DE3533720C2 - - Google Patents

Info

Publication number
DE3533720C2
DE3533720C2 DE3533720A DE3533720A DE3533720C2 DE 3533720 C2 DE3533720 C2 DE 3533720C2 DE 3533720 A DE3533720 A DE 3533720A DE 3533720 A DE3533720 A DE 3533720A DE 3533720 C2 DE3533720 C2 DE 3533720C2
Authority
DE
Germany
Prior art keywords
power transmission
transmission unit
motor
generator
hydraulic
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
Application number
DE3533720A
Other languages
German (de)
English (en)
Other versions
DE3533720A1 (de
Inventor
Burkhard Dipl.-Ing. 8012 Ottobrunn De Deter
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.)
Airbus Defence and Space GmbH
Original Assignee
Messerschmitt Bolkow Blohm AG
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 Messerschmitt Bolkow Blohm AG filed Critical Messerschmitt Bolkow Blohm AG
Priority to DE19853533720 priority Critical patent/DE3533720A1/de
Priority to US06/898,257 priority patent/US4754940A/en
Priority to FR8613173A priority patent/FR2587678B3/fr
Publication of DE3533720A1 publication Critical patent/DE3533720A1/de
Application granted granted Critical
Publication of DE3533720C2 publication Critical patent/DE3533720C2/de
Granted legal-status Critical Current

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
    • B64C13/38—Transmitting means with power amplification
    • B64C13/50—Transmitting means with power amplification using electrical energy
    • 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
    • B64C13/40—Transmitting means with power amplification using fluid pressure
    • B64C13/42—Transmitting means with power amplification using fluid pressure having duplication or stand-by provisions
    • 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
    • Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S60/00—Power plants
    • Y10S60/911—Fluid motor system incorporating electrical system

Landscapes

  • Engineering & Computer Science (AREA)
  • Automation & Control Theory (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Fluid-Pressure Circuits (AREA)
  • Stand-By Power Supply Arrangements (AREA)
  • Control Of Fluid Gearings (AREA)
DE19853533720 1985-09-21 1985-09-21 Notversorgungssystem Granted DE3533720A1 (de)

Priority Applications (3)

Application Number Priority Date Filing Date Title
DE19853533720 DE3533720A1 (de) 1985-09-21 1985-09-21 Notversorgungssystem
US06/898,257 US4754940A (en) 1985-09-21 1986-08-20 Emergency supply system for an aircraft control system
FR8613173A FR2587678B3 (fr) 1985-09-21 1986-09-19 Systeme d'alimentation de secours pour le maintien de la commande de vol de secours d'un avion

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19853533720 DE3533720A1 (de) 1985-09-21 1985-09-21 Notversorgungssystem

Publications (2)

Publication Number Publication Date
DE3533720A1 DE3533720A1 (de) 1987-04-16
DE3533720C2 true DE3533720C2 (enExample) 1988-10-20

Family

ID=6281586

Family Applications (1)

Application Number Title Priority Date Filing Date
DE19853533720 Granted DE3533720A1 (de) 1985-09-21 1985-09-21 Notversorgungssystem

Country Status (3)

Country Link
US (1) US4754940A (enExample)
DE (1) DE3533720A1 (enExample)
FR (1) FR2587678B3 (enExample)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102011108535A1 (de) * 2011-07-26 2013-01-31 Airbus Operations Gmbh Hydraulische Motor-Pumpen-Anordnung und Hydrauliksystem für ein Fahrzeug
DE102024118657A1 (de) * 2024-07-02 2026-01-08 Liebherr-Aerospace Lindenberg Gmbh Verschleißreduzierte Pumpenanordnung für ein Luftfahrzeug

Families Citing this family (41)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2603866A1 (fr) * 1986-09-12 1988-03-18 Messerschmitt Boelkow Blohm Systeme de commande de gouvernes de profondeur
US5074495A (en) * 1987-12-29 1991-12-24 The Boeing Company Load-adaptive hybrid actuator system and method for actuating control surfaces
US4912921A (en) * 1988-03-14 1990-04-03 Sundstrand Corporation Low speed spool emergency power extraction system
US5542445A (en) * 1995-04-20 1996-08-06 Adams; George R. Temperature and impact sensitive safety valve
US6023134A (en) * 1996-10-25 2000-02-08 Daimlerchrysler Aerospace Airbus Gmbh Power conversion system for bi-directional conversion between hydraulic power and electrical power
ES2200104T3 (es) * 1996-10-25 2004-03-01 Airbus Deutschland Gmbh Sistema convertidor de energia para la transformacion bidireccional entre energia hidraulica y electrica.
US5971319A (en) * 1997-09-05 1999-10-26 Zero-Gravity Corporation System for converting jet aircraft to parabolic flight operation
FR2787759B1 (fr) * 1998-12-28 2001-03-16 Aerospatiale Procede et systeme de commande d'une gouverne d'un aeronef a actionnement par verins hydrauliques multiples et a puissance modulable
US6464166B1 (en) 2001-05-29 2002-10-15 Romeo Yankee Ltd. Ducted fan vehicles particularly useful as VTOL aircraft
US7275712B2 (en) * 2002-05-28 2007-10-02 Urban Aeronautics, Ltd. Ducted fan vehicles particularly useful as VTOL aircraft
AU2002309237A1 (en) * 2001-06-04 2002-12-16 Romeo Yankee Ltd. Vehicles particularly useful as vtol vehicles
US6718762B2 (en) * 2002-03-07 2004-04-13 The Boeing Company Contingency hydraulic power unit
US20060113426A1 (en) * 2002-08-05 2006-06-01 Raphael Yoeli Vtol vehicles
US7857253B2 (en) 2003-10-27 2010-12-28 Urban Aeronautics Ltd. Ducted fan VTOL vehicles
CA2605111A1 (en) * 2005-01-10 2006-07-13 Raphael Yoeli Ducted fan vtol vehicles
US7600715B2 (en) * 2005-03-25 2009-10-13 Nabtesco Corporation Local backup hydraulic actuator for aircraft control systems
US7946528B2 (en) * 2005-04-15 2011-05-24 Urban Aeronautics, Ltd. Flight control system especially suited for VTOL vehicles
US7717368B2 (en) * 2005-06-07 2010-05-18 Urban Aeronautics Ltd. Apparatus for generating horizontal forces in aerial vehicles and related method
DE102005059423A1 (de) * 2005-12-13 2007-06-21 Airbus Deutschland Gmbh Verfahren und Einrichtung zur redundanten Versorgung von mehreren elektrischen Stell-oder Antriebsmotoren durch eine gemeinsame Leistungselektronikeinheit
WO2007099543A2 (en) 2006-03-01 2007-09-07 Urban Aeronautics Ltd. Ground effect vanes arrangement
EP2021240A2 (en) * 2006-05-03 2009-02-11 Urban Aeronautics Ltd. Ducted fan vtol vehicles
FR2902080B1 (fr) * 2006-06-13 2009-04-17 Airbus France Sas Dispositif et procede de suveillance d'un aeronef
WO2008065654A2 (en) 2006-11-27 2008-06-05 Urban Aeronautics Ltd. Wall effects on vtol vehicles
US20100076625A1 (en) * 2006-11-30 2010-03-25 Raphael Yoeli Flight control cockpit modes in ducted fan vtol vehicles
DE102007017820A1 (de) * 2007-01-16 2008-08-07 Liebherr-Aerospace Lindenberg Gmbh Energieversorgungssystem eines Luftfahrzeuges
US20080211309A1 (en) * 2007-03-01 2008-09-04 Nolte William J Systems and methods for modular battery replacement in aircraft
EP2152576A2 (en) 2007-05-02 2010-02-17 Urban Aeronautics Ltd. Control flows and forces in vtol vehicles
WO2009077968A2 (en) * 2007-12-14 2009-06-25 Urban Aeronautics Ltd. Redundancies and flows in vehicles
DE102008007840A1 (de) * 2008-02-07 2009-08-13 Airbus Deutschland Gmbh Triebwerksgetriebene Hydraulikpumpe
US8038094B2 (en) * 2008-03-31 2011-10-18 Honda Motor Co., Ltd. Hydraulic system for aircraft
US8342441B2 (en) 2008-09-02 2013-01-01 Urban Aeronautics Ltd. VTOL vehicle with coaxially tilted or tiltable rotors
FR2943036B1 (fr) * 2009-03-11 2011-04-15 Airbus France Systeme distribue de commande de vol implemente selon une architecture avionique modulaire integree.
US8882028B2 (en) * 2009-09-21 2014-11-11 Aerion Corporation Aircraft emergency and backup secondary power apparatus
US8434301B2 (en) 2010-04-16 2013-05-07 Nabtesco Corporation Local backup hydraulic actuator for aircraft control systems
US8876038B2 (en) 2010-10-05 2014-11-04 Urban Aeronautics Ltd. Ducted fan for VTOL vehicles with system and method to reduce roll moments
US9163562B2 (en) * 2012-03-14 2015-10-20 United Technologies Corporation Constant speed pump system for engine ECS loss elimination
CN105121188B (zh) 2013-03-15 2019-03-15 特力飞车股份有限公司 具有垂直起飞和固定翼巡航能力的组合的飞行/行驶车辆
WO2016049027A1 (en) * 2014-09-23 2016-03-31 Sikorsky Aircraft Corporation Hybrid electric power drive system for a rotorcraft
DE102015215430A1 (de) * 2015-08-13 2017-02-16 Siemens Aktiengesellschaft Luftfahrzeug und Verfahren zum Betrieb eines Luftfahrzeuges
CN109153302A (zh) 2016-04-15 2019-01-04 特力飞车股份有限公司 用于双模式飞行和驾驶车辆的电子换档器组件
CN106564587B (zh) * 2016-10-12 2019-10-11 天津远度科技有限公司 舵机保护系统及方法、无人机

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2616264A (en) * 1948-02-06 1952-11-04 Hughes Tool Co Hydraulic by-pass control
US2619304A (en) * 1950-01-09 1952-11-25 Northrop Aircraft Inc Full power hydraulic safety system
US2977071A (en) * 1957-01-23 1961-03-28 Hispano Suiza Sa Hydraulic control system for aircraft
US3315085A (en) * 1965-03-12 1967-04-18 Abex Corp Auxiliary hydraulic and electrical power supply system for aircraft
DE2315906A1 (de) * 1973-03-30 1974-10-10 Ver Flugtechnische Werke Anordnung zur ueberwachung und steuerung eines redundanten elektrohydraulischen stellantriebs
DE3111722C2 (de) * 1981-03-25 1984-11-15 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Passives Leitungssystem für Luftfahrzeuge zur Übertragung von Steuersignalen

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102011108535A1 (de) * 2011-07-26 2013-01-31 Airbus Operations Gmbh Hydraulische Motor-Pumpen-Anordnung und Hydrauliksystem für ein Fahrzeug
DE102024118657A1 (de) * 2024-07-02 2026-01-08 Liebherr-Aerospace Lindenberg Gmbh Verschleißreduzierte Pumpenanordnung für ein Luftfahrzeug

Also Published As

Publication number Publication date
DE3533720A1 (de) 1987-04-16
US4754940A (en) 1988-07-05
FR2587678A1 (fr) 1987-03-27
FR2587678B3 (fr) 1987-12-24

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Legal Events

Date Code Title Description
OP8 Request for examination as to paragraph 44 patent law
8120 Willingness to grant licences paragraph 23
D2 Grant after examination
8364 No opposition during term of opposition
8327 Change in the person/name/address of the patent owner

Owner name: DEUTSCHE AEROSPACE AG, 8000 MUENCHEN, DE

8327 Change in the person/name/address of the patent owner

Owner name: DAIMLER-BENZ AEROSPACE AKTIENGESELLSCHAFT, 80804 M

8339 Ceased/non-payment of the annual fee