BR8502246A - Sistema atuador hidraulico - Google Patents

Sistema atuador hidraulico

Info

Publication number
BR8502246A
BR8502246A BR8502246A BR8502246A BR8502246A BR 8502246 A BR8502246 A BR 8502246A BR 8502246 A BR8502246 A BR 8502246A BR 8502246 A BR8502246 A BR 8502246A BR 8502246 A BR8502246 A BR 8502246A
Authority
BR
Brazil
Prior art keywords
hydraulic actuator
actuator system
hydraulic
actuator
Prior art date
Application number
BR8502246A
Other languages
English (en)
Inventor
Philip Earle Barnes
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 BR8502246A publication Critical patent/BR8502246A/pt

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
BR8502246A 1984-05-14 1985-05-10 Sistema atuador hidraulico BR8502246A (pt)

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 (1)

Publication Number Publication Date
BR8502246A true BR8502246A (pt) 1986-01-14

Family

ID=24442876

Family Applications (1)

Application Number Title Priority Date Filing Date
BR8502246A BR8502246A (pt) 1984-05-14 1985-05-10 Sistema atuador hidraulico

Country Status (11)

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

Families Citing this family (12)

* 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
US10281033B2 (en) 2012-02-09 2019-05-07 Moog Inc. Multiple actuator and linkage system
US9086125B2 (en) * 2013-03-15 2015-07-21 Moog Inc. Rotary actuator
WO2017123987A1 (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

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
US4531448A (en) 1985-07-30
DE3515826C2 (de) 1994-04-07
GB2158972A (en) 1985-11-20
IL75158A (en) 1989-03-31
GB8511741D0 (en) 1985-06-19
JPS60260702A (ja) 1985-12-23
FR2564156B1 (fr) 1988-10-14
GB2158972B (en) 1987-12-16
AU579861B2 (en) 1988-12-15
IT8520699A0 (it) 1985-05-14
FR2564156A1 (fr) 1985-11-15
JPH0570721B2 (pt) 1993-10-05
ES543072A0 (es) 1986-05-16
IT1200479B (it) 1989-01-18
DE3515826A1 (de) 1985-11-14
CA1232826A (en) 1988-02-16
AU4205785A (en) 1985-11-21
ES8606819A1 (es) 1986-05-16
IL75158A0 (en) 1985-09-29

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Legal Events

Date Code Title Description
B21A Patent or certificate of addition expired [chapter 21.1 patent gazette]

Free format text: PATENTE EXTINTA EM 10/05/2000