CA2219293A1 - Power conversion system for bi-directional conversion between hydraulic energy and electrical energy - Google Patents
Power conversion system for bi-directional conversion between hydraulic energy and electrical energyInfo
- Publication number
- CA2219293A1 CA2219293A1 CA002219293A CA2219293A CA2219293A1 CA 2219293 A1 CA2219293 A1 CA 2219293A1 CA 002219293 A CA002219293 A CA 002219293A CA 2219293 A CA2219293 A CA 2219293A CA 2219293 A1 CA2219293 A1 CA 2219293A1
- Authority
- CA
- Canada
- Prior art keywords
- hydraulic
- electrical
- power
- machine
- control unit
- 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.)
- Granted
Links
- 238000006243 chemical reaction Methods 0.000 title abstract 5
Classifications
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02J—CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
- H02J4/00—Circuit arrangements for mains or distribution networks not specified as ac or dc
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D41/00—Power installations for auxiliary purposes
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02J—CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
- H02J2310/00—The network for supplying or distributing electric power characterised by its spatial reach or by the load
- H02J2310/40—The network being an on-board power network, i.e. within a vehicle
- H02J2310/44—The network being an on-board power network, i.e. within a vehicle for aircrafts
-
- 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
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/40—Weight reduction
Landscapes
- Engineering & Computer Science (AREA)
- Power Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Control Of Eletrric Generators (AREA)
- Control Of Electric Motors In General (AREA)
- Fluid-Pressure Circuits (AREA)
- Supply And Distribution Of Alternating Current (AREA)
- Electric Propulsion And Braking For Vehicles (AREA)
Abstract
A bi-directional power conversion system interconnects hydraulic and electrical power systems on-board a vehicle such as an aircraft, whereby the power conversion system can selectively convert available electrical power to needed hydraulic power or vice versa. The power conversion system includes a hydraulic machine connected to the hydraulic system of the vehicle, an electrical machine connected to the electrical system of the vehicle through a power converter and control unit, a rotational drive shaft mechanically interconnecting the hydraulic machine and the electrical machine, and a priority and safety control unit that controls the operation of the system. In a first operating mode, for example in the event of a failure of a primary electrical generator, the hydraulic machine operates as a hydraulic motor driven by available hydraulic power from the hydraulic system to drive the electrical machine which operates as an electrical generator to provide electrical power into the electrical system. In a second operating mode, for example in the event of a failure of a primary hydraulic pump, the electrical machine operates as an electric motor driven by electric power from the electrical system to drive the hydraulic machine operating as a hydraulic pump to provide hydraulic power into the hydraulic system. A hydraulic valve arrangement and an electrical switch arrangement, as well as pressure and speed regulators are controlled by the control unit, and the system operation is monitored by sensors connected to the control unit, to activate the appropriate operating mode.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE19644340 | 1996-10-25 | ||
DE19644340.7 | 1996-10-25 |
Publications (2)
Publication Number | Publication Date |
---|---|
CA2219293A1 true CA2219293A1 (en) | 1998-04-25 |
CA2219293C CA2219293C (en) | 2004-01-20 |
Family
ID=7809939
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CA002219293A Expired - Fee Related CA2219293C (en) | 1996-10-25 | 1997-10-27 | Power conversion system for bi-directional conversion between hydraulic energy and electrical energy |
Country Status (7)
Country | Link |
---|---|
EP (1) | EP0838396B1 (en) |
JP (1) | JP4044991B2 (en) |
CN (1) | CN1185421C (en) |
CA (1) | CA2219293C (en) |
DE (2) | DE59710114D1 (en) |
ES (1) | ES2200104T3 (en) |
RU (1) | RU2141912C1 (en) |
Families Citing this family (31)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB9926354D0 (en) * | 1999-11-08 | 2000-01-12 | Rolls Royce Plc | Power supply system for an aircraft |
US7210653B2 (en) * | 2002-10-22 | 2007-05-01 | The Boeing Company | Electric-based secondary power system architectures for aircraft |
US7439634B2 (en) * | 2004-08-24 | 2008-10-21 | Honeywell International Inc. | Electrical starting, generation, conversion and distribution system architecture for a more electric vehicle |
FR2882200B1 (en) * | 2005-02-17 | 2015-05-01 | Hispano Suiza Sa | ELECTRICAL POWER SUPPLY FOR GAS TURBINE AIRCRAFT ENGINE EQUIPMENT |
FR2892680B1 (en) | 2005-11-02 | 2008-02-08 | Giat Ind Sa | DEVICE FOR SAFEGUARDING ELECTRICAL SERVITUDES |
DE102008011141B4 (en) | 2008-02-26 | 2010-02-18 | Hydac System Gmbh | Energy conversion device |
US8667788B2 (en) * | 2010-04-09 | 2014-03-11 | Shipstone Corporation | System and method for energy storage and retrieval |
DE102011108535A1 (en) | 2011-07-26 | 2013-01-31 | Airbus Operations Gmbh | Hydraulic motor-pump assembly and hydraulic system for a vehicle |
GB2493711B (en) * | 2011-08-12 | 2018-04-25 | Openhydro Ip Ltd | Method and system for controlling hydroelectric turbines |
FR2983319B1 (en) * | 2011-11-25 | 2014-02-07 | Turbomeca | METHOD AND SYSTEM FOR CONTROLLING POWER IN CASE OF FAILURE OF AT LEAST ONE AIRCRAFT ENGINE |
CN103187860A (en) * | 2011-12-30 | 2013-07-03 | 哈米尔顿森德斯特兰德公司 | Fault-tolerant direct current (DC) power system |
EP2690007B1 (en) | 2012-07-26 | 2016-08-31 | Airbus Operations GmbH | Method for generating hydraulic power in an aircraft, use of a hybrid power control unit and drive system |
FR2995279B1 (en) * | 2012-09-10 | 2017-05-26 | European Aeronautic Defence & Space Co Eads France | RAIDI PANEL |
CN103117563B (en) * | 2012-12-10 | 2015-03-18 | 贵州电网公司电网规划研究中心 | High frequency predictive cutting machine and predictive speed regulating system of hydraulic power plant |
WO2014105334A1 (en) | 2012-12-28 | 2014-07-03 | General Electric Company | System and method for aviation electric power production |
CN103207603B (en) * | 2013-03-21 | 2015-09-23 | 乐山晟嘉电气有限公司 | Multi-pipeline transmission line automatic control system |
DE102014002034A1 (en) * | 2014-02-13 | 2015-08-13 | Macgregor Hatlapa Gmbh & Co. Kg | Rudder drive system and method |
US9209721B2 (en) * | 2014-04-29 | 2015-12-08 | The Boeing Company | Systems and methods for the control and operation of a parallel motor controller architecture |
ES2695403T3 (en) * | 2014-05-30 | 2019-01-04 | Parker Hannifin Corp | Integrated displacement controlled pump |
CN105134261B (en) * | 2015-08-11 | 2018-10-23 | 北京天地玛珂电液控制系统有限公司 | A kind of hydraulic energy absorption, conversion, stocking system and the smart valve devices of no external power supply |
CN107264812B (en) * | 2016-04-08 | 2019-10-18 | 陕西飞机工业(集团)有限公司 | A kind of aircraft emergency redundance power supply circuit |
US10587307B2 (en) | 2016-06-20 | 2020-03-10 | Ge Aviation Systems, Llc | Transmission of power and communication of signals over fuel and hydraulic lines in a vehicle |
CA2983854A1 (en) * | 2016-11-08 | 2018-05-08 | Ge Aviation Systems Llc | Transmission of power and communication of signals over fuel and hydraulic lines in a vehicle |
RU2661936C1 (en) * | 2017-05-31 | 2018-07-23 | Федеральное государственное бюджетное образовательное учреждение высшего образования "Амурский государственный университет" | Electric station in-house needs consumers power supply system |
GB201803947D0 (en) * | 2018-03-12 | 2018-04-25 | Evectek Ltd | Electric vehicle with an electro-hydraulic propulsion system |
CN108869462A (en) * | 2018-06-20 | 2018-11-23 | 浙江大学 | A kind of hydraulic cushion of hydraulic press device with energy recovery function |
CN109017641B (en) * | 2018-10-17 | 2023-08-29 | 山东驰航汽车科技有限公司 | Motor home circuit system |
CN110056469A (en) * | 2019-05-27 | 2019-07-26 | 自然资源部第一海洋研究所 | A kind of power generator based on wave energy |
CN113357211A (en) * | 2021-05-19 | 2021-09-07 | 中铁工程装备集团隧道设备制造有限公司 | Assembled movable power cabin for cantilever excavator and system thereof |
US11820528B2 (en) * | 2022-03-28 | 2023-11-21 | Hamilton Sundstrand Corporation | Electronic controller with off-load and anti-stall capability for Ram air turbine variable displacement hydraulic pump |
CN117780747B (en) * | 2024-02-27 | 2024-05-07 | 中国航空工业集团公司金城南京机电液压工程研究中心 | Electro-hydraulic conversion control method and system for aircraft |
Family Cites Families (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE3008478A1 (en) * | 1979-05-30 | 1980-12-11 | Sundstrand Corp | CONTROL ARRANGEMENT AND METHOD FOR ELECTRIC GENERATOR AND DISTRIBUTION SYSTEM |
EP0046875B1 (en) * | 1980-09-02 | 1989-09-20 | Messerschmitt-Bölkow-Blohm Gesellschaft mit beschränkter Haftung | Control signal transmission device, especially for aircraft |
DE3220782A1 (en) * | 1982-06-02 | 1983-12-08 | Messerschmitt-Bölkow-Blohm GmbH, 8000 München | Device for optimising the energy budget of aircraft operating systems |
DE3533720A1 (en) * | 1985-09-21 | 1987-04-16 | Messerschmitt Boelkow Blohm | EMERGENCY SUPPLY SYSTEM |
US4912921A (en) * | 1988-03-14 | 1990-04-03 | Sundstrand Corporation | Low speed spool emergency power extraction system |
-
1997
- 1997-10-10 DE DE59710114T patent/DE59710114D1/en not_active Expired - Lifetime
- 1997-10-10 EP EP97117546A patent/EP0838396B1/en not_active Expired - Lifetime
- 1997-10-10 ES ES97117546T patent/ES2200104T3/en not_active Expired - Lifetime
- 1997-10-16 DE DE19745747A patent/DE19745747A1/en not_active Withdrawn
- 1997-10-24 RU RU97118448A patent/RU2141912C1/en not_active IP Right Cessation
- 1997-10-25 CN CNB971208301A patent/CN1185421C/en not_active Expired - Fee Related
- 1997-10-27 JP JP29459697A patent/JP4044991B2/en not_active Expired - Fee Related
- 1997-10-27 CA CA002219293A patent/CA2219293C/en not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
CN1185421C (en) | 2005-01-19 |
ES2200104T3 (en) | 2004-03-01 |
EP0838396B1 (en) | 2003-05-21 |
JPH10169545A (en) | 1998-06-23 |
EP0838396A1 (en) | 1998-04-29 |
DE19745747A1 (en) | 1998-06-25 |
CA2219293C (en) | 2004-01-20 |
CN1190161A (en) | 1998-08-12 |
RU2141912C1 (en) | 1999-11-27 |
JP4044991B2 (en) | 2008-02-06 |
DE59710114D1 (en) | 2003-06-26 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
EEER | Examination request | ||
MKLA | Lapsed |