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
Application number
BRPI0816864A
Other languages
English (en)
Inventor
Stephan Andreas
Mischereit Stephan
Original Assignee
Airbus Operations Gmbh
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Airbus Operations Gmbh filed Critical Airbus Operations Gmbh
Publication of BRPI0816864A2 publication Critical patent/BRPI0816864A2/pt

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C1/00Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/06Frames; Stringers; Longerons ; Fuselage sections
    • B64C1/10Bulkheads

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)
  • Superstructure Of Vehicle (AREA)
  • Printing Plates And Materials Therefor (AREA)
  • Laminated Bodies (AREA)
  • Physical Vapour Deposition (AREA)
  • Tires In General (AREA)
BRPI0816864A 2007-09-18 2008-06-18 caverna de pressão e método para subdivisão de uma aeronave ou espaçonave. BRPI0816864A2 (pt)

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)

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* Cited by examiner, † Cited by third party
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.
CN102438993A (zh) * 2009-05-19 2012-05-02 陶氏益农公司 用于控制真菌的化合物和方法
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
ES2709346T3 (es) * 2015-03-06 2019-04-16 Airbus Operations Gmbh Mamparo de presión trasero extendido
EP3064429A1 (en) * 2015-03-06 2016-09-07 Airbus Operations GmbH Pressure bulkhead adapted to non-circular fuselage section
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
EP3176072B1 (en) * 2015-12-03 2019-04-03 Airbus Operations S.L. Pressure bulkhead
EP3181442B1 (en) * 2015-12-18 2019-12-18 Airbus Operations S.L. Pressure bulkhead for an aircraft
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
CN114802698B (zh) * 2021-01-27 2026-02-24 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
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

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US4674712A (en) * 1985-01-22 1987-06-23 The Boeing Company Double-lobe fuselage composite airplane
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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
EP2259965B1 (en) * 2008-03-31 2013-01-09 Honda Patents & Technologies North America, LLC Pressure bulkhead for aircraft
DE102010018933B4 (de) * 2010-04-30 2014-05-08 Airbus Operations Gmbh Druckschott zur Anordnung in einem Luftfahrzeugrumpf

Also Published As

Publication number Publication date
RU2471672C2 (ru) 2013-01-10
RU2010114853A (ru) 2011-10-27
EP2190734A1 (de) 2010-06-02
DE102007044388B4 (de) 2012-08-02
US8444089B2 (en) 2013-05-21
CN101801783A (zh) 2010-08-11
ATE502846T1 (de) 2011-04-15
DE502008002962D1 (de) 2011-05-05
JP2010538892A (ja) 2010-12-16
CN101801783B (zh) 2014-05-21
CA2698422A1 (en) 2009-03-26
DE102007044388A1 (de) 2009-04-02
WO2009037008A1 (de) 2009-03-26
US20100230539A1 (en) 2010-09-16
EP2190734B1 (de) 2011-03-23

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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]