ATE402346T1 - Verfahren und vorrichtung unter einsatz von exzenterbuchsen - Google Patents

Verfahren und vorrichtung unter einsatz von exzenterbuchsen

Info

Publication number
ATE402346T1
ATE402346T1 AT05745275T AT05745275T ATE402346T1 AT E402346 T1 ATE402346 T1 AT E402346T1 AT 05745275 T AT05745275 T AT 05745275T AT 05745275 T AT05745275 T AT 05745275T AT E402346 T1 ATE402346 T1 AT E402346T1
Authority
AT
Austria
Prior art keywords
bushing
passage
received
passages
eccentric
Prior art date
Application number
AT05745275T
Other languages
English (en)
Inventor
Christian Grover
William Skinner
Mark Weiss
Jude Restis
Original Assignee
Fatigue Technology Inc
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 Fatigue Technology Inc filed Critical Fatigue Technology Inc
Application granted granted Critical
Publication of ATE402346T1 publication Critical patent/ATE402346T1/de

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
    • B23P9/00—Treating or finishing surfaces mechanically, with or without calibrating, primarily to resist wear or impact, e.g. smoothing or roughening turbine blades or bearings; Features of such surfaces not otherwise provided for, their treatment being unspecified
    • B23P9/02—Treating or finishing by applying pressure, e.g. knurling
    • B23P9/025—Treating or finishing by applying pressure, e.g. knurling to inner walls of holes by using axially moving tools
    • 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
    • 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
    • B23P19/12—Alignment of parts for insertion into bores
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C5/00—Stabilising surfaces
    • B64C5/06—Fins
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16B—DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
    • F16B43/00—Washers or equivalent devices; Other devices for supporting bolt-heads or nuts
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16B—DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
    • F16B5/00—Joining sheets or plates, e.g. panels, to one another or to strips or bars parallel to them
    • F16B5/04—Joining sheets or plates, e.g. panels, to one another or to strips or bars parallel to them by means of 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
    • 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
    • Y10T403/32—Articulated members
    • Y10T403/32114—Articulated members including static joint
    • Y10T403/32131—One member is plate or side
    • Y10T403/32155—Bearing component clamped to plate or side, e.g., bolted, etc.

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Connection Of Plates (AREA)
  • Compressor (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Diaphragms For Electromechanical Transducers (AREA)
  • Insertion Pins And Rivets (AREA)
AT05745275T 2004-04-15 2005-04-15 Verfahren und vorrichtung unter einsatz von exzenterbuchsen ATE402346T1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US56278904P 2004-04-15 2004-04-15

Publications (1)

Publication Number Publication Date
ATE402346T1 true ATE402346T1 (de) 2008-08-15

Family

ID=34968663

Family Applications (1)

Application Number Title Priority Date Filing Date
AT05745275T ATE402346T1 (de) 2004-04-15 2005-04-15 Verfahren und vorrichtung unter einsatz von exzenterbuchsen

Country Status (6)

Country Link
US (1) US7406777B2 (de)
EP (1) EP1751432B1 (de)
AT (1) ATE402346T1 (de)
DE (1) DE602005008426D1 (de)
ES (1) ES2311224T3 (de)
WO (1) WO2005103505A1 (de)

Families Citing this family (44)

* Cited by examiner, † Cited by third party
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US7375277B1 (en) * 2000-06-26 2008-05-20 Fatigue Technology, Inc. Double flanged bushings and installation methods
US7448652B2 (en) * 2003-07-31 2008-11-11 Fatigue Technology Inc. Tubular metal fitting expandable in a wall opening and method of installation
US20050269436A1 (en) * 2004-06-04 2005-12-08 Innotech Solutions, Llc Cone rock crusher
US20050269435A1 (en) * 2004-06-04 2005-12-08 Innotech Solutions, Llc Bushing for a rock crusher
US7509829B2 (en) 2005-12-28 2009-03-31 Fatigue Technology, Inc. Mandrel assembly and method of using the same
WO2007082077A1 (en) 2006-01-11 2007-07-19 Fatigue Technology, Inc. Bushing kits, bearings, and methods of installation
DE102006058140B4 (de) * 2006-03-22 2009-06-10 Airbus Deutschland Gmbh Bolzenverbindung
DE102006013069B3 (de) * 2006-03-22 2007-12-06 Airbus Deutschland Gmbh Bolzenverbindung
EP2021635A2 (de) * 2006-04-27 2009-02-11 Fatigue Technology, Inc. Wellenentlastende geometrische merkmale von radial in werkstücke expandierbaren strukturelementen
ATE536957T1 (de) * 2006-04-27 2011-12-15 Fatigue Technology Inc Ausrichtungsvorrichtung und anwendungsverfahren
US7958766B2 (en) * 2006-06-29 2011-06-14 Fatigue Technology, Inc. Self-aligning tools and a mandrel with retention sleeve
US7857565B2 (en) * 2006-06-29 2010-12-28 The Boeing Company Compensator bushing assembly for fasteners with location variability
KR101468399B1 (ko) 2006-08-28 2014-12-03 퍼티구 테크놀로지 인코포레이티드 설치／처리 시스템 및 이를 사용하는 방법
US8661683B2 (en) * 2006-08-29 2014-03-04 The Boeing Company Method and apparatus for preventing lightning strike damage to a structural component
DE102006047238B4 (de) * 2006-10-04 2010-01-14 Airbus Deutschland Gmbh Frachtladesystem mit Führungsschienen und mit einer Stelleinrichtung zum Ausrichten von Lagerteilen an toleranzbehafteten Strukturen
DE102006047237B4 (de) * 2006-10-04 2010-01-14 Airbus Deutschland Gmbh Stelleinrichtung zum Ausrichten von Lagerteilen an toleranzbehafteten Strukturen
DE102006049075B4 (de) * 2006-10-13 2009-12-17 Airbus Deutschland Gmbh Stelleinrichtung zum Ausrichten von Lagerteilen an toleranzbehafteten Strukturen
RU2349503C1 (ru) * 2007-07-18 2009-03-20 Владимир Дмитриевич Гречишников Несущий винт
EP2210001B1 (de) 2007-10-16 2017-08-02 Fatigue Technology, Inc. Dehnbare befestigungsvorrichtungsanordnung mit deformiertem bund
EP2259884B1 (de) 2008-03-07 2018-11-28 Fatigue Technology, Inc. Dehnbares element mit welleninhibitor und anwendungsverfahren dafür
WO2010009442A2 (en) 2008-07-18 2010-01-21 Fatigue Technology, Inc. Nut plate assembly and methods of using the same
EP2417369B1 (de) 2009-04-10 2014-04-02 Fatigue Technology, Inc. Verbinderanordnung für eine aufweitbare hülse und ein befestiger mit einem ziehdorn
ES2378702B1 (es) * 2009-04-21 2013-02-28 Airbus Operations, S.L. Herrajes para la cogida del estabilizador vertical de cola de una aeronave.
US7861435B1 (en) * 2009-06-10 2011-01-04 Siemens Energy, Inc. Method and system for adjusting a turbomachine gland seal
US20110031713A1 (en) * 2009-08-04 2011-02-10 Ekbundit Michael W Rod end mounting bushing
US8267414B2 (en) * 2009-11-10 2012-09-18 Vertex Export And Import, Corp. Suspension arm assembly and method of retrofitting
US8647035B2 (en) 2009-12-16 2014-02-11 Fatigue Technology, Inc. Modular nut plate assemblies and methods of using the same
US8500407B1 (en) * 2010-03-28 2013-08-06 The Boeing Company Composite blade root-end drill-through lug and attachment method
ES2709896T3 (es) * 2010-09-24 2019-04-22 Airbus Operations Sl Fuselaje trasero de una aeronave
WO2012167136A2 (en) 2011-06-03 2012-12-06 Fatigue Technology, Inc. Expandable crack inhibitors and methods of using the same
WO2012174215A2 (en) 2011-06-15 2012-12-20 Fatigue Technology, Inc Modular nut plates with closed nut assemblies
US20130075150A1 (en) * 2011-09-27 2013-03-28 Christopher L. Newbolt Bushing for use in providing electromagnetic effects protection
US9108363B2 (en) * 2011-10-06 2015-08-18 The Boeing Company Thin wall bushing for robust electrical bonding to fiber-reinforced structures
EP2809482B1 (de) 2012-01-30 2018-11-07 Fatigue Technology, Inc. Verarbeitungssystem und betriebsverfahren dafür
EP2920068B1 (de) * 2012-11-15 2017-11-29 United Technologies Corporation Stabilisator mit struktureller box und opferoberflächen
US9698588B2 (en) * 2013-05-03 2017-07-04 Cooper Technology Company Universal bushing
US10119563B2 (en) 2015-04-04 2018-11-06 The Boeing Company Offset bushing and method of use
US10655671B2 (en) * 2016-12-29 2020-05-19 Goodrich Corporation Nested bushing arrangement
DE102017103895B3 (de) 2017-02-24 2018-07-26 Deutsches Zentrum für Luft- und Raumfahrt e.V. Verfahren und Verbindung zum Fügen zweier Bauelemente
GB2562748A (en) * 2017-05-23 2018-11-28 Airbus Operations Ltd Bearing assembly
US10750869B2 (en) * 2017-07-06 2020-08-25 Ashley Furniture Industries, Inc. Motion furniture mechanism with pre-aligned linkage member
US12612941B2 (en) * 2020-02-19 2026-04-28 Safran Landing Systems Canada Inc. Field serviceable landing gear bushing
US12071974B2 (en) * 2021-05-17 2024-08-27 Raytheon Company Eccentric bushing for redundant pinning of removable panels
US11905985B2 (en) 2022-02-17 2024-02-20 Goodrich Corporation Systems and methods for misalignment adjustment utilizing double eccentric bushings

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US2216208A (en) * 1939-08-07 1940-10-01 Joseph H M Michon Adjusting device for punchretaining blocks
US2424521A (en) * 1943-10-08 1947-07-22 Mcdonnell Aircraft Corp Airplane wing spar joint
US3076668A (en) * 1957-10-09 1963-02-05 Famely Max Fittings for retaining cylindrical members in place
GB1065414A (en) 1964-03-31 1967-04-12 Bendix Corp Improvements in and relating to force transmitting members
US3342507A (en) * 1965-09-02 1967-09-19 Rockwell Standard Co Steerable axle assembly having camber adjustment means
US3385624A (en) * 1966-04-20 1968-05-28 Baclini David Eccentric adjusting device
CH491313A (de) * 1968-01-23 1970-05-31 Sulzer Ag Wärmeübertrager
US3590461A (en) * 1968-12-19 1971-07-06 Joseph T Siler Alignment means for bushings having eccentric bores
US4244661A (en) * 1979-07-23 1981-01-13 Mcdonnell Douglas Corporation Fastener means and joint for laminates
US4309123A (en) * 1979-10-26 1982-01-05 Rajac Corporation Method and apparatus for fastening misaligned structural members
US4621961A (en) * 1985-02-28 1986-11-11 Bulent Gulistan Captive panel fastener
US4753615A (en) * 1986-06-30 1988-06-28 Amp Incorporated Electrical connection and fastener therefor
US5462381A (en) * 1990-04-20 1995-10-31 Reliance Electric Industrial Company Corrosion resistant bushing
DE29512237U1 (de) * 1995-07-28 1995-09-28 Krinner, Klaus, 94342 Straßkirchen Befestigungsvorrichtung für einen stab- oder pfostenförmigen Gegenstand
DE19906168C1 (de) * 1999-02-08 2000-09-21 Atec Weiss Gmbh & Co Kg Konusschraubverbindung für Lamellenpaket-Wellenkupplungen
US7375277B1 (en) * 2000-06-26 2008-05-20 Fatigue Technology, Inc. Double flanged bushings and installation methods
JP3762715B2 (ja) * 2002-04-16 2006-04-05 ジーイー・メディカル・システムズ・グローバル・テクノロジー・カンパニー・エルエルシー 位置決め具及び画像診断装置
DE10353376B4 (de) * 2003-11-14 2005-09-08 Airbus Deutschland Gmbh Vorrichtung und Verfahren zur mechanischen Verbindung von zwei Bauteilen

Also Published As

Publication number Publication date
DE602005008426D1 (de) 2008-09-04
US20050262682A1 (en) 2005-12-01
ES2311224T3 (es) 2009-02-01
WO2005103505A1 (en) 2005-11-03
EP1751432A1 (de) 2007-02-14
US7406777B2 (en) 2008-08-05
EP1751432B1 (de) 2008-07-23

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Legal Events

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RER Ceased as to paragraph 5 lit. 3 law introducing patent treaties