IT201700058891A1 - Metodo per verificare un guasto elettrico, elettronico e/o meccanico in un attuatore elettromeccanico lineare - Google Patents

Metodo per verificare un guasto elettrico, elettronico e/o meccanico in un attuatore elettromeccanico lineare

Info

Publication number
IT201700058891A1
IT201700058891A1 IT102017000058891A IT201700058891A IT201700058891A1 IT 201700058891 A1 IT201700058891 A1 IT 201700058891A1 IT 102017000058891 A IT102017000058891 A IT 102017000058891A IT 201700058891 A IT201700058891 A IT 201700058891A IT 201700058891 A1 IT201700058891 A1 IT 201700058891A1
Authority
IT
Italy
Prior art keywords
verify
electronic
electrical
electromechanical actuator
mechanical fault
Prior art date
Application number
IT102017000058891A
Other languages
English (en)
Inventor
Nicola Borgarelli
Luciano Pizzoni
Marco Nardeschi
Antonio Tomasiello
Original Assignee
Umbragroup S P A
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 Umbragroup S P A filed Critical Umbragroup S P A
Priority to IT102017000058891A priority Critical patent/IT201700058891A1/it
Priority to US16/617,656 priority patent/US11239728B2/en
Priority to EP18733683.9A priority patent/EP3630599B1/en
Priority to CN201880035418.2A priority patent/CN110709319A/zh
Priority to ES18733683T priority patent/ES2900587T3/es
Priority to PCT/IB2018/053831 priority patent/WO2018220539A1/en
Publication of IT201700058891A1 publication Critical patent/IT201700058891A1/it

Links

Classifications

    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02K—DYNAMO-ELECTRIC MACHINES
    • H02K7/00—Arrangements for handling mechanical energy structurally associated with dynamo-electric machines, e.g. structural association with mechanical driving motors or auxiliary dynamo-electric machines
    • H02K7/06—Means for converting reciprocating motion into rotary motion or vice versa
    • 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
    • B64C13/38—Transmitting means with power amplification
    • B64C13/50—Transmitting means with power amplification using electrical energy
    • B64C13/505—Transmitting means with power amplification using electrical energy having duplication or stand-by provisions
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16H—GEARING
    • F16H25/00—Gearings comprising primarily only cams, cam-followers and screw-and-nut mechanisms
    • F16H25/18—Gearings comprising primarily only cams, cam-followers and screw-and-nut mechanisms for conveying or interconverting oscillating or reciprocating motions
    • F16H25/20—Screw mechanisms
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D45/00—Aircraft indicators or protectors not otherwise provided for
    • B64D2045/0085—Devices for aircraft health monitoring, e.g. monitoring flutter or vibration
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16H—GEARING
    • F16H25/00—Gearings comprising primarily only cams, cam-followers and screw-and-nut mechanisms
    • F16H25/18—Gearings comprising primarily only cams, cam-followers and screw-and-nut mechanisms for conveying or interconverting oscillating or reciprocating motions
    • F16H25/20—Screw mechanisms
    • F16H2025/2059—Superposing movement by two screws, e.g. with opposite thread direction
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16H—GEARING
    • F16H25/00—Gearings comprising primarily only cams, cam-followers and screw-and-nut mechanisms
    • F16H25/18—Gearings comprising primarily only cams, cam-followers and screw-and-nut mechanisms for conveying or interconverting oscillating or reciprocating motions
    • F16H25/20—Screw mechanisms
    • F16H2025/2062—Arrangements for driving the actuator
    • F16H2025/2075—Coaxial drive motors

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Power Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Automation & Control Theory (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Transmission Devices (AREA)
IT102017000058891A 2017-05-30 2017-05-30 Metodo per verificare un guasto elettrico, elettronico e/o meccanico in un attuatore elettromeccanico lineare IT201700058891A1 (it)

Priority Applications (6)

Application Number Priority Date Filing Date Title
IT102017000058891A IT201700058891A1 (it) 2017-05-30 2017-05-30 Metodo per verificare un guasto elettrico, elettronico e/o meccanico in un attuatore elettromeccanico lineare
US16/617,656 US11239728B2 (en) 2017-05-30 2018-05-30 Methods for assessing presence of electrical, electronic, and/or mechanical faults in electromechanical linear actuators
EP18733683.9A EP3630599B1 (en) 2017-05-30 2018-05-30 Method for assessing the presence of an electrical, electronic and/or mechanical fault in an electromechanical linear actuator
CN201880035418.2A CN110709319A (zh) 2017-05-30 2018-05-30 评估机电线性致动器中电气、电子和/或机械故障的存在的方法
ES18733683T ES2900587T3 (es) 2017-05-30 2018-05-30 Método para evaluar de la presencia de una falla eléctrica, electrónica y/o mecánica en un actuador electromecánico lineal
PCT/IB2018/053831 WO2018220539A1 (en) 2017-05-30 2018-05-30 Method for assessing the presence of an electrical, electronic and/or mechanical fault in an electromechanical linear actuator

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
IT102017000058891A IT201700058891A1 (it) 2017-05-30 2017-05-30 Metodo per verificare un guasto elettrico, elettronico e/o meccanico in un attuatore elettromeccanico lineare

Publications (1)

Publication Number Publication Date
IT201700058891A1 true IT201700058891A1 (it) 2018-11-30

Family

ID=60182876

Family Applications (1)

Application Number Title Priority Date Filing Date
IT102017000058891A IT201700058891A1 (it) 2017-05-30 2017-05-30 Metodo per verificare un guasto elettrico, elettronico e/o meccanico in un attuatore elettromeccanico lineare

Country Status (6)

Country Link
US (1) US11239728B2 (it)
EP (1) EP3630599B1 (it)
CN (1) CN110709319A (it)
ES (1) ES2900587T3 (it)
IT (1) IT201700058891A1 (it)
WO (1) WO2018220539A1 (it)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102017111032A1 (de) 2017-05-20 2018-11-22 Inventus Engineering Gmbh Vorrichtung mit einem steuerbaren Drehdämpfer
DE102017128390A1 (de) * 2017-11-30 2019-06-06 U-Shin Deutschland Zugangssysteme Gmbh Spindelantriebsbaugruppe sowie Fahrzeugklappe mit einer Spindelantriebsbaugruppe
EP3524514A1 (en) * 2018-02-09 2019-08-14 Airbus Operations GmbH Actuation unit for actuating a foldable wing tip portion of a wing for an aircraft
IT201900018308A1 (it) * 2019-10-09 2021-04-09 Umbragroup S P A Trasmissione meccanica lineare a vite
CN111806913B (zh) * 2020-07-20 2022-05-06 北京航天发射技术研究所 一种保温舱开关盖装置
US11067156B1 (en) * 2020-07-21 2021-07-20 Hi-Lex Controls, Inc. Friction brake and power strut therewith
US11613357B2 (en) * 2020-07-24 2023-03-28 Victor D. Trotter Aerial dispersal mechanisms, aircrafts and retrofit methods
BR112023020792A2 (pt) * 2021-04-07 2023-12-12 Skyryse Inc Atuador eletromecânico com mecanismo de falha operacional integrado
US11616416B2 (en) * 2021-05-05 2023-03-28 Nidec Motor Corporation Electric linear actuator with optimized coupling

Citations (4)

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US4179944A (en) * 1977-06-27 1979-12-25 United Technologies Corporation Fail safe redundant actuator
US5214972A (en) * 1992-04-30 1993-06-01 Alliedsignal Aerospace Fault-tolerant linear electromechanical actuator
WO2007024220A1 (en) * 2005-08-24 2007-03-01 Kollmorgen Corporation Failure-tolerant redundant actuator system
US20100242643A1 (en) * 2005-05-31 2010-09-30 The Boeing Company Direct Drive Electromechanical Linear Actuators

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US3343427A (en) * 1966-01-04 1967-09-26 Giovanni J Silvestri Electro-mechanical linear motion actuator
WO1983002141A1 (en) * 1981-12-18 1983-06-23 Hans Fickler Linear drive device with two motors
US4637272A (en) * 1985-10-28 1987-01-20 Sundstrand Corporation Ballscrew actuator
US4876906A (en) * 1986-11-20 1989-10-31 Sundstrand Corporation Non-jamming actuator system
US4858491A (en) * 1988-01-21 1989-08-22 Plessey Incorporated Fail-free actuator assembly
US5041748A (en) * 1989-10-16 1991-08-20 Sundstrand Corporation Lightweight, direct drive electromechanical actuator
US6247667B1 (en) * 1999-08-06 2001-06-19 Bell Helicopter Textron Inc. Tiltrotor aircraft pylon conversion system
FR2839127B1 (fr) 2002-04-24 2004-06-25 Transrol Dispositif d'actionnement a elements roulants intermediaires
US7190096B2 (en) 2004-06-04 2007-03-13 The Boeing Company Fault-tolerant electro-mechanical actuator having motor armatures to drive a ram and having an armature release mechanism
US8230750B2 (en) * 2006-09-01 2012-07-31 Parker-Hannifin Corporation Electromechanical actuating assembly
US7963529B2 (en) 2008-09-08 2011-06-21 Bose Corporation Counter-rotating motors with linear output
GB0914576D0 (en) * 2009-08-20 2009-09-30 Airbus Operations Ltd Apparatus for use on an aircraft
US8310193B2 (en) * 2010-01-12 2012-11-13 Hamilton Sundstrand Corporation Minimum temperature control for electromechanical actuator
US8890461B2 (en) 2012-03-22 2014-11-18 Bose Corporation Actuator assembly with preloaded ball screws
US9024491B2 (en) * 2012-08-15 2015-05-05 Sinfonia Technology Co., Ltd. Electromechanical actuator
US9534644B2 (en) * 2014-01-31 2017-01-03 Bell Helicopter Textron Inc. Magnetorheological rotorcraft actuation system
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
CH712279A1 (de) * 2016-03-18 2017-09-29 Baltec Maschb Ag Vorrichtung zur Beaufschlagung eines Verbindungselements mit einer Beaufschlagungskraft.
US11105404B2 (en) * 2017-05-30 2021-08-31 UMBRAGROUP S.p.A. Fault-tolerant electromechanical linear actuators
US10975940B2 (en) * 2017-08-24 2021-04-13 Eaton Intelligent Power Limited Actuator and method
US10630138B2 (en) * 2017-09-13 2020-04-21 Schaeffler Technologies AG & Co. KG Reciprocating ramp motor

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4179944A (en) * 1977-06-27 1979-12-25 United Technologies Corporation Fail safe redundant actuator
US5214972A (en) * 1992-04-30 1993-06-01 Alliedsignal Aerospace Fault-tolerant linear electromechanical actuator
US20100242643A1 (en) * 2005-05-31 2010-09-30 The Boeing Company Direct Drive Electromechanical Linear Actuators
WO2007024220A1 (en) * 2005-08-24 2007-03-01 Kollmorgen Corporation Failure-tolerant redundant actuator system

Also Published As

Publication number Publication date
US11239728B2 (en) 2022-02-01
CN110709319A (zh) 2020-01-17
ES2900587T3 (es) 2022-03-17
EP3630599A1 (en) 2020-04-08
WO2018220539A1 (en) 2018-12-06
EP3630599B1 (en) 2021-09-15
US20200186005A1 (en) 2020-06-11

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