JP2012166506A5 - - Google Patents
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- Publication number
- JP2012166506A5 JP2012166506A5 JP2011030883A JP2011030883A JP2012166506A5 JP 2012166506 A5 JP2012166506 A5 JP 2012166506A5 JP 2011030883 A JP2011030883 A JP 2011030883A JP 2011030883 A JP2011030883 A JP 2011030883A JP 2012166506 A5 JP2012166506 A5 JP 2012166506A5
- Authority
- JP
- Japan
- Prior art keywords
- bolt
- spar
- jumper
- protrusions
- conductive layer
- 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
- 238000010586 diagram Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 230000000873 masking effect Effects 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
Priority Applications (8)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP2011030883A JP5773679B2 (ja) | 2011-02-16 | 2011-02-16 | 炭素繊維強化プラスチック構造体及びその製造方法 |
| RU2013137704/05A RU2540649C1 (ru) | 2011-02-16 | 2012-02-15 | Конструкция из пластика, армированного углеволокном, и способ изготовления такой конструкции |
| BR112013020146A BR112013020146B1 (pt) | 2011-02-16 | 2012-02-15 | estrutura de plástico reforçada com fibra de carbono e métodos para produção da mesma |
| CN201280008083.8A CN103347690B (zh) | 2011-02-16 | 2012-02-15 | 碳纤维强化塑料结构体及其制造方法 |
| EP12747044.1A EP2676792B1 (en) | 2011-02-16 | 2012-02-15 | Carbon-fiber-reinforced plastic structure and method for producing same |
| US13/985,363 US10080286B2 (en) | 2011-02-16 | 2012-02-15 | Carbon-fiber-reinforced plastic structure and method for producing same |
| PCT/JP2012/053522 WO2012111704A1 (ja) | 2011-02-16 | 2012-02-15 | 炭素繊維強化プラスチック構造体及びその製造方法 |
| CA2827396A CA2827396C (en) | 2011-02-16 | 2012-02-15 | Carbon-fiber-reinforced plastic structure and method for producing same |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP2011030883A JP5773679B2 (ja) | 2011-02-16 | 2011-02-16 | 炭素繊維強化プラスチック構造体及びその製造方法 |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| JP2012166506A JP2012166506A (ja) | 2012-09-06 |
| JP2012166506A5 true JP2012166506A5 (enExample) | 2013-10-24 |
| JP5773679B2 JP5773679B2 (ja) | 2015-09-02 |
Family
ID=46672617
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP2011030883A Expired - Fee Related JP5773679B2 (ja) | 2011-02-16 | 2011-02-16 | 炭素繊維強化プラスチック構造体及びその製造方法 |
Country Status (8)
| Country | Link |
|---|---|
| US (1) | US10080286B2 (enExample) |
| EP (1) | EP2676792B1 (enExample) |
| JP (1) | JP5773679B2 (enExample) |
| CN (1) | CN103347690B (enExample) |
| BR (1) | BR112013020146B1 (enExample) |
| CA (1) | CA2827396C (enExample) |
| RU (1) | RU2540649C1 (enExample) |
| WO (1) | WO2012111704A1 (enExample) |
Families Citing this family (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP5751871B2 (ja) * | 2011-03-10 | 2015-07-22 | 三菱重工業株式会社 | 燃料タンク |
| WO2013146335A1 (ja) | 2012-03-26 | 2013-10-03 | 三菱重工業株式会社 | 燃料タンク、主翼、航空機胴体、航空機及び移動体 |
| US9776732B2 (en) * | 2012-10-09 | 2017-10-03 | Mitsubishi Heavy Industries, Ltd. | Structural material for structure, fuel tank, main wing, and aircraft |
| JP6093192B2 (ja) * | 2013-01-25 | 2017-03-08 | 三菱航空機株式会社 | 航空機の機体用パネル、航空機の翼 |
| JP6071686B2 (ja) * | 2013-03-26 | 2017-02-01 | 三菱重工業株式会社 | 燃料タンク、主翼、航空機胴体、航空機及び移動体 |
| DE102015213271A1 (de) * | 2015-07-15 | 2017-01-19 | Siemens Aktiengesellschaft | Flugzeug mit einer Tragstruktur zur Übertragung elektrischer Energie zwischen einer Energiequelle und einem Energieverbraucher |
| CN119497357A (zh) * | 2023-08-14 | 2025-02-21 | 华为技术有限公司 | 一种结构件及电子设备 |
Family Cites Families (21)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3755713A (en) * | 1972-07-25 | 1973-08-28 | Boeing Co | Electrically conductive surface for aircraft |
| US3989984A (en) * | 1975-07-11 | 1976-11-02 | Mcdonnell Douglas Corporation | Aircraft lightning protection means |
| JPH0263725A (ja) * | 1988-05-27 | 1990-03-05 | Mitsubishi Heavy Ind Ltd | 炭素繊維強化プラスチツク部材の組立方法 |
| RU2041508C1 (ru) * | 1992-11-05 | 1995-08-09 | Московский авиационный технологический институт им.К.Э.Циолковского | Слоистый полимерный материал |
| US5866272A (en) | 1996-01-11 | 1999-02-02 | The Boeing Company | Titanium-polymer hybrid laminates |
| US6327132B1 (en) * | 1998-06-10 | 2001-12-04 | Aerospatiale Matra | Spark resistant structure, in particular for aircraft |
| JP4119205B2 (ja) * | 2002-08-27 | 2008-07-16 | 富士通株式会社 | 多層配線基板 |
| US8231751B2 (en) * | 2005-09-06 | 2012-07-31 | The Boeing Company | Repair technique for lightning strike protection |
| US7686905B2 (en) * | 2005-09-06 | 2010-03-30 | The Boeing Company | Copper grid repair technique for lightning strike protection |
| JP4908884B2 (ja) * | 2006-03-15 | 2012-04-04 | 三菱重工業株式会社 | 成形体表面の導電化方法及び表面導電性成形体 |
| DE102006031334A1 (de) * | 2006-07-06 | 2008-01-10 | Airbus Deutschland Gmbh | Verfahren zur Herstellung eines Faserverbundbauteils für die Luft- und Raumfahrt |
| US7599164B2 (en) * | 2006-12-07 | 2009-10-06 | The Boeing Company | Lightning protection system for aircraft composite structure |
| US7829796B2 (en) * | 2007-11-06 | 2010-11-09 | The Boeing Company | Circuit joining assembly materials for multi-layer lightning protection systems on composite aircraft |
| JP4719203B2 (ja) * | 2007-09-28 | 2011-07-06 | 三菱重工業株式会社 | 耐雷ファスナ |
| JP5055178B2 (ja) * | 2008-03-24 | 2012-10-24 | 三菱重工業株式会社 | 航空機組立品 |
| WO2010037991A1 (en) * | 2008-10-03 | 2010-04-08 | Short Brothers Plc | Fibre reinforced composite structures and method of manufacture |
| JP2010194749A (ja) * | 2009-02-23 | 2010-09-09 | Mitsubishi Heavy Ind Ltd | 樹脂基複合材の製造方法 |
| JP5769412B2 (ja) | 2010-12-17 | 2015-08-26 | 三菱重工業株式会社 | 構造物製造方法 |
| JP5730057B2 (ja) | 2011-02-16 | 2015-06-03 | 三菱重工業株式会社 | 炭素繊維強化プラスチック構造体 |
| JP5669635B2 (ja) * | 2011-03-14 | 2015-02-12 | 三菱航空機株式会社 | 機体構成部材の連結構造 |
| US9108363B2 (en) * | 2011-10-06 | 2015-08-18 | The Boeing Company | Thin wall bushing for robust electrical bonding to fiber-reinforced structures |
-
2011
- 2011-02-16 JP JP2011030883A patent/JP5773679B2/ja not_active Expired - Fee Related
-
2012
- 2012-02-15 EP EP12747044.1A patent/EP2676792B1/en active Active
- 2012-02-15 RU RU2013137704/05A patent/RU2540649C1/ru active
- 2012-02-15 CN CN201280008083.8A patent/CN103347690B/zh not_active Expired - Fee Related
- 2012-02-15 WO PCT/JP2012/053522 patent/WO2012111704A1/ja not_active Ceased
- 2012-02-15 US US13/985,363 patent/US10080286B2/en active Active
- 2012-02-15 CA CA2827396A patent/CA2827396C/en not_active Expired - Fee Related
- 2012-02-15 BR BR112013020146A patent/BR112013020146B1/pt not_active IP Right Cessation
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