FR3012415B1 - Actionneur electromecanique et unite d'actionneur - Google Patents

Actionneur electromecanique et unite d'actionneur Download PDF

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Publication number
FR3012415B1
FR3012415B1 FR1460220A FR1460220A FR3012415B1 FR 3012415 B1 FR3012415 B1 FR 3012415B1 FR 1460220 A FR1460220 A FR 1460220A FR 1460220 A FR1460220 A FR 1460220A FR 3012415 B1 FR3012415 B1 FR 3012415B1
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FR
France
Prior art keywords
actuator
electromechanical
unit
actuator unit
electromechanical actuator
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.)
Active
Application number
FR1460220A
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English (en)
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FR3012415A1 (fr
Inventor
Masanori Hirai
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.)
Nabtesco Corp
Original Assignee
Nabtesco 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 Nabtesco Corp filed Critical Nabtesco Corp
Publication of FR3012415A1 publication Critical patent/FR3012415A1/fr
Application granted granted Critical
Publication of FR3012415B1 publication Critical patent/FR3012415B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16HGEARING
    • F16H25/00Gearings comprising primarily only cams, cam-followers and screw-and-nut mechanisms
    • F16H25/18Gearings comprising primarily only cams, cam-followers and screw-and-nut mechanisms for conveying or interconverting oscillating or reciprocating motions
    • F16H25/20Screw mechanisms
    • F16H25/205Screw mechanisms comprising alternate power paths, e.g. for fail safe back-up
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C13/00Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
    • B64C13/24Transmitting means
    • B64C13/26Transmitting means without power amplification or where power amplification is irrelevant
    • B64C13/28Transmitting means without power amplification or where power amplification is irrelevant mechanical
    • B64C13/341Transmitting means without power amplification or where power amplification is irrelevant mechanical having duplication or stand-by provisions
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F15FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
    • F15BSYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
    • F15B15/00Fluid-actuated devices for displacing a member from one position to another; Gearing associated therewith
    • F15B15/08Characterised by the construction of the motor unit
    • F15B15/088Characterised by the construction of the motor unit the motor using combined actuation, e.g. electric and fluid actuation
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F15FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
    • F15BSYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
    • F15B9/00Servomotors with follow-up action, e.g. obtained by feed-back control, i.e. in which the position of the actuated member conforms with that of the controlling member
    • F15B9/02Servomotors with follow-up action, e.g. obtained by feed-back control, i.e. in which the position of the actuated member conforms with that of the controlling member with servomotors of the reciprocatable or oscillatable type
    • F15B9/08Servomotors with follow-up action, e.g. obtained by feed-back control, i.e. in which the position of the actuated member conforms with that of the controlling member with servomotors of the reciprocatable or oscillatable type controlled by valves affecting the fluid feed or the fluid outlet of the servomotor
    • F15B9/12Servomotors with follow-up action, e.g. obtained by feed-back control, i.e. in which the position of the actuated member conforms with that of the controlling member with servomotors of the reciprocatable or oscillatable type controlled by valves affecting the fluid feed or the fluid outlet of the servomotor in which both the controlling element and the servomotor control the same member influencing a fluid passage and are connected to that member by means of a differential gearing
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T74/00Machine element or mechanism
    • Y10T74/18Mechanical movements
    • Y10T74/18568Reciprocating or oscillating to or from alternating rotary
    • Y10T74/18576Reciprocating or oscillating to or from alternating rotary including screw and nut
    • Y10T74/18592Auxiliary drive [e.g., fluid piston, etc.] for load

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Automation & Control Theory (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Actuator (AREA)
  • Transmission Devices (AREA)
  • Fluid-Pressure Circuits (AREA)
  • Connection Of Motors, Electrical Generators, Mechanical Devices, And The Like (AREA)
FR1460220A 2013-10-24 2014-10-24 Actionneur electromecanique et unite d'actionneur Active FR3012415B1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP2013221165A JP6230873B2 (ja) 2013-10-24 2013-10-24 電動アクチュエータ及びアクチュエータユニット

Publications (2)

Publication Number Publication Date
FR3012415A1 FR3012415A1 (fr) 2015-05-01
FR3012415B1 true FR3012415B1 (fr) 2022-12-16

Family

ID=52821817

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1460220A Active FR3012415B1 (fr) 2013-10-24 2014-10-24 Actionneur electromecanique et unite d'actionneur

Country Status (3)

Country Link
US (1) US9618102B2 (fr)
JP (1) JP6230873B2 (fr)
FR (1) FR3012415B1 (fr)

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WO2011087939A2 (fr) * 2010-01-16 2011-07-21 Borgwarner Inc. Liaison de commande de turbocompresseur à écoulement de chaleur réduit
US9797490B2 (en) * 2014-03-27 2017-10-24 Lcdrives Corp. High reliability actuator
US9765867B2 (en) * 2014-04-23 2017-09-19 Nabtesco Corporation Electromechanical actuator
FR3054199B1 (fr) 2016-07-25 2019-08-02 Airbus Operations Systeme d’actionnement d’une surface de controle d’un aeronef.
US10994830B2 (en) * 2017-10-30 2021-05-04 Airbus Operations Gmbh Flap actuating system for use in an aircraft
US10723441B2 (en) 2018-04-13 2020-07-28 The Boeing Company High-speed-deployed, drum-brake, inertia disk for rack and pinion rotational inerter
US10737764B2 (en) 2018-04-13 2020-08-11 The Boeing Company Base flight control member orientation mechanism and control
US11072418B2 (en) 2018-04-13 2021-07-27 The Boeing Company Hydraulic system for an aircraft
US10793261B2 (en) 2018-04-13 2020-10-06 The Boeing Company Electro-mechanically biased supercritical flight control surface loading to reduce high pressure actuation cycles
US10526071B2 (en) * 2018-04-13 2020-01-07 The Boeing Company Hydraulic systems and methods to control a member
US10711809B2 (en) 2018-04-13 2020-07-14 The Boeing Company Aircraft hydraulic system with a dual spool valve and methods of use
US10947997B2 (en) 2018-04-13 2021-03-16 The Boeing Company Aircraft hydraulic system with a dual spool valve and methods of use
CN108953280B (zh) * 2018-08-22 2020-11-06 扬州市慧宇科技有限公司 一种新型电液推杆
US10935053B2 (en) * 2018-10-26 2021-03-02 Ellrich Engineering, Llc Space-constrained hybrid linear actuator
CN109592016A (zh) * 2018-11-06 2019-04-09 珠海隆华直升机科技有限公司 直升机直线式驱动装置及直升机
CN109592015A (zh) * 2018-11-06 2019-04-09 珠海隆华直升机科技有限公司 直升机直线式舵机及直升机
US11092175B1 (en) * 2020-03-23 2021-08-17 The Boeing Company Dual-independent hybrid actuator system
CN113028017B (zh) * 2021-02-24 2022-06-14 内蒙古工业大学 防卡滞的液压备份式机电作动器及其控制方法
US20230063097A1 (en) * 2021-08-27 2023-03-02 Viettel Group Electrical driving mechanism for sonic flying devices
US11773949B1 (en) * 2022-07-13 2023-10-03 Zoomlion Heavy Industry Na, Inc. Electro-hydraulic linear ball screw actuators

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US5144851A (en) * 1991-08-01 1992-09-08 Sundstrand Corp. Jam tolerant linear actuator
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FR2859770B1 (fr) * 2003-09-12 2006-02-03 Messier Bugatti Actionneur a deux modes de fonctionnement
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US7191593B1 (en) * 2005-11-28 2007-03-20 Northrop Grumman Corporation Electro-hydraulic actuator system
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JP5964575B2 (ja) * 2011-12-06 2016-08-03 ナブテスコ株式会社 アクチュエータ

Also Published As

Publication number Publication date
FR3012415A1 (fr) 2015-05-01
US9618102B2 (en) 2017-04-11
JP2015081673A (ja) 2015-04-27
US20150114151A1 (en) 2015-04-30
JP6230873B2 (ja) 2017-11-15

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