DE102006013069B3 - Bolzenverbindung - Google Patents

Bolzenverbindung Download PDF

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Publication number
DE102006013069B3
DE102006013069B3 DE102006013069A DE102006013069A DE102006013069B3 DE 102006013069 B3 DE102006013069 B3 DE 102006013069B3 DE 102006013069 A DE102006013069 A DE 102006013069A DE 102006013069 A DE102006013069 A DE 102006013069A DE 102006013069 B3 DE102006013069 B3 DE 102006013069B3
Authority
DE
Germany
Prior art keywords
bolt
component
bushing
bolt connection
obliquely
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 - Fee Related
Application number
DE102006013069A
Other languages
German (de)
English (en)
Inventor
Uwe Dipl.-Ing. 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
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
Priority to DE102006013069A priority Critical patent/DE102006013069B3/de
Application filed by Airbus Operations GmbH filed Critical Airbus Operations GmbH
Priority to EP07727005A priority patent/EP1996457A1/en
Priority to CNA2007800080254A priority patent/CN101395058A/zh
Priority to JP2009500834A priority patent/JP2009530169A/ja
Priority to RU2008137257/11A priority patent/RU2008137257A/ru
Priority to US12/281,087 priority patent/US20090314426A1/en
Priority to CA002640693A priority patent/CA2640693A1/en
Priority to BRPI0709058-7A priority patent/BRPI0709058A2/pt
Priority to PCT/EP2007/052526 priority patent/WO2007107521A1/en
Application granted granted Critical
Publication of DE102006013069B3 publication Critical patent/DE102006013069B3/de
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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)
  • Mutual Connection Of Rods And Tubes (AREA)
  • Pivots And Pivotal Connections (AREA)
DE102006013069A 2006-03-22 2006-03-22 Bolzenverbindung Expired - Fee Related DE102006013069B3 (de)

Priority Applications (9)

Application Number Priority Date Filing Date Title
DE102006013069A DE102006013069B3 (de) 2006-03-22 2006-03-22 Bolzenverbindung
CNA2007800080254A CN101395058A (zh) 2006-03-22 2007-03-16 螺栓接合
JP2009500834A JP2009530169A (ja) 2006-03-22 2007-03-16 ボルト継ぎ手
RU2008137257/11A RU2008137257A (ru) 2006-03-22 2007-03-16 Болтовое соединение
EP07727005A EP1996457A1 (en) 2006-03-22 2007-03-16 Bolted joint
US12/281,087 US20090314426A1 (en) 2006-03-22 2007-03-16 Bolted joint
CA002640693A CA2640693A1 (en) 2006-03-22 2007-03-16 Bolted joint
BRPI0709058-7A BRPI0709058A2 (pt) 2006-03-22 2007-03-16 ligação com parafusos de porca
PCT/EP2007/052526 WO2007107521A1 (en) 2006-03-22 2007-03-16 Bolted joint

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE102006013069A DE102006013069B3 (de) 2006-03-22 2006-03-22 Bolzenverbindung

Publications (1)

Publication Number Publication Date
DE102006013069B3 true DE102006013069B3 (de) 2007-12-06

Family

ID=38083573

Family Applications (1)

Application Number Title Priority Date Filing Date
DE102006013069A Expired - Fee Related DE102006013069B3 (de) 2006-03-22 2006-03-22 Bolzenverbindung

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)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102011119251A1 (de) * 2011-11-24 2013-05-29 Leichtbau-Zentrum Sachsen Gmbh Vorrichtung zur Krafteinleitung in ein Bauteil aus Faserverbundwerkstoff
DE102014221899A1 (de) * 2014-10-28 2016-04-28 Bayerische Motoren Werke Aktiengesellschaft Verbindung eines Bauteils mit einem Faserverbundbauteil
DE102018208605A1 (de) * 2018-05-30 2019-12-05 Bayerische Motoren Werke Aktiengesellschaft Bauteil sowie Verfahren zum Herstellen einer Bauteilverbindung

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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
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
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

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0633404B1 (en) * 1993-07-06 1997-10-01 Scania Cv Aktiebolag Positional error compensating arrangement for fastening auxiliary equipment to an internal combustion engine
EP1027566B1 (en) * 1998-06-04 2003-07-23 Raytheon Company Pin coupling for reduced side loads in a driven displacer - piston link and method
EP1027960B1 (de) * 1999-02-13 2006-06-07 Airbus Deutschland GmbH Einrichtung und Verfahren zum Lösen von Verbindungsbolzen

Family Cites Families (6)

* 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
US5622733A (en) * 1994-10-04 1997-04-22 Rockwell International Corporation Tooling for the fabrication of composite hollow crown-stiffened skins and panels
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
ES2311224T3 (es) * 2004-04-15 2009-02-01 Fatigue Technology, Inc. Metodo y aparato que emplea un casquillo excentrico.
DE102006007429B4 (de) * 2006-02-17 2011-08-18 Airbus Operations GmbH, 21129 Verfahren zum autoklavfreien Verkleben von Bauteilen für Luftfahrzeuge

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0633404B1 (en) * 1993-07-06 1997-10-01 Scania Cv Aktiebolag Positional error compensating arrangement for fastening auxiliary equipment to an internal combustion engine
EP1027566B1 (en) * 1998-06-04 2003-07-23 Raytheon Company Pin coupling for reduced side loads in a driven displacer - piston link and method
EP1027960B1 (de) * 1999-02-13 2006-06-07 Airbus Deutschland GmbH Einrichtung und Verfahren zum Lösen von Verbindungsbolzen

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102011119251A1 (de) * 2011-11-24 2013-05-29 Leichtbau-Zentrum Sachsen Gmbh Vorrichtung zur Krafteinleitung in ein Bauteil aus Faserverbundwerkstoff
DE102011119251B4 (de) * 2011-11-24 2015-05-07 Leichtbau-Zentrum Sachsen Gmbh Vorrichtung zur Krafteinleitung in ein Bauteil aus Faserverbundwerkstoff
US10266026B2 (en) 2011-11-24 2019-04-23 Leichtbau-Zentrum Sachsen Gmbh Device for introducing force into a component of fiber composite material
DE102014221899A1 (de) * 2014-10-28 2016-04-28 Bayerische Motoren Werke Aktiengesellschaft Verbindung eines Bauteils mit einem Faserverbundbauteil
DE102018208605A1 (de) * 2018-05-30 2019-12-05 Bayerische Motoren Werke Aktiengesellschaft Bauteil sowie Verfahren zum Herstellen einer Bauteilverbindung

Also Published As

Publication number Publication date
JP2009530169A (ja) 2009-08-27
CN101395058A (zh) 2009-03-25
WO2007107521A1 (en) 2007-09-27
US20090314426A1 (en) 2009-12-24
CA2640693A1 (en) 2007-09-27
BRPI0709058A2 (pt) 2011-06-21
RU2008137257A (ru) 2010-04-27
EP1996457A1 (en) 2008-12-03

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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

R119 Application deemed withdrawn, or ip right lapsed, due to non-payment of renewal fee