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

    • 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)
  • Compositions Of Oxide Ceramics (AREA)
  • Pressure Vessels And Lids Thereof (AREA)
  • Physical Vapour Deposition (AREA)
  • Superstructure Of Vehicle (AREA)
  • Laminated Bodies (AREA)
  • Printing Plates And Materials Therefor (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)

Families Citing this family (32)

* 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.
BRPI1011058A2 (pt) * 2009-05-19 2015-08-25 Dow Agrosciences Llc Compostos e metodos controlar fungos
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
EP3064430B1 (en) * 2015-03-06 2018-11-14 Airbus Operations GmbH Extended rear pressure bulkhead
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
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
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

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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
WO2009124023A1 (en) * 2008-03-31 2009-10-08 Honda Motor Co., Ltd. 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
CA2698422A1 (en) 2009-03-26
RU2010114853A (ru) 2011-10-27
JP2010538892A (ja) 2010-12-16
CN101801783A (zh) 2010-08-11
EP2190734A1 (de) 2010-06-02
CN101801783B (zh) 2014-05-21
DE102007044388B4 (de) 2012-08-02
DE102007044388A1 (de) 2009-04-02
US8444089B2 (en) 2013-05-21
RU2471672C2 (ru) 2013-01-10
DE502008002962D1 (de) 2011-05-05
US20100230539A1 (en) 2010-09-16
ATE502846T1 (de) 2011-04-15
EP2190734B1 (de) 2011-03-23
WO2009037008A1 (de) 2009-03-26

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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]