FR2507148B1 - - Google Patents
Info
- Publication number
- FR2507148B1 FR2507148B1 FR8209794A FR8209794A FR2507148B1 FR 2507148 B1 FR2507148 B1 FR 2507148B1 FR 8209794 A FR8209794 A FR 8209794A FR 8209794 A FR8209794 A FR 8209794A FR 2507148 B1 FR2507148 B1 FR 2507148B1
- Authority
- FR
- France
- 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
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C9/00—Adjustable control surfaces or members, e.g. rudders
- B64C9/14—Adjustable control surfaces or members, e.g. rudders forming slots
- B64C9/22—Adjustable control surfaces or members, e.g. rudders forming slots at the front of the wing
- B64C9/26—Adjustable control surfaces or members, e.g. rudders forming slots at the front of the wing by multiple flaps
-
- 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
-
- 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
- B64C3/50—Varying camber by leading or trailing edge flaps
-
- 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
-
- 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
- Y02T50/30—Wing lift efficiency
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Prostheses (AREA)
- Operating, Guiding And Securing Of Roll- Type Closing Members (AREA)
- Air-Flow Control Members (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE19813122137 DE3122137A1 (en) | 1981-06-04 | 1981-06-04 | FRONT EDGE FLAP SYSTEM FOR PLANE WINGS |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| FR2507148A1 FR2507148A1 (en) | 1982-12-10 |
| FR2507148B1 true FR2507148B1 (en) | 1985-03-08 |
Family
ID=6133868
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| FR8209794A Granted FR2507148A1 (en) | 1981-06-04 | 1982-06-04 | ATTACK EDGE SHUTTER SYSTEM FOR AIRCRAFT WING |
Country Status (3)
| Country | Link |
|---|---|
| DE (1) | DE3122137A1 (en) |
| FR (1) | FR2507148A1 (en) |
| GB (1) | GB2100684B (en) |
Families Citing this family (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS58500892A (en) * | 1981-06-10 | 1983-06-02 | ザ ボ−イング コンパニ− | leading edge vortex flap for wing |
| US7204454B2 (en) * | 2005-02-25 | 2007-04-17 | Northrop Grumman Corporation | Aircraft with articulated leading edge of fuselage and wings |
| US7246770B2 (en) | 2005-02-25 | 2007-07-24 | Northrop Grumman Corporation | Aircraft with rotatable leading edge of fuselage and wings |
| US7216835B2 (en) | 2005-02-25 | 2007-05-15 | Northrop Grumman Corporation | Aircraft with extendable leading edge of fuselage and wings |
| US9902486B2 (en) | 2013-04-15 | 2018-02-27 | Christian Emmanuel Norden | Transition arrangement for an aircraft |
| GB2579221A (en) * | 2018-11-26 | 2020-06-17 | Airbus Operations Ltd | Aircraft control mechanism |
Family Cites Families (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3047257A (en) * | 1958-04-24 | 1962-07-31 | Martin Marietta Corp | Device for changing airfoil profile |
| DE2751361C2 (en) * | 1977-11-17 | 1984-09-27 | Messerschmitt-Bölkow-Blohm GmbH, 8000 München | A method for controlling aircraft by controlling detached wing leading edge eddy currents |
| US4293110A (en) * | 1979-03-08 | 1981-10-06 | The Boeing Company | Leading edge vortex flap for wings |
-
1981
- 1981-06-04 DE DE19813122137 patent/DE3122137A1/en active Granted
-
1982
- 1982-06-01 GB GB08215918A patent/GB2100684B/en not_active Expired
- 1982-06-04 FR FR8209794A patent/FR2507148A1/en active Granted
Also Published As
| Publication number | Publication date |
|---|---|
| FR2507148A1 (en) | 1982-12-10 |
| DE3122137C2 (en) | 1987-06-25 |
| GB2100684B (en) | 1984-12-05 |
| GB2100684A (en) | 1983-01-06 |
| DE3122137A1 (en) | 1982-12-23 |
Similar Documents
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| ST | Notification of lapse |