DE50301402D1 - Anordnung zur Verbindung von dünnwandigen Metallstrukturen - Google Patents

Anordnung zur Verbindung von dünnwandigen Metallstrukturen

Info

Publication number
DE50301402D1
DE50301402D1 DE50301402T DE50301402T DE50301402D1 DE 50301402 D1 DE50301402 D1 DE 50301402D1 DE 50301402 T DE50301402 T DE 50301402T DE 50301402 T DE50301402 T DE 50301402T DE 50301402 D1 DE50301402 D1 DE 50301402D1
Authority
DE
Germany
Prior art keywords
rivet
plates
arrangement
metal structures
walled metal
Prior art date
Legal status (The legal status 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 status listed.)
Expired - Lifetime
Application number
DE50301402T
Other languages
English (en)
Inventor
Dr Assler
Hans-Juergen Schmidt
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Airbus Operations GmbH
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
Priority to DE50301402T priority Critical patent/DE50301402D1/de
Application granted granted Critical
Publication of DE50301402D1 publication Critical patent/DE50301402D1/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • 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
    • B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21J—FORGING; HAMMERING; PRESSING METAL; RIVETING; FORGE FURNACES
    • B21J15/00—Riveting
    • B21J15/02—Riveting procedures
    • 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
    • Y10T29/49826—Assembling or joining
    • Y10T29/49908—Joining by deforming
    • Y10T29/49938—Radially expanding part in cavity, aperture, or hollow body
    • Y10T29/49943—Riveting
    • 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
    • Y10T29/49826—Assembling or joining
    • Y10T29/49947—Assembling or joining by applying separate fastener
    • Y10T29/49948—Multipart cooperating fastener [e.g., bolt and nut]
    • 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
    • Y10T29/49826—Assembling or joining
    • Y10T29/49947—Assembling or joining by applying separate fastener
    • Y10T29/49954—Fastener deformed after application
    • Y10T29/49956—Riveting
    • 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
    • Y10T403/00—Joints and connections
    • Y10T403/75—Joints and connections having a joining piece extending through aligned openings in plural members

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Connection Of Plates (AREA)
  • Insertion Pins And Rivets (AREA)
  • Laminated Bodies (AREA)
  • Multi-Conductor Connections (AREA)
DE50301402T 2002-08-23 2003-07-08 Anordnung zur Verbindung von dünnwandigen Metallstrukturen Expired - Lifetime DE50301402D1 (de)

Priority Applications (1)

Application Number Priority Date Filing Date Title
DE50301402T DE50301402D1 (de) 2002-08-23 2003-07-08 Anordnung zur Verbindung von dünnwandigen Metallstrukturen

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE10238820A DE10238820A1 (de) 2002-08-23 2002-08-23 Anordung zur Erfindung von dünnwandigen Metallstrukturen
DE50301402T DE50301402D1 (de) 2002-08-23 2003-07-08 Anordnung zur Verbindung von dünnwandigen Metallstrukturen

Publications (1)

Publication Number Publication Date
DE50301402D1 true DE50301402D1 (de) 2006-03-02

Family

ID=31197311

Family Applications (2)

Application Number Title Priority Date Filing Date
DE10238820A Withdrawn DE10238820A1 (de) 2002-08-23 2002-08-23 Anordung zur Erfindung von dünnwandigen Metallstrukturen
DE50301402T Expired - Lifetime DE50301402D1 (de) 2002-08-23 2003-07-08 Anordnung zur Verbindung von dünnwandigen Metallstrukturen

Family Applications Before (1)

Application Number Title Priority Date Filing Date
DE10238820A Withdrawn DE10238820A1 (de) 2002-08-23 2002-08-23 Anordung zur Erfindung von dünnwandigen Metallstrukturen

Country Status (6)

Country Link
US (1) US7021856B2 (de)
EP (1) EP1393835B1 (de)
AT (1) ATE307297T1 (de)
BR (1) BR0303134B1 (de)
CA (1) CA2438136C (de)
DE (2) DE10238820A1 (de)

Families Citing this family (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6835020B2 (en) * 2003-04-02 2004-12-28 General Motors Corporation Bi-direction self-piercing riveting
US7374381B2 (en) * 2004-10-21 2008-05-20 Pem Management, Inc, Double flush clinch stud
FR2883548B1 (fr) * 2005-03-23 2007-06-15 Airbus France Sas Dispositif et procede d'eclissage mixte carbone-metal dissymetrique
GB0525896D0 (en) * 2005-12-20 2006-02-01 Airbus Uk Ltd A joint for use in aircraft construction
DE102007018753B4 (de) * 2007-04-20 2012-11-08 Airbus Operations Gmbh Brandschutzraum für Flugzeugpassagiere mit Hilfe von Rumpfbehäutung aus Faser-Metall-Laminaten
US20090193644A1 (en) * 2008-01-31 2009-08-06 Michael James Malloy Double nut bolted connection with cheese plate for reinforcing existing riveted or bolted structures under load
DE102008017650A1 (de) * 2008-04-04 2009-11-12 Airbus Deutschland Gmbh Vollniet zum Fügen von Composit-Bauteilen
US7798285B2 (en) * 2008-11-14 2010-09-21 Rohr, Inc. Acoustic barrel for aircraft engine nacelle including crack and delamination stoppers
US8422618B2 (en) * 2009-12-08 2013-04-16 Ge-Hitachi Nuclear Energy Americas Llc Apparatus and system for restricting the movement of a component
US9314070B2 (en) * 2011-05-02 2016-04-19 Yegise Koc Adjustable jewelry
US9016042B2 (en) 2011-05-20 2015-04-28 Rohr, Inc. Reinforcement members for aircraft propulsion system components configured to address delamination of the inner fixed structure
JP6045805B2 (ja) * 2012-03-26 2016-12-14 須藤 二三男 椅子のフレーム構造
FR2994888B1 (fr) 2012-08-30 2014-09-26 Airbus Operations Sas Assemblage de deux pieces en materiau composite
DE102012111022A1 (de) 2012-11-15 2014-06-26 Airbus Operations Gmbh Verstärktes Fahrzeugstrukturteil, Fahrzeug und Verfahren
US9828040B2 (en) * 2014-06-30 2017-11-28 Ford Global Technologies, Llc Multilayer component assembly for automobiles
CN104200092B (zh) * 2014-08-28 2017-06-09 上海飞机制造有限公司 一种飞机薄壁件自动钻铆多姿态变形建模方法
EP2993124B1 (de) * 2014-09-08 2019-04-03 Airbus Operations GmbH Vermeiden von Rissen an Schraub- oder Nietverbindungen von Flugzeugstrukturbauteilen
CN107282792B (zh) * 2017-07-21 2023-08-08 广东万和电气有限公司 一种太阳能集热器边框的铆接工装及方法

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2746579A (en) * 1951-11-09 1956-05-22 John T Gondek Structural joints
US4394096A (en) * 1981-08-27 1983-07-19 Menasha Corporation Attachment system for plastic liners
SU1574931A1 (ru) * 1988-03-01 1990-06-30 Харьковский Авиационный Институт Им.Жуковского Н.Е. Многор дное соединение деталей
DE4119934A1 (de) * 1991-06-17 1992-12-24 Sfs Stadler Holding Ag Nietverbinder
US5297760A (en) * 1992-08-21 1994-03-29 Mcdonnell Douglas Corporation Aircraft skin lap splice
FR2817926B1 (fr) * 2000-12-08 2003-02-28 Eads Airbus Sa Procede d'assemblage optimise de deux pieces sensiblement planes

Also Published As

Publication number Publication date
EP1393835A2 (de) 2004-03-03
BR0303134B1 (pt) 2011-03-09
EP1393835B1 (de) 2005-10-19
US7021856B2 (en) 2006-04-04
CA2438136C (en) 2010-10-26
EP1393835A3 (de) 2004-07-14
ATE307297T1 (de) 2005-11-15
CA2438136A1 (en) 2004-02-23
US20040052581A1 (en) 2004-03-18
DE10238820A1 (de) 2004-03-11
BR0303134A (pt) 2004-08-24

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition
8327 Change in the person/name/address of the patent owner

Owner name: AIRBUS OPERATIONS GMBH, 21129 HAMBURG, DE