CN102089207B - 具有凹陷表面的小翼和相关系统及方法 - Google Patents
具有凹陷表面的小翼和相关系统及方法 Download PDFInfo
- Publication number
- CN102089207B CN102089207B CN200980109250.6A CN200980109250A CN102089207B CN 102089207 B CN102089207 B CN 102089207B CN 200980109250 A CN200980109250 A CN 200980109250A CN 102089207 B CN102089207 B CN 102089207B
- Authority
- CN
- China
- Prior art keywords
- winglet
- wing
- point
- sunk area
- recessed
- 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.)
- Expired - Fee Related
Links
- 238000000034 method Methods 0.000 title claims abstract description 35
- 210000004744 fore-foot Anatomy 0.000 claims description 2
- 230000008901 benefit Effects 0.000 description 10
- 230000000694 effects Effects 0.000 description 2
- 238000009434 installation Methods 0.000 description 2
- 230000006641 stabilisation Effects 0.000 description 2
- 238000011105 stabilization Methods 0.000 description 2
- 241000272517 Anseriformes Species 0.000 description 1
- 241000220324 Pyrus Species 0.000 description 1
- 238000005452 bending Methods 0.000 description 1
- 230000037396 body weight Effects 0.000 description 1
- 150000001875 compounds Chemical class 0.000 description 1
- 230000006835 compression Effects 0.000 description 1
- 238000007906 compression Methods 0.000 description 1
- 230000001419 dependent effect Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 210000003746 feather Anatomy 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 235000021017 pears Nutrition 0.000 description 1
- 238000009418 renovation Methods 0.000 description 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)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Toys (AREA)
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US12/103,430 US8128035B2 (en) | 2008-04-15 | 2008-04-15 | Winglets with recessed surfaces, and associated systems and methods |
| US12/103,430 | 2008-04-15 | ||
| PCT/US2009/037868 WO2009129023A1 (en) | 2008-04-15 | 2009-03-20 | Winglets with recessed surfaces, and associated systems and methods |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN102089207A CN102089207A (zh) | 2011-06-08 |
| CN102089207B true CN102089207B (zh) | 2016-07-13 |
Family
ID=40887190
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN200980109250.6A Expired - Fee Related CN102089207B (zh) | 2008-04-15 | 2009-03-20 | 具有凹陷表面的小翼和相关系统及方法 |
Country Status (7)
| Country | Link |
|---|---|
| US (1) | US8128035B2 (enExample) |
| EP (1) | EP2276665B1 (enExample) |
| JP (1) | JP5490097B2 (enExample) |
| CN (1) | CN102089207B (enExample) |
| CA (1) | CA2713162C (enExample) |
| RU (1) | RU2492111C2 (enExample) |
| WO (1) | WO2009129023A1 (enExample) |
Families Citing this family (37)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE102006055090A1 (de) * | 2006-11-21 | 2008-05-29 | Airbus Deutschland Gmbh | Flügelendform für einen Flügel, insbesondere von Luftfahrzeugen |
| US7900876B2 (en) * | 2007-08-09 | 2011-03-08 | The Boeing Company | Wingtip feathers, including forward swept feathers, and associated aircraft systems and methods |
| US20090084904A1 (en) * | 2007-10-02 | 2009-04-02 | The Boeing Company | Wingtip Feathers, Including Paired, Fixed Feathers, and Associated Systems and Methods |
| US8128035B2 (en) * | 2008-04-15 | 2012-03-06 | The Boeing Company | Winglets with recessed surfaces, and associated systems and methods |
| US9302766B2 (en) * | 2008-06-20 | 2016-04-05 | Aviation Partners, Inc. | Split blended winglet |
| CA2728765C (en) | 2008-06-20 | 2017-06-13 | Aviation Partners, Inc. | Curved wing tip |
| DE102009019542A1 (de) * | 2009-04-30 | 2010-11-11 | Airbus Deutschland Gmbh | Nicht-planares Flügelendstück für Tragflügel von Flugzeugen sowie Tragflügel mit einem solchen Flügelendstück |
| US9162755B2 (en) | 2009-12-01 | 2015-10-20 | Tamarack Aerospace Group, Inc. | Multiple controllable airflow modification devices |
| US20110127383A1 (en) | 2009-12-01 | 2011-06-02 | Guida Associates Consulting, Inc. | Active winglet |
| GB201011843D0 (en) * | 2010-07-14 | 2010-09-01 | Airbus Operations Ltd | Wing tip device |
| CN106081070A (zh) * | 2011-06-09 | 2016-11-09 | 航空伙伴股份有限公司 | 螺旋形机翼末梢以及飞行器 |
| CN102442422A (zh) * | 2011-11-04 | 2012-05-09 | 哈尔滨飞机工业集团有限责任公司 | 一种提高时间域飞机平尾气动效率的小翼 |
| US8936219B2 (en) | 2012-03-30 | 2015-01-20 | The Boeing Company | Performance-enhancing winglet system and method |
| US9086053B2 (en) | 2012-03-30 | 2015-07-21 | General Electric Company | Enhanced wind turbine blade |
| EP3594115B1 (en) * | 2013-02-05 | 2023-08-23 | Tamarack Aerospace Group, Inc. | Controllable airflow modification device periodic load control |
| US10696387B2 (en) | 2013-09-27 | 2020-06-30 | Dann M Allen | Helicopter rotor with a mechanical means for configuring rotor tips to control brown outs |
| US10562613B2 (en) * | 2013-12-04 | 2020-02-18 | Tamarack Aerospace Group, Inc. | Adjustable lift modification wingtip |
| USD754053S1 (en) * | 2014-02-19 | 2016-04-19 | Aeronautical Testing Service, Inc. | Wing root leading edge extension |
| US9511850B2 (en) * | 2014-04-12 | 2016-12-06 | The Boeing Company | Wing tip device for an aircraft wing |
| GB201512480D0 (en) * | 2015-07-16 | 2015-08-19 | Fourth Dimensional Aerospace Technology Ltd | Fluid flow control for an aerofoil |
| US10690112B2 (en) | 2016-06-27 | 2020-06-23 | William Scott Keeley | Fluid turbine rotor blade with winglet design |
| EP3269635A1 (en) | 2016-07-12 | 2018-01-17 | The Aircraft Performance Company UG | Airplane wing |
| US10202961B2 (en) | 2016-11-30 | 2019-02-12 | William Scott Keeley | Fluid turbine semi-shroud and associated rotor blade dual-winglet design |
| US10293915B2 (en) | 2016-12-13 | 2019-05-21 | The Boeing Company | Apparatuses and methods for aerodynamic window assemblies |
| GB2559969A (en) * | 2017-02-22 | 2018-08-29 | Airbus Operations Ltd | A method of designing a winglet and winglet disigned thereby |
| US11312481B2 (en) | 2017-07-12 | 2022-04-26 | The Aircraft Performance Company Gmbh | Airplane wing |
| ES2819559T3 (es) | 2017-12-15 | 2021-04-16 | The Aircraft Performance Company Gmbh | Ala de aeroplano |
| ES2905192T3 (es) | 2018-01-15 | 2022-04-07 | The Aircraft Performance Company Gmbh | Ala de avión |
| GB2573281B (en) * | 2018-04-25 | 2020-12-30 | Airbus Operations Ltd | An aircraft wing and wing tip device |
| GB2576929A (en) * | 2018-09-07 | 2020-03-11 | Airbus Operations Ltd | A wing tip device |
| CN109885894B (zh) * | 2019-01-24 | 2023-05-05 | 江西理工大学 | 一种基于Trefftz多源点配点法的稀土矿层地下水渗流模型 |
| CN110080939A (zh) * | 2019-06-05 | 2019-08-02 | 上海电气风电集团有限公司 | 一种涡流发生器、风机叶片及其制造方法 |
| CN112124561B (zh) * | 2020-09-27 | 2022-02-25 | 中国商用飞机有限责任公司 | 用于飞行器的翼梢小翼的气动减阻结构及飞行器 |
| GB2615311A (en) * | 2022-01-31 | 2023-08-09 | Airbus Operations Ltd | Aircraft wing with movable wing tip device |
| GB2616252A (en) * | 2022-01-31 | 2023-09-06 | Airbus Operations Ltd | Aircraft with movable wing tip device |
| GB2628523B (en) * | 2022-11-16 | 2025-07-09 | Airbus Operations Ltd | Aircraft wing |
| CN120057248B (zh) * | 2025-04-17 | 2025-11-28 | 白鲸航线(常州)科技有限公司 | 一种翼梢小翼及飞机机翼 |
Citations (4)
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|---|---|---|---|---|
| US4382569A (en) * | 1979-12-26 | 1983-05-10 | Grumman Aerospace Corporation | Wing tip flow control |
| US4595160A (en) * | 1983-05-18 | 1986-06-17 | Jonathan Santos | Wing tip airfoils |
| FR2780700A1 (fr) * | 1998-07-02 | 2000-01-07 | Christian Hugues | Cavite cylindrique en spirale |
| CN1953900A (zh) * | 2004-02-20 | 2007-04-25 | 波音公司 | 用于控制尾流的方法和装置 |
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| US7900876B2 (en) | 2007-08-09 | 2011-03-08 | The Boeing Company | Wingtip feathers, including forward swept feathers, and associated aircraft systems and methods |
| US20090084904A1 (en) | 2007-10-02 | 2009-04-02 | The Boeing Company | Wingtip Feathers, Including Paired, Fixed Feathers, and Associated Systems and Methods |
| US20090224107A1 (en) | 2008-03-04 | 2009-09-10 | The Boeing Company | Reduced Span Wings with Wing Tip Devices, and Associated Systems and Methods |
| US8128035B2 (en) * | 2008-04-15 | 2012-03-06 | The Boeing Company | Winglets with recessed surfaces, and associated systems and methods |
-
2008
- 2008-04-15 US US12/103,430 patent/US8128035B2/en not_active Expired - Fee Related
-
2009
- 2009-03-20 CN CN200980109250.6A patent/CN102089207B/zh not_active Expired - Fee Related
- 2009-03-20 JP JP2011505065A patent/JP5490097B2/ja not_active Expired - Fee Related
- 2009-03-20 RU RU2010146134/11A patent/RU2492111C2/ru active
- 2009-03-20 EP EP20090733553 patent/EP2276665B1/en not_active Not-in-force
- 2009-03-20 WO PCT/US2009/037868 patent/WO2009129023A1/en not_active Ceased
- 2009-03-20 CA CA2713162A patent/CA2713162C/en active Active
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4382569A (en) * | 1979-12-26 | 1983-05-10 | Grumman Aerospace Corporation | Wing tip flow control |
| US4595160A (en) * | 1983-05-18 | 1986-06-17 | Jonathan Santos | Wing tip airfoils |
| FR2780700A1 (fr) * | 1998-07-02 | 2000-01-07 | Christian Hugues | Cavite cylindrique en spirale |
| CN1953900A (zh) * | 2004-02-20 | 2007-04-25 | 波音公司 | 用于控制尾流的方法和装置 |
Also Published As
| Publication number | Publication date |
|---|---|
| EP2276665A1 (en) | 2011-01-26 |
| EP2276665B1 (en) | 2015-05-06 |
| WO2009129023A1 (en) | 2009-10-22 |
| CA2713162A1 (en) | 2009-10-22 |
| RU2010146134A (ru) | 2012-05-20 |
| US8128035B2 (en) | 2012-03-06 |
| RU2492111C2 (ru) | 2013-09-10 |
| CN102089207A (zh) | 2011-06-08 |
| JP5490097B2 (ja) | 2014-05-14 |
| JP2011516345A (ja) | 2011-05-26 |
| CA2713162C (en) | 2012-08-21 |
| US20090256029A1 (en) | 2009-10-15 |
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| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
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