RU2561159C1 - Электромеханический исполнительный механизм для поверхности управления воздушным летательным аппаратом и воздушный летательный аппарат, оборудованный таким исполнительным механизмом - Google Patents

Электромеханический исполнительный механизм для поверхности управления воздушным летательным аппаратом и воздушный летательный аппарат, оборудованный таким исполнительным механизмом Download PDF

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Publication number
RU2561159C1
RU2561159C1 RU2014125270/11A RU2014125270A RU2561159C1 RU 2561159 C1 RU2561159 C1 RU 2561159C1 RU 2014125270/11 A RU2014125270/11 A RU 2014125270/11A RU 2014125270 A RU2014125270 A RU 2014125270A RU 2561159 C1 RU2561159 C1 RU 2561159C1
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RU
Russia
Prior art keywords
actuator
transmission
electric motor
aircraft
slider
Prior art date
Application number
RU2014125270/11A
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English (en)
Russian (ru)
Inventor
Давид СЕНЕГА
Жером МЕХЕС
Максим ЖЕСТЕН
Бертран СЕВАЖАН
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Сажем Дефанс Секюрите
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Publication of RU2561159C1 publication Critical patent/RU2561159C1/ru

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    • 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
    • B64C13/341—Transmitting means without power amplification or where power amplification is irrelevant mechanical having duplication or stand-by provisions
    • 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
    • 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
    • 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
    • F16H21/00—Gearings comprising primarily only links or levers, with or without slides
    • F16H21/10—Gearings comprising primarily only links or levers, with or without slides all movement being in, or parallel to, a single plane
    • F16H21/16—Gearings comprising primarily only links or levers, with or without slides all movement being in, or parallel to, a single plane for interconverting rotary motion and reciprocating motion
    • F16H21/18—Crank gearings; Eccentric gearings
    • F16H21/22—Crank gearings; Eccentric gearings with one connecting-rod and one guided slide to each crank or eccentric
    • 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
    • F16H35/00—Gearings or mechanisms with other special functional features
    • 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
    • F16H35/00—Gearings or mechanisms with other special functional features
    • F16H2035/005—Gearings or mechanisms preventing back-driving
    • 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
    • Y10T74/18—Mechanical movements
    • Y10T74/18056—Rotary to or from reciprocating or oscillating
    • Y10T74/18184—Crank, pitman, and lever
    • 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
    • Y10T74/18—Mechanical movements
    • Y10T74/18568—Reciprocating or oscillating to or from alternating rotary
    • Y10T74/18576—Reciprocating or oscillating to or from alternating rotary including screw and nut
    • Y10T74/18696—Reciprocating or oscillating to or from alternating rotary including screw and nut including means to selectively transmit power [e.g., clutch, etc.]
    • 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
    • Y10T74/18—Mechanical movements
    • Y10T74/18568—Reciprocating or oscillating to or from alternating rotary
    • Y10T74/18792—Reciprocating or oscillating to or from alternating rotary including worm

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  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Automation & Control Theory (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Transmission Devices (AREA)
  • Connection Of Motors, Electrical Generators, Mechanical Devices, And The Like (AREA)
  • Toys (AREA)
  • Retarders (AREA)
RU2014125270/11A 2011-11-22 2012-11-21 Электромеханический исполнительный механизм для поверхности управления воздушным летательным аппаратом и воздушный летательный аппарат, оборудованный таким исполнительным механизмом RU2561159C1 (ru)

Applications Claiming Priority (5)

Application Number Priority Date Filing Date Title
US201161562736P 2011-11-22 2011-11-22
US61/562,736 2011-11-22
FR1253023 2012-04-02
FR1253023A FR2988797B1 (fr) 2012-04-02 2012-04-02 Actionneur electromecanique de surface de vol d'aeronef et aeronef pourvu d'un tel actionneur
PCT/EP2012/073264 WO2013076158A1 (en) 2011-11-22 2012-11-21 An electromechanical actuator for an aircraft control surface, and an aircraft provided with such an actuator

Publications (1)

Publication Number Publication Date
RU2561159C1 true RU2561159C1 (ru) 2015-08-27

Family

ID=48469155

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2014125270/11A RU2561159C1 (ru) 2011-11-22 2012-11-21 Электромеханический исполнительный механизм для поверхности управления воздушным летательным аппаратом и воздушный летательный аппарат, оборудованный таким исполнительным механизмом

Country Status (9)

Country Link
US (1) US9038944B2 (cg-RX-API-DMAC7.html)
EP (1) EP2783135B1 (cg-RX-API-DMAC7.html)
CN (1) CN103946590B (cg-RX-API-DMAC7.html)
BR (1) BR112014012105A8 (cg-RX-API-DMAC7.html)
CA (1) CA2854239C (cg-RX-API-DMAC7.html)
FR (1) FR2988797B1 (cg-RX-API-DMAC7.html)
IN (1) IN2014CN04486A (cg-RX-API-DMAC7.html)
RU (1) RU2561159C1 (cg-RX-API-DMAC7.html)
WO (1) WO2013076158A1 (cg-RX-API-DMAC7.html)

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9493230B2 (en) 2013-11-21 2016-11-15 Hamilton Sundstrand Corporation Drive assembly with selective disconnect
FR3016607B1 (fr) * 2014-01-20 2016-01-22 Sagem Defense Securite Actionneur de commande d'un plan horizontal de stabilisation d'un aeronef
US10689097B2 (en) 2014-05-16 2020-06-23 Bombardier Inc. Actuators and methods for aircraft flight control surfaces
FR3022526B1 (fr) * 2014-06-20 2016-06-24 Sagem Defense Securite Actionneur electromecanique a limiteur de couple magnetique
EP3324079B1 (en) * 2016-11-21 2020-04-29 Ratier-Figeac SAS Flight control system and method of manufacturing a flight control system
FR3058983B1 (fr) * 2016-11-22 2018-11-02 Safran Electronics & Defense Actionneur a montage facilite
EP3739230B1 (en) * 2019-05-16 2022-04-27 Ratier-Figeac SAS Actuator with declutchable output lever
US12374956B2 (en) * 2022-03-11 2025-07-29 Parker-Hannifin Corporation Control surface actuator with bell crank assembly
EP4257484B1 (en) 2022-04-06 2025-02-26 Goodrich Actuation Systems SAS Runaway emergency actuator brake
EP4311768B1 (en) * 2022-07-27 2025-04-23 Goodrich Actuation Systems SAS Spoiler actuator
DE102022131677A1 (de) 2022-11-30 2024-06-06 Liebherr-Aerospace Lindenberg Gmbh Blockiereinheit, elektromechanische Einheit und Luftfahrzeug
US12269582B1 (en) 2023-10-05 2025-04-08 Woodward, Inc. Electromechanical aircraft spoiler
EP4542088A1 (en) 2023-10-19 2025-04-23 Goodrich Actuation Systems SAS Rotary ema

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4762205A (en) * 1987-05-20 1988-08-09 Simmonds Precision Flight control surface actuator for aircraft including remote braking failure detection
DE4413854A1 (de) * 1994-04-21 1995-10-26 Daimler Benz Aerospace Airbus Verschwenkeinrichtung
RU2277195C2 (ru) * 2003-02-07 2006-05-27 Государственное предприятие "Харьковское агрегатное конструкторское бюро" (ГП "ХАКБ") Приводной электромеханизм

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DE2725632C2 (de) * 1977-06-07 1982-11-11 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Querruder und Landeklappenantrieb für ein FLugzeug
US4637272A (en) * 1985-10-28 1987-01-20 Sundstrand Corporation Ballscrew actuator
US5918836A (en) * 1997-03-25 1999-07-06 Sundstrand Corporation Aircraft spoiler blow-down mechanism
US6109415A (en) * 1998-05-29 2000-08-29 The Boeing Company Bi-directional ballscrew no-back device
JP4182726B2 (ja) * 2002-02-20 2008-11-19 日本精工株式会社 リニアアクチュエータ
US7100870B2 (en) * 2003-10-15 2006-09-05 Parker-Hannifin Corporation Jam tolerant electromechanical actuation systems and methods of operation
DE102005062919A1 (de) * 2005-12-29 2007-07-12 Airbus Deutschland Gmbh Tragfläche für ein Flugzeug und Flugzeug
US8230750B2 (en) * 2006-09-01 2012-07-31 Parker-Hannifin Corporation Electromechanical actuating assembly
US8136418B2 (en) * 2007-02-07 2012-03-20 Parker-Hannifin Corporation Electromechanical actuating assembly
DE102008022092A1 (de) * 2008-05-05 2009-11-19 Airbus Deutschland Gmbh Fehlertolerantes Stellsystem zur Verstellung von Klappen eines Flugzeugs mit einer Verstell-Kinematik mit feststehender Drehachse
US8794084B2 (en) * 2010-03-18 2014-08-05 Parker-Hannifin Corporation Jam-tolerant electromechanical actuator

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4762205A (en) * 1987-05-20 1988-08-09 Simmonds Precision Flight control surface actuator for aircraft including remote braking failure detection
DE4413854A1 (de) * 1994-04-21 1995-10-26 Daimler Benz Aerospace Airbus Verschwenkeinrichtung
RU2277195C2 (ru) * 2003-02-07 2006-05-27 Государственное предприятие "Харьковское агрегатное конструкторское бюро" (ГП "ХАКБ") Приводной электромеханизм

Also Published As

Publication number Publication date
EP2783135B1 (en) 2017-03-22
US9038944B2 (en) 2015-05-26
IN2014CN04486A (cg-RX-API-DMAC7.html) 2015-09-11
US20140326828A1 (en) 2014-11-06
FR2988797A1 (fr) 2013-10-04
WO2013076158A1 (en) 2013-05-30
EP2783135A1 (en) 2014-10-01
BR112014012105A8 (pt) 2017-06-20
CN103946590B (zh) 2016-09-28
BR112014012105A2 (pt) 2017-06-13
CA2854239A1 (en) 2013-05-30
FR2988797B1 (fr) 2015-04-24
CN103946590A (zh) 2014-07-23
CA2854239C (en) 2016-06-14

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Effective date: 20201122