FR2479131A1 - Corps profile, notamment pour voilure d'aeronef - Google Patents
Corps profile, notamment pour voilure d'aeronef Download PDFInfo
- Publication number
- FR2479131A1 FR2479131A1 FR8105897A FR8105897A FR2479131A1 FR 2479131 A1 FR2479131 A1 FR 2479131A1 FR 8105897 A FR8105897 A FR 8105897A FR 8105897 A FR8105897 A FR 8105897A FR 2479131 A1 FR2479131 A1 FR 2479131A1
- Authority
- FR
- France
- Prior art keywords
- body according
- trailing edge
- strip
- edge
- profiled
- 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
- 239000012530 fluid Substances 0.000 claims description 6
- 230000009471 action Effects 0.000 claims description 3
- 230000015572 biosynthetic process Effects 0.000 abstract description 3
- 230000000694 effects Effects 0.000 description 5
- 230000008901 benefit Effects 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 238000013459 approach Methods 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- 238000010348 incorporation Methods 0.000 description 1
- 230000003993 interaction Effects 0.000 description 1
- 210000003739 neck Anatomy 0.000 description 1
- 238000005457 optimization Methods 0.000 description 1
- 235000021178 picnic Nutrition 0.000 description 1
- 230000009467 reduction Effects 0.000 description 1
- 238000004804 winding 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
-
- 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 (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB8009253 | 1980-03-25 |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| FR2479131A1 true FR2479131A1 (fr) | 1981-10-02 |
| FR2479131B1 FR2479131B1 (OSRAM) | 1984-12-28 |
Family
ID=10512206
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| FR8105897A Granted FR2479131A1 (fr) | 1980-03-25 | 1981-03-24 | Corps profile, notamment pour voilure d'aeronef |
Country Status (3)
| Country | Link |
|---|---|
| US (1) | US4444367A (OSRAM) |
| FR (1) | FR2479131A1 (OSRAM) |
| SE (1) | SE8101793L (OSRAM) |
Families Citing this family (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5634613A (en) * | 1994-07-18 | 1997-06-03 | Mccarthy; Peter T. | Tip vortex generation technology for creating a lift enhancing and drag reducing upwash effect |
| WO2004002823A1 (en) * | 2002-06-26 | 2004-01-08 | Mccarthy Peter T | High efficiency tip vortex reversal and induced drag reduction |
| EP1523374A1 (en) * | 2002-07-19 | 2005-04-20 | McCarthy, Peter T. | High deflection hydrofoils and swim fins |
| RU2008103327A (ru) * | 2005-06-30 | 2009-08-10 | Белл Хеликоптер Текстрон Инк. (Us) | Выдвижной турбулизатор |
| BRPI0700765A (pt) * | 2007-02-15 | 2007-12-04 | Embraer Aeronautica Sa | gerador de vórtice para melhorar o desempenho de entradas de ar embutidas |
| DE102018113800A1 (de) * | 2017-11-02 | 2019-05-02 | Klaus Röhm | Aerodynamische Vorrichtung für Flügel und Rotorblätter |
Citations (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4067518A (en) * | 1976-05-20 | 1978-01-10 | Lockheed Corporation | Drag reducer for lift surface of aircraft |
Family Cites Families (16)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2559823A (en) * | 1945-04-09 | 1951-07-10 | Northrop Aircraft Inc | Rudder for tailless airplanes |
| US2576981A (en) * | 1949-02-08 | 1951-12-04 | Vogt Richard | Twisted wing tip fin for airplanes |
| US2775419A (en) * | 1952-01-26 | 1956-12-25 | Josef S J Hlobil | Fractional aspect ratio aircraft |
| US2740596A (en) * | 1953-08-19 | 1956-04-03 | United Aircraft Corp | Vortex generator |
| GB1019061A (en) * | 1961-03-29 | 1966-02-02 | Herbert Harry Pearcey | Improvements relating to control of fluid flow past bodies and to reduction of drag of such bodies |
| US3270988A (en) * | 1962-12-26 | 1966-09-06 | Jr Clarence D Cone | Minimum induced drag airfoil body |
| US3369775A (en) * | 1965-01-11 | 1968-02-20 | Scott C. Rethorst | Aircraft wing system having zero induced drag |
| US3310262A (en) * | 1965-05-21 | 1967-03-21 | Augustine W Robins | Supersonic aircraft |
| US3693913A (en) * | 1970-08-24 | 1972-09-26 | Lockheed Aircraft Corp | Fluid flow control device |
| US3984070A (en) * | 1974-05-24 | 1976-10-05 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Wingtip vortex dissipator for aircraft |
| US3960345A (en) * | 1975-05-16 | 1976-06-01 | Grumman Aerospace Corporation | Means to reduce and/or eliminate vortices, caused by wing body combinations |
| US4050397A (en) * | 1976-04-26 | 1977-09-27 | The Boeing Company | Foil fence for hydrofoil craft |
| US4190219A (en) * | 1977-05-17 | 1980-02-26 | Lockheed Corporation | Vortex diffuser |
| USD256791S (en) | 1978-11-09 | 1980-09-09 | Fairchild Industries, Inc. | Aircraft |
| US4293110A (en) * | 1979-03-08 | 1981-10-06 | The Boeing Company | Leading edge vortex flap for wings |
| US4377267A (en) * | 1981-01-12 | 1983-03-22 | Juanita June Haworth | Vortex tranquilizer |
-
1981
- 1981-03-20 SE SE8101793A patent/SE8101793L/xx not_active Application Discontinuation
- 1981-03-24 FR FR8105897A patent/FR2479131A1/fr active Granted
- 1981-03-24 US US06/247,113 patent/US4444367A/en not_active Expired - Fee Related
Patent Citations (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4067518A (en) * | 1976-05-20 | 1978-01-10 | Lockheed Corporation | Drag reducer for lift surface of aircraft |
Also Published As
| Publication number | Publication date |
|---|---|
| US4444367A (en) | 1984-04-24 |
| SE8101793L (sv) | 1981-09-26 |
| FR2479131B1 (OSRAM) | 1984-12-28 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| ST | Notification of lapse |