DE3883365D1 - Betaetigungseinrichtung mit loesemechanismus fuer den stoerfall. - Google Patents
Betaetigungseinrichtung mit loesemechanismus fuer den stoerfall.Info
- Publication number
- DE3883365D1 DE3883365D1 DE8888310243T DE3883365T DE3883365D1 DE 3883365 D1 DE3883365 D1 DE 3883365D1 DE 8888310243 T DE8888310243 T DE 8888310243T DE 3883365 T DE3883365 T DE 3883365T DE 3883365 D1 DE3883365 D1 DE 3883365D1
- Authority
- DE
- Germany
- Prior art keywords
- fall
- operating device
- release mechanism
- release
- operating
- 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.)
- Expired - Lifetime
Links
Classifications
-
- 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
- F16H25/205—Screw mechanisms comprising alternate power paths, e.g. for fail safe back-up
-
- 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
- B64C13/38—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
- F16H2025/2062—Arrangements for driving the actuator
- F16H2025/2071—Disconnecting drive source from the actuator, e.g. using clutches for release of drive connection during manual control
-
- 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
- Y10T74/18624—Plural inputs, single output
-
- 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
- Y10T74/19—Gearing
- Y10T74/19023—Plural power paths to and/or from gearing
- Y10T74/19051—Single driven plural drives
- Y10T74/19056—Parallel
-
- 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
- Y10T74/19—Gearing
- Y10T74/19023—Plural power paths to and/or from gearing
- Y10T74/19144—Miscellaneous [plural power paths]
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US14630188A | 1988-01-21 | 1988-01-21 | |
US07/183,928 US4858491A (en) | 1988-01-21 | 1988-04-20 | Fail-free actuator assembly |
Publications (1)
Publication Number | Publication Date |
---|---|
DE3883365D1 true DE3883365D1 (de) | 1993-09-23 |
Family
ID=26843772
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE8888310243T Expired - Lifetime DE3883365D1 (de) | 1988-01-21 | 1988-11-01 | Betaetigungseinrichtung mit loesemechanismus fuer den stoerfall. |
Country Status (4)
Country | Link |
---|---|
US (1) | US4858491A (de) |
EP (1) | EP0325027B1 (de) |
JP (1) | JPH01238758A (de) |
DE (1) | DE3883365D1 (de) |
Families Citing this family (47)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5511439A (en) * | 1994-07-22 | 1996-04-30 | Las Navas Garcia; Jose M. | Pushing mechansim |
US5628234A (en) * | 1995-10-30 | 1997-05-13 | Gec-Marconi Aerospace Inc. | Fail-free actuator assembly |
US5918836A (en) * | 1997-03-25 | 1999-07-06 | Sundstrand Corporation | Aircraft spoiler blow-down mechanism |
US5957798A (en) * | 1997-09-10 | 1999-09-28 | Gec-Marconi Aerospace Inc. | Fail-free actuator assembly |
EP1167822B1 (de) * | 1997-11-03 | 2006-08-16 | Honeywell Ag | Einrichtung zur Erzeugung einer Längsbewegung und/oder einer Drehbewegung |
FR2778797B1 (fr) * | 1998-05-12 | 2000-08-04 | Lucas Aerospace Fcs | Actionneur electro-mecanique du type a systeme vis/ecrou |
US6461265B1 (en) * | 2000-02-02 | 2002-10-08 | Ex-Cello Machine Tools, Inc. | Coaxial gear box |
WO2001071217A1 (en) * | 2000-03-22 | 2001-09-27 | Alliedsignal Inc. | Dual load path ball screw with thrust bearing |
FR2832685A1 (fr) * | 2001-11-23 | 2003-05-30 | Conception & Dev Michelin Sa | Direction electrique pour vehicule, a redondance triple |
DE10308301B3 (de) * | 2003-02-26 | 2004-07-15 | Liebherr-Aerospace Lindenberg Gmbh | Flugzeughochauftriebssystem mit Überlastsicherung |
US20050084345A1 (en) * | 2003-10-17 | 2005-04-21 | Frye Randy C. | Dual motor tapping machine |
US7098619B2 (en) * | 2004-01-28 | 2006-08-29 | Stridsberg Innovation Ab | Actuator and movement linkage system |
US7834494B2 (en) * | 2004-06-04 | 2010-11-16 | The Boeing Company | Fault-tolerant electromechanical actuator having a torque sensing control system |
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 |
US7211971B2 (en) * | 2005-03-31 | 2007-05-01 | Hitachi Automotive Products (Usa), Inc. | Linear actuator |
US7560888B2 (en) * | 2005-09-08 | 2009-07-14 | Honeywell International Inc. | Electromechanical actuator including redundant, dissimilar position feedback |
US7536927B2 (en) * | 2006-06-05 | 2009-05-26 | Brose Fahrzeugteile GmbH & Co. Kommanditgesellschaft, Würzburg | Window lift drive for raising and lowering windows in a vehicle door |
EP2074026B1 (de) | 2006-10-18 | 2010-09-08 | Moog Inc. | Blockierungstolerante differential-stellglieder |
GB0719689D0 (en) * | 2007-10-09 | 2007-11-14 | Goodrich Actuation Systems Ltd | Actuator arrangement |
DE102008047521A1 (de) * | 2008-09-16 | 2010-04-15 | Mbb Palfinger Gmbh | Hubladebühne |
US8499653B1 (en) * | 2009-06-18 | 2013-08-06 | The Boeing Company | Fault tolerant electro-mechanical actuator |
BR112012000883A2 (pt) * | 2009-07-14 | 2016-03-08 | Woodward Hrt Inc | montagem de servo-válvula |
US8322242B2 (en) * | 2009-09-29 | 2012-12-04 | Hamilton Sundstrand Corporation | Velocity summing linear actuator |
US8127912B2 (en) * | 2009-12-15 | 2012-03-06 | Hamilton Sundstrand Corporation | Feedback torque limiter |
US8424416B2 (en) * | 2010-06-18 | 2013-04-23 | Hamilton Sundstrand Corporation | Layshaft generator |
EP2415669B1 (de) | 2010-08-04 | 2015-05-13 | AIRBUS HELICOPTERS DEUTSCHLAND GmbH | Steuersystem |
GB2489503A (en) * | 2011-03-31 | 2012-10-03 | Ge Aviat Systems Ltd | Rotary actuator and method of operation with failsafe mechanism |
GB2490959A (en) | 2011-05-20 | 2012-11-21 | Ge Aviat Systems Ltd | High integrity linear actuator |
EP2812242B1 (de) | 2012-02-09 | 2017-11-15 | Moog Inc. | Aktuatorsystem und methode |
US9255632B2 (en) | 2012-05-23 | 2016-02-09 | Hamilton Sundstrand Corporation | Integrated torque limiter/no-back device |
US9086125B2 (en) | 2013-03-15 | 2015-07-21 | Moog Inc. | Rotary actuator |
EP2981740A1 (de) * | 2013-04-03 | 2016-02-10 | Thomson Industries Inc. | Verdrehsichere vorrichtung für ein linearstellglied und linearstellglied damit |
CN103968811B (zh) * | 2013-04-18 | 2016-02-17 | 常州华达科捷光电仪器有限公司 | 一种调整机构及具有该调整机构的激光准直仪器 |
EP3052835A2 (de) * | 2013-10-02 | 2016-08-10 | Linak A/S | Linearer aktuator |
CN104595451B (zh) * | 2013-10-31 | 2017-04-05 | 北京精密机电控制设备研究所 | 一种双输入通道差速器式机电作动器 |
EP3143306B1 (de) | 2014-05-16 | 2021-06-23 | Bombardier Inc. | Aktuatoren und verfahren für flugzeugflugsteuerungsoberflächen |
US9586675B2 (en) * | 2014-06-09 | 2017-03-07 | The Boeing Company | Apparatus and method for arrestment of a flight control surface |
TWI550216B (zh) * | 2014-07-21 | 2016-09-21 | 第一傳動科技股份有限公司 | 線性致動器 |
US10066715B2 (en) | 2015-04-24 | 2018-09-04 | Moog Inc. | Fail-safe electromechanical actuator |
US10024405B2 (en) * | 2015-05-12 | 2018-07-17 | Hamilton Sundstrand Corporation | Dual redundant linear actuator |
WO2017123987A1 (en) | 2016-01-13 | 2017-07-20 | Moog Inc. | Summing and fault tolerant rotary actuator assembly |
FR3055308B1 (fr) * | 2016-08-26 | 2018-08-17 | Safran Aircraft Engines | Moyen de commande d'un systeme de changement de pas comprenant un dispositif anti-rotation, systeme de changement de pas equipe dudit moyen de commande et turbomachine correspondante |
IT201700058891A1 (it) * | 2017-05-30 | 2018-11-30 | Umbragroup S P A | Metodo per verificare un guasto elettrico, elettronico e/o meccanico in un attuatore elettromeccanico lineare |
CN111137437A (zh) * | 2019-12-27 | 2020-05-12 | 航天时代飞鸿技术有限公司 | 一种双余度电动舵机 |
TWM614035U (zh) * | 2021-03-09 | 2021-07-01 | 第一傳動科技股份有限公司 | 具有可限位快速釋放結構的線性致動器 |
US11591192B2 (en) * | 2021-03-29 | 2023-02-28 | Elgoteam Ltd | Electro mechanical operated bollard |
CN113697089A (zh) * | 2021-08-26 | 2021-11-26 | 航天时代飞鹏有限公司 | 一种电气双余度舵机 |
Family Cites Families (26)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2630022A (en) * | 1951-10-26 | 1953-03-03 | Boeing Co | Dual screw drive |
US3081664A (en) * | 1960-01-20 | 1963-03-19 | Voigtlaender Ag | Block type photographic viewfinder with parallax compensation |
US3277736A (en) * | 1964-07-27 | 1966-10-11 | Goodman Robert | Device for translating rotary motion into linear motion |
US3682283A (en) * | 1970-03-02 | 1972-08-08 | Mitumasa Sato | Motor-driven actuator and safety overload mechanism therefor |
US3766790A (en) * | 1971-12-29 | 1973-10-23 | Boeing Co | Non-jamming ball screw linear actuator |
US3735228A (en) * | 1972-01-03 | 1973-05-22 | E Systems Inc | Non-electronic servo actuator |
US3858452A (en) * | 1973-07-09 | 1975-01-07 | Vemco Products Inc | Emergency release for screw drive operator traveler assembly |
US3950686A (en) * | 1974-12-11 | 1976-04-13 | Trw Inc. | Series redundant drive system |
US4046241A (en) * | 1976-03-24 | 1977-09-06 | Essex Group, Inc. | Over-ride mechanism for screw drive actuator |
US4179944A (en) * | 1977-06-27 | 1979-12-25 | United Technologies Corporation | Fail safe redundant actuator |
US4094481A (en) * | 1977-06-30 | 1978-06-13 | Sperry Rand Corporation | Fail passive dual servo with continuous motor speed and acceleration and monitoring |
US4162438A (en) * | 1978-03-27 | 1979-07-24 | Sperry Rand Corporation | Dual servo automatic pilot with improved failure monitoring |
US4226129A (en) * | 1978-04-12 | 1980-10-07 | Harvey Henderson | Worm drive mechanism |
US4289996A (en) * | 1978-08-29 | 1981-09-15 | Frazer Nash Limited | Actuators |
US4304375A (en) * | 1979-05-17 | 1981-12-08 | Textron Inc. | Electrically controlled elevator |
FR2468798A1 (fr) * | 1979-09-11 | 1981-05-08 | Tech Integrale | Mecanisme debrayable, de vis et ecrou a roulement |
US4614128A (en) * | 1981-12-18 | 1986-09-30 | Lars International S.A., Luxembourg | Linear drive device with two motors |
US4591313A (en) * | 1983-12-30 | 1986-05-27 | The Boeing Company | Propeller pitch control system and apparatus |
US4574654A (en) * | 1984-01-30 | 1986-03-11 | Griffiths Edward E | Selectively engageable linear power actuator |
CA1238210A (en) * | 1984-02-07 | 1988-06-21 | Yvan Poulin | Drive mechanism |
FR2562028B1 (fr) * | 1984-04-03 | 1986-06-27 | Aerospatiale | Systeme pour la commande d'une surface aerodynamique horizontale a incidence variable d'un aeronef et agencement de commande hydraulique a servovalve pour un tel systeme |
US4603594A (en) * | 1984-05-31 | 1986-08-05 | Sundstrand Corporation | Fail safe actuator |
US4637272A (en) * | 1985-10-28 | 1987-01-20 | Sundstrand Corporation | Ballscrew actuator |
US4663985A (en) * | 1986-03-07 | 1987-05-12 | Sundstrand Corporation | Shaft relative speed limiting system |
US4751988A (en) * | 1986-03-17 | 1988-06-21 | Sundstrand Corporation | Torque limiting and overtravel stop device |
US4745815A (en) * | 1986-12-08 | 1988-05-24 | Sundstrand Corporation | Non-jamming screw actuator system |
-
1988
- 1988-04-20 US US07/183,928 patent/US4858491A/en not_active Expired - Lifetime
- 1988-11-01 EP EP88310243A patent/EP0325027B1/de not_active Expired - Lifetime
- 1988-11-01 DE DE8888310243T patent/DE3883365D1/de not_active Expired - Lifetime
-
1989
- 1989-01-20 JP JP1010120A patent/JPH01238758A/ja active Pending
Also Published As
Publication number | Publication date |
---|---|
EP0325027A1 (de) | 1989-07-26 |
EP0325027B1 (de) | 1993-08-18 |
US4858491A (en) | 1989-08-22 |
JPH01238758A (ja) | 1989-09-22 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
8332 | No legal effect for de |