JP2015504789A5 - - Google Patents
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- Publication number
- JP2015504789A5 JP2015504789A5 JP2014539996A JP2014539996A JP2015504789A5 JP 2015504789 A5 JP2015504789 A5 JP 2015504789A5 JP 2014539996 A JP2014539996 A JP 2014539996A JP 2014539996 A JP2014539996 A JP 2014539996A JP 2015504789 A5 JP2015504789 A5 JP 2015504789A5
- Authority
- JP
- Japan
- Prior art keywords
- core
- reinforcement
- sleeve
- strut
- producing
- 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
- 230000002787 reinforcement Effects 0.000 claims 15
- 238000000034 method Methods 0.000 claims 4
- 239000011347 resin Substances 0.000 claims 4
- 229920005989 resin Polymers 0.000 claims 4
- 239000002131 composite material Substances 0.000 claims 2
- 239000000835 fiber Substances 0.000 claims 2
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 claims 1
- 239000004918 carbon fiber reinforced polymer Substances 0.000 claims 1
- 239000000919 ceramic Substances 0.000 claims 1
- 238000005056 compaction Methods 0.000 claims 1
- 238000004519 manufacturing process Methods 0.000 claims 1
- 229910052751 metal Inorganic materials 0.000 claims 1
- 239000002184 metal Substances 0.000 claims 1
- 230000003014 reinforcing effect Effects 0.000 claims 1
- 239000010936 titanium Substances 0.000 claims 1
- 229910052719 titanium Inorganic materials 0.000 claims 1
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US13/326,005 | 2011-12-14 | ||
| US13/326,005 US9486965B2 (en) | 2011-11-03 | 2011-12-14 | Composite columnar structure having co-bonded reinforcement and fabrication method |
| PCT/US2012/061997 WO2013066727A1 (en) | 2011-11-03 | 2012-10-25 | Composite columnar structure having co-bonded reinforcement and fabrication method |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| JP2015504789A JP2015504789A (ja) | 2015-02-16 |
| JP2015504789A5 true JP2015504789A5 (enExample) | 2015-12-10 |
| JP6089041B2 JP6089041B2 (ja) | 2017-03-01 |
Family
ID=48610399
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP2014539996A Active JP6089041B2 (ja) | 2011-12-14 | 2012-10-25 | 共結合補強材を有する柱状複合材構造及び製作方法 |
Country Status (8)
| Country | Link |
|---|---|
| US (1) | US9486965B2 (enExample) |
| EP (1) | EP2790898B1 (enExample) |
| JP (1) | JP6089041B2 (enExample) |
| CN (1) | CN104023954B9 (enExample) |
| CA (1) | CA2851824C (enExample) |
| ES (1) | ES2665010T3 (enExample) |
| RU (1) | RU2615705C2 (enExample) |
| WO (1) | WO2013066727A1 (enExample) |
Families Citing this family (31)
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| US9586699B1 (en) | 1999-08-16 | 2017-03-07 | Smart Drilling And Completion, Inc. | Methods and apparatus for monitoring and fixing holes in composite aircraft |
| US9625361B1 (en) | 2001-08-19 | 2017-04-18 | Smart Drilling And Completion, Inc. | Methods and apparatus to prevent failures of fiber-reinforced composite materials under compressive stresses caused by fluids and gases invading microfractures in the materials |
| DE102010053850A1 (de) * | 2010-12-08 | 2012-06-14 | Daimler Ag | Kraftfahrzeugkarosserie mit Versteifungsstreben |
| US8904904B2 (en) * | 2011-11-03 | 2014-12-09 | The Boeing Company | Tubular composite strut having internal stiffening |
| 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 |
| CN202691565U (zh) * | 2012-06-05 | 2013-01-23 | 张家港中集圣达因低温装备有限公司 | 一种玻璃钢管及低温压力容器 |
| CN103286956B (zh) * | 2013-06-07 | 2015-11-25 | 莫凡 | 航空用碳纤维复合材料管型杆件及其制造方法 |
| CN104879646B (zh) * | 2015-05-08 | 2018-05-25 | 上海云逸民用航空科技有限公司 | 复合材料杆件 |
| CN105587752A (zh) * | 2015-12-09 | 2016-05-18 | 上海复合材料科技有限公司 | 复合材料连接杆及其制备方法 |
| US20170190149A1 (en) * | 2016-01-04 | 2017-07-06 | Caterpillar Inc. | Carbon fiber wrapped structural components for a machine |
| US10556673B2 (en) * | 2016-06-27 | 2020-02-11 | Goodrich Corporation | Manufacturing method of polymer composite/metal load transfer joint for landing gear |
| DE102017216085A1 (de) * | 2016-09-27 | 2018-03-29 | SKF Aerospace France S.A.S | Verfahren zum Herstellen einer Verstrebung und dadurch hergestellte Verstrebung |
| 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 |
| US11156245B2 (en) * | 2018-01-08 | 2021-10-26 | Goodrich Corporation | Hybrid metallic/composite axial tension/compression lobe joint |
| DE102018213321A1 (de) * | 2018-08-08 | 2020-02-13 | Zf Friedrichshafen Ag | Mehrpunktlenker für ein Fahrwerk eines Kraftfahrzeugs |
| US20220126192A1 (en) * | 2019-02-01 | 2022-04-28 | Pda Ecolab, Sas | Sliding board with corrugated mediums |
| EP3938076A1 (en) | 2019-03-12 | 2022-01-19 | Corning Incorporated | Ceramic honeycomb body with skin |
| CN109737134B (zh) * | 2019-03-14 | 2021-03-30 | 中国商用飞机有限责任公司 | 破损安全连杆 |
| RU194220U1 (ru) * | 2019-07-12 | 2019-12-03 | Федеральное государственное бюджетное образовательное учреждение высшего образования "Казанский национальный исследовательский технический университет им. А.Н. Туполева - КАИ" (КНИТУ-КАИ) | Полый стержень из композиционного материала ферменной конструкции |
| CN110978568B (zh) * | 2019-12-18 | 2022-04-08 | 航天特种材料及工艺技术研究所 | 一种纺织刚性热防护材料及其rtm成型方法 |
| DE102019220541A1 (de) * | 2019-12-23 | 2021-06-24 | Robert Bosch Gmbh | Gehäusekomponente einer Baueinheit |
| CN110937119A (zh) * | 2019-12-24 | 2020-03-31 | 肇庆市海特复合材料技术研究院 | 一种一体式全复合材料连杆结构 |
| KR102581366B1 (ko) * | 2021-09-29 | 2023-10-05 | 한국기술교육대학교 산학협력단 | 수소 연료전지 드론의 프레임 |
| KR102609529B1 (ko) * | 2021-11-11 | 2023-12-01 | 한국기술교육대학교 산학협력단 | 다공성 구조를 이용한 항공기 프레임 |
| CN114932694B (zh) * | 2022-04-28 | 2023-09-01 | 广联航空工业股份有限公司 | 一种轻质高强度抗扭复合材料机械臂杆的制备方法 |
| US12240188B2 (en) * | 2022-05-02 | 2025-03-04 | The Boeing Company | Apparatus and method for manufacturing thermoplastic wrinkle coupons |
| CN115071175B (zh) * | 2022-06-22 | 2024-01-23 | 沈阳飞机工业(集团)有限公司 | 大型筒段外多个高尺寸复合材料隔框成型工装 |
| US20250283504A1 (en) * | 2024-03-08 | 2025-09-11 | AvtechTyee, Inc. | 3d printed linkage |
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|---|---|---|---|---|
| US4014184A (en) | 1975-01-27 | 1977-03-29 | Stark Martin H | Propeller shaft liner and inserting apparatus |
| SU631621A1 (ru) * | 1976-05-14 | 1978-11-05 | Воронежский инженерно-строительный институт | Строительный элемент |
| 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 |
| US4238540A (en) | 1979-05-29 | 1980-12-09 | Celanese Corporation | Fiber reinforced composite shaft with metallic connector sleeves mounted by connector ring interlock |
| AT383319B (de) * | 1982-09-07 | 1987-06-25 | Fischer Gmbh | Rohrfoermiger hohlkoerper aus faserverstaerktem kunststoff, insbesondere strukturbauteil fuer ein fahrzeug, zur uebertragung von druck-,zug-,biege- und torsionskraeften |
| 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 |
| JPS61261035A (ja) | 1985-05-14 | 1986-11-19 | Sumitomo Electric Ind Ltd | 繊維強化プラスチツクス製サンドイツチ円筒体の製造方法 |
| 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 |
| JP3792515B2 (ja) | 1998-10-19 | 2006-07-05 | 美津濃株式会社 | 野球用またはソフトボール用バット |
| US6711783B2 (en) * | 1998-11-12 | 2004-03-30 | Lemole John M. | Anti-pinch knuckle for bidirectional sleeve |
| US6510961B1 (en) | 1999-04-14 | 2003-01-28 | A&P Technology | Integrally-reinforced braided tubular structure and method of producing the same |
| US20020006523A1 (en) * | 2000-07-07 | 2002-01-17 | Obeshaw Dale Francis | Structural members containing vibration damping mechanisms and methods for making the same |
| KR100427223B1 (ko) | 2001-01-18 | 2004-04-27 | 임홍섭 | 포울 및 그 제조 방법 |
| US20030060295A1 (en) | 2001-09-27 | 2003-03-27 | Myers Christopher Alan | Shaft assembly providing a surface for forming joints |
| US7527222B2 (en) | 2004-04-06 | 2009-05-05 | The Boeing Company | Composite barrel sections for aircraft fuselages and other structures, and methods and systems for manufacturing such barrel sections |
| KR100683943B1 (ko) * | 2004-10-29 | 2007-02-15 | 비젼이노텍(주) | 복합재료를 이용한 정밀가공용 공구 |
| 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 |
| JP4965347B2 (ja) | 2007-06-18 | 2012-07-04 | 大成プラス株式会社 | 管状複合体とその製造方法 |
| US8123996B2 (en) | 2008-02-07 | 2012-02-28 | The Boeing Company | Wrinkle control for composite tubes |
| FR2930611B3 (fr) * | 2008-04-23 | 2010-09-10 | Conseil Et Tech | Bielle realisee en materiau composite, et procede de realisation d'une bielle en materiau composite |
| US20100266790A1 (en) | 2009-04-16 | 2010-10-21 | Grzegorz Jan Kusinski | Structural Components for Oil, Gas, Exploration, Refining and Petrochemical Applications |
| FR2957843B1 (fr) | 2010-03-25 | 2014-05-16 | Epsilon Composite | Procede de realisation d'une piece de liaison en materiau composite et piece obtenue |
| US9180960B2 (en) | 2011-06-10 | 2015-11-10 | The Boeing Company | Boron fiber reinforced structural components |
-
2011
- 2011-12-14 US US13/326,005 patent/US9486965B2/en active Active
-
2012
- 2012-10-25 CA CA2851824A patent/CA2851824C/en active Active
- 2012-10-25 WO PCT/US2012/061997 patent/WO2013066727A1/en not_active Ceased
- 2012-10-25 RU RU2014128475A patent/RU2615705C2/ru active
- 2012-10-25 EP EP12795902.1A patent/EP2790898B1/en active Active
- 2012-10-25 ES ES12795902.1T patent/ES2665010T3/es active Active
- 2012-10-25 CN CN201280053017.2A patent/CN104023954B9/zh active Active
- 2012-10-25 JP JP2014539996A patent/JP6089041B2/ja active Active
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