BR112014019640A2 - - Google Patents

Info

Publication number
BR112014019640A2
BR112014019640A2 BR112014019640A BR112014019640A BR112014019640A2 BR 112014019640 A2 BR112014019640 A2 BR 112014019640A2 BR 112014019640 A BR112014019640 A BR 112014019640A BR 112014019640 A BR112014019640 A BR 112014019640A BR 112014019640 A2 BR112014019640 A2 BR 112014019640A2
Authority
BR
Brazil
Application number
BR112014019640A
Other versions
BR112014019640B1 (pt
BR112014019640A8 (pt
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 filed Critical
Publication of BR112014019640A2 publication Critical patent/BR112014019640A2/pt
Publication of BR112014019640A8 publication Critical patent/BR112014019640A8/pt
Publication of BR112014019640B1 publication Critical patent/BR112014019640B1/pt

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23P—METAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
    • B23P19/00—Machines for simply fitting together or separating metal parts or objects, or metal and non-metal parts, whether or not involving some deformation; Tools or devices therefor so far as not provided for in other classes
    • B23P19/10—Aligning parts to be fitted together
    • 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
    • B64C1/069—Joining arrangements therefor
    • 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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23P—METAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
    • B23P19/00—Machines for simply fitting together or separating metal parts or objects, or metal and non-metal parts, whether or not involving some deformation; Tools or devices therefor so far as not provided for in other classes
    • 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
    • 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
    • Y10T29/49623—Static structure, e.g., a building component
    • 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
    • Y10T29/53—Means to assemble or disassemble
    • Y10T29/53039—Means to assemble or disassemble with control means energized in response to activator stimulated by condition sensor
    • Y10T29/53061—Responsive to work or work-related machine element

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Manufacturing & Machinery (AREA)
  • Transportation (AREA)
  • Automatic Assembly (AREA)
  • Communication Control (AREA)
BR112014019640-0A 2012-02-09 2012-12-21 sistema e método automatizados para unir partes de um chassi BR112014019640B1 (pt)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
IT000111A ITTO20120111A1 (it) 2012-02-09 2012-02-09 Sistema automatico per la giunzione di porzioni di un telaio e metodo associato.
ITTO2012A000111 2012-02-09
PCT/IB2012/057627 WO2013117971A1 (en) 2012-02-09 2012-12-21 Automated system for joining portions of a chassis and method thereof

Publications (3)

Publication Number Publication Date
BR112014019640A2 true BR112014019640A2 (pt) 2017-06-20
BR112014019640A8 BR112014019640A8 (pt) 2017-07-11
BR112014019640B1 BR112014019640B1 (pt) 2021-05-25

Family

ID=46001453

Family Applications (1)

Application Number Title Priority Date Filing Date
BR112014019640-0A BR112014019640B1 (pt) 2012-02-09 2012-12-21 sistema e método automatizados para unir partes de um chassi

Country Status (11)

Country Link
US (1) US9643710B2 (pt)
EP (1) EP2812249B1 (pt)
KR (1) KR101933253B1 (pt)
CN (1) CN104245514B (pt)
BR (1) BR112014019640B1 (pt)
CA (1) CA2863745C (pt)
ES (1) ES2582634T3 (pt)
HK (1) HK1205491A1 (pt)
IT (1) ITTO20120111A1 (pt)
RU (1) RU2631437C2 (pt)
WO (1) WO2013117971A1 (pt)

Families Citing this family (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103991557B (zh) * 2014-04-17 2016-03-30 中国航空工业集团公司沈阳飞机设计研究所 一种伙伴加受油地面模拟试验系统
US10427254B2 (en) 2014-04-30 2019-10-01 The Boeing Company Flexible manufacturing for aircraft structures
US10017277B2 (en) 2014-04-30 2018-07-10 The Boeing Company Apparatus, system, and method for supporting a wing assembly
US10000298B2 (en) 2014-04-30 2018-06-19 The Boeing Company Metrology system for positioning assemblies
KR101687554B1 (ko) 2014-12-30 2016-12-19 한국항공우주산업 주식회사 항공기 동체 자동 장착 및 탈착 장치
KR101687562B1 (ko) * 2014-12-31 2016-12-19 한국항공우주산업 주식회사 회전익 항공기의 동체 자동 장착 및 탈착 장치
US10275565B2 (en) 2015-11-06 2019-04-30 The Boeing Company Advanced automated process for the wing-to-body join of an aircraft with predictive surface scanning
CN106404362A (zh) * 2016-08-09 2017-02-15 中国人民解放军第五七二工厂 一种飞行器空中受油插头检测装置
KR101841510B1 (ko) * 2016-12-23 2018-03-26 대한민국 항공기 사출좌석 장탈착 장비
CN106903506A (zh) * 2017-04-19 2017-06-30 宁波舜宇智能科技有限公司 装配系统及装配方法
FR3072656B1 (fr) * 2017-10-24 2019-11-08 Airbus Systeme d’outillage destine a la manipulation d’au moins un module superieur et /ou au moins un module inferieur.
US11989027B2 (en) 2018-04-09 2024-05-21 Lam Research Corporation Dual-mode autonomous guided vehicle
US10712730B2 (en) 2018-10-04 2020-07-14 The Boeing Company Methods of synchronizing manufacturing of a shimless assembly
EP3647207B1 (en) * 2018-10-31 2021-01-06 Aciturri Engineering S.L.U. Method of aligning hardpoints in aeronautical structures
CN109738002B (zh) * 2019-03-12 2023-12-05 湖南航天环宇通信科技股份有限公司 无损检测可调夹具
RU203726U1 (ru) * 2020-12-23 2021-04-19 Акционерное общество "Научно-производственная корпорация "Уралвагонзавод" имени Ф.Э. Дзержинского" Устройство для регулировки секций при сборке изделий модульного типа

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3698817A (en) * 1970-12-08 1972-10-17 Toshiba Machine Co Ltd Method and apparatus for manufacturing reference scales
JP3079186B2 (ja) * 1995-09-28 2000-08-21 株式会社小松製作所 構造物計測システム
JP5041616B2 (ja) * 1996-06-06 2012-10-03 ザ・ボーイング・カンパニー 機械の精度を高めるための方法
FR2821778B1 (fr) * 2001-03-07 2004-11-19 S O C O A Soc De Conception Co Procede d'assemblage automatisee de structures volumineuses notamment aeronautiques, dispositifs et produit logiciel permettant de le mettre en oeuvre
JP4444033B2 (ja) * 2004-08-10 2010-03-31 三菱重工業株式会社 航空機の機体の製造方法
DE102004056286B4 (de) * 2004-11-22 2015-12-24 Airbus Operations Gmbh Vorrichtung und Verfahren zum form- und/oder abmessungsunabhängigen Zusammenfügen und Heften von mehreren Einzelkomponenten zur Bildung von eigensteifen, transportfähigen Sektionen für Verkehrsmittel, insbesondere für Luftfahrzeuge
DE102006019917B4 (de) * 2006-04-28 2013-10-10 Airbus Operations Gmbh Verfahren und Vorrichtung zur Sicherung der Maßhaltigkeit von mehrsegmentigen Konstruktionsstrukturen beim Zusammenbau
DE102008045746A1 (de) * 2008-09-04 2010-03-25 Lufthansa Technik Ag Verfahren zum Vermessen des Innenraums eines Flugzeugs
DE102009018991A1 (de) * 2009-05-01 2010-11-04 Airbus Operations Gmbh Vorrichtung zur räumlichen Ausrichtung von mindestens zwei Untergruppenbauteilen sowie Verfahren
US8634950B2 (en) * 2009-12-14 2014-01-21 Embraer S.A. Automated positioning and alignment method and system for aircraft structures using robots
CN102001451B (zh) * 2010-11-12 2013-05-29 浙江大学 基于四个数控定位器、调姿平台和移动托架的飞机部件调姿、对接系统及方法

Also Published As

Publication number Publication date
EP2812249B1 (en) 2016-03-16
HK1205491A1 (en) 2015-12-18
US9643710B2 (en) 2017-05-09
RU2631437C2 (ru) 2017-09-22
BR112014019640B1 (pt) 2021-05-25
US20150367930A1 (en) 2015-12-24
RU2014132574A (ru) 2016-03-27
EP2812249A1 (en) 2014-12-17
CA2863745C (en) 2020-08-04
KR20150001719A (ko) 2015-01-06
ITTO20120111A1 (it) 2013-08-10
CN104245514A (zh) 2014-12-24
BR112014019640A8 (pt) 2017-07-11
ES2582634T3 (es) 2016-09-14
KR101933253B1 (ko) 2018-12-27
WO2013117971A1 (en) 2013-08-15
CN104245514B (zh) 2016-08-17
CA2863745A1 (en) 2013-08-15

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Legal Events

Date Code Title Description
B06F Objections, documents and/or translations needed after an examination request according [chapter 6.6 patent gazette]
B06U Preliminary requirement: requests with searches performed by other patent offices: procedure suspended [chapter 6.21 patent gazette]
B09A Decision: intention to grant [chapter 9.1 patent gazette]
B16A Patent or certificate of addition of invention granted [chapter 16.1 patent gazette]

Free format text: PRAZO DE VALIDADE: 20 (VINTE) ANOS CONTADOS A PARTIR DE 21/12/2012, OBSERVADAS AS CONDICOES LEGAIS.