ES2137641T3 - Procedimiento y dispositivo de comando del timon de direccion de una aeronave. - Google Patents
Procedimiento y dispositivo de comando del timon de direccion de una aeronave.Info
- Publication number
- ES2137641T3 ES2137641T3 ES96401948T ES96401948T ES2137641T3 ES 2137641 T3 ES2137641 T3 ES 2137641T3 ES 96401948 T ES96401948 T ES 96401948T ES 96401948 T ES96401948 T ES 96401948T ES 2137641 T3 ES2137641 T3 ES 2137641T3
- Authority
- ES
- Spain
- Prior art keywords
- aircraft
- procedure
- command device
- servocontrols
- corresponds
- 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
- 241000380131 Ammophila arenaria Species 0.000 abstract 1
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
- B64C13/40—Transmitting means with power amplification using fluid pressure
- B64C13/42—Transmitting means with power amplification using fluid pressure having duplication or stand-by provisions
-
- 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
- B64C13/504—Transmitting means with power amplification using electrical energy using electro-hydrostatic actuators [EHA's]
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
- G05D1/0055—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots with safety arrangements
-
- 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)
- Aviation & Aerospace Engineering (AREA)
- Automation & Control Theory (AREA)
- Physics & Mathematics (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- General Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Fluid-Pressure Circuits (AREA)
- Safety Devices In Control Systems (AREA)
Abstract
DISPOSITIVO DE CONTROL DEL TIMON (116) DE DIRECCION DE UNA AERONAVE. EL DISPOSITIVO LLEVA AL MENOS DOS SERVOCONTROLES (110, 112, 114( QUE TIENEN CADA UNO AL MENOS UNA ENTRADA DE CONTROL ELECTRICO (111A, 113A, 115A). AL MENOS UNO DE LOS SERVOCONTROLES (115), LLAMADO SERVO CONTROL MIXTO, LLEVA ADEMAS UNA ENTRADA DE CONTROL MECANICO (115B), Y UN SISTEMA DE CONDUCCION ELECTRICO DE LOS SERVOCONTROLES ES APTO PARA OCUPAR UN ESTADO QUE CORRESPONDE A UNA AVERIA DE UN PROPULSOR EN EL QUE AL MENOS DOS DE LOS SERVOCONTROLES ACCIONAN SIMULTANEAMENTE EL TIMON (116), Y UN ESTADO QUE CORRESPONDE A UNA AVERIA ELECTRICA, EN EL QUE, EL SERVOCONTROL MIXTO (115), ACCIONA EL TIMON CONTROLADO A PARTIR DE LA ENTRADA DE CONTROL MECANICO.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR9510847A FR2738796B1 (fr) | 1995-09-15 | 1995-09-15 | Procede et dispositif de commande de la gouverne de direction d'un aeronef |
Publications (1)
Publication Number | Publication Date |
---|---|
ES2137641T3 true ES2137641T3 (es) | 1999-12-16 |
Family
ID=9482597
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
ES96401948T Expired - Lifetime ES2137641T3 (es) | 1995-09-15 | 1996-09-12 | Procedimiento y dispositivo de comando del timon de direccion de una aeronave. |
Country Status (7)
Country | Link |
---|---|
US (1) | US5791596A (es) |
EP (1) | EP0763465B1 (es) |
CN (1) | CN1066405C (es) |
CA (1) | CA2185299C (es) |
DE (1) | DE69603807T2 (es) |
ES (1) | ES2137641T3 (es) |
FR (1) | FR2738796B1 (es) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
ES2174725A1 (es) * | 2000-09-20 | 2002-11-01 | Univ De A Coruna | Servo-posicionador de aleron realimentado por par de carga. |
Families Citing this family (37)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6206329B1 (en) * | 1995-09-15 | 2001-03-27 | Jean-Pierre Gautier | Process and device for the control of the rudder of an aircraft |
FR2760718B1 (fr) * | 1997-03-14 | 1999-05-28 | Aerospatiale | Procede et dispositif de commande d'une gouverne d'inclinaison ou de profondeur d'un aeronef |
FR2768697B1 (fr) | 1997-09-24 | 1999-12-03 | Aerospatiale | Dispositif et procede de commande de gouvernes d'aeronef |
FR2789500B1 (fr) * | 1999-02-04 | 2001-03-30 | Aerospatiale | Systeme pour la commande en lacet d'un aeronef |
JP3195918B2 (ja) * | 1999-03-12 | 2001-08-06 | 株式会社コミュータヘリコプタ先進技術研究所 | ヘリコプタ用飛行制御装置 |
US6572055B1 (en) | 1999-08-10 | 2003-06-03 | Bombardier Aerospace Corporation | Hydrostatic sidestick coupling |
US6586901B1 (en) | 2000-06-21 | 2003-07-01 | Honeywell International Inc. | Methods and apparatus suitable for facilitating control of an aircraft rudder |
GB0120747D0 (en) * | 2001-08-25 | 2001-10-17 | Lucas Western Inc | Control method |
JP3836422B2 (ja) * | 2002-11-27 | 2006-10-25 | ナブテスコ株式会社 | 翼駆動装置 |
US7229046B2 (en) * | 2005-10-25 | 2007-06-12 | Durant Cecil John | Servo mounting system for direct drive of an aircraft control surface |
FR2892699B1 (fr) * | 2005-10-27 | 2008-02-08 | Airbus France Sas | Procede et systeme de limitation d'un angle de braquage de la gouverne d'un aeronef |
FR2897838B1 (fr) * | 2006-02-27 | 2009-01-09 | Airbus France Sas | Systeme de commande electrique pour une gouverne de direction d'un avion. |
US9340278B2 (en) | 2006-05-17 | 2016-05-17 | Textron Innovations, Inc. | Flight control system |
US8725321B2 (en) * | 2006-05-17 | 2014-05-13 | Textron Innovations Inc. | Flight control system |
DE102007057023A1 (de) * | 2006-12-18 | 2008-06-19 | Sauer-Danfoss Aps | Aktuatorregelungssystem |
US20100089053A1 (en) * | 2008-10-13 | 2010-04-15 | Honeywell International Inc. | Hybrid electromechanical/hydro-mechanical actuation control system |
DE102010051216A1 (de) | 2010-11-12 | 2012-05-16 | Airbus Operations Gmbh | Seitenrudersystem an einem Flugzeug |
JP5711543B2 (ja) * | 2011-01-18 | 2015-05-07 | ナブテスコ株式会社 | 油圧アクチュエータシステム |
CN103702902B (zh) * | 2011-07-26 | 2015-12-02 | 里尔喷射机公司 | 方向舵偏置增益变换器 |
KR101842235B1 (ko) | 2012-02-09 | 2018-03-27 | 무그 인코포레이티드 | 액츄에이터 시스템 및 방법 |
CN103303466B (zh) * | 2012-03-09 | 2016-03-30 | 陕西飞机工业(集团)有限公司 | 一种飞机舵面锁防差错电气控制方法及其系统 |
CN103303465A (zh) * | 2012-03-09 | 2013-09-18 | 陕西飞机工业(集团)有限公司 | 一种飞机方向舵调整片偏角限制装置电气控制方法及其系统 |
CN103661922B (zh) * | 2012-08-31 | 2016-08-31 | 北京精密机电控制设备研究所 | 一种伺服机构用电燃气混合动力装置 |
CN103670801A (zh) * | 2012-09-07 | 2014-03-26 | 北京精密机电控制设备研究所 | 一种液氧煤油发动机推力矢量控制用多余度泵控伺服机构 |
US10180699B1 (en) | 2013-08-08 | 2019-01-15 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | System, apparatus and method for pedal control |
US9586675B2 (en) * | 2014-06-09 | 2017-03-07 | The Boeing Company | Apparatus and method for arrestment of a flight control surface |
CN104554711B (zh) * | 2014-09-12 | 2017-05-17 | 北京精密机电控制设备研究所 | 用于控制飞行器空气舵负载摆角的空气动力控制伺服系统 |
CN104527969B (zh) * | 2014-11-19 | 2018-04-13 | 中国航空工业集团公司沈阳飞机设计研究所 | 一种飞机前翼伺服作动系统及其伺服控制方法 |
CN104615140A (zh) * | 2015-02-17 | 2015-05-13 | 北京精密机电控制设备研究所 | 空气动力控制用机电伺服系统 |
CN105545851B (zh) * | 2015-12-21 | 2017-07-07 | 中国航空工业集团公司金城南京机电液压工程研究中心 | 一种适用于水上飞机的水舵操纵油路结构 |
WO2017123987A1 (en) | 2016-01-13 | 2017-07-20 | Moog Inc. | Summing and fault tolerant rotary actuator assembly |
US10318904B2 (en) | 2016-05-06 | 2019-06-11 | General Electric Company | Computing system to control the use of physical state attainment of assets to meet temporal performance criteria |
US10088006B2 (en) * | 2016-05-19 | 2018-10-02 | The Boeing Company | Rotational inerter and method for damping an actuator |
IT201700011606A1 (it) * | 2017-02-02 | 2018-08-02 | In & Tec Srl | Sistema di apertura / chiusura automatica mediante una porta, anta o similare di tipo scorrevole |
CN109250125B (zh) * | 2018-10-16 | 2022-04-26 | 太原理工大学 | 一种混合驱动的飞机作动系统 |
US11591074B1 (en) * | 2018-11-28 | 2023-02-28 | Zunum Aero, Inc. | System and methods for designing and building regional hybrid-to-electric systems and methods for designing and optimizing regional hybrid-to-electric aircraft |
CN112173073B (zh) * | 2020-09-25 | 2023-05-26 | 中国直升机设计研究所 | 一种单舵机控制双垂尾操纵结构 |
Family Cites Families (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE3151623A1 (de) * | 1981-12-28 | 1983-07-07 | Vereinigte Flugtechnische Werke Gmbh, 2800 Bremen | Steuereinrichtung zum einstellen von steuerflaechen fuer luftfahrzeuge |
FR2603866A1 (fr) * | 1986-09-12 | 1988-03-18 | Messerschmitt Boelkow Blohm | Systeme de commande de gouvernes de profondeur |
DE3638821A1 (de) * | 1986-09-12 | 1988-03-24 | Messerschmitt Boelkow Blohm | Hoehenruder-steuerungssystem |
DE3638820A1 (de) * | 1986-09-12 | 1988-03-24 | Messerschmitt Boelkow Blohm | Seitenruder-steuerungsanordnung fuer luftfahrzeuge |
JPS6441498A (en) * | 1987-08-07 | 1989-02-13 | Teijin Seiki Co Ltd | Controller for rudder surface |
-
1995
- 1995-09-15 FR FR9510847A patent/FR2738796B1/fr not_active Expired - Fee Related
-
1996
- 1996-09-05 US US08/708,698 patent/US5791596A/en not_active Expired - Lifetime
- 1996-09-11 CA CA002185299A patent/CA2185299C/en not_active Expired - Fee Related
- 1996-09-12 ES ES96401948T patent/ES2137641T3/es not_active Expired - Lifetime
- 1996-09-12 DE DE69603807T patent/DE69603807T2/de not_active Expired - Lifetime
- 1996-09-12 EP EP96401948A patent/EP0763465B1/fr not_active Expired - Lifetime
- 1996-09-14 CN CN96122729A patent/CN1066405C/zh not_active Expired - Fee Related
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
ES2174725A1 (es) * | 2000-09-20 | 2002-11-01 | Univ De A Coruna | Servo-posicionador de aleron realimentado por par de carga. |
Also Published As
Publication number | Publication date |
---|---|
CA2185299A1 (en) | 1997-03-16 |
EP0763465B1 (fr) | 1999-08-18 |
CN1066405C (zh) | 2001-05-30 |
DE69603807T2 (de) | 2000-04-20 |
EP0763465A1 (fr) | 1997-03-19 |
CA2185299C (en) | 2007-12-18 |
US5791596A (en) | 1998-08-11 |
DE69603807D1 (de) | 1999-09-23 |
FR2738796B1 (fr) | 1997-12-05 |
FR2738796A1 (fr) | 1997-03-21 |
CN1154325A (zh) | 1997-07-16 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
FG2A | Definitive protection |
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