IL75158A - Hydraulic two-actuator system with a single balanced output - Google Patents

Hydraulic two-actuator system with a single balanced output

Info

Publication number
IL75158A
IL75158A IL75158A IL7515885A IL75158A IL 75158 A IL75158 A IL 75158A IL 75158 A IL75158 A IL 75158A IL 7515885 A IL7515885 A IL 7515885A IL 75158 A IL75158 A IL 75158A
Authority
IL
Israel
Prior art keywords
hydraulic
actuator system
balanced output
single balanced
output
Prior art date
Application number
IL75158A
Other languages
English (en)
Other versions
IL75158A0 (en
Original Assignee
United Technologies Corp
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 United Technologies Corp filed Critical United Technologies Corp
Publication of IL75158A0 publication Critical patent/IL75158A0/xx
Publication of IL75158A publication Critical patent/IL75158A/xx

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F15—FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
    • F15B—SYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
    • F15B18/00—Parallel arrangements of independent servomotor systems

Landscapes

  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Fluid-Pressure Circuits (AREA)
  • Actuator (AREA)
  • Servomotors (AREA)
  • Steering Control In Accordance With Driving Conditions (AREA)
IL75158A 1984-05-14 1985-05-10 Hydraulic two-actuator system with a single balanced output IL75158A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US06/609,915 US4531448A (en) 1984-05-14 1984-05-14 Balanced output hydraulic actuator system

Publications (2)

Publication Number Publication Date
IL75158A0 IL75158A0 (en) 1985-09-29
IL75158A true IL75158A (en) 1989-03-31

Family

ID=24442876

Family Applications (1)

Application Number Title Priority Date Filing Date
IL75158A IL75158A (en) 1984-05-14 1985-05-10 Hydraulic two-actuator system with a single balanced output

Country Status (11)

Country Link
US (1) US4531448A (es)
JP (1) JPS60260702A (es)
AU (1) AU579861B2 (es)
BR (1) BR8502246A (es)
CA (1) CA1232826A (es)
DE (1) DE3515826C2 (es)
ES (1) ES8606819A1 (es)
FR (1) FR2564156B1 (es)
GB (1) GB2158972B (es)
IL (1) IL75158A (es)
IT (1) IT1200479B (es)

Families Citing this family (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4800798A (en) * 1984-12-11 1989-01-31 The United States Of America As Represented By The Secretary Of The Air Force Control surface dual redundant servomechanism
EP1195530A1 (en) * 2000-10-04 2002-04-10 MECAER Meccanica Aeronautica S.p.A. Refundant hydraulic actuator, particularly for an aircraft servocontrol
US8885315B2 (en) * 2009-10-15 2014-11-11 Hamilton Sundstrand Corporation Multi-actuator motion control system
JP5514527B2 (ja) * 2009-12-11 2014-06-04 ナブテスコ株式会社 航空機用リアクションリンク
JP5552340B2 (ja) * 2010-03-15 2014-07-16 ナブテスコ株式会社 アクチュエータ及びリンクの製造方法、アクチュエータ及びリンクの設計方法、アクチュエータ及びリンク
DE102010051216A1 (de) * 2010-11-12 2012-05-16 Airbus Operations Gmbh Seitenrudersystem an einem Flugzeug
DE102010053396B4 (de) 2010-12-03 2014-12-24 Airbus Defence and Space GmbH Übertragung einer Steuerungskraft
JP5784370B2 (ja) * 2011-06-02 2015-09-24 ナブテスコ株式会社 航空機用舵面駆動機構
ES2659412T3 (es) 2012-02-09 2018-03-15 Moog Inc. Sistema y método accionador
US9086125B2 (en) * 2013-03-15 2015-07-21 Moog Inc. Rotary actuator
CA3011439A1 (en) 2016-01-13 2017-07-20 Moog Inc. Summing and fault tolerant rotary actuator assembly
EP3255287B1 (en) * 2016-06-10 2024-03-20 Claverham Limited Adjustment system for a hydraulic actuator
CN108488123B (zh) * 2018-06-12 2024-07-09 山河智能装备股份有限公司 一种双液压油缸自动同步系统

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB652001A (en) * 1948-06-29 1951-04-11 Blackburn Aircraft Ltd Improvements in or relating to pilot's power assisted controls of aircraft
US2706886A (en) * 1950-06-14 1955-04-26 Honeywell Regulator Co Coordinated hydraulic control apparatus
US2729943A (en) * 1953-05-26 1956-01-10 Chambersburg Eng Co Fluid-pressure-actuated apparatus
US2859591A (en) * 1955-07-20 1958-11-11 Us Industries Inc Hydraulic synchronizer
GB828785A (en) * 1957-09-27 1960-02-24 Sperry Gyroscope Co Ltd Control apparatus for aircraft
GB897627A (en) * 1958-06-23 1962-05-30 Sperry Gyroscope Co Ltd Control apparatus for aircraft
CH514073A (fr) * 1963-05-25 1971-10-15 Vevey Atel Const Mec Installation de réglage de turbine hydraulique à hélice à pas réglable
US3272062A (en) * 1965-10-07 1966-09-13 Ltv Electrosystems Inc Servo valve synchronizer
US3677137A (en) * 1970-06-19 1972-07-18 Orville E Stockwell Reversible differential control valve and systems
US3726186A (en) * 1971-06-01 1973-04-10 Mc Donnell Douglas Corp Tandem control valve
DE2450330C3 (de) * 1974-10-23 1978-09-14 Messerschmitt-Boelkow-Blohm Gmbh, 8000 Muenchen Doppelhydraulischer Stellantrieb
US4231284A (en) * 1978-08-31 1980-11-04 Textron, Inc. Load equilization feedback for parallel channel servo actuators

Also Published As

Publication number Publication date
FR2564156A1 (fr) 1985-11-15
JPH0570721B2 (es) 1993-10-05
AU579861B2 (en) 1988-12-15
IT1200479B (it) 1989-01-18
ES8606819A1 (es) 1986-05-16
DE3515826A1 (de) 1985-11-14
GB8511741D0 (en) 1985-06-19
IL75158A0 (en) 1985-09-29
BR8502246A (pt) 1986-01-14
JPS60260702A (ja) 1985-12-23
IT8520699A0 (it) 1985-05-14
CA1232826A (en) 1988-02-16
GB2158972B (en) 1987-12-16
US4531448A (en) 1985-07-30
ES543072A0 (es) 1986-05-16
DE3515826C2 (de) 1994-04-07
FR2564156B1 (fr) 1988-10-14
GB2158972A (en) 1985-11-20
AU4205785A (en) 1985-11-21

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Legal Events

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