GB1404762A - Electro-hydraulic actuating systems for aircraft control surfaces - Google Patents

Electro-hydraulic actuating systems for aircraft control surfaces

Info

Publication number
GB1404762A
GB1404762A GB4662671A GB4662671A GB1404762A GB 1404762 A GB1404762 A GB 1404762A GB 4662671 A GB4662671 A GB 4662671A GB 4662671 A GB4662671 A GB 4662671A GB 1404762 A GB1404762 A GB 1404762A
Authority
GB
United Kingdom
Prior art keywords
flaps
valve
inputs
comparators
switch
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
Application number
GB4662671A
Other languages
English (en)
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.)
ZF International UK Ltd
Original Assignee
Lucas Industries Ltd
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 Lucas Industries Ltd filed Critical Lucas Industries Ltd
Priority to GB4662671A priority Critical patent/GB1404762A/en
Priority to US00294785A priority patent/US3794276A/en
Priority to FR7235317A priority patent/FR2156070B1/fr
Priority to IT53192/72A priority patent/IT966206B/it
Priority to DE2249011A priority patent/DE2249011A1/de
Priority to JP47100336A priority patent/JPS4846099A/ja
Publication of GB1404762A publication Critical patent/GB1404762A/en
Expired legal-status Critical Current

Links

Classifications

    • 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
    • G05D1/0077—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots with safety arrangements using redundant signals or controls

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Automation & Control Theory (AREA)
  • Servomotors (AREA)
  • Control Of Position Or Direction (AREA)
  • Fluid-Pressure Circuits (AREA)
GB4662671A 1971-10-07 1971-10-07 Electro-hydraulic actuating systems for aircraft control surfaces Expired GB1404762A (en)

Priority Applications (6)

Application Number Priority Date Filing Date Title
GB4662671A GB1404762A (en) 1971-10-07 1971-10-07 Electro-hydraulic actuating systems for aircraft control surfaces
US00294785A US3794276A (en) 1971-10-07 1972-10-04 Electro-hydraulic actuating systems for aircraft control surfaces
FR7235317A FR2156070B1 (https=) 1971-10-07 1972-10-05
IT53192/72A IT966206B (it) 1971-10-07 1972-10-05 Dispositivo di azionamento delle superfici alari di controllo di un aeroplano
DE2249011A DE2249011A1 (de) 1971-10-07 1972-10-06 Elektrohydraulische betaetigungsanordnung fuer flugzeug-steuerflaechen
JP47100336A JPS4846099A (https=) 1971-10-07 1972-10-07

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB4662671A GB1404762A (en) 1971-10-07 1971-10-07 Electro-hydraulic actuating systems for aircraft control surfaces

Publications (1)

Publication Number Publication Date
GB1404762A true GB1404762A (en) 1975-09-03

Family

ID=10441980

Family Applications (1)

Application Number Title Priority Date Filing Date
GB4662671A Expired GB1404762A (en) 1971-10-07 1971-10-07 Electro-hydraulic actuating systems for aircraft control surfaces

Country Status (6)

Country Link
US (1) US3794276A (https=)
JP (1) JPS4846099A (https=)
DE (1) DE2249011A1 (https=)
FR (1) FR2156070B1 (https=)
GB (1) GB1404762A (https=)
IT (1) IT966206B (https=)

Families Citing this family (31)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5074495A (en) * 1987-12-29 1991-12-24 The Boeing Company Load-adaptive hybrid actuator system and method for actuating control surfaces
US5686907A (en) * 1995-05-15 1997-11-11 The Boeing Company Skew and loss detection system for individual high lift devices
USRE44313E1 (en) 1996-10-22 2013-06-25 The Boeing Company Airplane with unswept slotted cruise wing airfoil
RU2158855C2 (ru) * 1999-01-18 2000-11-10 Открытое акционерное общество "Павловский машиностроительный завод ВОСХОД" Насосно-аккумуляторный гидропривод
RU2157503C1 (ru) * 1999-09-28 2000-10-10 Государственное унитарное предприятие "Конструкторское бюро приборостроения" Электропневматический рулевой привод управляемого снаряда
US6439512B1 (en) 2000-08-24 2002-08-27 Hr Textron, Inc. All-hydraulic powered horizontal stabilizer trim control surface position control system
US7258308B2 (en) * 2002-07-02 2007-08-21 The Boeing Company Method and apparatus for controlling airflow with a gapped trailing edge device having a flexible flow surface
US7243881B2 (en) 2003-06-03 2007-07-17 The Boeing Company Multi-function trailing edge devices and associated methods
US7059563B2 (en) * 2003-06-03 2006-06-13 The Boeing Company Systems, apparatuses, and methods for moving aircraft control surfaces
US6799739B1 (en) 2003-11-24 2004-10-05 The Boeing Company Aircraft control surface drive system and associated methods
US7424350B2 (en) * 2004-02-02 2008-09-09 The Boeing Company Vehicle control systems and corresponding sizing methods
US7357358B2 (en) * 2004-02-27 2008-04-15 The Boeing Company Aircraft leading edge device systems and corresponding sizing methods
US7270305B2 (en) * 2004-06-15 2007-09-18 The Boeing Company Aircraft leading edge apparatuses and corresponding methods
US6978971B1 (en) * 2004-06-15 2005-12-27 The Boeing Company Methods and apparatuses for controlling airflow proximate to engine/airfoil systems
RU2276771C2 (ru) * 2004-07-23 2006-05-20 Государственное унитарное предприятие "Конструкторское бюро приборостроения" Блок рулевого привода управляемого снаряда
US7494094B2 (en) * 2004-09-08 2009-02-24 The Boeing Company Aircraft wing systems for providing differential motion to deployable lift devices
US7264206B2 (en) * 2004-09-30 2007-09-04 The Boeing Company Leading edge flap apparatuses and associated methods
US7322547B2 (en) * 2005-01-31 2008-01-29 The Boeing Company Aerospace vehicle leading edge slat devices and corresponding methods
US7338018B2 (en) * 2005-02-04 2008-03-04 The Boeing Company Systems and methods for controlling aircraft flaps and spoilers
US7309043B2 (en) * 2005-04-27 2007-12-18 The Boeing Company Actuation device positioning systems and associated methods, including aircraft spoiler droop systems
US7300021B2 (en) * 2005-05-20 2007-11-27 The Boeing Company Aerospace vehicle fairing systems and associated methods
US7721999B2 (en) * 2005-05-20 2010-05-25 The Boeing Company Aerospace vehicle fairing systems and associated methods
US7367530B2 (en) * 2005-06-21 2008-05-06 The Boeing Company Aerospace vehicle yaw generating systems and associated methods
US7500641B2 (en) * 2005-08-10 2009-03-10 The Boeing Company Aerospace vehicle flow body systems and associated methods
US7611099B2 (en) * 2005-09-07 2009-11-03 The Boeing Company Seal assemblies for use with drooped spoilers and other control surfaces on aircraft
US7708231B2 (en) 2005-11-21 2010-05-04 The Boeing Company Aircraft trailing edge devices, including devices having forwardly positioned hinge lines, and associated methods
US7475854B2 (en) * 2005-11-21 2009-01-13 The Boeing Company Aircraft trailing edge devices, including devices with non-parallel motion paths, and associated methods
US7578484B2 (en) * 2006-06-14 2009-08-25 The Boeing Company Link mechanisms for gapped rigid krueger flaps, and associated systems and methods
US7954769B2 (en) 2007-12-10 2011-06-07 The Boeing Company Deployable aerodynamic devices with reduced actuator loads, and related systems and methods
US7766282B2 (en) * 2007-12-11 2010-08-03 The Boeing Company Trailing edge device catchers and associated systems and methods
US8382045B2 (en) * 2009-07-21 2013-02-26 The Boeing Company Shape-changing control surface

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2413907A (en) * 1944-09-30 1947-01-07 Adel Prec Products Corp Electrohydraulic position control system
GB612309A (en) * 1945-03-16 1948-11-11 Bristol Aeroplane Co Ltd Improvements in or relating to apparatus for actuating the control surfaces of aircraft
US2744698A (en) * 1949-03-11 1956-05-08 Baynes Aircraft Interiors Ltd High speed aircraft wing and tail surfaces having variable sweepback
GB917808A (en) * 1960-05-12 1963-02-06 Fairey Eng Improvements relating to servo systems
US3129645A (en) * 1962-05-02 1964-04-21 Double A Prod Co Electrically modulated fluid valve
US3247498A (en) * 1962-08-23 1966-04-19 Bendix Corp Worst condition indicating system
US3454849A (en) * 1965-04-01 1969-07-08 Bendix Corp Monitoring and testing system for a fail operative control system of an aircraft
GB1137490A (en) * 1965-06-30 1968-12-18 Elliott Brothers London Ltd Improvements in and relating to the monitoring of control systems
US3338139A (en) * 1965-12-23 1967-08-29 Bell Aerospace Corp Redundant control system
US3426650A (en) * 1965-12-23 1969-02-11 Bell Aerospace Corp Triple channel redundant hydraeric control system
US3603534A (en) * 1968-08-10 1971-09-07 Elliott Brothers London Ltd Synchronized power control

Also Published As

Publication number Publication date
DE2249011A1 (de) 1973-04-12
JPS4846099A (https=) 1973-06-30
FR2156070A1 (https=) 1973-05-25
IT966206B (it) 1974-02-11
FR2156070B1 (https=) 1975-03-14
US3794276A (en) 1974-02-26

Similar Documents

Publication Publication Date Title
GB1404762A (en) Electro-hydraulic actuating systems for aircraft control surfaces
EP0288034A3 (en) Flight control system employing three controllers operating a dual actuator
GB1515152A (en) Hydraulic control apparatus
EP0178819B1 (en) Electro-hydraulic actuator systems
GB1462879A (en) Hydraulic actuator controls
GB1098194A (en) Improvements in position control servo systems
IE43870B1 (en) Adaptive control system using position feedback
GB1462223A (en) Servovalve apparatus
GB1368347A (en) Control flap arrangement for aircraft
GB1173554A (en) Improvements in and relating to Servomechanism Systems.
GB1221451A (en) An actuator for operating aerodynamic devices, more especially spoilers, in aircraft
GB1131017A (en) Improvements relating to multiple channel servo systems
GB1273806A (en) Improvements in or relating to the control of water turbines
GB1131669A (en) Redundant control system
GB1292162A (en) Improvements in and relating to the electro-hydraulic remote control of hydraulic multi-position valves
US3034483A (en) Hydraulic servomotor
US3122972A (en) rasmussen
US3390615A (en) Hydraulic servo valve having uniform response to input signals independent of magnitude and direction of load
GB1408126A (en) Arrangement for monitoring and controlling a redundant hydraulic adjusting drive
GB1481409A (en) Monitor systems
GB1137490A (en) Improvements in and relating to the monitoring of control systems
GB1411002A (en) Ships rudder control systems
US3742324A (en) Control mode switching system for a servomechanism
GB1089470A (en) System for controlling hydraulic servo motors
GB2038511A (en) Servo control valve

Legal Events

Date Code Title Description
PS Patent sealed [section 19, patents act 1949]
PCNP Patent ceased through non-payment of renewal fee