FR2137300A1 - - Google Patents

Info

Publication number
FR2137300A1
FR2137300A1 FR7117933A FR7117933A FR2137300A1 FR 2137300 A1 FR2137300 A1 FR 2137300A1 FR 7117933 A FR7117933 A FR 7117933A FR 7117933 A FR7117933 A FR 7117933A FR 2137300 A1 FR2137300 A1 FR 2137300A1
Authority
FR
France
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.)
Granted
Application number
FR7117933A
Other languages
French (fr)
Other versions
FR2137300B1 (en:Method
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.)
Airbus Group SAS
Original Assignee
Airbus Group SAS
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 Airbus Group SAS filed Critical Airbus Group SAS
Priority to FR7117933A priority Critical patent/FR2137300B1/fr
Priority to DE19722220243 priority patent/DE2220243C3/de
Priority to US00252292A priority patent/US3750984A/en
Priority to GB2237572A priority patent/GB1359242A/en
Publication of FR2137300A1 publication Critical patent/FR2137300A1/fr
Application granted granted Critical
Publication of FR2137300B1 publication Critical patent/FR2137300B1/fr
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
    • B64C13/24—Transmitting means
    • B64C13/26—Transmitting means without power amplification or where power amplification is irrelevant
    • B64C13/28—Transmitting means without power amplification or where power amplification is irrelevant mechanical
    • B64C13/345—Transmitting means without power amplification or where power amplification is irrelevant mechanical with artificial feel
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T74/00—Machine element or mechanism
    • Y10T74/20—Control lever and linkage systems

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Automation & Control Theory (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Control Devices (AREA)
  • Braking Arrangements (AREA)
  • Transmission Devices (AREA)
  • Manipulator (AREA)
  • Toys (AREA)
FR7117933A 1971-05-18 1971-05-18 Expired FR2137300B1 (en:Method)

Priority Applications (4)

Application Number Priority Date Filing Date Title
FR7117933A FR2137300B1 (en:Method) 1971-05-18 1971-05-18
DE19722220243 DE2220243C3 (de) 1971-05-18 1972-04-25 Mechanische Abstützvorrichtung für einen zwischen einem Handsteuerorgan und einer Steuerfläche eines Luftfahrzeugs eingeschalteten Stellmotor
US00252292A US3750984A (en) 1971-05-18 1972-05-11 Mechanical transmission relay for a control facility comprising a manual element and a servo-motor, and its use in aircraft control systems
GB2237572A GB1359242A (en) 1971-05-18 1972-05-12 Control system

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR7117933A FR2137300B1 (en:Method) 1971-05-18 1971-05-18

Publications (2)

Publication Number Publication Date
FR2137300A1 true FR2137300A1 (en:Method) 1972-12-29
FR2137300B1 FR2137300B1 (en:Method) 1974-04-05

Family

ID=9077227

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7117933A Expired FR2137300B1 (en:Method) 1971-05-18 1971-05-18

Country Status (3)

Country Link
US (1) US3750984A (en:Method)
FR (1) FR2137300B1 (en:Method)
GB (1) GB1359242A (en:Method)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2330591A1 (fr) * 1975-11-04 1977-06-03 Equip Navigation Aerienne Verin a loi d'effort incorporee
FR2438585A2 (fr) * 1978-10-10 1980-05-09 Equip Navigation Aerienne Perfectionnement a verin a loi d'effort incorporee
FR2937704A1 (fr) * 2008-10-28 2010-04-30 Skf Aerospace France Ensemble de transmission d'efforts et ensemble de commande comprenant un tel ensemble
FR2938822A1 (fr) * 2008-11-21 2010-05-28 Eurocopter France Verin rotatif a loi d'effort integree et procede de reduction du jeu d'un tel verin rotatif.
FR3137661A1 (fr) * 2022-07-11 2024-01-12 Safran Electronics & Defense Actionneur comprenant une connexion fusible et un dispositif d’éjection de ladite connexion fusible, et véhicule, notamment aéronef, muni dudit actionneur

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2273709A1 (fr) * 1974-06-06 1976-01-02 Aerospatiale Dispositif de commande de la position du point d'ancrage d'une chaine de pilotage d'un aerodyne
US4117740A (en) * 1977-07-12 1978-10-03 Thermo King Corporation Multi-stroke throttle linkage mechanism
US7108232B2 (en) * 2004-02-05 2006-09-19 Hoh Roger H Helicopter force-feel and stability augmentation system with parallel servo-actuator
FR2872306B1 (fr) * 2004-06-29 2006-09-22 Sagem Dispositif de commande a distance de gouvernes d'un aeronef
FR2920744B1 (fr) * 2007-09-07 2010-04-09 Eurocopter France Verin de compensation pour commande de vol de giravion
CN103076807B (zh) * 2012-12-27 2015-11-04 北京航空航天大学 一种欠驱动柔性航天器姿态稳定的控制方法
ES2684388T3 (es) * 2014-05-20 2018-10-02 Mecaer Aviation Group S.P.A. Sistema de control de vuelo híbrido de avión

Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR870995A (fr) * 1939-02-07 1942-04-01 Luftfahrtgeratewerk Hakenfelde Dispositif de manoeuvre au moteur de gouvernail, notamment pour avions
FR901208A (fr) * 1942-11-07 1945-07-20 Luftfahrtgeratewerk Hakenfelde Commande automatique de gouvernail pour avion
FR958331A (en:Method) * 1947-11-27 1950-03-07
US2678177A (en) * 1951-12-13 1954-05-11 Sperry Corp Manual booster and automatic pilot servo system
FR1079904A (fr) * 1953-03-30 1954-12-03 Applic Mach Motrices Servo-commande hydraulique de gouverne pour pilotage manuel et pilotage automatique
US2705940A (en) * 1950-11-06 1955-04-12 Mcdonnell Aircraft Corp Controllable power actuator for aircraft control surface
GB777273A (en) * 1954-12-14 1957-06-19 Hobson Ltd H M Improvements in or relating to aircraft controls
FR1234220A (fr) * 1959-05-12 1960-10-14 Snecma Dispositif de commande secondaire d'une transmission de commande

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3043539A (en) * 1960-01-08 1962-07-10 Bendix Corp Control stick torque sensor to selectively effect autopilot and manual control of aircraft control surfaces
US3096045A (en) * 1961-10-09 1963-07-02 Kaman Aircraft Corp Helicopter control mechanism
US3534930A (en) * 1969-02-24 1970-10-20 Nasa Mechanical stability augmentation system

Patent Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR870995A (fr) * 1939-02-07 1942-04-01 Luftfahrtgeratewerk Hakenfelde Dispositif de manoeuvre au moteur de gouvernail, notamment pour avions
FR901208A (fr) * 1942-11-07 1945-07-20 Luftfahrtgeratewerk Hakenfelde Commande automatique de gouvernail pour avion
FR958331A (en:Method) * 1947-11-27 1950-03-07
US2705940A (en) * 1950-11-06 1955-04-12 Mcdonnell Aircraft Corp Controllable power actuator for aircraft control surface
US2678177A (en) * 1951-12-13 1954-05-11 Sperry Corp Manual booster and automatic pilot servo system
FR1079904A (fr) * 1953-03-30 1954-12-03 Applic Mach Motrices Servo-commande hydraulique de gouverne pour pilotage manuel et pilotage automatique
GB777273A (en) * 1954-12-14 1957-06-19 Hobson Ltd H M Improvements in or relating to aircraft controls
FR1234220A (fr) * 1959-05-12 1960-10-14 Snecma Dispositif de commande secondaire d'une transmission de commande

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2330591A1 (fr) * 1975-11-04 1977-06-03 Equip Navigation Aerienne Verin a loi d'effort incorporee
FR2438585A2 (fr) * 1978-10-10 1980-05-09 Equip Navigation Aerienne Perfectionnement a verin a loi d'effort incorporee
FR2937704A1 (fr) * 2008-10-28 2010-04-30 Skf Aerospace France Ensemble de transmission d'efforts et ensemble de commande comprenant un tel ensemble
WO2010049644A1 (fr) * 2008-10-28 2010-05-06 Skf Aerospace France Ensemble de transmission d'efforts et ensemble de commande comprenant un tel ensemble
US8601904B2 (en) 2008-10-28 2013-12-10 Fly By Wire Systems France Force transmission assembly and a control assembly including such an assembly
FR2938822A1 (fr) * 2008-11-21 2010-05-28 Eurocopter France Verin rotatif a loi d'effort integree et procede de reduction du jeu d'un tel verin rotatif.
US8181550B2 (en) 2008-11-21 2012-05-22 Eurocopter Rotary actuator incorporating a force relationship, and a method of reducing angular slack in such a rotary actuator
FR3137661A1 (fr) * 2022-07-11 2024-01-12 Safran Electronics & Defense Actionneur comprenant une connexion fusible et un dispositif d’éjection de ladite connexion fusible, et véhicule, notamment aéronef, muni dudit actionneur

Also Published As

Publication number Publication date
GB1359242A (en) 1974-07-10
DE2220243B2 (de) 1976-05-26
US3750984A (en) 1973-08-07
FR2137300B1 (en:Method) 1974-04-05
DE2220243A1 (de) 1972-11-30

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ST Notification of lapse