ES2033045T3 - Dispositivo de accionamiento redundante. - Google Patents

Dispositivo de accionamiento redundante.

Info

Publication number
ES2033045T3
ES2033045T3 ES198989107732T ES89107732T ES2033045T3 ES 2033045 T3 ES2033045 T3 ES 2033045T3 ES 198989107732 T ES198989107732 T ES 198989107732T ES 89107732 T ES89107732 T ES 89107732T ES 2033045 T3 ES2033045 T3 ES 2033045T3
Authority
ES
Spain
Prior art keywords
drive device
redundant drive
drive
redundant
electromotors
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
Application number
ES198989107732T
Other languages
English (en)
Inventor
Roland Felkai
Uwe Lenk
Hilmar Petrowitsch
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Erno Raumfahrttechnik GmbH
Original Assignee
Erno Raumfahrttechnik GmbH
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 Erno Raumfahrttechnik GmbH filed Critical Erno Raumfahrttechnik GmbH
Application granted granted Critical
Publication of ES2033045T3 publication Critical patent/ES2033045T3/es
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02KDYNAMO-ELECTRIC MACHINES
    • H02K16/00Machines with more than one rotor or stator
    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02KDYNAMO-ELECTRIC MACHINES
    • H02K7/00Arrangements for handling mechanical energy structurally associated with dynamo-electric machines, e.g. structural association with mechanical driving motors or auxiliary dynamo-electric machines
    • H02K7/10Structural association with clutches, brakes, gears, pulleys or mechanical starters
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T74/00Machine element or mechanism
    • Y10T74/19Gearing
    • Y10T74/19014Plural prime movers selectively coupled to common output

Abstract

DISPOSITIVO DE IMPULSO REDUNDANTE, EN QUE ACTUAN DOS ELECTROMOTORES SOBRE UN MECANISMO EN UN EJE IMPULSOR Y EN QUE AL BLOQUEAR UNO DE LOS MOTORES UN DISPOSITIVO DE ACOPLAMIENTO MECANICO CUIDA DE LA SEPARACION DEL MOTOR DEFECTUOSO DE LA CONEXION IMPULSORA.
ES198989107732T 1988-05-25 1989-04-28 Dispositivo de accionamiento redundante. Expired - Lifetime ES2033045T3 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE3817651A DE3817651A1 (de) 1988-05-25 1988-05-25 Redundante antriebsvorrichtung

Publications (1)

Publication Number Publication Date
ES2033045T3 true ES2033045T3 (es) 1993-03-01

Family

ID=6355042

Family Applications (1)

Application Number Title Priority Date Filing Date
ES198989107732T Expired - Lifetime ES2033045T3 (es) 1988-05-25 1989-04-28 Dispositivo de accionamiento redundante.

Country Status (6)

Country Link
US (1) US5028828A (es)
EP (1) EP0343397B1 (es)
JP (1) JPH0746892B2 (es)
AT (1) ATE77012T1 (es)
DE (1) DE3817651A1 (es)
ES (1) ES2033045T3 (es)

Families Citing this family (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2661476B1 (fr) * 1990-04-27 1995-02-17 Aviac Dispositif d'entrainement electromecanique muni de moyens de secours.
US5134902A (en) * 1991-05-30 1992-08-04 Hung Chin S Auxiliary driving device for a rolling door
US5310138A (en) * 1991-12-30 1994-05-10 Alliedsignal Inc. Wing fold actuator system for aircraft
FR2686855B1 (fr) * 1992-02-03 1994-04-01 Messier Bugatti Actionneur lineaire, notamment pour la manóoeuvre d'une jambe d'atterrisseur d'avion.
IT1309008B1 (it) * 1999-02-24 2002-01-15 Vf Venieri S P A Gruppo di propulsione per veicoli elettrici a quattro ruote motriciper movimento terra e agricoltura
US7011275B2 (en) * 2002-08-07 2006-03-14 Redfern Daniel J Internal spur gear drive
US7028583B2 (en) * 2003-07-30 2006-04-18 Arvinmeritor Technology, Llc Axle assembly with transverse mounted electric motors
US20060087123A1 (en) * 2004-10-22 2006-04-27 Stout David E Dual-rotor, single input/output starter-generator
DE102005044526A1 (de) * 2005-09-16 2007-03-29 Deutsches Zentrum für Luft- und Raumfahrt e.V. Redundantes elektromotorisches Antriebssystem
FR2899871B1 (fr) * 2006-04-12 2008-07-04 Messier Bugatti Sa Atterisseur comportant plusieurs actionneurs electromecaniques d'orientation
US8072172B2 (en) * 2008-12-17 2011-12-06 Honeywell International Inc. Redundant electromechanical actuator for control surfaces
WO2011012101A2 (de) * 2009-07-28 2011-02-03 Schaeffler Technologies Gmbh & Co. Kg Fahrzeugantrieb
DE102009047502A1 (de) * 2009-12-04 2011-06-09 Robert Bosch Gmbh Elektromotor
CN101789648B (zh) * 2009-12-30 2012-07-18 上海交通大学 冗余输入驱动器
DE102011016336A1 (de) 2011-04-07 2012-10-11 Airbus Operations Gmbh Hochauftriebssystem für ein Luftfahrzeug
DE102013212959A1 (de) 2013-07-03 2015-01-22 Deutsches Zentrum für Luft- und Raumfahrt e.V. Redundantes elektromotorisches Ein- oder Mehrphasen-Antriebssystem
EP4264086A1 (en) 2020-12-21 2023-10-25 CEF Industries, LLC Dual drive redundant load transmission device and process

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2427135A (en) * 1943-12-17 1947-09-09 Unit Rig & Equip Drive unit
DE2039174C2 (de) * 1970-08-06 1983-01-27 Lucas Industries Ltd., Birmingham, West Midlands Freilaufvorrichtung
GB1389403A (en) * 1971-06-01 1975-04-03 Westland Aircraft Ltd Helicopter power transmission systems
GB1525571A (en) * 1975-08-22 1978-09-20 High Temperature Eng Ltd Drive trains
US4179944A (en) * 1977-06-27 1979-12-25 United Technologies Corporation Fail safe redundant actuator
US4392393A (en) * 1980-12-01 1983-07-12 General Motors Corporation Dual engine drive
US4607180A (en) * 1983-11-14 1986-08-19 General Dynamics Corporation/Convair Div. Failure tolerant linear drive mechanism intended for celestial space applications
US4685550A (en) * 1985-09-26 1987-08-11 Sundstrand Corporation Quick disconnect mechanism

Also Published As

Publication number Publication date
JPH0223051A (ja) 1990-01-25
DE3817651A1 (de) 1989-12-07
EP0343397B1 (de) 1992-06-03
ATE77012T1 (de) 1992-06-15
US5028828A (en) 1991-07-02
DE3817651C2 (es) 1990-05-03
EP0343397A1 (de) 1989-11-29
JPH0746892B2 (ja) 1995-05-17

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