CA2613680C - Integrated wingtip extensions for jet transport aircraft and other types of aircraft - Google Patents
Integrated wingtip extensions for jet transport aircraft and other types of aircraft Download PDFInfo
- Publication number
- CA2613680C CA2613680C CA2613680A CA2613680A CA2613680C CA 2613680 C CA2613680 C CA 2613680C CA 2613680 A CA2613680 A CA 2613680A CA 2613680 A CA2613680 A CA 2613680A CA 2613680 C CA2613680 C CA 2613680C
- Authority
- CA
- Canada
- Prior art keywords
- wing
- tapered
- baseline
- aircraft
- control surface
- 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.)
- Active
Links
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 (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US11/187,443 | 2005-07-21 | ||
| 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 (2)
| Publication Number | Publication Date |
|---|---|
| CA2613680A1 CA2613680A1 (en) | 2007-02-15 |
| CA2613680C true CA2613680C (en) | 2010-11-02 |
Family
ID=37069684
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CA2613680A Active CA2613680C (en) | 2005-07-21 | 2006-06-26 | Integrated wingtip extensions for jet transport aircraft and other types of aircraft |
Country Status (8)
| Country | Link |
|---|---|
| US (1) | US8544800B2 (enExample) |
| EP (1) | EP1934090B1 (enExample) |
| JP (1) | JP5230413B2 (enExample) |
| CN (2) | CN101228067A (enExample) |
| AT (1) | ATE438561T1 (enExample) |
| CA (1) | CA2613680C (enExample) |
| DE (1) | DE602006008332D1 (enExample) |
| WO (1) | WO2007018785A1 (enExample) |
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| 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 |
| US20040135032A1 (en) * | 2002-06-20 | 2004-07-15 | Gregg Robert D | Spanwise tailoring of a trailing edge wedge to a wing |
| 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 EP EP06773970A patent/EP1934090B1/en active Active
- 2006-06-26 CN CNA2006800266282A patent/CN101228067A/zh active Pending
- 2006-06-26 AT AT06773970T patent/ATE438561T1/de not_active IP Right Cessation
- 2006-06-26 CA CA2613680A patent/CA2613680C/en active Active
- 2006-06-26 DE DE602006008332T patent/DE602006008332D1/de active Active
- 2006-06-26 WO PCT/US2006/024739 patent/WO2007018785A1/en not_active Ceased
- 2006-06-26 CN CN201310712766.8A patent/CN103661930B/zh active Active
- 2006-06-26 JP JP2008522792A patent/JP5230413B2/ja not_active Expired - Fee Related
Also Published As
| Publication number | Publication date |
|---|---|
| CN103661930B (zh) | 2018-01-02 |
| WO2007018785A1 (en) | 2007-02-15 |
| CN101228067A (zh) | 2008-07-23 |
| JP2009501678A (ja) | 2009-01-22 |
| US20070018049A1 (en) | 2007-01-25 |
| US8544800B2 (en) | 2013-10-01 |
| JP5230413B2 (ja) | 2013-07-10 |
| EP1934090A1 (en) | 2008-06-25 |
| ATE438561T1 (de) | 2009-08-15 |
| DE602006008332D1 (de) | 2009-09-17 |
| CN103661930A (zh) | 2014-03-26 |
| CA2613680A1 (en) | 2007-02-15 |
| EP1934090B1 (en) | 2009-08-05 |
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| EEER | Examination request |