FR2893909B1 - Procede pour assurer la securite d'un aeronef volant horizontalement a faible vitesse. - Google Patents
Procede pour assurer la securite d'un aeronef volant horizontalement a faible vitesse.Info
- Publication number
- FR2893909B1 FR2893909B1 FR0512048A FR0512048A FR2893909B1 FR 2893909 B1 FR2893909 B1 FR 2893909B1 FR 0512048 A FR0512048 A FR 0512048A FR 0512048 A FR0512048 A FR 0512048A FR 2893909 B1 FR2893909 B1 FR 2893909B1
- Authority
- FR
- France
- Prior art keywords
- ensuring
- safety
- low speed
- speed aircraft
- horizontally low
- 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
- B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
- B64C13/02—Initiating means
- B64C13/16—Initiating means actuated automatically, e.g. responsive to gust detectors
Landscapes
- Engineering & Computer Science (AREA)
- Automation & Control Theory (AREA)
- Aviation & Aerospace Engineering (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
- Transmission Devices (AREA)
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0512048A FR2893909B1 (fr) | 2005-11-29 | 2005-11-29 | Procede pour assurer la securite d'un aeronef volant horizontalement a faible vitesse. |
US11/604,296 US8561948B2 (en) | 2005-11-29 | 2006-11-27 | Method for ensuring the safety of an aircraft flying horizontally at low speed |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0512048A FR2893909B1 (fr) | 2005-11-29 | 2005-11-29 | Procede pour assurer la securite d'un aeronef volant horizontalement a faible vitesse. |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2893909A1 FR2893909A1 (fr) | 2007-06-01 |
FR2893909B1 true FR2893909B1 (fr) | 2007-12-21 |
Family
ID=36862487
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR0512048A Expired - Fee Related FR2893909B1 (fr) | 2005-11-29 | 2005-11-29 | Procede pour assurer la securite d'un aeronef volant horizontalement a faible vitesse. |
Country Status (2)
Country | Link |
---|---|
US (1) | US8561948B2 (fr) |
FR (1) | FR2893909B1 (fr) |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102009017653A1 (de) * | 2009-04-16 | 2010-10-21 | Airbus Deutschland Gmbh | Hochauftriebssystem eines Flugzeugs, Flugzeugsystem und Propeller-Flugzeug mit einem Hochauftriebssystem |
CN105912006B (zh) * | 2016-05-31 | 2019-02-12 | 中国航空工业集团公司西安飞机设计研究所 | 一种飞行器复飞控制方法 |
RU2761687C1 (ru) * | 2021-05-20 | 2021-12-13 | Федеральное государственное унитарное предприятие "Центральный аэрогидродинамический институт имени профессора Н.Е. Жуковского" (ФГУП "ЦАГИ") | Способ управления самолётом при выводе на большие углы атаки |
Family Cites Families (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB823592A (en) * | 1955-09-28 | 1959-11-11 | Power Jets Res & Dev Ltd | Aircraft powered by turbo-prop engines |
US3138353A (en) * | 1962-03-21 | 1964-06-23 | Boeing Co | Method and apparatus for preventing complete stalls of an aircraft at slow speeds |
US3275269A (en) * | 1963-10-23 | 1966-09-27 | Sperry Rand Corp | Dual period aircraft control system |
US3522729A (en) * | 1968-01-22 | 1970-08-04 | Sperry Rand Corp | Airspeed command system |
US3575363A (en) * | 1969-08-28 | 1971-04-20 | Mc Donnell Douglas Corp | Horizontal tail for aircraft |
US3822047A (en) * | 1972-12-14 | 1974-07-02 | Collins Radio Co | Takeoff and go-around climb-out profile pitch command formulation for aircraft |
US4043523A (en) * | 1976-03-11 | 1977-08-23 | Ball Brothers Research Corporation | Apparatus for aircraft pitch trim |
US4106730A (en) * | 1976-10-01 | 1978-08-15 | The Boeing Company | Engine out control system for STOL aircraft |
US4319219A (en) * | 1980-06-30 | 1982-03-09 | The Boeing Company | Automatic approach landing and go-around control system for aircraft |
FR2661149B1 (fr) * | 1990-04-24 | 1992-08-14 | Aerospatiale | Systeme pour le pilotage d'un avion en tangage. |
FR2865999B1 (fr) * | 2004-02-06 | 2006-04-07 | Airbus France | Procede pour ameliorer l'atterrissage d'un aeronef. |
FR2869588B1 (fr) * | 2004-04-28 | 2006-07-14 | Airbus France Sas | Procede d'aide au decollage d'un aeronef. |
FR2877312B1 (fr) * | 2004-11-02 | 2007-01-12 | Airbus France Sas | Procede et dispositif pour ameliorer l'efficacite de freinage d'un aeronef roulant sur le sol |
-
2005
- 2005-11-29 FR FR0512048A patent/FR2893909B1/fr not_active Expired - Fee Related
-
2006
- 2006-11-27 US US11/604,296 patent/US8561948B2/en not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
FR2893909A1 (fr) | 2007-06-01 |
US8561948B2 (en) | 2013-10-22 |
US20080272242A1 (en) | 2008-11-06 |
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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 |
|
PLFP | Fee payment |
Year of fee payment: 15 |
|
ST | Notification of lapse |
Effective date: 20210706 |