ES2165001T3 - Sistema para el mando de un aleron compensador para el timon de aeronave. - Google Patents

Sistema para el mando de un aleron compensador para el timon de aeronave.

Info

Publication number
ES2165001T3
ES2165001T3 ES97400980T ES97400980T ES2165001T3 ES 2165001 T3 ES2165001 T3 ES 2165001T3 ES 97400980 T ES97400980 T ES 97400980T ES 97400980 T ES97400980 T ES 97400980T ES 2165001 T3 ES2165001 T3 ES 2165001T3
Authority
ES
Spain
Prior art keywords
control
timon
aircraft
aleron
compensator
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
Application number
ES97400980T
Other languages
English (en)
Inventor
Michel Durandeau
Etienne Foch
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Aerospatiale Matra
Original Assignee
Aerospatiale Matra
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Aerospatiale Matra filed Critical Aerospatiale Matra
Application granted granted Critical
Publication of ES2165001T3 publication Critical patent/ES2165001T3/es
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/10—Adjustable control surfaces or members, e.g. rudders one surface adjusted by movement of another, e.g. servo tabs

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Mechanical Control Devices (AREA)
  • Transmission Devices (AREA)
  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)

Abstract

SEGUN LA INVENCION, LOS DETECTORES DE POSICION (12 Y 15) PROPORCIONAN INFORMACION ACERCA DEL TIMON (3) Y ACERCA DE LA POSICION DEL GATO (13) RESPECTIVAMENTE, Y EL DISPOSITIVO DE CONTROL ELABORA, A PARTIR DE LAS SEÑALES GENERADAS POR DICHOS DETECTORES (12 Y 15) ASI COMO EVENTUALMENTE A PARTIR DE AL MENOS UN PARAMETRO (P) PROCEDENTE DEL AERONAVE (VELOCIDAD DEL AIRE, POSICIONES DE LOS DISPOSITIVOS HIPERSUSTENTADORES, ESFUERZOS EJERCIDOS POR EL PILOTO SOBRE EL ORGANO DE CONTROL (1),...), UNA ORDEN DE CONTROL PARA DICHO GATO (1-3).
ES97400980T 1996-05-17 1997-04-30 Sistema para el mando de un aleron compensador para el timon de aeronave. Expired - Lifetime ES2165001T3 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR9606144A FR2748720B1 (fr) 1996-05-17 1996-05-17 Systeme pour la commande d'un volet compensateur de gouverne d'aeronef

Publications (1)

Publication Number Publication Date
ES2165001T3 true ES2165001T3 (es) 2002-03-01

Family

ID=9492219

Family Applications (1)

Application Number Title Priority Date Filing Date
ES97400980T Expired - Lifetime ES2165001T3 (es) 1996-05-17 1997-04-30 Sistema para el mando de un aleron compensador para el timon de aeronave.

Country Status (9)

Country Link
US (1) US5913492A (es)
EP (1) EP0807573B1 (es)
CN (1) CN1080226C (es)
BR (1) BR9702390A (es)
CA (1) CA2204445C (es)
DE (1) DE69707196T2 (es)
ES (1) ES2165001T3 (es)
FR (1) FR2748720B1 (es)
ID (1) ID16899A (es)

Families Citing this family (36)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
SE508672C2 (sv) * 1997-12-30 1998-10-26 Saab Ab Anordning och metod för styrkraftreglering vid ett mekaniskt styrsystem för ett flygplan
US6257528B1 (en) * 1999-07-20 2001-07-10 The Boeing Company Vehicle control system and method employing control surface and geared tab
GB9918289D0 (en) * 1999-08-03 2000-05-24 British Aerospace Actuator system for aerospace controls and functions
US7424988B2 (en) * 2001-05-24 2008-09-16 Mcdonnell Helicopter Company Llc Use of aerodynamic forces to assist in the control and positioning of aircraft control surfaces and variable geometry systems
US6672540B1 (en) 2002-12-03 2004-01-06 Rockwell Collins, Inc. Actuator for aircraft stabilizers with a failure responsive lock control mechanism
US7182297B2 (en) * 2003-01-17 2007-02-27 The Insitu Group, Inc. Method and apparatus for supporting aircraft components, including actuators
US6827311B2 (en) * 2003-04-07 2004-12-07 Honeywell International, Inc. Flight control actuation system
US7770842B2 (en) * 2004-08-24 2010-08-10 Honeywell International Inc. Aircraft flight control surface actuation system communication architecture
US7549605B2 (en) * 2005-06-27 2009-06-23 Honeywell International Inc. Electric flight control surface actuation system for aircraft flaps and slats
US20070007385A1 (en) * 2005-06-27 2007-01-11 Honeywell International, Inc. Electric flight control surface actuation system electronic architecture
US20080237402A1 (en) * 2005-12-19 2008-10-02 Marc Ausman Aircraft trim safety system and backup controls
US8340842B2 (en) 2005-12-19 2012-12-25 Vertical Power, Inc. Aircraft emergency handling
US7622818B2 (en) * 2005-12-19 2009-11-24 Vertical Power, Inc. Backup electrical power system for solid-state aircraft power distribution systems
US8346409B2 (en) 2005-12-19 2013-01-01 Vertical Power, Inc. Variable speed flap retraction and notification
US7796054B2 (en) * 2005-12-19 2010-09-14 Vertical Power, Inc. Aircraft electrical system evaluation
US20070142980A1 (en) * 2005-12-19 2007-06-21 Marc Ausman Avionics method and apparatus
US8103393B2 (en) * 2005-12-19 2012-01-24 Vertical Power, Inc. Aircraft exhaust gas temperature monitor
US7883059B2 (en) * 2007-05-17 2011-02-08 Insitu, Inc. Actuator systems and associated methods for unmanned air vehicles and other applications
US8876063B2 (en) * 2007-12-10 2014-11-04 The Boeing Company Flight control using multiple actuators on primary control surfaces with tabs
FR2927308B1 (fr) * 2008-02-08 2010-10-22 Airbus France Systeme distribue de commande de vol.
US7973533B2 (en) 2008-02-27 2011-07-05 Vertical Power, Inc. In-circuit testing for integrity of solid-state switches
DE102008022092A1 (de) * 2008-05-05 2009-11-19 Airbus Deutschland Gmbh Fehlertolerantes Stellsystem zur Verstellung von Klappen eines Flugzeugs mit einer Verstell-Kinematik mit feststehender Drehachse
DE102008034444B4 (de) * 2008-05-14 2013-09-05 Diehl Aerospace Gmbh Eingabesystem für eine Landeklappensteuerung eines Flugzeugs
US8235327B2 (en) 2009-03-18 2012-08-07 Insitu, Inc. Adjustable servomechanism assemblies and associated systems and methods
DE102009002435A1 (de) * 2009-04-16 2010-10-21 Airbus Deutschland Gmbh Hochauftriebssystem für ein Flugzeug und Verfahren zum Detektieren von Fehlern in einem Hochauftriebssystem für ein Flugzeug
WO2013120031A1 (en) * 2012-02-10 2013-08-15 Merlin Technology, Inc. Autopilot control arrangement and methods
CN103043209B (zh) * 2012-12-11 2016-04-20 江西洪都航空工业集团有限责任公司 一种农林飞机升降舵配平机构
US9180961B2 (en) * 2013-01-28 2015-11-10 The Boeing Company Control surface for creating variable camber along a wing
EP2805879B1 (en) * 2013-05-22 2017-07-05 Airbus Operations GmbH Flap arrangement for a wing of an aircraft and an aircraft with a wing comprising such a flap arrangement
CN104648657A (zh) * 2013-11-22 2015-05-27 中国航空工业集团公司西安飞机设计研究所 一种可抑制振动的带调整片操纵面
CN103761899B (zh) * 2013-12-31 2017-01-11 中国人民解放军空军航空大学军事仿真技术研究所 飞行模拟器可逆式操纵负荷系统力感仿真方法
CN106184715B (zh) * 2015-04-29 2018-07-24 陕西飞机工业（集团）有限公司 一种飞机驾驶杆配平系统
CN106184713B (zh) * 2015-04-29 2018-07-24 陕西飞机工业（集团）有限公司 一种飞机升降舵调整片自动配平方法
CA3022226A1 (en) * 2016-04-25 2017-11-02 Bombardier Inc. Aircraft pitch control system with electronically geared elevator
CN109747813B (zh) * 2017-11-07 2021-09-28 中国科学院沈阳自动化研究所 一种大载荷无人机尾翼驱动系统
CN110450940B (zh) * 2019-06-24 2022-09-20 陕西飞机工业（集团）有限公司 一种飞机的升降舵配平控制电路

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2383779A (en) * 1942-05-14 1945-08-28 Bell Aircraft Corp Aircraft control means
US2563757A (en) * 1945-07-23 1951-08-07 Lockheed Aircraft Corp All-movable horizontal tail
US2568719A (en) * 1947-04-09 1951-09-25 Sperry Corp Control system for aircraft control surface and tab
US2577439A (en) * 1947-10-18 1951-12-04 Curtiss Wright Corp Differential spring balance tab
US2640665A (en) * 1948-06-02 1953-06-02 Cons Vultee Aircraft Corp Aircraft trim tab control
FR1015687A (fr) * 1949-03-04 1952-10-17 A V Roe Canada Ltd Dispositif de commande d'aéronefs en vol
US2557426A (en) * 1950-01-13 1951-06-19 Lockheed Aircraft Corp Tab actuating mechanism
US2719684A (en) * 1951-09-04 1955-10-04 North American Aviation Inc Aircraft control
US2817483A (en) * 1951-10-17 1957-12-24 Glenn L Martin Co Aircraft control force modifier
US2721716A (en) * 1952-03-31 1955-10-25 Beadle John Charles William Collapsible parachute
US3149272A (en) * 1962-04-10 1964-09-15 Sperry Rand Corp Discriminating safety monitor for servo systems
US4595458A (en) * 1985-05-17 1986-06-17 Olin Corporation Process for using selected fatty acid adducts of a 1,2,4-triazole as sizing or waterproofing agents for cellulosic materials
FR2600035B1 (fr) * 1986-06-16 1988-10-21 Aerospatiale Systeme pour la commande d'une surface aerodynamique mobile d'un aeronef.

Also Published As

Publication number Publication date
DE69707196D1 (de) 2001-11-15
CA2204445C (fr) 2005-07-05
CN1176208A (zh) 1998-03-18
DE69707196T2 (de) 2002-05-29
ID16899A (id) 1997-11-20
EP0807573A1 (fr) 1997-11-19
CA2204445A1 (fr) 1997-11-17
FR2748720A1 (fr) 1997-11-21
US5913492A (en) 1999-06-22
BR9702390A (pt) 1998-09-01
CN1080226C (zh) 2002-03-06
FR2748720B1 (fr) 1998-07-24
EP0807573B1 (fr) 2001-10-10

Similar Documents

Publication Publication Date Title
ES2165001T3 (es) Sistema para el mando de un aleron compensador para el timon de aeronave.
ES2099391T3 (es) Procedimiento y dispositivo para evitar las colisiones de aeronaves con el suelo.
DE602007009419D1 (de) G des fluges von drachen
HK1071120A1 (en) Device to create a temporary working space for elevators
GT200100007A (es) Antagonistas del factor liberador de corticotropina.
BRPI0515693A (pt) método de escape para uma aeronave, sistema de escape para uma aeronave e aeronave
DE59911450D1 (de) Integration eines Feldleitgerätes in ein Anlagenleitsystem
DE59908311D1 (de) Beleuchtungsanlage, z.b. flughafen- oder strassenbefeuerungsanlage
ES2152102T3 (es) Sistema y metodo para controlar cajas de cambios servocontroladas en vehiculos.
ES2110517T3 (es) Coordinacion de viraje a baja velocidad para helicoptero.
ES2146565T1 (es) Volante de direccion ventilado.
SE8104100L (sv) Luftplattformsanordning
AU2003299402A1 (en) Portable helicopter landing area and use method thereof
DE69902147D1 (de) Luftfedervorrichtung
ATE505757T1 (de) Flugkontrollsystem
SE9803896L (sv) Manipulator samt förfaranden vid framställning och igpngsättning av en manipulator
IT8025428A0 (it) Sistema di controllo di carico ciclico per turbina a gas.
ES2139143T3 (es) Gel micro-mesoporoso y procedimiento para su preparacion.
BR0304101A (pt) Método/sistema de controle de taxa de rampa de aceleração para um veìculo
ITVI20040192A1 (it) Sistema integrato di sicurezza del traffico, particolarmente in condizioni di scarsa visibilita', e metodo d'uso di tale sistema
AR110338A1 (es) Procedimiento para operar una instalación de funicular e instalación de funicular para realizar este procedimiento operativo
DE602004000754D1 (de) Auf dem coanda Effekt basierende Luftverteilungsvorrichtung
ES2082248T3 (es) Dispositivo de ventilacion.
DE50205991D1 (de) Wurfsystem für einen Gefechtskopf mit einer Richtvorrichtung zur Neutralisierung von Minen
ATE312320T1 (de) Lüftungsvorrichtung und damit ausgerüstetes lüftungssystem

Legal Events

Date Code Title Description
FG2A Definitive protection

Ref document number: 807573

Country of ref document: ES