CN104245514B - 用于连结底盘的部分的自动系统及其方法 - Google Patents

用于连结底盘的部分的自动系统及其方法 Download PDF

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Publication number
CN104245514B
CN104245514B CN201280071705.1A CN201280071705A CN104245514B CN 104245514 B CN104245514 B CN 104245514B CN 201280071705 A CN201280071705 A CN 201280071705A CN 104245514 B CN104245514 B CN 104245514B
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CN
China
Prior art keywords
control unit
central control
segment
chassis
data
Prior art date
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Active
Application number
CN201280071705.1A
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English (en)
Chinese (zh)
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CN104245514A (zh
Inventor
F·阿图奇
G·纳瓦拉
F·马格里
R·阿夸蒂
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Alenia Aermacchi SpA
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Alenia Aermacchi SpA
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Publication of CN104245514A publication Critical patent/CN104245514A/zh
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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

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Manufacturing & Machinery (AREA)
  • Transportation (AREA)
  • Automatic Assembly (AREA)
  • Communication Control (AREA)
CN201280071705.1A 2012-02-09 2012-12-21 用于连结底盘的部分的自动系统及其方法 Active CN104245514B (zh)

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 (2)

Publication Number Publication Date
CN104245514A CN104245514A (zh) 2014-12-24
CN104245514B true CN104245514B (zh) 2016-08-17

Family

ID=46001453

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201280071705.1A Active CN104245514B (zh) 2012-02-09 2012-12-21 用于连结底盘的部分的自动系统及其方法

Country Status (10)

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

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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
US10017277B2 (en) 2014-04-30 2018-07-10 The Boeing Company Apparatus, system, and method for supporting a wing assembly
US10427254B2 (en) 2014-04-30 2019-10-01 The Boeing Company Flexible manufacturing for aircraft structures
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
ES2864734T3 (es) * 2018-10-31 2021-10-14 Aciturri Eng S L U Procedimiento de alineamiento de puntos duros en estructuras aeronáuticas
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
US11608649B2 (en) * 2020-03-12 2023-03-21 The Boeing Company Locking mechanism for fall protection
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

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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
WO1997046925A1 (en) * 1996-06-06 1997-12-11 The Boeing Company Method for improving the accuracy of machines
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
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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
BR112014019640B1 (pt) 2021-05-25
HK1205491A1 (en) 2015-12-18
EP2812249A1 (en) 2014-12-17
US20150367930A1 (en) 2015-12-24
EP2812249B1 (en) 2016-03-16
CN104245514A (zh) 2014-12-24
ES2582634T3 (es) 2016-09-14
KR101933253B1 (ko) 2018-12-27
BR112014019640A8 (pt) 2017-07-11
RU2631437C2 (ru) 2017-09-22
RU2014132574A (ru) 2016-03-27
US9643710B2 (en) 2017-05-09
CA2863745A1 (en) 2013-08-15
CA2863745C (en) 2020-08-04
BR112014019640A2 (enExample) 2017-06-20
ITTO20120111A1 (it) 2013-08-10
WO2013117971A1 (en) 2013-08-15
KR20150001719A (ko) 2015-01-06

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