BRPI0717929A2 - Invólucro reforçado para uma aeronave ou espaçonave com uma trave de laminado de alta rigidez e trave de laminado correspondente - Google Patents

Invólucro reforçado para uma aeronave ou espaçonave com uma trave de laminado de alta rigidez e trave de laminado correspondente

Info

Publication number
BRPI0717929A2
BRPI0717929A2 BRPI0717929-4A2A BRPI0717929A BRPI0717929A2 BR PI0717929 A2 BRPI0717929 A2 BR PI0717929A2 BR PI0717929 A BRPI0717929 A BR PI0717929A BR PI0717929 A2 BRPI0717929 A2 BR PI0717929A2
Authority
BR
Brazil
Prior art keywords
laminate body
spacon
correspondent
aircraft
high rigidity
Prior art date
Application number
BRPI0717929-4A2A
Other languages
English (en)
Inventor
Thomas Beumler
Original Assignee
Airbus 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 Gmbh filed Critical Airbus Gmbh
Publication of BRPI0717929A2 publication Critical patent/BRPI0717929A2/pt

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B15/00—Layered products comprising a layer of metal
    • B32B15/14—Layered products comprising a layer of metal next to a fibrous or filamentary layer
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B15/00—Layered products comprising a layer of metal
    • B32B15/20—Layered products comprising a layer of metal comprising aluminium or copper
    • 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
    • B64C1/064—Stringers; Longerons
    • 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
    • B64C1/068—Fuselage sections
    • 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)
  • Laminated Bodies (AREA)
  • Body Structure For Vehicles (AREA)
BRPI0717929-4A2A 2006-11-03 2007-11-02 Invólucro reforçado para uma aeronave ou espaçonave com uma trave de laminado de alta rigidez e trave de laminado correspondente BRPI0717929A2 (pt)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US85647106P 2006-11-03 2006-11-03
DE102006051989A DE102006051989B4 (de) 2006-11-03 2006-11-03 Versteifte Beplankung für ein Luft- oder Raumfahrzeug mit einem Laminat-Stringer hoher Steifigkeit
PCT/EP2007/061829 WO2008053041A1 (en) 2006-11-03 2007-11-02 Stiffened casing for an aircraft or spacecraft with a laminate stringer of high rigidity and corresponding laminate stringer

Publications (1)

Publication Number Publication Date
BRPI0717929A2 true BRPI0717929A2 (pt) 2013-11-05

Family

ID=39277445

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI0717929-4A2A BRPI0717929A2 (pt) 2006-11-03 2007-11-02 Invólucro reforçado para uma aeronave ou espaçonave com uma trave de laminado de alta rigidez e trave de laminado correspondente

Country Status (9)

Country Link
US (1) US8317134B2 (pt)
EP (1) EP2077942A1 (pt)
JP (1) JP2010508203A (pt)
CN (1) CN101535044B (pt)
BR (1) BRPI0717929A2 (pt)
CA (1) CA2662141A1 (pt)
DE (1) DE102006051989B4 (pt)
RU (1) RU2430856C2 (pt)
WO (1) WO2008053041A1 (pt)

Families Citing this family (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102006051989B4 (de) 2006-11-03 2010-09-30 Airbus Deutschland Gmbh Versteifte Beplankung für ein Luft- oder Raumfahrzeug mit einem Laminat-Stringer hoher Steifigkeit
WO2009048881A2 (en) * 2007-10-12 2009-04-16 Abe Karem Composite bulkhead and skin construction
DE102011004844A1 (de) * 2011-02-28 2012-08-30 Airbus Operations Gmbh Türrahmenverbund, Rumpfabschnitt sowie Luft- oder Raumfahrzeug
CN103518025B (zh) 2011-03-04 2016-09-07 M·I·布罗克韦尔 具有能量吸收作用的外部拉伸结构构件
CN102416739B (zh) * 2011-08-19 2013-09-18 北京航空航天大学 一种飞艇蒙皮材料及其制备方法
US9120276B2 (en) * 2012-07-25 2015-09-01 The Boeing Company Laminated composite bending and stiffening members with reinforcement by inter-laminar metal sheets
JP5959558B2 (ja) * 2014-03-13 2016-08-02 アイシン高丘株式会社 複合構造体及びその製造方法
EP3023669B1 (fr) * 2014-11-20 2020-12-30 Airbus (Sas) Dispositif d'absorption d'énergie cinétique et aéronef comportant un tel dispositif
US10093406B2 (en) 2014-12-10 2018-10-09 The Boeing Company Aircraft frame for tailstrike angle enhancement
EP3109152B1 (en) * 2015-06-24 2019-08-07 Airbus Operations GmbH Stiffened fuselage component as well as method and apparatus for manufacturing a stiffened fuselage component
CN105836104B (zh) * 2016-05-03 2019-02-01 中国乐凯集团有限公司 一种太阳能无人机机翼蒙皮材料及其制备方法
US10220935B2 (en) * 2016-09-13 2019-03-05 The Boeing Company Open-channel stiffener
RU2708862C1 (ru) * 2019-01-18 2019-12-11 Публичное акционерное общество "Авиационная холдинговая компания "Сухой" Способ изготовления детали и деталь из гибридного композиционного материала
US20200282694A1 (en) * 2019-03-07 2020-09-10 The Boeing Company Composite structure and method of forming thereof
RU2763410C1 (ru) * 2021-03-17 2021-12-29 Общество с ограниченной ответственностью "С 7 Космические Транспортные Системы" Топливный бак и способ его изготовления
CN114147994B (zh) * 2021-11-24 2023-05-05 航天特种材料及工艺技术研究所 一种复合材料舱体结构整体成型方法

Family Cites Families (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5429326A (en) 1992-07-09 1995-07-04 Structural Laminates Company Spliced laminate for aircraft fuselage
RU2143365C1 (ru) 1999-07-06 1999-12-27 Закрытое акционерное общество "Интеллект" Стрингер судна
DE19956394B4 (de) * 1999-11-24 2005-02-03 Airbus Deutschland Gmbh Verfahren zur Herstellung eines Profiles aus einem Hybridwerkstoff
DE10031510A1 (de) 2000-06-28 2002-01-17 Airbus Gmbh Strukturbauteil für ein Flugzeug
US6648273B2 (en) * 2001-10-30 2003-11-18 The Boeing Company Light weight and high strength fuselage
EP1336469A1 (en) * 2002-02-19 2003-08-20 Alenia Aeronautica S.P.A. Methods of manufacturing a stiffening element for an aircraft skin panel and a skin panel provided with the stiffening element
US7195210B2 (en) * 2002-10-10 2007-03-27 The Boeing Company Fiber matrix for a geometric morphing wing
US6910661B2 (en) * 2002-10-10 2005-06-28 The Boeing Company Geometric morphing wing
NL1022706C2 (nl) * 2003-02-17 2004-08-19 Stichting Fmlc Laminaat uit metaalplaten en elkaar kruisende dradenlagen uit verschillende materialen in kunststof.
US20050175813A1 (en) * 2004-02-10 2005-08-11 Wingert A. L. Aluminum-fiber laminate
US7255916B2 (en) * 2005-01-04 2007-08-14 Airbus Deutschland Gmbh Metallic layer material, reinforced with basalt fibers, as well as products made thereof
NL1030515C2 (nl) * 2005-11-24 2007-05-25 Gtm Consulting B V Laminaat uit metaalplaten en kunststof.
US7997529B2 (en) * 2006-01-19 2011-08-16 The Boeing Company Compliant panel for aircraft
US7766277B2 (en) * 2006-01-19 2010-08-03 The Boeing Company Deformable forward pressure bulkhead for an aircraft
NL2000100C2 (nl) * 2006-06-13 2007-12-14 Gtm Consulting B V Laminaat uit metaalplaten en kunststof.
NL2000232C2 (nl) * 2006-09-12 2008-03-13 Gtm Consulting B V Huidpaneel voor een vliegtuigromp.
DE102006051989B4 (de) 2006-11-03 2010-09-30 Airbus Deutschland Gmbh Versteifte Beplankung für ein Luft- oder Raumfahrzeug mit einem Laminat-Stringer hoher Steifigkeit
US7798443B2 (en) * 2006-12-18 2010-09-21 The Boeing Company Composite material for geometric morphing wing

Also Published As

Publication number Publication date
US8317134B2 (en) 2012-11-27
RU2430856C2 (ru) 2011-10-10
RU2009119050A (ru) 2010-12-10
WO2008053041B1 (en) 2008-06-19
CN101535044B (zh) 2013-11-06
CN101535044A (zh) 2009-09-16
US20100148004A1 (en) 2010-06-17
CA2662141A1 (en) 2008-05-08
DE102006051989A1 (de) 2008-05-15
WO2008053041A1 (en) 2008-05-08
JP2010508203A (ja) 2010-03-18
EP2077942A1 (en) 2009-07-15
DE102006051989B4 (de) 2010-09-30

Similar Documents

Publication Publication Date Title
BRPI0717929A2 (pt) Invólucro reforçado para uma aeronave ou espaçonave com uma trave de laminado de alta rigidez e trave de laminado correspondente
BRPI0917959A2 (pt) placa de blindagem e estrutura de veículo provida com a placa de blindagem
BRPI1012006A2 (pt) "disposição de articulação e/ou de mancal com uma camada intermediária elástica"
EP2080741A4 (en) HEATING ACCELERATOR AND SPRAYING TECHNOLOGY THEREWITH
EP2088980A4 (en) ELASTIC LAMINATE AND ABSORBENT ARTICLE COMPRISING THE LAMINATE
EP2080448A4 (en) DESK WALL AND DESK WITH DESK WORKING WALL
EP2370765A4 (en) HINGE ARRANGEMENT AND REFRIGERATOR WITH IT
BRPI0822842A2 (pt) Composição de estrutura de película e papelão tendo uma estrutura de película laminada com o mesmo
GB0607291D0 (en) Computing with both lock-step and free-step processor modes
DE602006015708D1 (de) en mit der Folie und Behälter mit den Formen oder mit den Etiketten versehen
TWI319089B (en) Probe block and probe assembly including the same
BRPI0923205A2 (pt) painéis de porta isolados flexíveis com defletores internos
EP2110408A4 (en) ADHESIVE AND MULTILAYER BODY USING THE SAME
BRPI0813038A2 (pt) "atuador para abrir uma carenagem de nacela de avião e nacela de motor de avião"
PL2034940T3 (pl) Artykuł jednorazowego użytku z praktycznymi oznaczeniami
ATE446738T1 (de) Körpergleitmittel mit polyethylenoxid
BRPI0911572A2 (pt) unidade de propulsão para uma aeronave e estrutura de entrada de ar para a referida unidade de propulsão
HK1140547A1 (en) Diagnosis and risk classification of acute coronary syndrome by means of ct-proet-1 in combination with nt-probnp ct-proet-1 nt-probnp
BRPI0719495A2 (pt) "Placa para onda"
DE112007002502A5 (de) Verschiebeeinheit und Gelenkwelle mit einer Verschiebeeinheit
GB2435457B (en) Aircraft wings and their assembly
GB0611215D0 (en) Static wing for an aircraft
BRPI0814081A2 (pt) Óxidos de nióbio de alta voltagem e capacitores contendo os mesmos
FR2937006B1 (fr) Porte de cabine d'aeronef
DE502006000632D1 (de) Flügelanordnung sowie Flugkörper

Legal Events

Date Code Title Description
B25D Requested change of name of applicant approved

Owner name: AIRBUS OPERATIONS GMBH (DE)

B08F Application dismissed because of non-payment of annual fees [chapter 8.6 patent gazette]

Free format text: REFERENTE A 7A ANUIDADE.

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: REFERENTE AO DESPACHO 8.6 PUBLICADO NA RPI 2278 DE 02/09/2014.