BR112014019610A2 - - Google Patents
Info
- Publication number
- BR112014019610A2 BR112014019610A2 BR112014019610A BR112014019610A BR112014019610A2 BR 112014019610 A2 BR112014019610 A2 BR 112014019610A2 BR 112014019610 A BR112014019610 A BR 112014019610A BR 112014019610 A BR112014019610 A BR 112014019610A BR 112014019610 A2 BR112014019610 A2 BR 112014019610A2
- Authority
- BR
- Brazil
Links
Classifications
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- 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
- F16H61/00—Control functions within control units of change-speed- or reversing-gearings for conveying rotary motion ; Control of exclusively fluid gearing, friction gearing, gearings with endless flexible members or other particular types of gearing
- F16H61/26—Generation or transmission of movements for final actuating mechanisms
- F16H61/28—Generation or transmission of movements for final actuating mechanisms with at least one movement of the final actuating mechanism being caused by a non-mechanical force, e.g. power-assisted
- F16H61/2807—Generation or transmission of movements for final actuating mechanisms with at least one movement of the final actuating mechanism being caused by a non-mechanical force, e.g. power-assisted using electric control signals for shift actuators, e.g. electro-hydraulic control therefor
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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
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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
- B64C13/30—Transmitting means without power amplification or where power amplification is irrelevant mechanical using cable, chain, or rod mechanisms
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05B—CONTROL OR REGULATING SYSTEMS IN GENERAL; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS OR ELEMENTS
- G05B15/00—Systems controlled by a computer
- G05B15/02—Systems controlled by a computer electric
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Automation & Control Theory (AREA)
- General Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Transmission Devices (AREA)
- Manipulator (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| PCT/US2012/024558 WO2013119242A1 (en) | 2012-02-09 | 2012-02-09 | Actuator system and method |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| BR112014019610A2 true BR112014019610A2 (US07935481-20110503-C00024.png) | 2017-06-20 |
| BR112014019610A8 BR112014019610A8 (pt) | 2017-07-11 |
Family
ID=45771905
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| BR112014019610A BR112014019610A8 (pt) | 2012-02-09 | 2012-02-09 | Sistema de atuador, atuador, e, método de controlar um sistema de atuador |
Country Status (9)
Families Citing this family (30)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB201214952D0 (en) * | 2012-08-22 | 2012-10-03 | Moog Wolverhampton Ltd | Control surface actuation assembly |
| US9816537B2 (en) | 2013-02-27 | 2017-11-14 | Woodward, Inc. | Rotary piston type actuator with a central actuation assembly |
| US9631645B2 (en) | 2013-02-27 | 2017-04-25 | Woodward, Inc. | Rotary piston actuator anti-rotation configurations |
| US9163648B2 (en) | 2013-02-27 | 2015-10-20 | Woodward, Inc. | Rotary piston type actuator with a central actuation assembly |
| US9593696B2 (en) | 2013-02-27 | 2017-03-14 | Woodward, Inc. | Rotary piston type actuator with hydraulic supply |
| US9234535B2 (en) | 2013-02-27 | 2016-01-12 | Woodward, Inc. | Rotary piston type actuator |
| US8955425B2 (en) | 2013-02-27 | 2015-02-17 | Woodward, Inc. | Rotary piston type actuator with pin retention features |
| US9476434B2 (en) | 2013-02-27 | 2016-10-25 | Woodward, Inc. | Rotary piston type actuator with modular housing |
| US9086125B2 (en) * | 2013-03-15 | 2015-07-21 | Moog Inc. | Rotary actuator |
| GB2520693A (en) | 2013-11-27 | 2015-06-03 | Airbus Operations Ltd | Aircraft electric braking system |
| GB2520694A (en) | 2013-11-27 | 2015-06-03 | Airbus Operations Ltd | Aircraft electric braking system |
| GB2520696A (en) | 2013-11-27 | 2015-06-03 | Airbus Operations Ltd | Aircraft electric braking system |
| US10503131B2 (en) * | 2014-08-06 | 2019-12-10 | Danny Harris | Precision shaft alignment system |
| US9950782B2 (en) * | 2014-10-31 | 2018-04-24 | The Boeing Company | Methods and apparatus for integrating rotary actuators in flight control systems |
| US10618645B2 (en) * | 2015-08-25 | 2020-04-14 | Aerovironment, Inc. | Ganged servo flight control system for an unmanned aerial vehicle |
| CA3011439A1 (en) * | 2016-01-13 | 2017-07-20 | Moog Inc. | Summing and fault tolerant rotary actuator assembly |
| US10315753B2 (en) * | 2016-03-29 | 2019-06-11 | The Boeing Company | System and method for controlling aircraft wing flap motion |
| US20190024786A1 (en) * | 2017-07-18 | 2019-01-24 | Dura Operating, Llc | Actuator assembly for a transmission shifter |
| US11149846B2 (en) * | 2017-07-18 | 2021-10-19 | Dus Operating Inc. | Actuator assembly for a transmission shifter |
| JP6779183B2 (ja) * | 2017-07-18 | 2020-11-04 | 川崎重工業株式会社 | 電気機械式アクチュエータを備える航空機操舵システム |
| US10611462B2 (en) * | 2017-08-18 | 2020-04-07 | The Boeing Company | Actuator assemblies for control surfaces of an aircraft, aircraft including the actuator assemblies, and methods of utilizing the same |
| US10487923B2 (en) * | 2017-09-14 | 2019-11-26 | Whippany Actuation Systems Llc | Multi-bar linkage mechanism |
| US10920866B2 (en) * | 2018-06-04 | 2021-02-16 | American Axle & Manufacturing, Inc. | Vehicle driveline component with latching actuator |
| CN111670533B (zh) * | 2019-03-28 | 2022-10-21 | 炼马机电（东莞）有限公司 | 双马达驱动器 |
| US11199248B2 (en) | 2019-04-30 | 2021-12-14 | Woodward, Inc. | Compact linear to rotary actuator |
| WO2021174080A1 (en) | 2020-02-28 | 2021-09-02 | Moog Inc. | Fault tolerant multiple rotary actuator assembly |
| WO2021207482A1 (en) | 2020-04-08 | 2021-10-14 | Woodward, Inc. | Rotary piston type actuator with a central actuation assembly |
| US11208160B1 (en) | 2020-06-25 | 2021-12-28 | AISIN Technical Center of America, Inc. | Adjustable airfoil system for a vehicle |
| CN112550674A (zh) * | 2020-12-16 | 2021-03-26 | 北京北航天宇长鹰无人机科技有限公司 | 舵面传动机构及无人机 |
| CA3160376A1 (en) * | 2021-05-28 | 2022-11-28 | Eaton Intelligent Power Limited | A flight control device and method for increased rigging precision |
Family Cites Families (62)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US129497A (en) | 1872-07-16 | Improvement in windlasses | ||
| GB593642A (en) * | 1945-06-18 | 1947-10-22 | Blackburn Aircraft Ltd | Improvements in or relating to operating mechanisms for interconnectable steering devices |
| US1294970A (en) | 1914-10-31 | 1919-02-18 | Hubert Spence Thomas | Manufacture of tin and terne plates and other like metal-coated plates or sheets and machinery or apparatus to be employed in said manufacture. |
| US2652995A (en) * | 1948-05-18 | 1953-09-22 | Saunders Roe Ltd | Flying controls for aircraft |
| US2695145A (en) | 1950-05-04 | 1954-11-23 | Lear Inc | Boost control system |
| GB730561A (en) | 1951-09-28 | 1955-05-25 | British Messier Ltd | Improvements in or relating to hydraulic jacks |
| US2855793A (en) | 1956-03-05 | 1958-10-14 | English Electric Co Ltd | Control lever mechanism for thin aerofoils |
| FR70758E (fr) | 1956-09-21 | 1959-07-10 | Dispositif d'auto-verrouillage de vérins hydrauliques | |
| DE1555232A1 (de) | 1967-03-07 | 1970-08-13 | Daimler Benz Ag | Getriebe zur UEbertragung einer Bewegung |
| FR1536322A (fr) | 1967-06-30 | 1968-08-10 | Rhone Poulenc Sa | Dispositif pour l'entraînement successif de pièces tournantes |
| FR2030532A5 (US07935481-20110503-C00024.png) * | 1969-07-03 | 1970-11-13 | Snecma | |
| JPS5077044A (US07935481-20110503-C00024.png) | 1973-12-24 | 1975-06-24 | ||
| GB1500404A (en) | 1976-09-03 | 1978-02-08 | Kermode D | Torque generating actuator |
| US4228386A (en) | 1978-06-02 | 1980-10-14 | Sperry Corporation | Aircraft servoactuator apparatus |
| US4225110A (en) | 1978-09-27 | 1980-09-30 | Baker Gac Inc. | Actuator for converting linear to rotary motion |
| US4555978A (en) | 1984-02-14 | 1985-12-03 | Sundstrand Corporation | Multiple displacement motor driven power drive unit |
| SE441385B (sv) | 1984-03-28 | 1985-09-30 | Moveco System Ab | Vridmekanism |
| US4531448A (en) | 1984-05-14 | 1985-07-30 | United Technologies Corporation | Balanced output hydraulic actuator system |
| US4605358A (en) | 1984-12-24 | 1986-08-12 | Sundstrand Corporation | Integrated power drive and power transfer system |
| CN1006929B (zh) * | 1985-05-14 | 1990-02-21 | 联合工艺公司 | 有平衡输出的液压作动器系统 |
| US4685550A (en) | 1985-09-26 | 1987-08-11 | Sundstrand Corporation | Quick disconnect mechanism |
| US4808955A (en) * | 1987-10-05 | 1989-02-28 | Bei Electronics, Inc. | Moving coil linear actuator with interleaved magnetic circuits |
| US4858491A (en) | 1988-01-21 | 1989-08-22 | Plessey Incorporated | Fail-free actuator assembly |
| DE3904869A1 (de) | 1989-02-17 | 1990-08-30 | Dornier Luftfahrt | Einrichtung zur verstellung von rudern, insbesondere fuer luft- oder wasserfahrzeuge |
| JPH03113156A (ja) | 1989-09-27 | 1991-05-14 | Japan Aviation Electron Ind Ltd | 冗長アクチュエータ機構 |
| US5120285A (en) | 1990-10-01 | 1992-06-09 | Sundstrand Corporation | Jam tolerant geared rotary actuator for multiple actuator systems with a single prime mover |
| US5152381A (en) | 1991-09-30 | 1992-10-06 | Rockwell International Corporation | Multiple fail operational rotary actuator with series mounted motor stages |
| FR2706966B1 (US07935481-20110503-C00024.png) | 1993-06-25 | 1995-08-04 | Valeo Thermique Habitacle | |
| US5518466A (en) | 1994-11-29 | 1996-05-21 | Curtiss Wright Flight Systems Inc. | Jam-tolerant rotary actuator |
| FR2738796B1 (fr) * | 1995-09-15 | 1997-12-05 | Aerospatiale | Procede et dispositif de commande de la gouverne de direction d'un aeronef |
| US5701801A (en) | 1995-10-18 | 1997-12-30 | Mcdonnell Douglas Corporation | Mechanically redundant actuator assembly |
| US5628234A (en) | 1995-10-30 | 1997-05-13 | Gec-Marconi Aerospace Inc. | Fail-free actuator assembly |
| US5806806A (en) | 1996-03-04 | 1998-09-15 | Mcdonnell Douglas Corporation | Flight control mechanical backup system |
| JPH10141499A (ja) | 1996-11-15 | 1998-05-29 | Isuzu Motors Ltd | ４位置アクチュエータ及びこれを用いた自動変速機 |
| US5957798A (en) | 1997-09-10 | 1999-09-28 | Gec-Marconi Aerospace Inc. | Fail-free actuator assembly |
| US6189436B1 (en) | 1998-11-03 | 2001-02-20 | Richard L. Brooks | Radial bellcrank actuator |
| JP2001271808A (ja) | 2000-03-23 | 2001-10-05 | Ckd Corp | エアベアリングシリンダ |
| DE10021324A1 (de) | 2000-05-02 | 2001-11-08 | Franz Kirsching | Drehzylinder mit hohem Drehmoment |
| FR2825680B1 (fr) | 2001-06-07 | 2003-09-26 | Sagem | Actionneur de commande de vol primaire a moteur a vibration |
| US20040080197A1 (en) | 2002-10-25 | 2004-04-29 | Robert Kopetzky | Transmission amplifier for bowden cables and method of using the same |
| KR100478986B1 (ko) | 2003-04-03 | 2005-03-31 | 유근형 | 작동 변위 조절기능이 구비된 액츄에이터 |
| FR2882543B1 (fr) | 2005-02-28 | 2008-10-10 | Eurocopter France | Dispositif de verrouillage d'une structure de fixation d'une pale au moyeu d'un rotor de giravion |
| US20060255207A1 (en) | 2005-05-11 | 2006-11-16 | Honeywell International, Inc. | Flight control surface actuation system with redundantly configured actuator assemblies |
| US7607611B2 (en) | 2005-05-11 | 2009-10-27 | Honeywell International Inc. | Flight control surface actuation system with redundantly configured and lockable actuator assemblies |
| US20070068291A1 (en) | 2005-08-24 | 2007-03-29 | Reinhard Beatty | Failure-tolerant redundant actuator system |
| US7651051B2 (en) | 2005-11-08 | 2010-01-26 | University Of Delaware | Mechanism for biaxial rotation of a wing and vehicle containing such mechanism |
| DE202006003589U1 (de) | 2006-03-07 | 2007-07-19 | Kinshofer Gmbh | Drehmotor |
| US20080203223A1 (en) | 2006-06-22 | 2008-08-28 | Cyrot Luc P | Aircraft stabilizer actuator |
| US7463004B2 (en) * | 2006-07-10 | 2008-12-09 | Xerox Corporation | Planetary dual stepper drives |
| GB0616730D0 (en) | 2006-08-23 | 2006-10-04 | Airbus Uk Ltd | Jam-tolerant actuator |
| WO2008028184A2 (en) | 2006-09-01 | 2008-03-06 | Parker Hannifin Corporation | Electromechanical actuating assembly |
| FR2906220B1 (fr) | 2006-09-21 | 2009-10-02 | Airbus France Sas | Avion a servocommandes deportees |
| ES2353975T3 (es) | 2006-10-18 | 2011-03-08 | Moog Inc. | Accionadores de tipo diferencial con redundancia, resistentes al bloqueo. |
| DE202006016354U1 (de) | 2006-10-23 | 2008-02-28 | Asturia Automotive Systems Ag | Einrichtung zum Ausgleich und/oder zur Übertragung von Kräften/Momenten und Drehbewegungen zwischen zwei Bauteilen |
| US7418912B2 (en) * | 2006-10-26 | 2008-09-02 | Northrop Grumman Systems Corporation | Steering system and an associated vessel |
| JP4901438B2 (ja) | 2006-11-30 | 2012-03-21 | 株式会社クボタ | トラクタのｐｔｏ構造 |
| JP4451461B2 (ja) | 2007-03-29 | 2010-04-14 | ナブテスコ株式会社 | ステアリングアクチュエータシステム |
| WO2009020452A1 (en) * | 2007-08-08 | 2009-02-12 | Moog Inc. | Fault-tolerant actuator assembly, and method of moving a member relative to a support |
| US8336818B2 (en) | 2007-10-30 | 2012-12-25 | Parker-Hannifin Corporation | Jam tolerant electromechanical actuation systems and methods of operation |
| US7994672B2 (en) | 2008-12-30 | 2011-08-09 | Woodward Hrt, Inc. | Limited angle external rotor motor actuator system |
| DE102010024121B4 (de) * | 2010-06-17 | 2017-04-06 | Airbus Defence and Space GmbH | Stellantriebseinheit |
| US8847691B2 (en) | 2011-11-16 | 2014-09-30 | Qualcomm Incorporated | Apparatus and method for recovering burst-mode pulse width modulation (PWM) and non-return-to-zero (NRZ) data |
-
2012
- 2012-02-09 ES ES12706371.7T patent/ES2659412T3/es active Active
- 2012-02-09 CA CA2863583A patent/CA2863583C/en active Active
- 2012-02-09 BR BR112014019610A patent/BR112014019610A8/pt not_active IP Right Cessation
- 2012-02-09 US US14/376,000 patent/US10281033B2/en active Active
- 2012-02-09 KR KR1020147025432A patent/KR101842235B1/ko active IP Right Grant
- 2012-02-09 CN CN201280072035.5A patent/CN104540732B/zh active Active
- 2012-02-09 WO PCT/US2012/024558 patent/WO2013119242A1/en active Application Filing
- 2012-02-09 EP EP12706371.7A patent/EP2812242B1/en active Active
- 2012-02-09 JP JP2014556527A patent/JP6203199B2/ja not_active Expired - Fee Related
-
2019
- 2019-05-03 US US16/402,542 patent/US11248698B2/en active Active
Also Published As
| Publication number | Publication date |
|---|---|
| CN104540732A (zh) | 2015-04-22 |
| EP2812242B1 (en) | 2017-11-15 |
| CA2863583A1 (en) | 2013-08-15 |
| US11248698B2 (en) | 2022-02-15 |
| CN104540732B (zh) | 2018-02-06 |
| US20150081102A1 (en) | 2015-03-19 |
| JP2015506876A (ja) | 2015-03-05 |
| KR101842235B1 (ko) | 2018-03-27 |
| ES2659412T3 (es) | 2018-03-15 |
| US20190257419A1 (en) | 2019-08-22 |
| US10281033B2 (en) | 2019-05-07 |
| KR20140138715A (ko) | 2014-12-04 |
| EP2812242A1 (en) | 2014-12-17 |
| JP6203199B2 (ja) | 2017-09-27 |
| BR112014019610A8 (pt) | 2017-07-11 |
| WO2013119242A1 (en) | 2013-08-15 |
| CA2863583C (en) | 2019-03-26 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| B08F | Application dismissed because of non-payment of annual fees [chapter 8.6 patent gazette] | ||
| B08K | Patent lapsed as no evidence of payment of the annual fee has been furnished to inpi [chapter 8.11 patent gazette] |