BRPI0916856A2 - método de reforçar uma nervura - Google Patents

método de reforçar uma nervura

Info

Publication number
BRPI0916856A2
BRPI0916856A2 BRPI0916856A BRPI0916856A BRPI0916856A2 BR PI0916856 A2 BRPI0916856 A2 BR PI0916856A2 BR PI0916856 A BRPI0916856 A BR PI0916856A BR PI0916856 A BRPI0916856 A BR PI0916856A BR PI0916856 A2 BRPI0916856 A2 BR PI0916856A2
Authority
BR
Brazil
Prior art keywords
rib
reinforcing
Prior art date
Application number
BRPI0916856A
Other languages
English (en)
Inventor
Stephen Williams
Original Assignee
Airbus Operations Ltd
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 Ltd filed Critical Airbus Operations Ltd
Publication of BRPI0916856A2 publication Critical patent/BRPI0916856A2/pt

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/18—Spars; Ribs; Stringers
    • B64C3/187—Ribs
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
    • B64F5/00—Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
    • B64F5/10—Manufacturing or assembling aircraft, e.g. jigs therefor
    • 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)
  • Aviation & Aerospace Engineering (AREA)
  • Manufacturing & Machinery (AREA)
  • Mechanical Engineering (AREA)
  • Transportation (AREA)
  • Moulding By Coating Moulds (AREA)
  • Pressure Vessels And Lids Thereof (AREA)
  • Connection Of Plates (AREA)
  • Gasket Seals (AREA)
BRPI0916856A 2008-07-25 2009-07-20 método de reforçar uma nervura BRPI0916856A2 (pt)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GBGB0813584.0A GB0813584D0 (en) 2008-07-25 2008-07-25 Method of stiffening a rib
PCT/GB2009/050889 WO2010010382A2 (en) 2008-07-25 2009-07-20 Method of stiffening a rib

Publications (1)

Publication Number Publication Date
BRPI0916856A2 true BRPI0916856A2 (pt) 2016-02-10

Family

ID=39746885

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI0916856A BRPI0916856A2 (pt) 2008-07-25 2009-07-20 método de reforçar uma nervura

Country Status (9)

Country Link
US (1) US8523111B2 (pt)
EP (1) EP2315699B1 (pt)
JP (1) JP5694931B2 (pt)
CN (1) CN102105354B (pt)
BR (1) BRPI0916856A2 (pt)
CA (1) CA2728509C (pt)
GB (1) GB0813584D0 (pt)
RU (1) RU2518104C2 (pt)
WO (1) WO2010010382A2 (pt)

Families Citing this family (27)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB201008186D0 (en) * 2010-05-17 2010-06-30 Airbus Operations Ltd A structural assembly for an aircraft
WO2012010305A1 (de) 2010-07-20 2012-01-26 Airbus Operations Gmbh Strukturbauteil mit zumindest einer hauptlast-tragende beplankungsschale und einer trägerstruktur zur befestigung der hauptlast-tragenden beplankungsschale sowie strömungskörper mit einem solchen strukturbauteil
FR2978372B1 (fr) * 2011-07-27 2013-09-13 Airbus Operations Sas Panneau raidi pour aeronef, comprenant des raidisseurs a ames entaillees
CN102554827B (zh) * 2011-12-28 2014-03-12 西北工业大学 一种用于装配飞机内前襟翼的定位夹紧装置
CN102554826B (zh) * 2011-12-28 2014-03-12 西北工业大学 一种定位夹紧装置
DE102012202504A1 (de) * 2012-02-17 2013-08-22 Airbus Operations Gmbh Strukturbauteil für ein Luft- oder Raumfahrzeug
GB201214575D0 (en) 2012-08-15 2012-09-26 Airbus Operations Ltd Rib for an aircraft wing
US9341207B2 (en) * 2013-07-30 2016-05-17 Gulfstream Aerospace Corporation Web component and method of making a web component
US9849967B2 (en) 2015-04-01 2017-12-26 The Boeing Company Composite rib for an aircraft
US9517833B2 (en) * 2015-04-28 2016-12-13 The Boeing Company Apparatuses and methods for manufacturing a structure
FR3040684A1 (fr) * 2015-09-04 2017-03-10 Airbus Operations Sas Nervure simplifiee pour caisson central de voilure d'aeronef.
GB201601492D0 (en) 2016-01-27 2016-03-09 Airbus Operations Ltd Aircraft fuel system
US10513325B2 (en) * 2016-02-08 2019-12-24 Bell Helicopter Textron Inc. Joint member for a composite wing structure
US10696373B2 (en) * 2016-09-13 2020-06-30 The Boeing Company Aircraft wings and aircraft including such aircraft wings
JP6638679B2 (ja) * 2017-03-23 2020-01-29 テイ・エス テック株式会社 シートバックフレームの補強構造
GB2568654B (en) * 2017-09-27 2022-05-04 Gkn Aerospace Services Ltd Box rib
US11273899B2 (en) * 2018-01-25 2022-03-15 The Boeing Company Wing rib, wing having wing rib, and method for manufacturing the same
GB2581816A (en) * 2019-02-28 2020-09-02 Airbus Operations Ltd Sealing tool for sealing an opening in an aircraft rib
GB2584423A (en) * 2019-05-28 2020-12-09 Airbus Operations Ltd Rib mounting assembly
CN110979725B (zh) * 2020-01-02 2023-04-14 上海蓝享机械制造有限公司 一种飞机翼肋及其生产工艺
US11685508B2 (en) * 2020-04-08 2023-06-27 The Boeing Company Systems and methods for constructing a bonded structure
GB2599169A (en) * 2020-09-29 2022-03-30 Airbus Operations Ltd A rigid temporary reinforcement structure
US11891193B2 (en) * 2020-11-18 2024-02-06 The Boeing Company Assembly line fabrication and assembly of aircraft wings
CN113428378B (zh) * 2021-08-12 2023-10-20 中航西安飞机工业集团股份有限公司 一种机翼翼肋定位和检验方法
US12134458B2 (en) * 2022-07-18 2024-11-05 Textron Innovations Inc. System, apparatus, and method of manufacture for a rib structure
GB2634738A (en) * 2023-10-17 2025-04-23 Airbus Operations Ltd Manufacturing a rib for an aircraft wing
US12576959B2 (en) 2024-09-06 2026-03-17 The Boeing Company Multipiece ribs for aircraft wing

Family Cites Families (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3669807A (en) * 1970-05-21 1972-06-13 American Aviat Corp Airplane tooling
US5249785A (en) * 1992-04-20 1993-10-05 Boeing Commercial Airplane Group Reconfigurable holding fixture
US6170157B1 (en) * 1996-03-22 2001-01-09 The Boeing Company Determinant spar assembly
US7509740B2 (en) * 2001-11-13 2009-03-31 The Boeing Company Method of manufacturing a wing
WO1997034734A1 (en) 1996-03-22 1997-09-25 The Boeing Company Determinant wing assembly
US6173925B1 (en) * 1998-04-16 2001-01-16 Daimlerchrysler Ag Skin-rib structure
JP2000312989A (ja) * 1999-04-28 2000-11-14 Toyota Motor Corp 薄板のクランプ方法
US6719870B2 (en) * 2000-12-15 2004-04-13 The Boeing Company Fastenerless internal support for hollow structures
US6386481B1 (en) * 2001-01-08 2002-05-14 Patria Finavicomp Oy Arrangement for fastening stringers to aircraft wing ribs
GB0122050D0 (en) * 2001-09-13 2001-10-31 Bae Systems Plc Composite material structure
US8156711B2 (en) * 2003-02-24 2012-04-17 Bell Helicopter Textron Inc. Contact stiffeners for structural skins
US7080805B2 (en) * 2004-05-05 2006-07-25 The Boeing Company Stiffened structures and associated methods
GB2417228A (en) 2004-08-18 2006-02-22 Airbus Uk Ltd Aircraft wing
US7398586B2 (en) * 2005-11-01 2008-07-15 The Boeing Company Methods and systems for manufacturing a family of aircraft wings and other composite structures
ES2346834B1 (es) * 2007-04-30 2011-08-17 Airbus Operations, S.L. Estructura de costilla para cajones de torsion de un ala o de un estabilizador de una aeronave.
US7861969B2 (en) * 2007-05-24 2011-01-04 The Boeing Company Shaped composite stringers and methods of making
ITTO20070507A1 (it) * 2007-07-11 2009-01-12 Alenia Aeronautica Spa Procedimento di fabbricazione di una struttura d'ala monolitica a profilo integrale

Also Published As

Publication number Publication date
US20110147522A1 (en) 2011-06-23
CA2728509C (en) 2015-03-24
EP2315699A2 (en) 2011-05-04
RU2518104C2 (ru) 2014-06-10
CN102105354B (zh) 2014-05-28
CN102105354A (zh) 2011-06-22
EP2315699B1 (en) 2013-01-09
RU2011105096A (ru) 2012-08-27
CA2728509A1 (en) 2010-01-28
JP2011529006A (ja) 2011-12-01
JP5694931B2 (ja) 2015-04-01
US8523111B2 (en) 2013-09-03
WO2010010382A3 (en) 2010-05-06
GB0813584D0 (en) 2008-09-03
WO2010010382A2 (en) 2010-01-28

Similar Documents

Publication Publication Date Title
BRPI0916856A2 (pt) método de reforçar uma nervura
BRPI0820939A2 (pt) Método de estabelecimento de uma conexão
BR112012002068A2 (pt) auto-geração de uma representação visual
BRPI0915331A2 (pt) método de formação de uma membrana assimétrica remolhável
LTC3214083I2 (lt) Kvinolono junginių gamybos būdas
IT1393131B1 (it) Controvento a ingobbamento limitato
BRPI0817625A2 (pt) Método de moldagem de um charge
BRPI0919116A2 (pt) método
BRPI0921153A2 (pt) reforço de armadura
BRPI0907376A8 (pt) fotobiorreator
FR2952790B1 (fr) Chaussure a semelage ameliore
EP2281080A4 (en) POLYLACTIC ACID FIBERS
FR2951069B1 (fr) Element de renfort d'un treillis
BR112012002402A2 (pt) método de fabricação de uma composição de polióximetileno
BR112012014162A2 (pt) método de fabricação de uma nanomanta
BRPI0905374A2 (pt) Método de perfurar através de uma formação
DK2313489T3 (da) Fremstillingsmetode
BR112012002296A2 (pt) processo de reparo de uma parede, notadamente uma parede compósita, constituída de várias camadas
BRPI1015032A2 (pt) comando de aletas de uma máquina de aletas
BR112012002585A2 (pt) reforço revestido
PT2417312E (pt) Método de reforçar uma estrutura
BRPI0916597A2 (pt) Método
BRPI0920591A2 (pt) uma montagem de misturador
BRPI1014060A2 (pt) método de operação de uma válvula
FI20105832A0 (fi) Menetelmä kenkien tekemiseksi

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]