DE2135366C2 - Steuereinrichtung zum Einstellen eines Steuerelementes in Abhängigkeit von elektrischen Steuersignalen - Google Patents

Steuereinrichtung zum Einstellen eines Steuerelementes in Abhängigkeit von elektrischen Steuersignalen

Info

Publication number
DE2135366C2
DE2135366C2 DE2135366A DE2135366A DE2135366C2 DE 2135366 C2 DE2135366 C2 DE 2135366C2 DE 2135366 A DE2135366 A DE 2135366A DE 2135366 A DE2135366 A DE 2135366A DE 2135366 C2 DE2135366 C2 DE 2135366C2
Authority
DE
Germany
Prior art keywords
signals
control
transducers
gates
control device
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
DE2135366A
Other languages
German (de)
English (en)
Other versions
DE2135366A1 (de
Inventor
William Guy Dallas Tex. Redmond jun.
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.)
LTV ELECTROSYSTEMS Inc DALLAS TEX US
Original Assignee
LTV ELECTROSYSTEMS Inc DALLAS TEX US
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 LTV ELECTROSYSTEMS Inc DALLAS TEX US filed Critical LTV ELECTROSYSTEMS Inc DALLAS TEX US
Publication of DE2135366A1 publication Critical patent/DE2135366A1/de
Application granted granted Critical
Publication of DE2135366C2 publication Critical patent/DE2135366C2/de
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)
  • Safety Devices In Control Systems (AREA)
  • Fluid-Pressure Circuits (AREA)
DE2135366A 1970-07-20 1971-07-15 Steuereinrichtung zum Einstellen eines Steuerelementes in Abhängigkeit von elektrischen Steuersignalen Expired DE2135366C2 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US5655170A 1970-07-20 1970-07-20

Publications (2)

Publication Number Publication Date
DE2135366A1 DE2135366A1 (de) 1972-02-03
DE2135366C2 true DE2135366C2 (de) 1982-04-01

Family

ID=22005144

Family Applications (1)

Application Number Title Priority Date Filing Date
DE2135366A Expired DE2135366C2 (de) 1970-07-20 1971-07-15 Steuereinrichtung zum Einstellen eines Steuerelementes in Abhängigkeit von elektrischen Steuersignalen

Country Status (4)

Country Link
US (1) US3679156A (enExample)
DE (1) DE2135366C2 (enExample)
FR (1) FR2099479B1 (enExample)
GB (1) GB1328592A (enExample)

Families Citing this family (26)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1488667A (en) * 1973-12-07 1977-10-12 Lucas Industries Ltd Actuating arrangement for aircraft control surfaces
US4270809A (en) * 1978-05-12 1981-06-02 Honda Giken Kogyo Kabushiki Kaisha Device for diagnosing trouble in a control circuit for electromagnetic actuators
GB2026705A (en) * 1978-07-21 1980-02-06 Honda Motor Co Ltd Monitoring control circuit operation
GB2095002B (en) * 1980-09-02 1985-02-27 Rockwell International Corp Actuator system for a control surface of an aircraft
US4466597A (en) * 1981-12-02 1984-08-21 Pneumo Corporation Electro-mechanical direct drive valve servo system with rotary to linear valve drive mechanism
DE3462866D1 (en) * 1984-01-09 1987-05-07 Aerospatiale Aircraft flight control system
FR2557854B1 (fr) * 1984-01-09 1987-01-23 Aerospatiale Systeme de commandes de vol pour aeronef
FR2557853B1 (fr) * 1984-01-09 1986-04-25 Aerospatiale Systeme de commandes de vol pour aeronef
US5074495A (en) * 1987-12-29 1991-12-24 The Boeing Company Load-adaptive hybrid actuator system and method for actuating control surfaces
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
US5182505A (en) * 1991-06-19 1993-01-26 Honeywell Inc. Aircraft control surface position transducer
FR2683502B1 (fr) * 1991-11-12 1994-02-25 Aerospatiale Ste Nationale Indle Systeme pour la commande en mouvement d'un organe mecanique mobile, et un systeme de commandes de vol pour aeronef le comportant.
US5493497A (en) * 1992-06-03 1996-02-20 The Boeing Company Multiaxis redundant fly-by-wire primary flight control system
US5670856A (en) * 1994-11-07 1997-09-23 Alliedsignal Inc. Fault tolerant controller arrangement for electric motor driven apparatus
US5678786A (en) * 1995-12-06 1997-10-21 Mcdonnell Douglas Helicopter Co. Reconfigurable helicopter flight control system
DE19628395C2 (de) * 1996-07-13 1998-06-04 Daimler Benz Aerospace Airbus System zur Regelung der Abluftmengenströme eines Flugzeuges
US5806805A (en) * 1996-08-07 1998-09-15 The Boeing Company Fault tolerant actuation system for flight control actuators
US6209825B1 (en) 1998-02-27 2001-04-03 Lockheed Martin Corporation Low power loss electro hydraulic actuator
US6481203B1 (en) 1999-06-10 2002-11-19 Tecumseh Products Company Electric shifting of a variable speed transmission
US6443399B1 (en) * 2000-07-14 2002-09-03 Honeywell International Inc. Flight control module merged into the integrated modular avionics
US6439512B1 (en) * 2000-08-24 2002-08-27 Hr Textron, Inc. All-hydraulic powered horizontal stabilizer trim control surface position control system
US6923405B2 (en) * 2003-11-17 2005-08-02 The Boeing Company Enhanced rudder control system
US7786684B2 (en) * 2007-10-22 2010-08-31 Honeywell International Inc. Electromechanical flight control system and method for rotorcraft
US8172174B2 (en) * 2008-11-13 2012-05-08 Honeywell International Inc. Hybrid electromechanical/hydromechanical actuator and actuation control system
WO2012131330A1 (en) * 2011-03-29 2012-10-04 Bae Systems Plc Actuator control system

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2898889A (en) * 1958-10-03 1959-08-11 John V Foster Mechanically-limited, electrically operated hydraulic valve system for aircraft controls
US3027878A (en) * 1959-06-10 1962-04-03 Honeywell Regulator Co Fluid motor control apparatus
US3198082A (en) * 1962-11-09 1965-08-03 Lockheed Aircraft Corp Electrical primary flight control system utilizing redundant channels
US3469162A (en) * 1965-04-13 1969-09-23 Hawker Siddeley Dynamics Ltd Multiplex-type control apparatus
US3401600A (en) * 1965-12-23 1968-09-17 Bell Aerospace Corp Control system having a plurality of control chains each of which may be disabled in event of failure thereof
US3426650A (en) * 1965-12-23 1969-02-11 Bell Aerospace Corp Triple channel redundant hydraeric control system
US3422767A (en) * 1966-12-05 1969-01-21 Webster Electric Co Inc Variable displacement swashplate pumps
US3554084A (en) * 1967-11-17 1971-01-12 Honeywell Inc Redundant force summing servo unit
US3505929A (en) * 1968-04-16 1970-04-14 Gen Electric Redundant flight control servoactuator

Also Published As

Publication number Publication date
GB1328592A (en) 1973-08-30
DE2135366A1 (de) 1972-02-03
FR2099479A1 (enExample) 1972-03-17
US3679156A (en) 1972-07-25
FR2099479B1 (enExample) 1975-02-21

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Legal Events

Date Code Title Description
OD Request for examination
D2 Grant after examination