JP2010523397A5 - - Google Patents
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- Publication number
- JP2010523397A5 JP2010523397A5 JP2010502225A JP2010502225A JP2010523397A5 JP 2010523397 A5 JP2010523397 A5 JP 2010523397A5 JP 2010502225 A JP2010502225 A JP 2010502225A JP 2010502225 A JP2010502225 A JP 2010502225A JP 2010523397 A5 JP2010523397 A5 JP 2010523397A5
- Authority
- JP
- Japan
- Prior art keywords
- web
- flange
- flange plate
- sheets
- skin
- 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
- 239000002131 composite material Substances 0.000 claims 6
- 238000004519 manufacturing process Methods 0.000 claims 1
- 230000002093 peripheral effect Effects 0.000 claims 1
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US11/697,162 US8490362B2 (en) | 2007-04-05 | 2007-04-05 | Methods and systems for composite structural truss |
| US11/697,162 | 2007-04-05 | ||
| PCT/US2008/058799 WO2008124352A1 (en) | 2007-04-05 | 2008-03-29 | Methods and systems for composite structural truss |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| JP2010523397A JP2010523397A (ja) | 2010-07-15 |
| JP2010523397A5 true JP2010523397A5 (cg-RX-API-DMAC7.html) | 2011-05-06 |
| JP5475639B2 JP5475639B2 (ja) | 2014-04-16 |
Family
ID=39688780
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP2010502225A Expired - Fee Related JP5475639B2 (ja) | 2007-04-05 | 2008-03-29 | 複合トラス構造のための方法とシステム |
Country Status (6)
| Country | Link |
|---|---|
| US (2) | US8490362B2 (cg-RX-API-DMAC7.html) |
| EP (1) | EP2139761B1 (cg-RX-API-DMAC7.html) |
| JP (1) | JP5475639B2 (cg-RX-API-DMAC7.html) |
| CN (1) | CN102317154B (cg-RX-API-DMAC7.html) |
| ES (1) | ES2622680T3 (cg-RX-API-DMAC7.html) |
| WO (1) | WO2008124352A1 (cg-RX-API-DMAC7.html) |
Families Citing this family (21)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US9903848B2 (en) * | 2008-12-30 | 2018-02-27 | Sikorsky Aircraft Corporation | Non-destructive inspection method with objective evaluation |
| EP2330294B1 (en) * | 2009-12-02 | 2013-01-16 | Bladena ApS | Reinforced airfoil shaped body |
| DE102010043850A1 (de) * | 2010-11-12 | 2012-05-16 | Airbus Operations Gmbh | Strukturelement für ein Luft- und/oder Raumfahrzeug und Verfahren zum Herstellen eines derartigen Strukturelementes |
| US10907609B2 (en) * | 2014-07-15 | 2021-02-02 | Ge Renewable Technologies | Apparatus and method for modifying a geometry of a turbine part |
| CA2857297C (en) * | 2014-07-21 | 2021-08-17 | Alstom Renewable Technologies | Apparatus and method for modifying a geometry of a turbine part |
| US9610728B2 (en) | 2014-07-18 | 2017-04-04 | The Boeing Company | Apparatus and methods for bonding laminate structures |
| CN104554704B (zh) * | 2015-01-27 | 2016-09-28 | 新誉集团有限公司 | 可横向组装的大展弦比机翼结构及其组装方法 |
| ES2705124T3 (es) * | 2015-09-29 | 2019-03-21 | Airbus Operations Sl | Costilla de composite para una caja de torsión de aeronave y procedimiento de fabricación de la misma |
| EP3231702B1 (en) | 2016-04-11 | 2020-06-17 | Asco Industries NV | High-lift device |
| US10286998B2 (en) * | 2016-05-05 | 2019-05-14 | The Boeing Company | Mechanical fastening system and associated structural assembly and method |
| EP3498591A1 (en) * | 2017-12-13 | 2019-06-19 | AIRBUS HELICOPTERS DEUTSCHLAND GmbH | A composite truss beam with a sandwich web |
| ES2889577T3 (es) * | 2018-07-06 | 2022-01-12 | Airbus Operations Sl | Método para fabricar las costillas del borde de salida y las costillas de soporte de los bordes de salida de superficies de elevación de aeronaves |
| CN111056047B (zh) * | 2018-10-17 | 2021-07-30 | 哈尔滨工业大学 | 基于形状记忆聚合物复合材料的桁架式可收展太空舱 |
| US11046420B2 (en) * | 2019-10-23 | 2021-06-29 | The Boeing Company | Trailing edge flap having a waffle grid interior structure |
| US20210316343A1 (en) * | 2020-04-09 | 2021-10-14 | Imperial Systems, Inc. | Fume Hood Having Structurally Integrated Components |
| CN113733595B (zh) * | 2021-08-30 | 2022-06-14 | 北京航空航天大学 | 一种全包裹式复合材料泡沫夹芯翼肋加工方法 |
| US12157572B2 (en) * | 2021-08-31 | 2024-12-03 | The Boeing Company | Method of making a control surface |
| US11987353B2 (en) | 2022-04-19 | 2024-05-21 | The Boeing Company | Thermoplastic skin panels, torque box and method |
| US20240066762A1 (en) * | 2022-08-29 | 2024-02-29 | The Boeing Company | Curing Composites Out-Of-Autoclave Using Induction Heating with Smart Susceptors |
| US12286221B2 (en) * | 2022-10-04 | 2025-04-29 | The Boeing Company | Tubular wing structures and methods of manufacture |
| US12431835B1 (en) * | 2023-03-28 | 2025-09-30 | Fushun Ma | Aerodynamic solar cell system |
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| US1343707A (en) * | 1918-11-25 | 1920-06-15 | Edmund B Carns | Aircraft |
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| US1571239A (en) * | 1923-02-17 | 1926-02-02 | Firm Dornier Metallbauten Gmbh | Metal girder for light metal structures |
| US1840643A (en) * | 1925-07-11 | 1932-01-12 | Ford Motor Co | Airplane |
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| US2392818A (en) * | 1940-11-18 | 1946-01-15 | Lockheed Aircraft Corp | Double skin sheet metal structural element |
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| US2389917A (en) * | 1941-10-16 | 1945-11-27 | Frederic A Leisen | Aircraft structure |
| US2386019A (en) * | 1943-01-28 | 1945-10-02 | Budd Edward G Mfg Co | Truss structure and parts thereof |
| US2514607A (en) * | 1946-02-07 | 1950-07-11 | Dravo Corp | Truss construction |
| US2589193A (en) * | 1946-11-29 | 1952-03-11 | Goodyear Aircraft Corp | Airfoil, and particularly helicopter blade |
| US3901465A (en) * | 1974-03-05 | 1975-08-26 | Lawrence J Deangelis | Variable-area variable incidence wing and aircraft incorporating same |
| GB1534697A (en) * | 1975-03-27 | 1978-12-06 | Heath Charles William | Model aircraft wing construction jig |
| US4002116A (en) * | 1975-05-09 | 1977-01-11 | Jack N. Schmitt | Apparatus for forming trusses |
| US4051289A (en) * | 1976-04-12 | 1977-09-27 | General Electric Company | Composite airfoil construction |
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| US4223053A (en) * | 1978-08-07 | 1980-09-16 | The Boeing Company | Truss core panels |
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| US4452657A (en) * | 1982-09-15 | 1984-06-05 | The Boeing Company | Composite integral web stiffening method |
| 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 |
| US4887406A (en) * | 1987-12-31 | 1989-12-19 | Saia Wilburn H F | Structural member for buildings |
| JPH0823095B2 (ja) * | 1989-06-06 | 1996-03-06 | 東レ株式会社 | 補強繊維織物 |
| JPH03123798U (cg-RX-API-DMAC7.html) * | 1990-03-30 | 1991-12-16 | ||
| US5332178A (en) * | 1992-06-05 | 1994-07-26 | Williams International Corporation | Composite wing and manufacturing process thereof |
| GB9215827D0 (en) * | 1992-07-24 | 1992-09-09 | British Aerospace | A lightning shield |
| CA2077429C (en) * | 1992-09-02 | 1999-03-30 | Ernest R. Bodnar | Roll formed metal member |
| US5375324A (en) * | 1993-07-12 | 1994-12-27 | Flowind Corporation | Vertical axis wind turbine with pultruded blades |
| US5632940A (en) * | 1994-03-29 | 1997-05-27 | Whatley; Bradford L. | Method of making an integrally stiffened article |
| RU2116934C1 (ru) * | 1997-05-06 | 1998-08-10 | Акционерное общество "Центр перспективных разработок акционерного общества "Центральный научно-исследовательский институт специального машиностроения" | Нервюра из композиционных материалов (варианты) и устройство для изготовления ее плоской реберно-ячеистой структуры |
| JP2000006893A (ja) * | 1998-06-23 | 2000-01-11 | Fuji Heavy Ind Ltd | 複合材翼構造 |
| DE19922295C1 (de) * | 1999-05-14 | 2000-07-27 | Eurocopter Deutschland | Unterbodenstruktur einer Rumpfzelle eines Luftfahrzeuges |
| US6513757B1 (en) * | 1999-07-19 | 2003-02-04 | Fuji Jukogyo Kabushiki Kaisha | Wing of composite material and method of fabricating the same |
| JP4316059B2 (ja) * | 1999-08-06 | 2009-08-19 | 富士重工業株式会社 | 複合材翼の製造方法 |
| US6889937B2 (en) * | 1999-11-18 | 2005-05-10 | Rocky Mountain Composites, Inc. | Single piece co-cure composite wing |
| US6655633B1 (en) * | 2000-01-21 | 2003-12-02 | W. Cullen Chapman, Jr. | Tubular members integrated to form a structure |
| JP4416900B2 (ja) * | 2000-03-10 | 2010-02-17 | 富士重工業株式会社 | 複合材パネルおよびその製造方法 |
| FR2817608B1 (fr) * | 2000-12-04 | 2004-11-05 | Eads Airbus Sa | Poutre composite a initiateur de rupture integre et fuselage d'aeronef integrant de telles poutres |
| US6638466B1 (en) * | 2000-12-28 | 2003-10-28 | Raytheon Aircraft Company | Methods of manufacturing separable structures |
| JP4545339B2 (ja) * | 2001-04-05 | 2010-09-15 | 富士重工業株式会社 | 複合材翼およびその製造方法 |
| US6945727B2 (en) * | 2002-07-19 | 2005-09-20 | The Boeing Company | Apparatuses and methods for joining structural members, such as composite structural members |
| CA2404320C (en) * | 2002-09-30 | 2005-02-08 | Ernest R. Bodnar | Steel stud with openings and edge formations and method |
| US20040191441A1 (en) * | 2003-01-30 | 2004-09-30 | Martin Bureau | Laminated polymer composite material |
| US7587877B2 (en) * | 2003-10-28 | 2009-09-15 | Best Joist Inc | Cold-formed steel joists |
| US20060032702A1 (en) * | 2004-07-29 | 2006-02-16 | Oshkosh Truck Corporation | Composite boom assembly |
| GB0426944D0 (en) * | 2004-12-08 | 2005-01-12 | Airbus Uk Ltd | A trussed structure |
| US7387277B2 (en) * | 2004-12-29 | 2008-06-17 | The Boeing Company | Aircraft wing composed of composite and metal panels |
| FI118761B (fi) * | 2006-02-09 | 2008-03-14 | Patria Aerostructures Oy | Ilma-aluksen siipi, kiinnitysjärjestely sekä välituki |
| JP4657189B2 (ja) * | 2006-11-02 | 2011-03-23 | 本田技研工業株式会社 | 飛行機の翼構造 |
| US7575194B2 (en) * | 2006-11-30 | 2009-08-18 | The Boeing Company | Apparatuses and methods for joining composite members and other structural members in aircraft wing boxes and other structures |
-
2007
- 2007-04-05 US US11/697,162 patent/US8490362B2/en not_active Expired - Fee Related
-
2008
- 2008-03-29 CN CN200880014861.8A patent/CN102317154B/zh not_active Expired - Fee Related
- 2008-03-29 ES ES08744703.3T patent/ES2622680T3/es active Active
- 2008-03-29 EP EP08744703.3A patent/EP2139761B1/en not_active Not-in-force
- 2008-03-29 JP JP2010502225A patent/JP5475639B2/ja not_active Expired - Fee Related
- 2008-03-29 WO PCT/US2008/058799 patent/WO2008124352A1/en not_active Ceased
-
2013
- 2013-06-20 US US13/922,654 patent/US8677717B2/en active Active
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