ES2190179T3 - Sistema de control mixto para superficie aerodinamica de una aeronave. - Google Patents
Sistema de control mixto para superficie aerodinamica de una aeronave.Info
- Publication number
- ES2190179T3 ES2190179T3 ES99400927T ES99400927T ES2190179T3 ES 2190179 T3 ES2190179 T3 ES 2190179T3 ES 99400927 T ES99400927 T ES 99400927T ES 99400927 T ES99400927 T ES 99400927T ES 2190179 T3 ES2190179 T3 ES 2190179T3
- Authority
- ES
- Spain
- Prior art keywords
- aerodynamic surface
- aircraft
- well
- control system
- machine
- 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 - Lifetime
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
- B64C13/24—Transmitting means
- B64C13/38—Transmitting means with power amplification
- B64C13/50—Transmitting means with power amplification using electrical energy
- B64C13/503—Fly-by-Wire
-
- 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
- B64C13/505—Transmitting means with power amplification using electrical energy having duplication or stand-by provisions
Landscapes
- Engineering & Computer Science (AREA)
- Automation & Control Theory (AREA)
- Aviation & Aerospace Engineering (AREA)
- Fluid-Pressure Circuits (AREA)
- Vibration Prevention Devices (AREA)
- Control Of Electric Motors In General (AREA)
- Retarders (AREA)
Abstract
SISTEMA PARA EL CONTROL DE UNA SUPERFICIE AERODINAMICA (1) (ALETA, ALERON, TIMON,...) DE UNA AERONAVE. SEGUN LA INVENCION, ESTE SISTEMA COMPRENDE: - UNA MAQUINA ELECTRICA (8) QUE PUEDE FUNCIONAR BIEN CON MOTOR, BIEN CON GENERADOR, CUYA SALIDA ESTA CONECTADA MECANICAMENTE A DICHA SUPERFICIE AERODINAMICA (1) Y - UN DISPOSITIVO LOGICO (17) QUE RECIBE INFORMACIONES ACERCA DE LOS ESTADOS DE FUNCIONAMIENTO DE LA ALIMENTACION ELECTRICA (11) DE LA MAQUINA (8) Y DEL SERVOCONTROL HIDRAULICO (2,5) Y QUE CONTROLA EL ACCIONAMIENTO DE DICHA SUPERFICIE (1) BIEN POR DICHA MAQUINA (8), BIEN POR DICHO SERVOCONTROL (2, 5).
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR9805399A FR2778164B1 (fr) | 1998-04-29 | 1998-04-29 | Systeme de commande mixte pour surface aerodynamique d'aeronef |
Publications (1)
Publication Number | Publication Date |
---|---|
ES2190179T3 true ES2190179T3 (es) | 2003-07-16 |
Family
ID=9525829
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
ES99400927T Expired - Lifetime ES2190179T3 (es) | 1998-04-29 | 1999-04-16 | Sistema de control mixto para superficie aerodinamica de una aeronave. |
Country Status (7)
Country | Link |
---|---|
US (1) | US6241182B1 (es) |
EP (1) | EP0953505B1 (es) |
JP (1) | JP4180190B2 (es) |
CA (1) | CA2270753C (es) |
DE (1) | DE69904772T2 (es) |
ES (1) | ES2190179T3 (es) |
FR (1) | FR2778164B1 (es) |
Families Citing this family (46)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5060961A (en) * | 1987-11-18 | 1991-10-29 | Keith Bontrager | Mechanically joined steering assembly |
FR2809080B1 (fr) * | 2000-05-22 | 2002-08-30 | Lucas Aerospace Fcs | Dispositif d'actionnement, notamment pour commande de vol d'aeronef |
WO2002064426A1 (en) * | 2001-02-14 | 2002-08-22 | Airscooter Corporation | Ultralight coaxial rotor aircraft |
US6886777B2 (en) * | 2001-02-14 | 2005-05-03 | Airscooter Corporation | Coaxial helicopter |
US6755375B2 (en) * | 2002-10-22 | 2004-06-29 | The Boeing Company | Method and apparatus for controlling aircraft devices with multiple actuators |
US7210653B2 (en) * | 2002-10-22 | 2007-05-01 | The Boeing Company | Electric-based secondary power system architectures for aircraft |
US6827311B2 (en) * | 2003-04-07 | 2004-12-07 | Honeywell International, Inc. | Flight control actuation system |
US6923405B2 (en) * | 2003-11-17 | 2005-08-02 | The Boeing Company | Enhanced rudder control system |
DE102004007667B4 (de) * | 2004-02-17 | 2005-12-29 | Liebherr-Aerospace Lindenberg Gmbh | Aktuator |
US7424989B2 (en) | 2004-03-11 | 2008-09-16 | The Boeing Company | Intelligent multifunctional actuation system for vibration and buffet suppression |
DE102004047008A1 (de) * | 2004-09-28 | 2006-03-30 | Liebherr-Aerospace Lindenberg Gmbh | Vorrichtung zur Einstellung von Flugzeughöhenflossen |
US7513119B2 (en) * | 2005-02-03 | 2009-04-07 | The Boeing Company | Systems and methods for starting aircraft engines |
US8401716B2 (en) * | 2006-05-17 | 2013-03-19 | Textron Innovations Inc. | Flight control systems |
US8380364B2 (en) * | 2006-05-17 | 2013-02-19 | Textron Innovations, Inc. | Manual and computerized flight control system with natural feedback |
US8725321B2 (en) * | 2006-05-17 | 2014-05-13 | Textron Innovations Inc. | Flight control system |
US9340278B2 (en) | 2006-05-17 | 2016-05-17 | Textron Innovations, Inc. | Flight control system |
US20080203223A1 (en) * | 2006-06-22 | 2008-08-28 | Cyrot Luc P | Aircraft stabilizer actuator |
US8033509B2 (en) * | 2007-02-27 | 2011-10-11 | Honeywell International Inc. | Load optimized redundant flight control surface actuation system and method |
US7871038B2 (en) * | 2007-05-17 | 2011-01-18 | The Boeing Company | Systems and methods for providing airflow in an aerospace vehicle |
US7687927B2 (en) | 2007-11-21 | 2010-03-30 | The Boeing Company | Electrical systems architecture for an aircraft, and related operating methods |
US20090302516A1 (en) * | 2008-06-05 | 2009-12-10 | Lockheed Martin Corporation | System, method and apparatus for control surface with dynamic compensation |
DE102008048275B4 (de) | 2008-09-22 | 2014-07-24 | Airbus Operations Gmbh | Treibstoffmanagement-System |
US20100089053A1 (en) * | 2008-10-13 | 2010-04-15 | Honeywell International Inc. | Hybrid electromechanical/hydro-mechanical actuation control system |
US8172174B2 (en) * | 2008-11-13 | 2012-05-08 | Honeywell International Inc. | Hybrid electromechanical/hydromechanical actuator and actuation control system |
US8504221B2 (en) * | 2009-01-16 | 2013-08-06 | The Boeing Company | Apparatus and method for controlling a control surface of a vehicle based on a load identified on the control surface |
FR2947870B1 (fr) * | 2009-07-09 | 2011-07-08 | Aircelle Sa | Systeme d'actionnement pour element mobile de nacelle de moteur d'aeronef, tel qu'un capot d'inverseur de poussee |
US8657227B1 (en) | 2009-09-11 | 2014-02-25 | The Boeing Company | Independent power generation in aircraft |
DE102010021576A1 (de) * | 2010-05-26 | 2011-12-01 | Airbus Operations Gmbh | Vorrichtung für eine Stellklappe eines Tragflügels |
DE102010053396B4 (de) | 2010-12-03 | 2014-12-24 | Airbus Defence and Space GmbH | Übertragung einer Steuerungskraft |
US8738268B2 (en) | 2011-03-10 | 2014-05-27 | The Boeing Company | Vehicle electrical power management and distribution |
RU2503585C1 (ru) * | 2012-05-21 | 2014-01-10 | Федеральное государственное бюджетное образовательное учреждение высшего профессионального образования "Уфимский государственный авиационный технический университет" | Система автоматического управления углом курса и ограничения нормальной перегрузки летательного аппарата |
GB201214952D0 (en) * | 2012-08-22 | 2012-10-03 | Moog Wolverhampton Ltd | Control surface actuation assembly |
JP6178571B2 (ja) * | 2012-12-26 | 2017-08-09 | 三菱航空機株式会社 | 動翼のアクチュエータ装置、航空機の動翼、及び、航空機 |
US10017243B2 (en) | 2013-09-24 | 2018-07-10 | The Boeing Company | Adaptive trailing edge actuator system and method |
US10570936B2 (en) * | 2014-03-07 | 2020-02-25 | Parker-Hannifin Corporation | Symmetrically loaded dual hydraulic fly-by-wire actuator |
US9586675B2 (en) * | 2014-06-09 | 2017-03-07 | The Boeing Company | Apparatus and method for arrestment of a flight control surface |
US10239633B2 (en) | 2014-11-26 | 2019-03-26 | Embraer S.A. | System and method to interchange flight control inceptors in an aircraft flight control system and cockpit |
CN105711819B (zh) * | 2014-12-03 | 2018-01-19 | 武汉航空仪表有限责任公司 | 一种电动方向舵控制装置 |
US10088006B2 (en) * | 2016-05-19 | 2018-10-02 | The Boeing Company | Rotational inerter and method for damping an actuator |
US10696380B2 (en) * | 2017-07-20 | 2020-06-30 | Hamilton Sunstrand Corporation | Aerodynamic control surface operating system for aircraft using variable transmission |
US10337776B2 (en) * | 2017-09-19 | 2019-07-02 | The Boeing Company | Refrigeration system having valves and valve control actuators |
US11027824B2 (en) * | 2018-09-05 | 2021-06-08 | The Boeing Company | Distributed trailing edge wing flap systems |
EP3650336A1 (en) * | 2018-11-12 | 2020-05-13 | Goodrich Actuation Systems SAS | Trim control system |
EP3868654B1 (en) * | 2020-02-19 | 2023-05-10 | Microtecnica S.r.l. | Servo-actuator architecture with electromechanical-stability and control augmentation system |
EP4020789A1 (en) | 2020-12-23 | 2022-06-29 | Hamilton Sundstrand Corporation | Motor drive system |
US11407496B1 (en) * | 2021-08-17 | 2022-08-09 | Beta Air, Llc | Systems and methods for redundant flight control in an aircraft |
Family Cites Families (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3809191A (en) * | 1969-08-04 | 1974-05-07 | Index Ind Inc | Auxiliary braking system |
DE3220782A1 (de) * | 1982-06-02 | 1983-12-08 | Messerschmitt-Bölkow-Blohm GmbH, 8000 München | Einrichtung zum optimieren des energiehaushaltes von flugzeugbetaetigungssystemen |
US4533097A (en) * | 1983-07-11 | 1985-08-06 | Sundstrand Corporation | Multi-motor actuation system for a power drive unit |
DE3638820A1 (de) * | 1986-09-12 | 1988-03-24 | Messerschmitt Boelkow Blohm | Seitenruder-steuerungsanordnung fuer luftfahrzeuge |
US4876906A (en) * | 1986-11-20 | 1989-10-31 | Sundstrand Corporation | Non-jamming actuator system |
US4745815A (en) * | 1986-12-08 | 1988-05-24 | Sundstrand Corporation | Non-jamming screw actuator system |
GB8918431D0 (en) * | 1989-08-12 | 1989-09-20 | Lucas Ind Plc | Apparatus for aircraft flight |
US5033694A (en) * | 1989-09-08 | 1991-07-23 | Daiichi Electric Kabushiki Kaisha | Attitude control device for air or sea transportation craft |
US5082208A (en) * | 1989-09-29 | 1992-01-21 | The Boeing Company | System and method for controlling an aircraft flight control member |
FR2686310B1 (fr) * | 1992-01-20 | 1994-04-08 | Aerospatiale Ste Nationale Indle | Systeme pour la commande d'une surface aerodynamique d'un aeronef. |
DE19854142C1 (de) * | 1998-11-24 | 2000-03-23 | Festo Ag & Co | Mehrzahl von Linearantrieben |
-
1998
- 1998-04-29 FR FR9805399A patent/FR2778164B1/fr not_active Expired - Fee Related
-
1999
- 1999-04-16 ES ES99400927T patent/ES2190179T3/es not_active Expired - Lifetime
- 1999-04-16 EP EP99400927A patent/EP0953505B1/fr not_active Expired - Lifetime
- 1999-04-16 DE DE69904772T patent/DE69904772T2/de not_active Expired - Lifetime
- 1999-04-28 US US09/300,915 patent/US6241182B1/en not_active Expired - Lifetime
- 1999-04-28 CA CA002270753A patent/CA2270753C/fr not_active Expired - Fee Related
- 1999-04-30 JP JP12460799A patent/JP4180190B2/ja not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
CA2270753C (fr) | 2007-04-03 |
FR2778164B1 (fr) | 2000-06-23 |
US6241182B1 (en) | 2001-06-05 |
CA2270753A1 (fr) | 1999-10-29 |
EP0953505A1 (fr) | 1999-11-03 |
JPH11342898A (ja) | 1999-12-14 |
JP4180190B2 (ja) | 2008-11-12 |
DE69904772T2 (de) | 2003-11-06 |
DE69904772D1 (de) | 2003-02-13 |
FR2778164A1 (fr) | 1999-11-05 |
EP0953505B1 (fr) | 2003-01-08 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
ES2190179T3 (es) | Sistema de control mixto para superficie aerodinamica de una aeronave. | |
ES2055908T3 (es) | Dispositivo accionador de cierre electrico. | |
ES2050430T3 (es) | Dispositivo accionador para un elevalunas electrico. | |
ES2071514T3 (es) | Disposicion de accionamiento para un vehiculo automovil. | |
BR0316658A (pt) | Circuito de abastecimento de energia de um motor elétrico de alta velocidade | |
BR0016335A (pt) | Dispositivo autÈnomo de comando a distância, aparelho e instalação elétrica que comporta esse dispositivo | |
ES2183105T3 (es) | Sistema de mando electrico para inversor de empuje de turborreactor. | |
ES2098867T3 (es) | Disposicion generadora de energia electrica. | |
ATE375027T1 (de) | Stellantrieb mit einer fliehkraftbremse | |
ES2179440T3 (es) | Dispositivo de arranque para una turbina de gas en una aeronave. | |
BRPI0407590A (pt) | sistema de suprimento de energia para um automóvel | |
DE60200753D1 (de) | Flugverriegelungsstellantrieb mit zwei Energiequellen | |
BR9815337A (pt) | Sistema de suprimento de energia de um motor elétrico de comutação eletrônica para dispositivos de ar-condicionado a ser instalado dentro de veículos a motor | |
ATE110897T1 (de) | Vorrichtung zur stromversorgung einer mit magnetischen drucklagern versehenen vakuumpumpe mit einer notstromversorgung für die drucklager im falle eines stromausfalles im netz. | |
ES2125588T3 (es) | Disposicion de ajuste para una chapaleta de flujo de aire. | |
ES2083800T3 (es) | Dispositivo de control de la velocidad de un motor electrico y su procedimiento de funcionamiento. | |
ES2078223T3 (es) | Dispositivo para el ajuste de potencia para sistemas electricos de potencia, en particular para sistemas electricos en potencia con hornos electricos. | |
BR112022023717A2 (pt) | Sistema de alimentação de energia e método para controlar sistema de alimentação de energia | |
ES2160193T3 (es) | Unidad de accionamiento de vehiculo con metodo de control relacionado. | |
AR245901A1 (es) | Un mecanismo mejorado para posicionamiento de un miembro de salida. | |
WO2003029910A3 (de) | Verfahren zur erzeugung einer ausgangsspannung | |
CN203340360U (zh) | 一种新型led应急灯控制电路 | |
DE59807903D1 (de) | Luftkissenfahrzeug | |
ES2157840B1 (es) | Sistema alternativo para generar energia electrica. | |
US10312843B2 (en) | System including light emitting semiconductors for dissipating power |