BR112018015496A2 - aparelho de fixação do dispositivo de retenção - Google Patents

aparelho de fixação do dispositivo de retenção

Info

Publication number
BR112018015496A2
BR112018015496A2 BR112018015496A BR112018015496A BR112018015496A2 BR 112018015496 A2 BR112018015496 A2 BR 112018015496A2 BR 112018015496 A BR112018015496 A BR 112018015496A BR 112018015496 A BR112018015496 A BR 112018015496A BR 112018015496 A2 BR112018015496 A2 BR 112018015496A2
Authority
BR
Brazil
Prior art keywords
retainer
attachment
units
clamping units
fixture
Prior art date
Application number
BR112018015496A
Other languages
English (en)
Inventor
Azuma Hiroki
Hirai Makoto
Takahagi Michinobu
Original Assignee
Mitsubishi Heavy Ind 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 Mitsubishi Heavy Ind Ltd filed Critical Mitsubishi Heavy Ind Ltd
Publication of BR112018015496A2 publication Critical patent/BR112018015496A2/pt

Links

Classifications

    • 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
    • B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21J—FORGING; HAMMERING; PRESSING METAL; RIVETING; FORGE FURNACES
    • B21J15/00—Riveting
    • B21J15/10—Riveting machines
    • B21J15/28—Control devices specially adapted to riveting machines not restricted to one of the preceding subgroups
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21J—FORGING; HAMMERING; PRESSING METAL; RIVETING; FORGE FURNACES
    • B21J15/00—Riveting
    • B21J15/10—Riveting machines
    • B21J15/14—Riveting machines specially adapted for riveting specific articles, e.g. brake lining machines
    • B21J15/142—Aerospace structures
    • 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
    • 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
    • B23P2700/00—Indexing scheme relating to the articles being treated, e.g. manufactured, repaired, assembled, connected or other operations covered in the subgroups
    • B23P2700/01—Aircraft parts

Abstract

é objeto da invenção fornecer um aparelho de fixação de acessório de re-tenção que pode garantir precisão de posicionamento e precisão de forma de um acessório de retenção móvel, permitindo assim que um painel de aeronave seja montado com alta precisão. um aparelho de fixação de acessório de retenção (2) inclui uma pluralidade de unidades de fixação (20) configuradas para suportar e fixar um acessório de retenção (1), que retém um painel de fuselagem (10) tendo uma forma curva em seção transversal, a partir de uma superfície inferior do acessó-rio de retenção (1), as unidades de fixação (20) sendo providas sobre uma superfí-cie de instalação, em que a pluralidade de unidades de fixação (20) é proporciona-da correspondendo a pelo menos quatro cantos da superfície inferior do acessório de retenção ( 1).
BR112018015496A 2016-02-02 2016-11-17 aparelho de fixação do dispositivo de retenção BR112018015496A2 (pt)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
JP2016018425A JP6513584B2 (ja) 2016-02-02 2016-02-02 保持治具固定装置
PCT/JP2016/084047 WO2017134898A1 (ja) 2016-02-02 2016-11-17 保持治具固定装置

Publications (1)

Publication Number Publication Date
BR112018015496A2 true BR112018015496A2 (pt) 2018-12-18

Family

ID=59499705

Family Applications (1)

Application Number Title Priority Date Filing Date
BR112018015496A BR112018015496A2 (pt) 2016-02-02 2016-11-17 aparelho de fixação do dispositivo de retenção

Country Status (7)

Country Link
US (1) US11034464B2 (pt)
EP (1) EP3412581A4 (pt)
JP (1) JP6513584B2 (pt)
CN (1) CN108495790A (pt)
BR (1) BR112018015496A2 (pt)
CA (1) CA3013175C (pt)
WO (1) WO2017134898A1 (pt)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107585324A (zh) * 2017-10-11 2018-01-16 重庆通用飞机工业有限公司 一种直升机尾梁装配架
CN108791950B (zh) * 2018-06-26 2023-12-29 中电科芜湖钻石飞机制造有限公司 飞机大型部件装配用装配设备
FR3086268A1 (fr) * 2018-09-25 2020-03-27 Airbus Operations Procede d’assemblage d’un troncon de fuselage d’aeronef a partir de deux parties superieure et inferieure superposees, support de montage polyvalent, outillage et unite de production de troncons de fuselage pour la mise en œuvre dudit procede
US11827380B2 (en) * 2021-01-26 2023-11-28 The Boeing Company System and method for positioning a sub-assembly for installation
CN112935873B (zh) * 2021-02-05 2022-05-31 中国十七冶集团有限公司 一种异型钢结构弯扭构件用辅助定位系统及其定位方法
US11866201B2 (en) 2022-05-03 2024-01-09 The Boeing Company Method and apparatus for the application of frame to fuselage pull-up force via fuselage skin waterline tensioning

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US4937768A (en) 1987-04-14 1990-06-26 Northrop Corporation Integrated assembly system
JPS6464740A (en) * 1987-04-14 1989-03-10 Northrop Corp Built-up data model system
JP2518088B2 (ja) 1990-05-18 1996-07-24 三菱自動車工業株式会社 車両のアクセル全閉位置検出装置
US5560102A (en) * 1992-10-13 1996-10-01 The Boeing Company Panel and fuselage assembly
EP0888202B1 (en) 1996-03-22 2005-08-10 The Boeing Company Determinant wing assembly
ES2146140B1 (es) * 1996-10-15 2001-04-01 Torres Martinez M Maquina para el soporte y mecanizado de piezas.
US6505393B2 (en) 1998-07-31 2003-01-14 Airbus Deutschland Gmbh Two-part riveting apparatus and method for riveting barrel-shaped components such as aircraft fuselage components
ES2169620B1 (es) * 1999-01-22 2003-11-01 Torres Ingenieria De Procesos Util para el montaje de secciones del fuselaje de aeronaves.
DE102004056284B4 (de) * 2004-11-22 2010-08-26 Airbus Deutschland Gmbh Vorrichtung zum Transport von Bauteilen für Verkehrsmittel
JP2006247757A (ja) 2005-03-08 2006-09-21 Toyota Industries Corp ワーク保持装置及びワーク保持方法
CN100565406C (zh) * 2008-09-19 2009-12-02 浙江大学 一种基于四个定位器的飞机部件位姿调整系统及方法
CN101537887A (zh) 2009-03-17 2009-09-23 成都飞机工业（集团）有限责任公司 一种机身三点浮动入位方法
JP2011208992A (ja) * 2010-03-29 2011-10-20 Ntn Corp 空間座標測定システムおよび空間座標測定方法
EP2580119B1 (en) 2010-06-14 2017-03-08 LORD Corporation A helicopter engine mounting system and methods
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
JP5943557B2 (ja) * 2011-06-01 2016-07-05 キヤノン株式会社 位置決め装置、露光装置およびデバイス製造方法
JP2013198918A (ja) * 2012-03-23 2013-10-03 Mitsubishi Heavy Ind Ltd 自動打鋲装置
CN103465039A (zh) 2013-02-27 2013-12-25 中航飞机股份有限公司西安飞机分公司 一种可实现多自由度运动的调姿连接机构
JP6219055B2 (ja) 2013-03-29 2017-10-25 三菱重工業株式会社 機体結合方法及びストロングバック
DE102013006506A1 (de) * 2013-04-16 2014-10-16 Brötje-Automation GmbH Bearbeitungsanlage für Flugzeugstrukturbauteile
FR3016606B1 (fr) * 2014-01-21 2016-02-19 Airbus Operations Sas Procede de fabrication d'une partie d'un fuselage d'un aeronef et outillage pour la mise en oeuvre dudit procede
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CN105109706B (zh) 2015-08-26 2017-05-31 西北工业大学 一种用于飞机薄壁件定位夹持实验装置

Also Published As

Publication number Publication date
WO2017134898A1 (ja) 2017-08-10
CN108495790A (zh) 2018-09-04
EP3412581A4 (en) 2019-07-24
CA3013175A1 (en) 2017-08-10
CA3013175C (en) 2020-08-25
EP3412581A1 (en) 2018-12-12
JP6513584B2 (ja) 2019-05-15
JP2017136928A (ja) 2017-08-10
US20190031372A1 (en) 2019-01-31
US11034464B2 (en) 2021-06-15

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Legal Events

Date Code Title Description
B06U Preliminary requirement: requests with searches performed by other patent offices: procedure suspended [chapter 6.21 patent gazette]
B11B Dismissal acc. art. 36, par 1 of ipl - no reply within 90 days to fullfil the necessary requirements
B350 Update of information on the portal [chapter 15.35 patent gazette]