JP2015502504A5 - - Google Patents
Download PDFInfo
- Publication number
- JP2015502504A5 JP2015502504A5 JP2014539962A JP2014539962A JP2015502504A5 JP 2015502504 A5 JP2015502504 A5 JP 2015502504A5 JP 2014539962 A JP2014539962 A JP 2014539962A JP 2014539962 A JP2014539962 A JP 2014539962A JP 2015502504 A5 JP2015502504 A5 JP 2015502504A5
- Authority
- JP
- Japan
- Prior art keywords
- mandrel
- composite
- stiffener
- composite tube
- forming
- 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
Links
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US13/288,491 | 2011-11-03 | ||
| US13/288,491 US8904904B2 (en) | 2011-11-03 | 2011-11-03 | Tubular composite strut having internal stiffening |
| PCT/US2012/058994 WO2013066565A1 (en) | 2011-11-03 | 2012-10-05 | Tubular composite strut having internal stiffening and method for making the same |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| JP2015502504A JP2015502504A (ja) | 2015-01-22 |
| JP2015502504A5 true JP2015502504A5 (enExample) | 2015-11-26 |
| JP6189312B2 JP6189312B2 (ja) | 2017-08-30 |
Family
ID=47089159
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP2014539962A Active JP6189312B2 (ja) | 2011-11-03 | 2012-10-05 | 内部補剛を有する管状複合ストラットおよびそれを作製するための方法 |
Country Status (9)
| Country | Link |
|---|---|
| US (1) | US8904904B2 (enExample) |
| EP (1) | EP2773497B1 (enExample) |
| JP (1) | JP6189312B2 (enExample) |
| CN (1) | CN103889692B (enExample) |
| BR (1) | BR112014010465B1 (enExample) |
| CA (1) | CA2850628C (enExample) |
| ES (1) | ES2770654T3 (enExample) |
| PT (1) | PT2773497T (enExample) |
| WO (1) | WO2013066565A1 (enExample) |
Families Citing this family (35)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2960468B1 (fr) * | 2010-05-31 | 2013-03-29 | Commissariat Energie Atomique | Structure gonflable articulee et bras robotise comportant une telle structure |
| DE102011053480A1 (de) * | 2011-06-22 | 2012-12-27 | Mt Aerospace Ag | Bauteil zur Aufnahme und/oder Übertragung von mechanischen Kräften und/oder Momenten, ein Verfahren zu dessen Herstellung und dessen Verwendung |
| US10457011B2 (en) | 2011-11-03 | 2019-10-29 | The Boeing Company | Composite columnar structure having co-bonded reinforcement and fabrication method |
| US10464656B2 (en) * | 2011-11-03 | 2019-11-05 | The Boeing Company | Tubular composite strut having internal stiffening and method for making the same |
| US8973281B1 (en) | 2012-10-11 | 2015-03-10 | The Boeing Company | Edge distance gauge |
| WO2015053940A1 (en) * | 2013-10-07 | 2015-04-16 | United Technologies Corporation | Additively grown enhanced impact resistance features for improved structure and joint protection |
| US20160101543A1 (en) * | 2013-12-03 | 2016-04-14 | The Boeing Company | Hybrid Laminate and Molded Composite Structures |
| US11034113B2 (en) * | 2014-01-29 | 2021-06-15 | Sikorsky Aircraft Corporation | Method of assembling a composite spar removable mandrel |
| US20160339661A1 (en) * | 2014-01-29 | 2016-11-24 | Sikorsky Aircraft Corporation | Composite spar removable mandrel |
| EP3131742B1 (en) * | 2014-04-16 | 2023-01-25 | Hexcel Reinforcements SAS | Method of manufacturing a composite part |
| CN106255584B (zh) * | 2014-04-30 | 2019-05-03 | 麦格纳国际公司 | 用于形成三维物体的装置及方法 |
| FR3020780B1 (fr) * | 2014-05-09 | 2017-01-13 | Airbus Operations Sas | Procede de fabrication d'une piece en materiau composite pour structure d'aeronef par pultrusion et cocuisson |
| DE102014222385A1 (de) * | 2014-11-03 | 2016-05-04 | Bayerische Motoren Werke Aktiengesellschaft | Krafteinleitungsbauteil sowie Verfahren zur Herstellung von Composite- Rohrverbindungen mit einem Krafteinleitungsbauteil |
| EP3274145B1 (en) * | 2015-03-25 | 2023-03-22 | Sikorsky Aircraft Corporation | Processes for manufacturing parts employing additive manufacturing |
| DE102015215026A1 (de) * | 2015-08-06 | 2017-02-09 | Robert Bosch Gmbh | Mechanische und/oder elektrische Baugruppe |
| US20170190149A1 (en) * | 2016-01-04 | 2017-07-06 | Caterpillar Inc. | Carbon fiber wrapped structural components for a machine |
| CN105836098A (zh) * | 2016-03-25 | 2016-08-10 | 哈尔滨飞机工业集团有限责任公司 | 一种嵌套式复合材料的圆筒结构 |
| US10272991B2 (en) * | 2016-06-23 | 2019-04-30 | Goodrich Corporation | Metallic composite joint |
| US10563690B2 (en) | 2016-07-28 | 2020-02-18 | Goodrich Corporation | Thin-skin side stay beams and landing gear assemblies |
| US10744727B2 (en) | 2017-03-21 | 2020-08-18 | Textron Innovations Inc. | Methods of making a specimen with a predetermined wrinkle defect |
| US10746640B2 (en) * | 2017-03-21 | 2020-08-18 | Textron Innovations Inc. | Methods of making a tubular specimen with a predetermined wrinkle defect |
| DE102017107463B3 (de) * | 2017-04-06 | 2018-05-09 | THK RHYTHM AUTOMOTIVE GmbH | Fahrwerkbauteil und Verfahren zu dessen Herstellung |
| KR101858723B1 (ko) * | 2017-05-23 | 2018-05-16 | 주식회사 오즈인더스트리 | 래싱바 및 이의 제조방법 |
| GB2566947B (en) * | 2017-09-27 | 2021-12-08 | Ge Aviat Systems Ltd | Strut and method of forming strut |
| CN108253033A (zh) * | 2017-12-08 | 2018-07-06 | 贵州华烽电器有限公司 | 防操纵机构卡死的拉杆设计 |
| US11001369B2 (en) * | 2018-04-02 | 2021-05-11 | Bell Helicopter Textron Inc. | Hybrid light weight rotorcraft hub trunnions |
| DE102018208282A1 (de) * | 2018-05-25 | 2019-11-28 | Zf Friedrichshafen Ag | Fahrwerklenker für ein Kraftfahrzeug |
| EP3597410A1 (en) * | 2018-07-20 | 2020-01-22 | Crompton Technology Group Limited | Composite component and manufacture thereof |
| DE102018213322A1 (de) * | 2018-08-08 | 2020-02-13 | Zf Friedrichshafen Ag | Mehrpunktlenker für ein Fahrwerk eines Kraftfahrzeugs |
| US12078207B2 (en) * | 2018-09-21 | 2024-09-03 | Tirsan Kardan Sanayi Ve Ticaret A.S. | Production assembly and method for hybrid composite driveshaft tube |
| GB2579217B (en) * | 2018-11-26 | 2023-04-26 | Polar Tech Management Group Limited | Gears |
| US11773896B2 (en) * | 2019-07-22 | 2023-10-03 | Hamilton Sundstrand Corporation | Composite drive shaft under dominant unidirectional torque |
| CN111059137A (zh) * | 2019-11-14 | 2020-04-24 | 中国商用飞机有限责任公司北京民用飞机技术研究中心 | 一种复合材料杆件与金属接头的连接结构及成型方法 |
| DE102019220541A1 (de) * | 2019-12-23 | 2021-06-24 | Robert Bosch Gmbh | Gehäusekomponente einer Baueinheit |
| CN119712699A (zh) * | 2023-09-27 | 2025-03-28 | 上海交通大学 | 无人机复合材料螺旋桨安装轴及其制备工艺 |
Family Cites Families (24)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4014184A (en) * | 1975-01-27 | 1977-03-29 | Stark Martin H | Propeller shaft liner and inserting apparatus |
| US4275122A (en) * | 1978-07-17 | 1981-06-23 | Gkn Transmissions Limited | Shaft and universal joint member assembly |
| US4272971A (en) * | 1979-02-26 | 1981-06-16 | Rockwell International Corporation | Reinforced tubular structure |
| US4469730A (en) | 1982-12-30 | 1984-09-04 | The Boeing Company | Composite base structure and end fitting joint and method |
| FR2540430A3 (fr) | 1983-02-07 | 1984-08-10 | Sardou Max | Structure en materiaux composites capable de transmettre des efforts de compression et de traction |
| US4851065A (en) * | 1986-01-17 | 1989-07-25 | Tyee Aircraft, Inc. | Construction of hollow, continuously wound filament load-bearing structure |
| FR2604768B1 (fr) | 1986-10-07 | 1988-12-30 | Inst Francais Du Petrole | Raccord et procede de fabrication de ce raccord pour arbre comportant une armature de renfort |
| GB2215008A (en) | 1988-02-17 | 1989-09-13 | Smith Corp A O | Fiber reinforced resin drive shaft having improved resistance to torsional buckling |
| US5439750A (en) | 1993-06-15 | 1995-08-08 | General Electric Company | Titanium metal matrix composite inserts for stiffening turbine engine components |
| US5866272A (en) | 1996-01-11 | 1999-02-02 | The Boeing Company | Titanium-polymer hybrid laminates |
| JP2000108210A (ja) * | 1998-10-02 | 2000-04-18 | Toyota Autom Loom Works Ltd | Ｆｒｐ製筒部品の製造方法及び中子 |
| WO2000023151A1 (fr) | 1998-10-19 | 2000-04-27 | Mizuno Corporation | Baton de baseball ou de softball |
| US6711783B2 (en) | 1998-11-12 | 2004-03-30 | Lemole John M. | Anti-pinch knuckle for bidirectional sleeve |
| KR100427223B1 (ko) | 2001-01-18 | 2004-04-27 | 임홍섭 | 포울 및 그 제조 방법 |
| JP2003001716A (ja) * | 2001-06-21 | 2003-01-08 | Toyota Industries Corp | 繊維強化プラスチック製パイプの製造方法 |
| JP2004293714A (ja) * | 2003-03-27 | 2004-10-21 | Toyota Industries Corp | 動力伝達シャフト及びその製造方法並びに治具 |
| FR2887601B1 (fr) * | 2005-06-24 | 2007-10-05 | Snecma Moteurs Sa | Piece mecanique et procede de fabrication d'une telle piece |
| FR2890591B1 (fr) * | 2005-09-12 | 2012-10-19 | Eads | Procede de fabrication d'une piece composite rtm et piece composite obtenue selon ce procede |
| US7452156B2 (en) | 2006-11-17 | 2008-11-18 | The Boeing Company | Composite structural member and method for making the same |
| US8414724B2 (en) | 2006-12-02 | 2013-04-09 | The Boeing Company | Composite tube having cobonded end fittings and method of making same |
| DE102007015909A1 (de) | 2007-04-02 | 2008-10-09 | Mt Aerospace Ag | Verfahren zur Herstellung faserverstärkter Hohlkörper |
| US8123996B2 (en) | 2008-02-07 | 2012-02-28 | The Boeing Company | Wrinkle control for composite tubes |
| FR2957843B1 (fr) | 2010-03-25 | 2014-05-16 | Epsilon Composite | Procede de realisation d'une piece de liaison en materiau composite et piece obtenue |
| US9486965B2 (en) * | 2011-11-03 | 2016-11-08 | The Boeing Company | Composite columnar structure having co-bonded reinforcement and fabrication method |
-
2011
- 2011-11-03 US US13/288,491 patent/US8904904B2/en active Active
-
2012
- 2012-10-05 EP EP12779233.1A patent/EP2773497B1/en active Active
- 2012-10-05 CA CA2850628A patent/CA2850628C/en active Active
- 2012-10-05 CN CN201280050049.7A patent/CN103889692B/zh active Active
- 2012-10-05 ES ES12779233T patent/ES2770654T3/es active Active
- 2012-10-05 JP JP2014539962A patent/JP6189312B2/ja active Active
- 2012-10-05 PT PT127792331T patent/PT2773497T/pt unknown
- 2012-10-05 BR BR112014010465-4A patent/BR112014010465B1/pt active IP Right Grant
- 2012-10-05 WO PCT/US2012/058994 patent/WO2013066565A1/en not_active Ceased
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| JP2015502504A5 (enExample) | ||
| CN104723579B (zh) | 一种全复合材料波纹夹层圆柱壳的组合模具 | |
| TWI623672B (zh) | Composite pipe for supporting structure and preparation method thereof | |
| CA2861312C (en) | Systems and methods of constructing composite assemblies | |
| RU2011100296A (ru) | Слоистая панель с интегрированной усиливающей структурой и способ ее производства | |
| RU2013128408A (ru) | Композитный шляпообразный профиль усиления, композитные усиленные шляпообразными профилями гермоперегородки и способы их изготовления | |
| WO2010101741A3 (en) | Method for producing contoured composite structures and structures produced thereby | |
| CN103889692A (zh) | 内部加强的管状复合支杆及其制造方法 | |
| CA2633393A1 (en) | Ceramic matrix composite structure having fluted core and method of making the same | |
| JP2015199347A5 (enExample) | ||
| CN101758923B (zh) | 一种复合材料盒形肋及其制作方法 | |
| JP2011235635A5 (enExample) | ||
| WO2010019948A3 (en) | Method and system for forming composite lattice support structures | |
| CN101954744B (zh) | 一种采用纤维编织布制备金字塔型点阵夹芯板的方法 | |
| CN106470830B (zh) | 由层压件制成的面板及其制造方法 | |
| CN105946246A (zh) | 一种碳纤维蜂窝芯材的制备方法 | |
| CN104385624A (zh) | 一种采用卧式安装的复合材料筒壳的成形方法 | |
| JP2015074229A5 (enExample) | ||
| CN103600498A (zh) | 分段式风电叶片的制造以及装配方法 | |
| CN103692664B (zh) | 一种中空复合材料接头的拼接方法 | |
| CN101973129A (zh) | 采用纤维编织预浸布制备复合材料点阵夹芯板的方法 | |
| CN102785371B (zh) | 采用预浸纤维束制备复合材料点阵夹芯板的制备方法 | |
| RU2559446C1 (ru) | Способ изготовления трехслойной панели из композиционного материала | |
| CN104149358A (zh) | 复合材料夹芯管材的制造方法 | |
| CN203093159U (zh) | 一种杆件与面板新型连接的复合材料点阵结构 |