BRPI0816863A2 - componente estrutural e método para enrijecimento de um revestimento externo. - Google Patents

componente estrutural e método para enrijecimento de um revestimento externo.

Info

Publication number
BRPI0816863A2
BRPI0816863A2 BRPI0816863A BRPI0816863A BRPI0816863A2 BR PI0816863 A2 BRPI0816863 A2 BR PI0816863A2 BR PI0816863 A BRPI0816863 A BR PI0816863A BR PI0816863 A BRPI0816863 A BR PI0816863A BR PI0816863 A2 BRPI0816863 A2 BR PI0816863A2
Authority
BR
Brazil
Prior art keywords
reinforcing element
outer skin
reinforcing
spatial direction
structural component
Prior art date
Application number
BRPI0816863A
Other languages
English (en)
Inventor
Stephan Andreas
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 BRPI0816863A2 publication Critical patent/BRPI0816863A2/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
    • B64C1/12—Construction or attachment of skin panels
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49616—Structural member making
    • Y10T29/49622—Vehicular structural member making

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Connection Of Plates (AREA)
  • Application Of Or Painting With Fluid Materials (AREA)
  • Moulding By Coating Moulds (AREA)
  • Body Structure For Vehicles (AREA)
  • Laminated Bodies (AREA)
BRPI0816863A 2007-09-18 2008-06-10 componente estrutural e método para enrijecimento de um revestimento externo. BRPI0816863A2 (pt)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US97329107P 2007-09-18 2007-09-18
DE102007044386A DE102007044386A1 (de) 2007-09-18 2007-09-18 Strukturbauteil und Verfahren zum Versteifen einer Außenhaut
PCT/EP2008/057210 WO2009037005A1 (de) 2007-09-18 2008-06-10 STRUKTURBAUTEIL UND VERFAHREN ZUM VERSTEIFEN EINER AUßENHAUT

Publications (1)

Publication Number Publication Date
BRPI0816863A2 true BRPI0816863A2 (pt) 2017-05-16

Family

ID=40384065

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI0816863A BRPI0816863A2 (pt) 2007-09-18 2008-06-10 componente estrutural e método para enrijecimento de um revestimento externo.

Country Status (10)

Country Link
US (1) US8480030B2 (pt)
EP (1) EP2195234B1 (pt)
JP (1) JP2010538889A (pt)
CN (1) CN101848835B (pt)
AT (1) ATE519671T1 (pt)
BR (1) BRPI0816863A2 (pt)
CA (1) CA2698853A1 (pt)
DE (1) DE102007044386A1 (pt)
RU (1) RU2010108340A (pt)
WO (1) WO2009037005A1 (pt)

Families Citing this family (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102008012252B4 (de) * 2008-03-03 2014-07-31 Airbus Operations Gmbh Verbund sowie Luft- oder Raumfahrzeug mit einem derartigen Verbund
US20090266936A1 (en) 2008-04-29 2009-10-29 Fernando Ferreira Fernandez Aircraft fuselage structural components and methods of making same
DE102008002117B4 (de) * 2008-05-30 2013-10-31 Airbus Operations Gmbh Verbund und Struktur
DE102008044229A1 (de) * 2008-12-01 2010-06-10 Airbus Deutschland Gmbh Schalenbauteil für ein Luft- oder Raumfahrzeug
DE102009033444A1 (de) 2009-07-16 2011-01-27 Airbus Operations Gmbh Schalensegment zur Herstellung einer Rumpfzellensektion für eine Rumpfzelle eines Flugzeugs
FR2953158B1 (fr) * 2009-11-30 2012-01-20 Airbus Operations Sas Procede pour realiser une jonction etanche entre des pieces d'aeronef
ES2400771B1 (es) * 2011-03-30 2014-02-14 Airbus Operations S.L. Fuselaje de aeronave con cuadernas altamente resistentes.
DE102011085937B4 (de) * 2011-11-08 2017-06-01 Airbus Operations Gmbh Leichtbaustruktur, insbesondere Flugzeugprimärstruktur oder untergeordnete Baugruppe, sowie Verfahren zu deren Herstellung
FR3007735B1 (fr) * 2013-06-28 2015-08-07 Airbus Operations Sas Liaison d'un element de fuselage d'aeronef et d'un cadre par une entretoise et une cale
US9656319B2 (en) * 2013-11-13 2017-05-23 The Boeing Company Positioning system for electromagnetic riveting
EP2905221B1 (en) 2014-02-10 2018-07-04 Airbus Operations GmbH Method and apparatus for manufacturing a shell component for an aircraft or spacecraft
USD777014S1 (en) * 2014-08-12 2017-01-24 Servi-Sure, LLC Integrated stiffener
USD762456S1 (en) * 2015-05-29 2016-08-02 The Manadnock Company Stringer clip
USD762457S1 (en) * 2015-05-29 2016-08-02 The Monadnock Company Stringer clip
USD762106S1 (en) * 2015-05-29 2016-07-26 The Monadnock Company Stringer clip
US10590615B2 (en) 2016-06-28 2020-03-17 Vigor Industrial Llc Orthotropic deck
US10392132B2 (en) * 2016-07-29 2019-08-27 The Boeing Company Curved aircraft substructure repair systems and methods
GB2565351A (en) * 2017-08-11 2019-02-13 Airbus Operations Ltd Panel assembly
GB2579216A (en) * 2018-11-26 2020-06-17 Airbus Operations Ltd Aircraft fuel tank aperture sealing
DE102020205840B3 (de) * 2020-05-08 2021-06-10 Premium Aerotec Gmbh Verbinder und Verfahren zum Verbinden eines Spants und eines Stringers einer Rumpfstruktur eines Luftfahrzeugs, Rumpfstruktur und Luftfahrzeug

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5242523A (en) * 1992-05-14 1993-09-07 The Boeing Company Caul and method for bonding and curing intricate composite structures
US6766984B1 (en) * 1998-07-16 2004-07-27 Icom Engineering Corporation Stiffeners for aircraft structural panels
DE19844035C1 (de) * 1998-09-25 1999-11-25 Daimler Chrysler Aerospace Schalenbauteil für ein Flugzeug und Verfahren zur Herstellung
JP4526698B2 (ja) * 2000-12-22 2010-08-18 富士重工業株式会社 複合材成形品及びその製造方法
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
DE102004001049B4 (de) * 2004-01-05 2009-12-10 Airbus Deutschland Gmbh Isolierpaket-Anordnung zur Innenisolierung eines Flugzeugrumpfes
US7134629B2 (en) * 2004-04-06 2006-11-14 The Boeing Company Structural panels for use in aircraft fuselages and other structures
US7410352B2 (en) * 2005-04-13 2008-08-12 The Boeing Company Multi-ring system for fuselage barrel formation

Also Published As

Publication number Publication date
ATE519671T1 (de) 2011-08-15
US8480030B2 (en) 2013-07-09
RU2010108340A (ru) 2011-09-20
EP2195234B1 (de) 2011-08-10
WO2009037005A1 (de) 2009-03-26
CN101848835A (zh) 2010-09-29
CN101848835B (zh) 2014-02-19
CA2698853A1 (en) 2009-03-26
JP2010538889A (ja) 2010-12-16
US20100237195A1 (en) 2010-09-23
EP2195234A1 (de) 2010-06-16
DE102007044386A1 (de) 2009-04-02

Similar Documents

Publication Publication Date Title
BRPI0816863A2 (pt) componente estrutural e método para enrijecimento de um revestimento externo.
BRPI0712214A2 (pt) Montagem para painel de cobertura da asa e painel de cobertura da asa para uma asa de aeroplano e um método de formação da mesma
BRPI0920950A2 (pt) aeronave e método de controlar a direção a direção de vôo de uma aeronave
FR2928621B1 (fr) Commande de vol d'un aeronef.
PA8794201A1 (es) Anticuerpos anti-cxcr5 humanizados, derivados de los mismos y su uso
BRPI0816899A2 (pt) componente estrutural e fuselagem de uma aeronave ou espaçonave
FR3032941B1 (fr) Soufflante non carenee de turbomachine d'aeronef
DK3308759T3 (da) Bærbart system, der gør det muligt for blinde eller synshæmmede personer at fortolke omgivelserne ved hjælp af lyd eller berøring
BRPI0911880A2 (pt) método para revestir um componente de compósito de fibra para uma aeronave ou veículo espacial e componente de compósito de fibra produzido pelo referido método
ECSP19077969A (es) Compuesto heterociclico
BR112016027750A2 (pt) Laminado de uma chapa metálica e uma camada adesiva ligada à mesma
GB2606681B (en) Profiled structure for an aircraft or turbomachine for an aircraft
FR3050303B1 (fr) Securisation du sequencement du plan de vol d'un aeronef
DE502007007018D1 (de) Abdeckung, verkleidung oder dergleichen von bauwerken bzw. bauwerksteilen
ES1183633Y (es) Herraje de fijación de paneles
MA50028A (fr) Deploiement d'un element aerodynamique de carrosserie
EP3872805C0 (en) FASTENING ELEMENT FOR FASTENING AN END PIN TO THE MAIN BODY OF A MUSICAL INSTRUMENT, AND MUSICAL INSTRUMENT EQUIPPED THEREWITH
MA51273A (fr) Systèmes de commande d'aéronef
BRPI0921933A2 (pt) componente estrutural de uma aeronave ou espaçonave e uma disposição de componente de fuselagem de uma aeronave ou espaçonave.
BRPI0922769A2 (pt) componente de construção de casco para aeronaves ou veículos espaciais
ES1214723Y (es) Cabina de ducha portátil
BR112018006258A2 (pt) ?estrutura adesiva com um substrato e um revestimento adesivo?
DK3523431T3 (da) Forbedringer af eller vedrørende gendæmpning ("silencing")
ES1261040Y (es) Cabina de ducha
CL2020002689S1 (es) Ensamble de cabina

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]