JP2009530169A5 - - Google Patents

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Publication number
JP2009530169A5
JP2009530169A5 JP2009500834A JP2009500834A JP2009530169A5 JP 2009530169 A5 JP2009530169 A5 JP 2009530169A5 JP 2009500834 A JP2009500834 A JP 2009500834A JP 2009500834 A JP2009500834 A JP 2009500834A JP 2009530169 A5 JP2009530169 A5 JP 2009530169A5
Authority
JP
Japan
Prior art keywords
component
bolt
bushing
joint
slots
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.)
Pending
Application number
JP2009500834A
Other languages
English (en)
Japanese (ja)
Other versions
JP2009530169A (ja
Filing date
Publication date
Priority claimed from DE102006013069A external-priority patent/DE102006013069B3/de
Application filed filed Critical
Publication of JP2009530169A publication Critical patent/JP2009530169A/ja
Publication of JP2009530169A5 publication Critical patent/JP2009530169A5/ja
Pending legal-status Critical Current

Links

JP2009500834A 2006-03-22 2007-03-16 ボルト継ぎ手 Pending JP2009530169A (ja)

Applications Claiming Priority (2)

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

Publications (2)

Publication Number Publication Date
JP2009530169A JP2009530169A (ja) 2009-08-27
JP2009530169A5 true JP2009530169A5 (enExample) 2011-05-12

Family

ID=38083573

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2009500834A Pending JP2009530169A (ja) 2006-03-22 2007-03-16 ボルト継ぎ手

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

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