CN101389532A - 用于飞机的转向舵面的电气控制系统 - Google Patents
用于飞机的转向舵面的电气控制系统 Download PDFInfo
- Publication number
- CN101389532A CN101389532A CNA2007800066153A CN200780006615A CN101389532A CN 101389532 A CN101389532 A CN 101389532A CN A2007800066153 A CNA2007800066153 A CN A2007800066153A CN 200780006615 A CN200780006615 A CN 200780006615A CN 101389532 A CN101389532 A CN 101389532A
- Authority
- CN
- China
- Prior art keywords
- aircraft
- travel limit
- determining
- steering vane
- order
- 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
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Images
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
- B64C13/24—Transmitting means
- B64C13/38—Transmitting means with power amplification
- B64C13/50—Transmitting means with power amplification using electrical energy
- B64C13/503—Fly-by-Wire
-
- 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
- Y02T50/40—Weight reduction
Landscapes
- Engineering & Computer Science (AREA)
- Automation & Control Theory (AREA)
- Aviation & Aerospace Engineering (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
- Traffic Control Systems (AREA)
- Control Of Electric Motors In General (AREA)
- Control Of Multiple Motors (AREA)
- Power Steering Mechanism (AREA)
- Mechanical Control Devices (AREA)
Abstract
Description
Claims (5)
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0601671A FR2897838B1 (fr) | 2006-02-27 | 2006-02-27 | Systeme de commande electrique pour une gouverne de direction d'un avion. |
FR0601671 | 2006-02-27 | ||
PCT/FR2007/000290 WO2007096507A1 (fr) | 2006-02-27 | 2007-02-19 | Systeme de commande electrique pour une gouverne de direction d'un avion |
Publications (2)
Publication Number | Publication Date |
---|---|
CN101389532A true CN101389532A (zh) | 2009-03-18 |
CN101389532B CN101389532B (zh) | 2011-06-01 |
Family
ID=37102126
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN2007800066153A Active CN101389532B (zh) | 2006-02-27 | 2007-02-19 | 用于飞机的转向舵面的电气控制系统 |
Country Status (10)
Country | Link |
---|---|
US (1) | US20090014595A1 (zh) |
EP (1) | EP1989104B1 (zh) |
JP (1) | JP5124489B2 (zh) |
CN (1) | CN101389532B (zh) |
AT (1) | ATE533691T1 (zh) |
BR (1) | BRPI0706975A2 (zh) |
CA (1) | CA2640521C (zh) |
FR (1) | FR2897838B1 (zh) |
RU (1) | RU2397111C2 (zh) |
WO (1) | WO2007096507A1 (zh) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN102566579A (zh) * | 2010-12-14 | 2012-07-11 | 波音公司 | 用于使飞机滑行的转向方法 |
CN105083534A (zh) * | 2014-05-23 | 2015-11-25 | 空中客车德国运营有限责任公司 | 飞行器的高升力系统及确定其中部件位置的方法和飞行器 |
Families Citing this family (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US9708054B2 (en) | 2009-03-26 | 2017-07-18 | The Boeing Company | Method and apparatus for optimizing a load in a flight control system while an aircraft is on the ground |
GB2481180B (en) * | 2009-03-26 | 2013-09-18 | Boeing Co | Method and apparatus for optimizing a load in a flight control system while an aircraft is on the ground |
FR2959575B1 (fr) * | 2010-05-03 | 2014-08-29 | Airbus Operations Sas | Procede et dispositif pour la reduction des charges engendrees sur un avion par une perturbation aerodynamique. |
US8933383B2 (en) * | 2010-09-01 | 2015-01-13 | The United States Of America As Represented By The Secretary Of The Army | Method and apparatus for correcting the trajectory of a fin-stabilized, ballistic projectile using canards |
CN102435410B (zh) * | 2011-12-01 | 2013-09-25 | 中国航天空气动力技术研究院 | 一种燃气舵搭载发动机热试车的试验系统 |
US11120669B2 (en) * | 2013-11-26 | 2021-09-14 | Ncr Corporation | Media depository |
FR3030449B1 (fr) * | 2014-12-19 | 2017-11-24 | Airbus Operations Sas | Procede et systeme de commande de direction pour un aeronef |
CN104677201B (zh) * | 2015-02-09 | 2016-08-24 | 浙江理工大学 | 快速调整攻角用折叠舵展开机构 |
Family Cites Families (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3051416A (en) * | 1958-11-06 | 1962-08-28 | Honeywell Regulator Co | Maneuver limiting autopilot monitor |
US5170969A (en) * | 1988-11-23 | 1992-12-15 | The Boeing Company | Aircraft rudder command system |
US5598991A (en) * | 1995-05-12 | 1997-02-04 | The Boeing Company | Method and apparatus for detecting oscillatory phenomena indicative of airflow separation |
FR2738796B1 (fr) * | 1995-09-15 | 1997-12-05 | Aerospatiale | Procede et dispositif de commande de la gouverne de direction d'un aeronef |
JP3645038B2 (ja) * | 1996-07-05 | 2005-05-11 | 富士重工業株式会社 | 航空機の飛行制御装置 |
FR2793765B1 (fr) * | 1999-05-18 | 2001-07-13 | Eurocopter France | Dispositif de commande de vol d'un aeronef |
FR2809373B1 (fr) * | 2000-05-29 | 2002-08-09 | Aerospatiale Matra Airbus | Systeme de commande electrique pour une gouverne de direction d'aeronef |
FR2844251B1 (fr) * | 2002-09-09 | 2005-05-27 | Airbus France | Procede et systeme pour deplacer une gouverne d'un aeronef. |
FR2850084B1 (fr) * | 2003-01-21 | 2005-12-30 | Airbus France | Procede et systeme de commande d'une gouverne d'aeronef. |
-
2006
- 2006-02-27 FR FR0601671A patent/FR2897838B1/fr not_active Expired - Fee Related
-
2007
- 2007-02-19 RU RU2008138527/11A patent/RU2397111C2/ru not_active IP Right Cessation
- 2007-02-19 BR BRPI0706975-8A patent/BRPI0706975A2/pt not_active Application Discontinuation
- 2007-02-19 JP JP2008555831A patent/JP5124489B2/ja active Active
- 2007-02-19 AT AT07731001T patent/ATE533691T1/de active
- 2007-02-19 WO PCT/FR2007/000290 patent/WO2007096507A1/fr active Application Filing
- 2007-02-19 EP EP07731001A patent/EP1989104B1/fr active Active
- 2007-02-19 US US12/162,465 patent/US20090014595A1/en not_active Abandoned
- 2007-02-19 CA CA2640521A patent/CA2640521C/fr active Active
- 2007-02-19 CN CN2007800066153A patent/CN101389532B/zh active Active
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN102566579A (zh) * | 2010-12-14 | 2012-07-11 | 波音公司 | 用于使飞机滑行的转向方法 |
CN105083534A (zh) * | 2014-05-23 | 2015-11-25 | 空中客车德国运营有限责任公司 | 飞行器的高升力系统及确定其中部件位置的方法和飞行器 |
US9701421B2 (en) | 2014-05-23 | 2017-07-11 | Airbus Operations Gmbh | Method for determining the position of a component in a high lift system of an aircraft, high lift system of an aircraft and aircraft |
Also Published As
Publication number | Publication date |
---|---|
CA2640521A1 (fr) | 2007-08-30 |
BRPI0706975A2 (pt) | 2011-04-12 |
CA2640521C (fr) | 2014-01-28 |
FR2897838B1 (fr) | 2009-01-09 |
JP5124489B2 (ja) | 2013-01-23 |
RU2397111C2 (ru) | 2010-08-20 |
EP1989104B1 (fr) | 2011-11-16 |
CN101389532B (zh) | 2011-06-01 |
ATE533691T1 (de) | 2011-12-15 |
RU2008138527A (ru) | 2010-04-10 |
FR2897838A1 (fr) | 2007-08-31 |
EP1989104A1 (fr) | 2008-11-12 |
JP2009528202A (ja) | 2009-08-06 |
WO2007096507A1 (fr) | 2007-08-30 |
US20090014595A1 (en) | 2009-01-15 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
C06 | Publication | ||
PB01 | Publication | ||
C10 | Entry into substantive examination | ||
SE01 | Entry into force of request for substantive examination | ||
C14 | Grant of patent or utility model | ||
GR01 | Patent grant | ||
ASS | Succession or assignment of patent right |
Owner name: AIRBUS OPERATIONS S.A.S. Free format text: FORMER OWNER: AIRBUS FRANCE Effective date: 20120117 |
|
C41 | Transfer of patent application or patent right or utility model | ||
TR01 | Transfer of patent right |
Effective date of registration: 20120117 Address after: France Toulouse Co-patentee after: AIRBUS Patentee after: Airbus Operations S.A.S. Address before: France Toulouse Co-patentee before: Airbus Patentee before: Airbus France Effective date of registration: 20120117 Address after: France Toulouse Co-patentee after: AIRBUS Patentee after: AIRBUS FRANCE Address before: France Toulouse Co-patentee before: Airbus Patentee before: Airbus France |