FR2906220B1 - AIRCRAFT SERVOCOMMANDS DEPORTEES - Google Patents
AIRCRAFT SERVOCOMMANDS DEPORTEESInfo
- Publication number
- FR2906220B1 FR2906220B1 FR0653871A FR0653871A FR2906220B1 FR 2906220 B1 FR2906220 B1 FR 2906220B1 FR 0653871 A FR0653871 A FR 0653871A FR 0653871 A FR0653871 A FR 0653871A FR 2906220 B1 FR2906220 B1 FR 2906220B1
- Authority
- FR
- France
- Prior art keywords
- servocommands
- deportees
- aircraft
- servocommands deportees
- aircraft servocommands
- 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
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
- B64C23/076—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 the wing tip airfoil devices comprising one or more separate moveable members thereon affecting the vortices, e.g. 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
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0653871A FR2906220B1 (en) | 2006-09-21 | 2006-09-21 | AIRCRAFT SERVOCOMMANDS DEPORTEES |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0653871A FR2906220B1 (en) | 2006-09-21 | 2006-09-21 | AIRCRAFT SERVOCOMMANDS DEPORTEES |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2906220A1 FR2906220A1 (en) | 2008-03-28 |
FR2906220B1 true FR2906220B1 (en) | 2009-10-02 |
Family
ID=37888165
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR0653871A Expired - Fee Related FR2906220B1 (en) | 2006-09-21 | 2006-09-21 | AIRCRAFT SERVOCOMMANDS DEPORTEES |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR2906220B1 (en) |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB201105108D0 (en) * | 2011-03-28 | 2011-05-11 | Airbus Operations Ltd | Wing tip pod |
CA2863583C (en) | 2012-02-09 | 2019-03-26 | Moog Inc. | Actuator system and method |
CA3011439A1 (en) | 2016-01-13 | 2017-07-20 | Moog Inc. | Summing and fault tolerant rotary actuator assembly |
Family Cites Families (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3128971A (en) * | 1964-04-14 | Aircraft landing gear | ||
FR1141117A (en) * | 1956-01-16 | 1957-08-26 | Sncan | Advanced aerodyne |
US2846165A (en) * | 1956-06-25 | 1958-08-05 | John A Axelson | Aircraft control system |
DE2355979B2 (en) * | 1973-11-09 | 1976-12-02 | Dornier Gmbh, 7990 Friedrichshafen | ADDITIONAL CONTROL DEVICE FOR AIRCRAFT |
US4455004A (en) * | 1982-09-07 | 1984-06-19 | Lockheed Corporation | Flight control device for airplanes |
ES2274658B1 (en) * | 2003-12-31 | 2008-04-16 | Airbus España, S.L. | MECHANISM TO DELETE LIMIT CYCLE OSCILLATIONS IN SERVOCONTROLATED AERODYNAMIC CONTROL SURFACES. |
-
2006
- 2006-09-21 FR FR0653871A patent/FR2906220B1/en not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
FR2906220A1 (en) | 2008-03-28 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
CA | Change of address |
Effective date: 20110916 |
|
CD | Change of name or company name |
Owner name: AIRBUS HOLDING, FR Effective date: 20110916 |
|
CJ | Change in legal form |
Effective date: 20110916 |
|
TP | Transmission of property |
Owner name: AIRBUS HOLDING, FR Effective date: 20110913 |
|
PLFP | Fee payment |
Year of fee payment: 11 |
|
PLFP | Fee payment |
Year of fee payment: 12 |
|
PLFP | Fee payment |
Year of fee payment: 13 |
|
PLFP | Fee payment |
Year of fee payment: 14 |
|
ST | Notification of lapse |
Effective date: 20210506 |