BR112014012105A2 - atuador eletromecânico para uma superfície de controle de aeronave e aeronave provida com um tal atuador - Google Patents
atuador eletromecânico para uma superfície de controle de aeronave e aeronave provida com um tal atuadorInfo
- Publication number
- BR112014012105A2 BR112014012105A2 BR112014012105A BR112014012105A BR112014012105A2 BR 112014012105 A2 BR112014012105 A2 BR 112014012105A2 BR 112014012105 A BR112014012105 A BR 112014012105A BR 112014012105 A BR112014012105 A BR 112014012105A BR 112014012105 A2 BR112014012105 A2 BR 112014012105A2
- Authority
- BR
- Brazil
- Prior art keywords
- aircraft
- actuator
- control surface
- surface provided
- rotation
- Prior art date
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
- B64C13/341—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
-
- 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
Landscapes
- 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)
- Retarders (AREA)
- Toys (AREA)
Abstract
1/1 resumo “atuador eletromecânico para uma superfície de controle de aeronave e aeronave provida com um tal atuador" um atuador eletromecânico para uma superfície de controle de voo móvel de uma aeronave, o atuador compreendendo um motor elétrico (2) tendo um eixo de saída (20) com primeira e segunda direções de rotação, uma transmissão de movimento (1) arranjada para conectar o eixo de saída do motor à superfície de controle de voo móvel, e uma unidade de controle (3) para controlar o motor. a transmissão incorpora um dispositivo de lingueta (18) arranjado para se opor à transmissão de movimento na primeira direção de rotação, e a unidade de controle é conectada a um elemento de desengate de lingueta (19) para desengatar a lingueta e permitir que movimento seja transmitido na primeira direção de rotação.
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US201161562736P | 2011-11-22 | 2011-11-22 | |
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 (2)
Publication Number | Publication Date |
---|---|
BR112014012105A2 true BR112014012105A2 (pt) | 2017-06-13 |
BR112014012105A8 BR112014012105A8 (pt) | 2017-06-20 |
Family
ID=48469155
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BR112014012105A BR112014012105A8 (pt) | 2011-11-22 | 2012-11-21 | atuador eletromecânico para uma superfície de controle de aeronave e aeronave provida com um tal atuador |
Country Status (9)
Country | Link |
---|---|
US (1) | US9038944B2 (pt) |
EP (1) | EP2783135B1 (pt) |
CN (1) | CN103946590B (pt) |
BR (1) | BR112014012105A8 (pt) |
CA (1) | CA2854239C (pt) |
FR (1) | FR2988797B1 (pt) |
IN (1) | IN2014CN04486A (pt) |
RU (1) | RU2561159C1 (pt) |
WO (1) | WO2013076158A1 (pt) |
Families Citing this family (8)
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 |
WO2015173755A1 (en) * | 2014-05-16 | 2015-11-19 | 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 |
DE102022131677A1 (de) * | 2022-11-30 | 2024-06-06 | Liebherr-Aerospace Lindenberg Gmbh | Blockiereinheit, elektromechanische Einheit und Luftfahrzeug |
Family Cites Families (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
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 |
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 |
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 |
RU2277195C2 (ru) * | 2003-02-07 | 2006-05-27 | Государственное предприятие "Харьковское агрегатное конструкторское бюро" (ГП "ХАКБ") | Приводной электромеханизм |
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 |
-
2012
- 2012-04-02 FR FR1253023A patent/FR2988797B1/fr active Active
- 2012-11-21 EP EP12788544.0A patent/EP2783135B1/en active Active
- 2012-11-21 CN CN201280057269.2A patent/CN103946590B/zh active Active
- 2012-11-21 WO PCT/EP2012/073264 patent/WO2013076158A1/en active Application Filing
- 2012-11-21 US US14/358,651 patent/US9038944B2/en active Active
- 2012-11-21 BR BR112014012105A patent/BR112014012105A8/pt not_active IP Right Cessation
- 2012-11-21 CA CA2854239A patent/CA2854239C/en not_active Expired - Fee Related
- 2012-11-21 IN IN4486CHN2014 patent/IN2014CN04486A/en unknown
- 2012-11-21 RU RU2014125270/11A patent/RU2561159C1/ru not_active IP Right Cessation
Also Published As
Publication number | Publication date |
---|---|
CA2854239C (en) | 2016-06-14 |
CA2854239A1 (en) | 2013-05-30 |
US20140326828A1 (en) | 2014-11-06 |
CN103946590B (zh) | 2016-09-28 |
BR112014012105A8 (pt) | 2017-06-20 |
FR2988797B1 (fr) | 2015-04-24 |
RU2561159C1 (ru) | 2015-08-27 |
FR2988797A1 (fr) | 2013-10-04 |
IN2014CN04486A (pt) | 2015-09-11 |
US9038944B2 (en) | 2015-05-26 |
EP2783135B1 (en) | 2017-03-22 |
CN103946590A (zh) | 2014-07-23 |
WO2013076158A1 (en) | 2013-05-30 |
EP2783135A1 (en) | 2014-10-01 |
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Legal Events
Date | Code | Title | Description |
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B06F | Objections, documents and/or translations needed after an examination request according [chapter 6.6 patent gazette] | ||
B08F | Application fees: application dismissed [chapter 8.6 patent gazette] |
Free format text: REFERENTE A 7A ANUIDADE. |
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B08K | Patent lapsed as no evidence of payment of the annual fee has been furnished to inpi [chapter 8.11 patent gazette] |
Free format text: EM VIRTUDE DO ARQUIVAMENTO PUBLICADO NA RPI 2541 DE 17-09-2019 E CONSIDERANDO AUSENCIA DE MANIFESTACAO DENTRO DOS PRAZOS LEGAIS, INFORMO QUE CABE SER MANTIDO O ARQUIVAMENTO DO PEDIDO DE PATENTE, CONFORME O DISPOSTO NO ARTIGO 12, DA RESOLUCAO 113/2013. |
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B350 | Update of information on the portal [chapter 15.35 patent gazette] |