FR2346214A1 - Aile d'aeronef a profil aerodynamique variable - Google Patents
Aile d'aeronef a profil aerodynamique variableInfo
- Publication number
- FR2346214A1 FR2346214A1 FR7709219A FR7709219A FR2346214A1 FR 2346214 A1 FR2346214 A1 FR 2346214A1 FR 7709219 A FR7709219 A FR 7709219A FR 7709219 A FR7709219 A FR 7709219A FR 2346214 A1 FR2346214 A1 FR 2346214A1
- Authority
- FR
- France
- Prior art keywords
- aircraft wing
- aerodynamic profile
- variable aerodynamic
- variable
- profile
- 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
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/38—Adjustment of complete wings or parts thereof
- B64C3/44—Varying camber
- B64C3/48—Varying camber by relatively-movable parts of wing structures
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Invalid Beds And Related Equipment (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Percussion Or Vibration Massage (AREA)
- Building Environments (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB13337/76A GB1536331A (en) | 1976-04-01 | 1976-04-01 | Aerofoils |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| FR2346214A1 true FR2346214A1 (fr) | 1977-10-28 |
| FR2346214B1 FR2346214B1 (enExample) | 1982-10-29 |
Family
ID=10021109
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| FR7709219A Granted FR2346214A1 (fr) | 1976-04-01 | 1977-03-28 | Aile d'aeronef a profil aerodynamique variable |
Country Status (9)
| Country | Link |
|---|---|
| US (1) | US4113210A (enExample) |
| JP (1) | JPS52140199A (enExample) |
| CA (1) | CA1064456A (enExample) |
| DE (1) | DE2713902A1 (enExample) |
| FR (1) | FR2346214A1 (enExample) |
| GB (1) | GB1536331A (enExample) |
| IT (1) | IT1116292B (enExample) |
| NL (1) | NL7703404A (enExample) |
| SE (1) | SE428913B (enExample) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO1999036313A1 (en) * | 1998-01-15 | 1999-07-22 | Sridhar Kota | System for varying a surface contour |
Families Citing this family (26)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4718619A (en) * | 1983-07-28 | 1988-01-12 | Ministry Of Defence | Manoeuverable supercritical wing section |
| JPS6377899U (enExample) * | 1986-11-11 | 1988-05-23 | ||
| DE4005968C2 (de) * | 1990-02-26 | 1995-08-03 | Otto Lift Systeme Gmbh | Müllsammelfahrzeug |
| DE4007694A1 (de) * | 1990-03-10 | 1991-09-12 | Deutsche Forsch Luft Raumfahrt | Tragfluegel mit veraenderbarem profil im hinteren tragfluegelbereich |
| DE19643222C2 (de) * | 1996-10-19 | 1998-12-10 | Daimler Benz Ag | Auftriebskörper mit veränderbarer Wölbung |
| US5842666A (en) * | 1997-02-21 | 1998-12-01 | Northrop Grumman Coporation | Laminar supersonic transport aircraft |
| DE19741326C2 (de) * | 1997-09-19 | 2003-11-20 | Deutsch Zentr Luft & Raumfahrt | Anströmprofil mit variabler Profiladaption |
| DE19741490C2 (de) * | 1997-09-19 | 2000-06-08 | Deutsch Zentr Luft & Raumfahrt | Anströmprofil mit variabler Profiladaption |
| RU2130858C1 (ru) * | 1997-10-22 | 1999-05-27 | Акционерное общество открытого типа "ОКБ Сухого" | Крыло изменяемой кривизны летательного аппарата |
| EP0958999B2 (en) | 1998-05-21 | 2007-08-29 | McDonnell Douglas Corporation | Aerofoil |
| US6129308A (en) * | 1998-09-21 | 2000-10-10 | Northrop Grumman Corporation | Delta-shaped aircraft with variable camber fuselage and wing |
| DE19936721B4 (de) * | 1999-08-06 | 2005-09-15 | Deutsches Zentrum für Luft- und Raumfahrt e.V. | Tragflügelprofil mit adaptiver Verwölbung |
| DE20004499U1 (de) * | 2000-03-14 | 2000-12-07 | DaimlerChrysler AG, 70567 Stuttgart | Aerodynamisches Strömungsprofil mit Vorderkantenklappe |
| DE10055961B4 (de) * | 2000-11-11 | 2004-09-09 | Eads Deutschland Gmbh | Variabler Flügelbereich mit einstellbarer, sich in Spannweiten-Richtung erstreckender Profilform |
| DE102004045651B4 (de) * | 2004-09-21 | 2010-09-16 | Airbus Deutschland Gmbh | Flügel, insbesondere Tragflügel eines Flugzeugs, mit veränderbarem Profil |
| DE102004062998B4 (de) * | 2004-12-22 | 2010-09-09 | Airbus Deutschland Gmbh | Flügel, insbesondere Tragflügel eines Flugzeugs, mit veränderlicher Profilform |
| CA2650535A1 (en) * | 2006-04-27 | 2007-12-21 | Flexsys, Inc. | Compliant structure design for varying surface contours |
| WO2008131800A1 (en) * | 2007-04-30 | 2008-11-06 | Vestas Wind Systems A/S | A wind turbine blade |
| DE102008025414B4 (de) * | 2008-05-27 | 2014-09-04 | Eurocopter Deutschland Gmbh | Aerodynamisches Profil mit reversibel verformbarer Kontur für Luftfahrzeuge, insbesondere für Drehflügelflugzeuge |
| DE102010047918A1 (de) | 2010-10-08 | 2014-04-30 | Smart Blade Gmbh | Flexible Hinterkante eines Rotorblattes einer Windkraftanlage |
| US8925870B1 (en) | 2012-03-09 | 2015-01-06 | The Boeing Company | Morphing wing leading edge |
| US9598167B2 (en) | 2014-03-04 | 2017-03-21 | The Boeing Company | Morphing airfoil leading edge |
| US9415856B2 (en) | 2014-06-04 | 2016-08-16 | The Boeing Company | Dual-rib morphing leading edge |
| RU2657062C1 (ru) * | 2017-07-06 | 2018-06-08 | Федеральное государственное унитарное предприятие "Центральный аэрогидродинамический институт имени профессора Н.Е. Жуковского" (ФГУП "ЦАГИ") | Адаптивная аэродинамическая поверхность |
| CN111907693B (zh) * | 2020-06-22 | 2022-02-22 | 哈尔滨工业大学(深圳)(哈尔滨工业大学深圳科技创新研究院) | 一种可变弯度的机翼 |
| CN112520013B (zh) * | 2020-12-16 | 2022-02-25 | 中国空气动力研究与发展中心设备设计及测试技术研究所 | 一种基于连杆驱动弯度可变的变形机翼 |
Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR495650A (fr) * | 1919-02-08 | 1919-10-14 | Auguste Pertus | Aile à courbures variables pour appareils d'aviation |
| US1500358A (en) * | 1923-05-19 | 1924-07-08 | Antoni Guido | Aeroplane |
| US3698668A (en) * | 1971-04-08 | 1972-10-17 | Boeing Co | Variable camber airfoil |
Family Cites Families (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US1365346A (en) * | 1920-07-02 | 1921-01-11 | Schenkel Gottfried | Adjusting device for aeroplanes |
| US1868748A (en) * | 1931-11-28 | 1932-07-26 | Herbert J Hogan | Variable camber airfoil |
| US2448712A (en) * | 1944-02-26 | 1948-09-07 | William J Hampshire | Means for controlling the operation of wing and tail-plane elements of an airplane |
| US3179357A (en) * | 1962-02-27 | 1965-04-20 | Donald G Lyon | Variable shaped airfoil |
| US3836099A (en) * | 1973-09-28 | 1974-09-17 | Us Navy | Airfoil camber change system |
-
1976
- 1976-04-01 GB GB13337/76A patent/GB1536331A/en not_active Expired
-
1977
- 1977-03-28 US US05/781,866 patent/US4113210A/en not_active Expired - Lifetime
- 1977-03-28 FR FR7709219A patent/FR2346214A1/fr active Granted
- 1977-03-29 NL NL7703404A patent/NL7703404A/xx not_active Application Discontinuation
- 1977-03-29 DE DE19772713902 patent/DE2713902A1/de not_active Withdrawn
- 1977-03-31 SE SE7703764A patent/SE428913B/xx not_active IP Right Cessation
- 1977-03-31 IT IT7767713A patent/IT1116292B/it active
- 1977-03-31 CA CA275,276A patent/CA1064456A/en not_active Expired
- 1977-04-01 JP JP3623777A patent/JPS52140199A/ja active Pending
Patent Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR495650A (fr) * | 1919-02-08 | 1919-10-14 | Auguste Pertus | Aile à courbures variables pour appareils d'aviation |
| US1500358A (en) * | 1923-05-19 | 1924-07-08 | Antoni Guido | Aeroplane |
| US3698668A (en) * | 1971-04-08 | 1972-10-17 | Boeing Co | Variable camber airfoil |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO1999036313A1 (en) * | 1998-01-15 | 1999-07-22 | Sridhar Kota | System for varying a surface contour |
Also Published As
| Publication number | Publication date |
|---|---|
| JPS52140199A (en) | 1977-11-22 |
| SE7703764L (sv) | 1977-10-02 |
| IT1116292B (it) | 1986-02-10 |
| DE2713902A1 (de) | 1977-10-06 |
| FR2346214B1 (enExample) | 1982-10-29 |
| GB1536331A (en) | 1978-12-20 |
| CA1064456A (en) | 1979-10-16 |
| NL7703404A (nl) | 1977-10-04 |
| SE428913B (sv) | 1983-08-01 |
| US4113210A (en) | 1978-09-12 |
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|---|---|---|
| FR2346214A1 (fr) | Aile d'aeronef a profil aerodynamique variable | |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| ST | Notification of lapse |