ATE438561T1 - Integrierte flügelspitzenverlängerungen und verfahren zum vergrössern der flügeloberfläche eines flugzeuggrundmodells - Google Patents
Integrierte flügelspitzenverlängerungen und verfahren zum vergrössern der flügeloberfläche eines flugzeuggrundmodellsInfo
- Publication number
- ATE438561T1 ATE438561T1 AT06773970T AT06773970T ATE438561T1 AT E438561 T1 ATE438561 T1 AT E438561T1 AT 06773970 T AT06773970 T AT 06773970T AT 06773970 T AT06773970 T AT 06773970T AT E438561 T1 ATE438561 T1 AT E438561T1
- Authority
- AT
- Austria
- Prior art keywords
- wing
- increase
- surface area
- end portion
- integrated
- Prior art date
Links
- 239000002131 composite material Substances 0.000 abstract 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C23/00—Influencing air flow over aircraft surfaces, not otherwise provided for
- B64C23/06—Influencing air flow over aircraft surfaces, not otherwise provided for by generating vortices
- B64C23/065—Influencing air flow over aircraft surfaces, not otherwise provided for by generating vortices at the wing tips
- B64C23/069—Influencing air flow over aircraft surfaces, not otherwise provided for by generating vortices at the wing tips using one or more wing tip airfoil devices, e.g. winglets, splines, wing tip fences or raked wingtips
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/10—Drag reduction
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Toys (AREA)
- Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Looms (AREA)
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US11/187,443 US8544800B2 (en) | 2005-07-21 | 2005-07-21 | Integrated wingtip extensions for jet transport aircraft and other types of aircraft |
| PCT/US2006/024739 WO2007018785A1 (en) | 2005-07-21 | 2006-06-26 | Integrated wingtip extensions for jet transport aircraft and other types of aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| ATE438561T1 true ATE438561T1 (de) | 2009-08-15 |
Family
ID=37069684
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| AT06773970T ATE438561T1 (de) | 2005-07-21 | 2006-06-26 | Integrierte flügelspitzenverlängerungen und verfahren zum vergrössern der flügeloberfläche eines flugzeuggrundmodells |
Country Status (8)
| Country | Link |
|---|---|
| US (1) | US8544800B2 (de) |
| EP (1) | EP1934090B1 (de) |
| JP (1) | JP5230413B2 (de) |
| CN (2) | CN103661930B (de) |
| AT (1) | ATE438561T1 (de) |
| CA (1) | CA2613680C (de) |
| DE (1) | DE602006008332D1 (de) |
| WO (1) | WO2007018785A1 (de) |
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| JP2000006893A (ja) * | 1998-06-23 | 2000-01-11 | Fuji Heavy Ind Ltd | 複合材翼構造 |
| US5975464A (en) * | 1998-09-22 | 1999-11-02 | Scaled Composites, Inc. | Aircraft with removable structural payload module |
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| US6484968B2 (en) * | 2000-12-11 | 2002-11-26 | Fort F. Felker | Aircraft with elliptical winglets |
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| US6578798B1 (en) * | 2002-04-08 | 2003-06-17 | Faruk Dizdarevic | Airlifting surface division |
| US6547181B1 (en) * | 2002-05-29 | 2003-04-15 | The Boeing Company | Ground effect wing having a variable sweep winglet |
| US6726149B2 (en) * | 2002-05-31 | 2004-04-27 | The Boeing Company | Derivative aircraft and methods for their manufacture |
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| FR2841532B1 (fr) * | 2002-06-27 | 2004-12-17 | Airbus France | Avion a controle actif du vrillage de ses ailes |
| US7048228B2 (en) * | 2002-10-09 | 2006-05-23 | The Boeing Company | Slotted aircraft wing |
| US6886778B2 (en) * | 2003-06-30 | 2005-05-03 | The Boeing Company | Efficient wing tip devices and methods for incorporating such devices into existing wing designs |
| GB0326228D0 (en) * | 2003-11-10 | 2003-12-17 | Airbus Uk Ltd | Wing tip device |
| US7246998B2 (en) * | 2004-11-18 | 2007-07-24 | Sikorsky Aircraft Corporation | Mission replaceable rotor blade tip section |
| CN201296357Y (zh) * | 2008-09-09 | 2009-08-26 | 中国船舶重工集团公司第七○二研究所 | 一种地效翼船船体 |
| US20110127383A1 (en) * | 2009-12-01 | 2011-06-02 | Guida Associates Consulting, Inc. | Active winglet |
-
2005
- 2005-07-21 US US11/187,443 patent/US8544800B2/en not_active Expired - Fee Related
-
2006
- 2006-06-26 CA CA2613680A patent/CA2613680C/en active Active
- 2006-06-26 CN CN201310712766.8A patent/CN103661930B/zh active Active
- 2006-06-26 WO PCT/US2006/024739 patent/WO2007018785A1/en not_active Ceased
- 2006-06-26 JP JP2008522792A patent/JP5230413B2/ja not_active Expired - Fee Related
- 2006-06-26 AT AT06773970T patent/ATE438561T1/de not_active IP Right Cessation
- 2006-06-26 EP EP06773970A patent/EP1934090B1/de not_active Not-in-force
- 2006-06-26 DE DE602006008332T patent/DE602006008332D1/de active Active
- 2006-06-26 CN CNA2006800266282A patent/CN101228067A/zh active Pending
Also Published As
| Publication number | Publication date |
|---|---|
| US8544800B2 (en) | 2013-10-01 |
| CN101228067A (zh) | 2008-07-23 |
| CN103661930A (zh) | 2014-03-26 |
| JP2009501678A (ja) | 2009-01-22 |
| JP5230413B2 (ja) | 2013-07-10 |
| CA2613680C (en) | 2010-11-02 |
| EP1934090A1 (de) | 2008-06-25 |
| US20070018049A1 (en) | 2007-01-25 |
| EP1934090B1 (de) | 2009-08-05 |
| CA2613680A1 (en) | 2007-02-15 |
| CN103661930B (zh) | 2018-01-02 |
| DE602006008332D1 (de) | 2009-09-17 |
| WO2007018785A1 (en) | 2007-02-15 |
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| Date | Code | Title | Description |
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| RER | Ceased as to paragraph 5 lit. 3 law introducing patent treaties |