BRPI0818306A2 - estrutura, em particular uma estrutura de fuselagem de uma aeronave ou espaçonave. - Google Patents
estrutura, em particular uma estrutura de fuselagem de uma aeronave ou espaçonave.Info
- Publication number
- BRPI0818306A2 BRPI0818306A2 BRPI0818306A BRPI0818306A BRPI0818306A2 BR PI0818306 A2 BRPI0818306 A2 BR PI0818306A2 BR PI0818306 A BRPI0818306 A BR PI0818306A BR PI0818306 A BRPI0818306 A BR PI0818306A BR PI0818306 A2 BRPI0818306 A2 BR PI0818306A2
- Authority
- BR
- Brazil
- Prior art keywords
- tension struts
- pressure cap
- cross
- aircraft
- spaceship
- 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)
- Pressure Vessels And Lids Thereof (AREA)
- Clamps And Clips (AREA)
- Tires In General (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
- Radio Relay Systems (AREA)
- Cooling, Air Intake And Gas Exhaust, And Fuel Tank Arrangements In Propulsion Units (AREA)
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US98403807P | 2007-10-31 | 2007-10-31 | |
DE102007052140A DE102007052140B4 (de) | 2007-10-31 | 2007-10-31 | Struktur, insbesondere Rumpfstruktur eines Luft- oder Raumfahrzeugs |
PCT/EP2008/064843 WO2009056643A2 (de) | 2007-10-31 | 2008-10-31 | Struktur, insbesondere rumpfstruktur eines luft- oder raumfahrzeugs |
Publications (1)
Publication Number | Publication Date |
---|---|
BRPI0818306A2 true BRPI0818306A2 (pt) | 2019-09-24 |
Family
ID=40530426
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BRPI0818306A BRPI0818306A2 (pt) | 2007-10-31 | 2008-10-31 | estrutura, em particular uma estrutura de fuselagem de uma aeronave ou espaçonave. |
Country Status (10)
Country | Link |
---|---|
US (1) | US8366043B2 (pt) |
EP (1) | EP2214957B1 (pt) |
JP (1) | JP2011500452A (pt) |
CN (1) | CN101842286B (pt) |
AT (1) | ATE506253T1 (pt) |
BR (1) | BRPI0818306A2 (pt) |
CA (1) | CA2703188A1 (pt) |
DE (2) | DE102007052140B4 (pt) |
RU (1) | RU2010116972A (pt) |
WO (1) | WO2009056643A2 (pt) |
Families Citing this family (30)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102007044389A1 (de) * | 2007-09-18 | 2009-04-02 | Airbus Deutschland Gmbh | Strukturbauteil und Rumpf eines Luft- oder Raumfahrzeugs |
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 |
DE102009033444A1 (de) * | 2009-07-16 | 2011-01-27 | Airbus Operations Gmbh | Schalensegment zur Herstellung einer Rumpfzellensektion für eine Rumpfzelle eines Flugzeugs |
DE102009035265B4 (de) | 2009-07-29 | 2013-06-06 | Airbus Operations Gmbh | Druckrumpf eines Luft- oder Raumfahrzeuges mit Druckkalotte |
DE102009049007A1 (de) | 2009-10-09 | 2011-04-21 | Airbus Operations Gmbh | Druckrumpf eines Flugzeuges mit heckseitiger Druckkalotte |
FR2953193B1 (fr) * | 2009-11-30 | 2012-03-16 | Airbus Operations Sas | Aeronef comportant une cloison interne |
WO2011144971A1 (en) * | 2010-05-20 | 2011-11-24 | Tecsis Tecnologia E Sistemas Avançados Ltda | A bulkhead for an aerogenerator blade root |
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 |
DE102011085793A1 (de) * | 2011-11-04 | 2013-05-08 | Airbus Operations Gmbh | Halterungsvorrichtung zum Haltern eines Kabels oder einer Leitung an einer Strukturkomponente eines Luft- oder Raumfahrzeugs sowie Luft- oder Raumfahrzeug |
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 |
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 |
EP2902229B1 (en) * | 2014-01-30 | 2019-03-06 | Airbus Operations GmbH | Door construction with gap sealing device and method for sealing a gap between a door and a door frame |
EP3064429A1 (en) * | 2015-03-06 | 2016-09-07 | Airbus Operations GmbH | Pressure bulkhead adapted to non-circular fuselage section |
EP3064430B1 (en) * | 2015-03-06 | 2018-11-14 | Airbus Operations GmbH | Extended rear pressure bulkhead |
DE102015111160B4 (de) * | 2015-07-09 | 2018-09-06 | Airbus Operations Gmbh | Rumpfstruktur und Verfahren zum Herstellen einer Rumpfstruktur |
US10173765B2 (en) * | 2016-04-07 | 2019-01-08 | The Boeing Company | Pressure bulkhead apparatus |
FR3049928B1 (fr) * | 2016-04-07 | 2018-04-20 | Airbus Operations | Troncon d'aeronef comprenant une cloison de pressurisation plane a poutres verticales |
US10926857B2 (en) * | 2016-06-17 | 2021-02-23 | The Boeing Company | Pressurized bulkhead |
US10926858B2 (en) * | 2017-08-07 | 2021-02-23 | The Boeing Company | Pressure bulkhead system |
CN109018437B (zh) * | 2018-06-21 | 2020-06-05 | 北京空间飞行器总体设计部 | 一种适用于航天器密封舱的舱板 |
EP3771635B1 (en) | 2019-07-30 | 2021-12-29 | Airbus SAS | Pressure bulkhead |
US11655016B2 (en) * | 2020-04-06 | 2023-05-23 | The Boeing Company | Pressurized monocoque structure with abrupt change in shape |
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 |
EP4035993A1 (en) | 2021-01-27 | 2022-08-03 | The Boeing Company | Connector to connect a center wing box to a bulkhead of an aircraft |
RU207867U1 (ru) * | 2021-04-26 | 2021-11-22 | Акционерное общество "Государственный ракетный центр имени академика В.П. Макеева" | Резьбовое соединение отсеков корпуса летательного аппарата |
EP4129818B1 (en) | 2021-08-03 | 2024-10-09 | Airbus Operations GmbH | An aircraft or spacecraft fuselage with a structural junction |
Family Cites Families (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE3534719A1 (de) | 1985-09-28 | 1987-04-02 | Messerschmitt Boelkow Blohm | Druckwand fuer einen unter inneren ueberdruck setzbaren rumpf eines luftfahrzeuges |
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 |
DE19652172C2 (de) * | 1996-12-14 | 1998-09-17 | Daimler Benz Aerospace Airbus | Druckspant für einen Flugzeugrumpf |
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 |
US5979831A (en) * | 1998-06-25 | 1999-11-09 | Mcdonnell Douglas Corporation | System and method for attaching a structural component to an aerospace vehicle |
US6213426B1 (en) * | 1999-07-09 | 2001-04-10 | The Boeing Company | Monolithic structure with redundant load paths |
JP2004339962A (ja) * | 2003-05-13 | 2004-12-02 | Honda Motor Co Ltd | 船外機における排気管のシール構造 |
US7766277B2 (en) * | 2006-01-19 | 2010-08-03 | The Boeing Company | Deformable forward pressure bulkhead for an aircraft |
DE102006044683A1 (de) * | 2006-02-07 | 2007-08-23 | Grob, Margret | Flugzeugkörper und Verfahren zu seiner Herstellung |
DE102007052140B4 (de) * | 2007-10-31 | 2012-10-25 | Airbus Operations Gmbh | Struktur, insbesondere Rumpfstruktur eines Luft- oder Raumfahrzeugs |
-
2007
- 2007-10-31 DE DE102007052140A patent/DE102007052140B4/de not_active Expired - Fee Related
-
2008
- 2008-10-31 JP JP2010531539A patent/JP2011500452A/ja active Pending
- 2008-10-31 CA CA2703188A patent/CA2703188A1/en not_active Abandoned
- 2008-10-31 DE DE502008003315T patent/DE502008003315D1/de active Active
- 2008-10-31 BR BRPI0818306A patent/BRPI0818306A2/pt not_active IP Right Cessation
- 2008-10-31 CN CN200880114416.9A patent/CN101842286B/zh not_active Expired - Fee Related
- 2008-10-31 EP EP08844468A patent/EP2214957B1/de not_active Not-in-force
- 2008-10-31 AT AT08844468T patent/ATE506253T1/de active
- 2008-10-31 RU RU2010116972/11A patent/RU2010116972A/ru not_active Application Discontinuation
- 2008-10-31 WO PCT/EP2008/064843 patent/WO2009056643A2/de active Application Filing
- 2008-10-31 US US12/740,880 patent/US8366043B2/en not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
DE102007052140B4 (de) | 2012-10-25 |
EP2214957B1 (de) | 2011-04-20 |
EP2214957A2 (de) | 2010-08-11 |
RU2010116972A (ru) | 2011-12-10 |
JP2011500452A (ja) | 2011-01-06 |
ATE506253T1 (de) | 2011-05-15 |
WO2009056643A4 (de) | 2009-08-13 |
CN101842286A (zh) | 2010-09-22 |
CA2703188A1 (en) | 2009-05-07 |
US8366043B2 (en) | 2013-02-05 |
CN101842286B (zh) | 2014-02-26 |
WO2009056643A2 (de) | 2009-05-07 |
WO2009056643A3 (de) | 2009-06-18 |
DE102007052140A1 (de) | 2009-05-14 |
DE502008003315D1 (de) | 2011-06-01 |
US20110233334A1 (en) | 2011-09-29 |
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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] |
Free format text: EM VIRTUDE DO ARQUIVAMENTO PUBLICADO NA RPI 2543 DE 01-10-2019 E CONSIDERANDO AUSENCIA DE MANIFESTACAO DENTRO DOS PRAZOS LEGAIS, INFORMO QUE CABE SER MANTIDO O ARQUIVAMENTO DO PEDIDO DE PATENTE, CONFORME O DISPOSTO NO ARTIGO 12, DA RESOLUCAO 113/2013. |