JP2010512268A5 - - Google Patents
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- Publication number
- JP2010512268A5 JP2010512268A5 JP2009540494A JP2009540494A JP2010512268A5 JP 2010512268 A5 JP2010512268 A5 JP 2010512268A5 JP 2009540494 A JP2009540494 A JP 2009540494A JP 2009540494 A JP2009540494 A JP 2009540494A JP 2010512268 A5 JP2010512268 A5 JP 2010512268A5
- Authority
- JP
- Japan
- Prior art keywords
- metal part
- composite material
- hybrid composite
- metal component
- composite
- 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
Links
- 229910052751 metal Inorganic materials 0.000 claims 37
- 239000002184 metal Substances 0.000 claims 37
- 239000002131 composite material Substances 0.000 claims 23
- 238000000034 method Methods 0.000 claims 4
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 claims 2
- 239000011347 resin Substances 0.000 claims 2
- 229920005989 resin Polymers 0.000 claims 2
- 239000010936 titanium Substances 0.000 claims 2
- 229910052719 titanium Inorganic materials 0.000 claims 2
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims 1
- 238000000151 deposition Methods 0.000 claims 1
- 229910002804 graphite Inorganic materials 0.000 claims 1
- 239000010439 graphite Substances 0.000 claims 1
- 238000010438 heat treatment Methods 0.000 claims 1
- 230000001678 irradiating effect Effects 0.000 claims 1
- 230000005855 radiation Effects 0.000 claims 1
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US11/608,534 US20080283667A1 (en) | 2006-12-08 | 2006-12-08 | Hybrid composite-metal aircraft landing gear and engine support beams |
| PCT/US2007/086744 WO2008118229A2 (en) | 2006-12-08 | 2007-12-07 | Hybrid composite-metal aircraft landing gear and engine support beams |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JP2010512268A JP2010512268A (ja) | 2010-04-22 |
| JP2010512268A5 true JP2010512268A5 (https=) | 2011-02-03 |
Family
ID=39789166
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP2009540494A Pending JP2010512268A (ja) | 2006-12-08 | 2007-12-07 | 航空機のハイブリッド複合金属ランディングギア及びエンジンサポートビーム |
Country Status (6)
| Country | Link |
|---|---|
| US (1) | US20080283667A1 (https=) |
| EP (1) | EP2097255A2 (https=) |
| JP (1) | JP2010512268A (https=) |
| CN (1) | CN101583487A (https=) |
| CA (1) | CA2666595A1 (https=) |
| WO (1) | WO2008118229A2 (https=) |
Families Citing this family (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2473007B (en) | 2009-08-26 | 2012-11-21 | Messier Dowty Ltd | Apparatus comprising an end fitting connected to a body |
| JP5514527B2 (ja) * | 2009-12-11 | 2014-06-04 | ナブテスコ株式会社 | 航空機用リアクションリンク |
| EP2913267B1 (en) * | 2014-02-27 | 2019-10-30 | Airbus Operations S.L. | Aircraft with a nacelle-housed main landing gear |
| US12060473B2 (en) | 2018-07-03 | 2024-08-13 | University Of Notre Dame Du Lac | Polymer/exfoliated nano-composite films with superior mechanical properties |
| EP3611390B1 (en) | 2018-08-16 | 2020-12-23 | Crompton Technology Group Limited | Composite structure having a tapered joint and a method for making the same |
| EP3792173B1 (en) | 2019-09-16 | 2022-04-27 | SKF Aerospace France | Fail-safe system intended for use in an aircraft |
Family Cites Families (17)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2584832A (en) * | 1945-04-07 | 1952-02-05 | Bendix Aviat Corp | Method of making a trunnion for aircraft landing gear |
| US3416975A (en) * | 1965-05-04 | 1968-12-17 | Nasa | Etching of aluminum for bonding |
| US3623203A (en) * | 1970-03-24 | 1971-11-30 | Avco Corp | Reinforced structural members and method of making same |
| US4185472A (en) * | 1978-03-27 | 1980-01-29 | Celanese Corporation | Fiber reinforced composite shaft with metallic connector sleeves mounted by radial pin interlock |
| CA1107769A (en) * | 1978-05-10 | 1981-08-25 | Henry E. Wilson | Composite fibrous tube energy absorber |
| US4300439A (en) * | 1979-09-10 | 1981-11-17 | United Technologies Corporation | Ballistic tolerant hydraulic control actuator and method of fabricating same |
| DE3017336A1 (de) * | 1980-05-06 | 1981-11-12 | Paul Dr. 1000 Berlin Mader | Auf biegung beanspruchter rohrfoermiger koerper |
| DE3103646C2 (de) * | 1981-02-04 | 1984-03-29 | Aluminium-Walzwerke Singen Gmbh, 7700 Singen | Druckbehälter zur Lagerung sowie zum Transport gasförmiger Strömungsmittel |
| US4581077A (en) * | 1984-04-27 | 1986-04-08 | Nippon Mining Co., Ltd. | Method of manufacturing rolled titanium alloy sheets |
| US4923751A (en) * | 1986-10-21 | 1990-05-08 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Seamless metal-clad fiber-reinforced organic matrix composite structures, and process for their manufacture |
| FR2675563B1 (fr) * | 1991-04-22 | 1993-08-27 | Aerospatiale | Procede d'assemblage mecanique d'un tube en materiau composite et d'une piece metallique et assemblage ainsi realise. |
| US5332049A (en) * | 1992-09-29 | 1994-07-26 | Brunswick Corporation | Composite drill pipe |
| JPH0960676A (ja) * | 1995-08-25 | 1997-03-04 | Yokohama Rubber Co Ltd:The | 衝撃緩和材及びその製造方法 |
| US6893733B2 (en) * | 2000-07-07 | 2005-05-17 | Delphi Technologies, Inc. | Modified contoured crushable structural members and methods for making the same |
| US6830223B1 (en) * | 2000-11-16 | 2004-12-14 | Tyee Aircraft | Force sensor rod |
| US6582172B2 (en) * | 2001-08-29 | 2003-06-24 | The United States Of America As Represented By The Secretary Of The Navy | Isolated mechanical fastening system |
| DE102004008523B4 (de) * | 2004-02-20 | 2007-02-01 | Liebherr-Aerospace Lindenberg Gmbh | Verfahren zur Herstellung eines Druckzylinders und Kolbenstange für Aktuatoren oder Stoßdämpfer und Verfahren zu deren Herstellung |
-
2006
- 2006-12-08 US US11/608,534 patent/US20080283667A1/en not_active Abandoned
-
2007
- 2007-12-07 WO PCT/US2007/086744 patent/WO2008118229A2/en not_active Ceased
- 2007-12-07 CA CA002666595A patent/CA2666595A1/en not_active Abandoned
- 2007-12-07 CN CNA2007800417978A patent/CN101583487A/zh active Pending
- 2007-12-07 JP JP2009540494A patent/JP2010512268A/ja active Pending
- 2007-12-07 EP EP07873665A patent/EP2097255A2/en not_active Withdrawn
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