparo de presión trasero extendido |
| EP3095688B1 (en) | 2015-05-20 | 2017-10-04 | Airbus Operations GmbH | A pressure bulkhead for an aircraft fuselage |
| EP3095689B1 (en) | 2015-05-20 | 2017-10-04 | Airbus Operations GmbH | A pressure bulkhead for an aircraft fuselage |
| DE102015111160B4 (de) * | 2015-07-09 | 2018-09-06 | Airbus Operations Gmbh | Rumpfstruktur und Verfahren zum Herstellen einer Rumpfstruktur |
| DE102015111935A1 (de) * | 2015-07-22 | 2017-01-26 | Airbus Operations Gmbh | Druckschott für einen Flugzeugrumpf |
| ES2733055T3 (es) * | 2015-12-03 | 2019-11-27 | Airbus Operations Sl | Mamparo de presión |
| ES2777281T3 (es) * | 2015-12-18 | 2020-08-04 | Airbus Operations Sl | Mamparo de presión |
| US10173765B2 (en) | 2016-04-07 | 2019-01-08 | The Boeing Company | Pressure bulkhead apparatus |
| US10926857B2 (en) * | 2016-06-17 | 2021-02-23 | The Boeing Company | Pressurized bulkhead |
| CN106392427A (zh) * | 2016-11-25 | 2017-02-15 | 哈尔滨工业大学 | 一种用于t型结构梁肋焊接定位装置 |
| US10926858B2 (en) * | 2017-08-07 | 2021-02-23 | The Boeing Company | Pressure bulkhead system |
| DE102017219213A1 (de) * | 2017-10-26 | 2019-05-02 | Airbus Operations Gmbh | Flaches Druckschott für ein Luft- oder Raumfahrzeug und Luft- oder Raumfahrzeug |
| DE102017130816A1 (de) * | 2017-12-20 | 2019-06-27 | Airbus Operations Gmbh | Druckschott für eine Druckkabine eines Luft- und Raumfahrzeugs sowie Luft- und Raumfahrzeug |
| US20200122816A1 (en) * | 2018-10-22 | 2020-04-23 | The Boeing Company | Bulkhead joint assembly |
| CN109590726B (zh) * | 2018-11-26 | 2020-09-15 | 首都航天机械有限公司 | 一种超大直径筒段壳体的装配方法 |
| CN109878692B (zh) * | 2019-02-28 | 2022-03-04 | 西北工业大学 | 一种用于非圆截面增压舱尖角处自气密的气囊装置 |
| EP4035993A1 (en) * | 2021-01-27 | 2022-08-03 | The Boeing Company | Connector to connect a center wing box to a bulkhead of an aircraft |
| 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 |
| CN112849420B (zh) * | 2021-02-03 | 2022-12-13 | 中国工程物理研究院总体工程研究所 | 一种分区域分舱密封结构 |
| CN114715442B (zh) * | 2022-04-18 | 2023-01-10 | 北京理工大学 | 载人航天器的头锥结构 |
| CN115817788B (zh) * | 2022-12-28 | 2026-01-30 | 中国商用飞机有限责任公司 | 货舱挡板连接结构、货舱挡板组件及包括该组件的飞机 |
| CN119872924B (zh) * | 2025-01-06 | 2025-11-07 | 北京空间飞行器总体设计部 | 一种大跨度连续加筋整体壁板式密封舱壳体结构 |
Family Cites Families (25)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB576091A (en) * | 1942-07-16 | 1946-03-19 | Westland Aircraft Ltd | Improvements in or relating to hinging devices for aircraft doors or bulkheads |
| US4674712A (en) * | 1985-01-22 | 1987-06-23 | The Boeing Company | Double-lobe fuselage composite airplane |
| DE3534719A1 (de) * | 1985-09-28 | 1987-04-02 | Messerschmitt Boelkow Blohm | Druckwand fuer einen unter inneren ueberdruck setzbaren rumpf eines luftfahrzeuges |
| JPS62203899A (ja) * | 1986-03-02 | 1987-09-08 | 有吉 一夫 | 航空機胴体尾部の圧力隔壁保持構造 |
| DE3844080C2 (de) * | 1988-12-28 | 1993-12-23 | Deutsche Aerospace Airbus | Druckwand für einen Flugzeugrumpf |
| DE3923871A1 (de) * | 1989-02-28 | 1991-01-31 | Dornier Luftfahrt | Druckspant |
| DE4002447C1 (en) * | 1990-01-27 | 1991-03-14 | Deutsche Airbus Gmbh, 2103 Hamburg, De | Decompression panel esp. for aircraft - consists of plate which is releasably held in de-compression opening and consists of two inter-strapped plate parts |
| JPH07291197A (ja) | 1994-04-22 | 1995-11-07 | Mitsubishi Heavy Ind Ltd | サンドイッチ球殻構造物及びその製作方法 |
| FR2735166B1 (fr) * | 1995-06-08 | 1997-08-29 | Aerospatiale | Procede de fabrication d'un panneau ou analogue a proprietes structurale et acoustique et panneau ainsi obtenu |
| AT405813B (de) * | 1997-11-10 | 1999-11-25 | Fischer Adv Components Gmbh | Druckspant, insbesondere für flugzeuge |
| US5899412A (en) * | 1997-12-19 | 1999-05-04 | Northrop Grumman Corporation | Aircraft pressure containment assembly module |
| US6276866B1 (en) * | 1998-09-22 | 2001-08-21 | Elbert Rutan | Tensioned structural composite joint |
| US6213426B1 (en) | 1999-07-09 | 2001-04-10 | The Boeing Company | Monolithic structure with redundant load paths |
| JP3997047B2 (ja) * | 2000-05-01 | 2007-10-24 | 本田技研工業株式会社 | スキンと圧力隔壁の接合構造体 |
| CN1162302C (zh) * | 2001-02-26 | 2004-08-18 | 厦门航空有限公司 | 一种延长飞机货舱侧壁板寿命的方法及防撞型侧壁板结构 |
| US6494404B1 (en) * | 2001-08-14 | 2002-12-17 | John C. Meyer | Passenger airplane container system |
| CN1723122A (zh) * | 2002-10-10 | 2006-01-18 | 霍尼韦尔国际公司 | 耐冲击和耐火复合材料 |
| ITMI20031086A1 (it) * | 2003-05-30 | 2004-11-30 | Milano Politecnico | Struttura localmente cedevole ad alto assorbimento di energia e metodo per aumentare la sicurezza passiva di una struttura, in particolare una struttura per applicazioni aeronautiche |
| FR2862607B1 (fr) * | 2003-11-24 | 2007-03-23 | Airbus France | Cloison pour aeronef destinee a separer une partie cargo d'un cockpit ou d'un compartiment passager |
| DE102006029231B4 (de) * | 2006-06-26 | 2013-09-26 | Airbus Operations Gmbh | Druckschott für einen Rumpf für die Luft- und Raumfahrt |
| US20080179459A1 (en) * | 2007-01-30 | 2008-07-31 | Airbus Espana, S.L. | Pressure bulkhead made of composite material for an aircraft |
| 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 |
| ES2399173T3 (es) * | 2008-03-31 | 2013-03-26 | Honda Patents & Technologies North America, Llc | Mamparo de presión para avión |
| DE102010018933B4 (de) * | 2010-04-30 | 2014-05-08 | Airbus Operations Gmbh | Druckschott zur Anordnung in einem Luftfahrzeugrumpf |
-
2007
- 2007-09-18 DE DE102007044388A patent/DE102007044388B4/de not_active Expired - Fee Related
-
2008
- 2008-06-18 WO PCT/EP2008/057700 patent/WO2009037008A1/de not_active Ceased
- 2008-06-18 US US12/678,723 patent/US8444089B2/en not_active Expired - Fee Related
- 2008-06-18 AT AT08774132T patent/ATE502846T1/de active
- 2008-06-18 RU RU2010114853/11A patent/RU2471672C2/ru not_active IP Right Cessation
- 2008-06-18 EP EP08774132A patent/EP2190734B1/de not_active Not-in-force
- 2008-06-18 DE DE502008002962T patent/DE502008002962D1/de active Active
- 2008-06-18 CN CN200880107542.1A patent/CN101801783B/zh active Active
- 2008-06-18 JP JP2010524422A patent/JP2010538892A/ja active Pending
- 2008-06-18 CA CA2698422A patent/CA2698422A1/en not_active Abandoned
- 2008-06-18 BR BRPI0816864A patent/BRPI0816864A2/pt not_active IP Right Cessation
Also Published As
| Publication number | Publication date |
|---|---|
| EP2190734A1 (de) | 2010-06-02 |
| RU2010114853A (ru) | 2011-10-27 |
| JP2010538892A (ja) | 2010-12-16 |
| CA2698422A1 (en) | 2009-03-26 |
| CN101801783B (zh) | 2014-05-21 |
| DE502008002962D1 (de) | 2011-05-05 |
| EP2190734B1 (de) | 2011-03-23 |
| US8444089B2 (en) | 2013-05-21 |
| DE102007044388A1 (de) | 2009-04-02 |
| US20100230539A1 (en) | 2010-09-16 |
| RU2471672C2 (ru) | 2013-01-10 |
| ATE502846T1 (de) | 2011-04-15 |
| CN101801783A (zh) | 2010-08-11 |
| WO2009037008A1 (de) | 2009-03-26 |
| DE102007044388B4 (de) | 2012-08-02 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| B08F | Application dismissed because of non-payment of annual fees [chapter 8.6 patent gazette] | ||
| B08K | Patent lapsed as no evidence of payment of the annual fee has been furnished to inpi [chapter 8.11 patent gazette] | ||
| B350 | Update of information on the portal [chapter 15.35 patent gazette] |