CA2640693A1 - Bolted joint - Google Patents

Bolted joint Download PDF

Info

Publication number
CA2640693A1
CA2640693A1 CA002640693A CA2640693A CA2640693A1 CA 2640693 A1 CA2640693 A1 CA 2640693A1 CA 002640693 A CA002640693 A CA 002640693A CA 2640693 A CA2640693 A CA 2640693A CA 2640693 A1 CA2640693 A1 CA 2640693A1
Authority
CA
Canada
Prior art keywords
bolt
structural part
bushing
bolted joint
structural
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.)
Abandoned
Application number
CA002640693A
Other languages
English (en)
French (fr)
Inventor
Uwe Steinke
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
Individual
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 Individual filed Critical Individual
Publication of CA2640693A1 publication Critical patent/CA2640693A1/en
Abandoned legal-status Critical Current

Links

Classifications

    • 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
    • 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
    • F16B3/00—Key-type connections; Keys
    • F16B3/06—Key-type connections; Keys using taper sleeves
    • 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
    • F16B35/00—Screw-bolts; Stay-bolts; Screw-threaded studs; Screws; Set screws
    • F16B35/04—Screw-bolts; Stay-bolts; Screw-threaded studs; Screws; Set screws with specially-shaped head or shaft in order to fix the bolt on or in an object
    • F16B35/041—Specially-shaped shafts
    • 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
    • F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C11/00—Pivots; Pivotal connections
    • F16C11/04—Pivotal connections
    • F16C11/045—Pivotal connections with at least a pair of arms pivoting relatively to at least one other arm, all arms being mounted on one pin
    • 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
    • B64C2001/0054—Fuselage structures substantially made from particular materials
    • B64C2001/0072—Fuselage structures substantially made from particular materials from composite materials
    • 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
    • B64C2001/0054—Fuselage structures substantially made from particular materials
    • B64C2001/0081—Fuselage structures substantially made from particular materials from metallic materials
    • 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
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/40—Weight reduction

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Connection Of Plates (AREA)
  • Pivots And Pivotal Connections (AREA)
  • Mutual Connection Of Rods And Tubes (AREA)
CA002640693A 2006-03-22 2007-03-16 Bolted joint Abandoned CA2640693A1 (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
DE102006013069.3 2006-03-22
DE102006013069A DE102006013069B3 (de) 2006-03-22 2006-03-22 Bolzenverbindung
PCT/EP2007/052526 WO2007107521A1 (en) 2006-03-22 2007-03-16 Bolted joint

Publications (1)

Publication Number Publication Date
CA2640693A1 true CA2640693A1 (en) 2007-09-27

Family

ID=38083573

Family Applications (1)

Application Number Title Priority Date Filing Date
CA002640693A Abandoned CA2640693A1 (en) 2006-03-22 2007-03-16 Bolted joint

Country Status (9)

Country Link
US (1) US20090314426A1 (enExample)
EP (1) EP1996457A1 (enExample)
JP (1) JP2009530169A (enExample)
CN (1) CN101395058A (enExample)
BR (1) BRPI0709058A2 (enExample)
CA (1) CA2640693A1 (enExample)
DE (1) DE102006013069B3 (enExample)
RU (1) RU2008137257A (enExample)
WO (1) WO2007107521A1 (enExample)

Families Citing this family (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102011119251B4 (de) * 2011-11-24 2015-05-07 Leichtbau-Zentrum Sachsen Gmbh Vorrichtung zur Krafteinleitung in ein Bauteil aus Faserverbundwerkstoff
CN103644185B (zh) * 2013-11-28 2016-04-06 江西洪都航空工业集团有限责任公司 承弯螺栓连接结构
CN103671469B (zh) * 2013-12-10 2016-02-17 中联重科股份有限公司 销轴组件的安装结构和具有其的工程机械
FR3024890B1 (fr) 2014-08-13 2017-03-17 Safran Assemblage de type liaison pivot
DE102014221899A1 (de) * 2014-10-28 2016-04-28 Bayerische Motoren Werke Aktiengesellschaft Verbindung eines Bauteils mit einem Faserverbundbauteil
EP3199455B1 (en) * 2016-01-29 2020-04-22 AIRBUS HELICOPTERS DEUTSCHLAND GmbH Rotary aircraft with an interface frame joining the fuselage tail boom and the tail cone
CN105757114A (zh) * 2016-05-11 2016-07-13 四川中物技术股份有限公司 结简阻尼轴
CN106346793B (zh) * 2016-10-20 2018-09-18 中国电子科技集团公司第三十八研究所 一种用于碳纤维泡沫夹芯复合材料梁快速对接的拼装机构
EP3366584B1 (en) * 2017-02-27 2019-04-17 AIRBUS HELICOPTERS DEUTSCHLAND GmbH Pitch control device for a ducted tail rotor of a rotorcraft
DE102018208605A1 (de) * 2018-05-30 2019-12-05 Bayerische Motoren Werke Aktiengesellschaft Bauteil sowie Verfahren zum Herstellen einer Bauteilverbindung
KR102153511B1 (ko) * 2019-01-08 2020-09-10 에어버스 헬리콥터스 도이칠란트 게엠베하 덕트된 회전익기 테일 로터의 피치 제어 장치용 제어 이동 부재
CN111998129B (zh) * 2020-08-17 2022-05-27 中国二冶集团有限公司 一种地埋管道安装辅助装置及安装方法
CN112112883B (zh) * 2020-08-29 2024-11-08 天地科技股份有限公司上海分公司 花瓣式铰接结构及其安装方法
CN115958798B (zh) * 2022-09-28 2024-12-17 陕西飞机工业有限责任公司 一种提高金属型材与复合材料胶接表面质量的方法

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2169372B (en) * 1985-01-07 1988-09-14 Rexnord Inc Improvements in and relating to fasteners
SE501741C2 (sv) * 1993-07-06 1995-05-02 Saab Scania Ab Lägesfelkompenserande infästningsanordning för infästning av en hjälpapparat vid en förbränningsmotor
US5622733A (en) * 1994-10-04 1997-04-22 Rockwell International Corporation Tooling for the fabrication of composite hollow crown-stiffened skins and panels
US5966936A (en) * 1998-06-04 1999-10-19 Raytheon Company Pin coupling for reduced side loads in a driven displacer-piston link and method
DE19906126C2 (de) * 1999-02-13 2000-11-30 Daimler Chrysler Aerospace Einrichtung und Verfahren zum Lösen von Verbindungsbolzen
GB2383105A (en) * 2001-12-11 2003-06-18 Rolls Royce Plc Expansion bolt assembly
US20050126699A1 (en) * 2003-12-15 2005-06-16 Anna Yen Process for the manufacture of composite structures
ATE402346T1 (de) * 2004-04-15 2008-08-15 Fatigue Technology Inc Verfahren und vorrichtung unter einsatz von exzenterbuchsen
DE102006007429B4 (de) * 2006-02-17 2011-08-18 Airbus Operations GmbH, 21129 Verfahren zum autoklavfreien Verkleben von Bauteilen für Luftfahrzeuge

Also Published As

Publication number Publication date
EP1996457A1 (en) 2008-12-03
CN101395058A (zh) 2009-03-25
JP2009530169A (ja) 2009-08-27
BRPI0709058A2 (pt) 2011-06-21
RU2008137257A (ru) 2010-04-27
US20090314426A1 (en) 2009-12-24
DE102006013069B3 (de) 2007-12-06
WO2007107521A1 (en) 2007-09-27

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Legal Events

Date Code Title Description
FZDE Discontinued