JP2015072042A5 - - Google Patents

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Publication number
JP2015072042A5
JP2015072042A5 JP2013207663A JP2013207663A JP2015072042A5 JP 2015072042 A5 JP2015072042 A5 JP 2015072042A5 JP 2013207663 A JP2013207663 A JP 2013207663A JP 2013207663 A JP2013207663 A JP 2013207663A JP 2015072042 A5 JP2015072042 A5 JP 2015072042A5
Authority
JP
Japan
Prior art keywords
groove
joint
fitting shape
fitting
shape
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.)
Granted
Application number
JP2013207663A
Other languages
English (en)
Japanese (ja)
Other versions
JP2015072042A (ja
JP6090931B2 (ja
Filing date
Publication date
Application filed filed Critical
Priority claimed from JP2013207663A external-priority patent/JP6090931B2/ja
Priority to JP2013207663A priority Critical patent/JP6090931B2/ja
Priority to PCT/JP2014/063384 priority patent/WO2015049895A1/ja
Priority to US14/908,743 priority patent/US10071794B2/en
Priority to EP14851380.7A priority patent/EP3015721B1/en
Priority to CN201480043091.5A priority patent/CN105452679B/zh
Priority to CA2919618A priority patent/CA2919618C/en
Priority to BR112016002134A priority patent/BR112016002134A2/pt
Priority to RU2016102799A priority patent/RU2636373C2/ru
Publication of JP2015072042A publication Critical patent/JP2015072042A/ja
Publication of JP2015072042A5 publication Critical patent/JP2015072042A5/ja
Publication of JP6090931B2 publication Critical patent/JP6090931B2/ja
Application granted granted Critical
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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JP2013207663A 2013-10-02 2013-10-02 継手及び航空機構造 Active JP6090931B2 (ja)

Priority Applications (8)

Application Number Priority Date Filing Date Title
JP2013207663A JP6090931B2 (ja) 2013-10-02 2013-10-02 継手及び航空機構造
BR112016002134A BR112016002134A2 (pt) 2013-10-02 2014-05-20 união e estrutura de aeronave
US14/908,743 US10071794B2 (en) 2013-10-02 2014-05-20 Joint, and aircraft structure
EP14851380.7A EP3015721B1 (en) 2013-10-02 2014-05-20 Joint, and aircraft structure
CN201480043091.5A CN105452679B (zh) 2013-10-02 2014-05-20 接头及航空机结构
CA2919618A CA2919618C (en) 2013-10-02 2014-05-20 Joint, and aircraft structure
PCT/JP2014/063384 WO2015049895A1 (ja) 2013-10-02 2014-05-20 継手及び航空機構造
RU2016102799A RU2636373C2 (ru) 2013-10-02 2014-05-20 Соединение и конструкция летательного аппарата

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP2013207663A JP6090931B2 (ja) 2013-10-02 2013-10-02 継手及び航空機構造

Publications (3)

Publication Number Publication Date
JP2015072042A JP2015072042A (ja) 2015-04-16
JP2015072042A5 true JP2015072042A5 (enExample) 2016-07-07
JP6090931B2 JP6090931B2 (ja) 2017-03-08

Family

ID=52778492

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2013207663A Active JP6090931B2 (ja) 2013-10-02 2013-10-02 継手及び航空機構造

Country Status (8)

Country Link
US (1) US10071794B2 (enExample)
EP (1) EP3015721B1 (enExample)
JP (1) JP6090931B2 (enExample)
CN (1) CN105452679B (enExample)
BR (1) BR112016002134A2 (enExample)
CA (1) CA2919618C (enExample)
RU (1) RU2636373C2 (enExample)
WO (1) WO2015049895A1 (enExample)

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9199715B2 (en) * 2013-10-10 2015-12-01 The Boeing Company Self-aligning fitting assemblies and systems and methods including the same
CN109641408A (zh) * 2016-06-28 2019-04-16 维斯塔斯风力系统有限公司 风轮机叶片的制造方法
US10696373B2 (en) * 2016-09-13 2020-06-30 The Boeing Company Aircraft wings and aircraft including such aircraft wings
US10703419B2 (en) * 2017-05-19 2020-07-07 Divergent Technologies, Inc. Apparatus and methods for joining panels
US10605631B2 (en) * 2017-08-03 2020-03-31 Sikorsky Aircraft Corporation Structural pi joint with integrated fiber optic sensing
US11091266B2 (en) 2017-08-29 2021-08-17 Goodrich Corporation Conformable tank fabricated using additive manufacturing
US10703481B2 (en) 2017-08-29 2020-07-07 Goodrich Corporation Conformable tank with sandwich structure walls
US11939105B2 (en) 2017-08-29 2024-03-26 Goodrich Corporation 3D woven conformable tank
US10816138B2 (en) 2017-09-15 2020-10-27 Goodrich Corporation Manufacture of a conformable pressure vessel
CN109236819B (zh) * 2018-09-19 2023-11-24 苏州富强科技有限公司 用于对l形零件进行定位保压的设备
EP3954907B1 (en) * 2019-04-12 2024-07-10 IHI Aerospace Co., Ltd. Joint structure and assembly method for same
US12220877B2 (en) 2022-01-04 2025-02-11 Rohr, Inc. Component with monolithic structure having blind interface joint
GB2617556A (en) * 2022-04-08 2023-10-18 Airbus Operations Ltd Wing-box structure

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US4671470A (en) * 1985-07-15 1987-06-09 Beech Aircraft Corporation Method for fastening aircraft frame elements to sandwich skin panels covering same using woven fiber connectors
US5474635A (en) * 1994-03-07 1995-12-12 United Technologies Corporation Joining non-coplanar panels and structures of fiber reinforced composites
JP3667200B2 (ja) * 2000-07-12 2005-07-06 株式会社イシモク・コーポレーション 木製品の連結構造
US6374570B1 (en) * 2000-08-25 2002-04-23 Lockheed Martin Corporation Apparatus and method for joining dissimilar materials to form a structural support member
US6849150B1 (en) * 2001-01-16 2005-02-01 Lockheed Martin Corporation System and method of forming structural assemblies with 3-D woven joint pre-forms
US6863767B2 (en) * 2001-08-23 2005-03-08 Lockheed Martin Corporation Paste-bond clevis joint
US7205066B1 (en) * 2002-05-23 2007-04-17 Rohr, Inc. Structural element with rib-receiving member
US6749155B2 (en) 2002-09-13 2004-06-15 The Boeing Company Composite assembly with integrated composite joints
JP3659249B2 (ja) * 2002-12-27 2005-06-15 住友金属工業株式会社 鋼矢板および矢板式鋼製壁
JP2004216672A (ja) * 2003-01-14 2004-08-05 Pearl Mannequin:Kk 中空合体式成型体及び成形型
US7037568B1 (en) * 2003-07-15 2006-05-02 Rogers Terry W Joining member for mechanically joining a skin to a supporting rib
US20060115320A1 (en) 2004-11-30 2006-06-01 The Boeing Company Determinant assembly features for vehicle structures
US8272618B2 (en) 2004-11-30 2012-09-25 The Boeing Company Minimum bond thickness assembly feature assurance
US7555873B2 (en) 2004-11-30 2009-07-07 The Boeing Company Self-locating feature for a pi-joint assembly
US7393488B2 (en) * 2005-05-25 2008-07-01 The Boeing Company Methods of joining structures and joints formed thereby
US7670527B2 (en) * 2006-05-09 2010-03-02 Lockheed Martin Corporation Failsafe injected adhesive joint
US8082667B2 (en) * 2007-05-31 2011-12-27 The Boeing Company Apparatus and methods for securing a first structural member and a second structural member to one another
US8747988B2 (en) 2008-12-04 2014-06-10 Bayer Materialscience Ag Glued composite plastic part, method for the production thereof, and part made therefrom
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FR2954200B1 (fr) 2009-12-23 2012-03-02 Snecma Procede de realisation d'un renfort metallique d'aube de turbomachine
CN102473881A (zh) * 2010-02-02 2012-05-23 松下电器产业株式会社 电池收纳盒及具备该电池收纳盒的电池组件
US9073267B1 (en) * 2010-03-10 2015-07-07 The Boeing Company Method of assembling panels and adhesively bonded joints used therein
RU103588U1 (ru) * 2010-08-20 2011-04-20 Владимир Владимирович Жебелев Клеевое соединение транца с днищем
DE102010064060A1 (de) 2010-12-23 2012-06-28 Airbus Operations Gmbh Befestigungsanordnung zum Befestigen einer Komponente eines Luft- oder Raumfahrzeuges, Klebehalter einer derartigen Befestigungsanordnung und Luft- oder Raumfahrzeug mit einer derartigen Befestigungsanordnung und/oder einem derartigen Klebehalter
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CN202244075U (zh) * 2011-06-03 2012-05-30 哈尔滨飞机工业集团有限责任公司 一种框与壁板的连接结构
US8393871B2 (en) * 2011-07-19 2013-03-12 General Electric Company Wind turbine blade shear web connection assembly
US9017510B2 (en) * 2011-12-13 2015-04-28 The Boeing Company Method and apparatus for fabricating large scale integrated airfoils
US9681527B2 (en) * 2013-03-29 2017-06-13 The Boeing Company Method and apparatus for providing a current return network in an aircraft structure

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