WO2005045215A1 - Hybrid engine accessory power system - Google Patents
Hybrid engine accessory power system Download PDFInfo
- Publication number
- WO2005045215A1 WO2005045215A1 PCT/US2004/035489 US2004035489W WO2005045215A1 WO 2005045215 A1 WO2005045215 A1 WO 2005045215A1 US 2004035489 W US2004035489 W US 2004035489W WO 2005045215 A1 WO2005045215 A1 WO 2005045215A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- power
- generator
- engine
- supplying
- gearbox
- Prior art date
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
- F02C9/16—Control of working fluid flow
- F02C9/18—Control of working fluid flow by bleeding, bypassing or acting on variable working fluid interconnections between turbines or compressors or their stages
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C6/00—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas- turbine plants for special use
- F02C6/04—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output
- F02C6/06—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output providing compressed gas
- F02C6/08—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output providing compressed gas the gas being bled from the gas-turbine compressor
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/32—Arrangement, mounting, or driving, of auxiliaries
-
- 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
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
Abstract
Description
Claims
Priority Applications (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP04796461A EP1682758B1 (en) | 2003-10-27 | 2004-10-26 | Hybrid engine accessory power system |
DE602004030611T DE602004030611D1 (en) | 2003-10-27 | 2004-10-26 | HYBRID ENGINE ACCESSORY DRIVE SYSTEM |
AT04796461T ATE491876T1 (en) | 2003-10-27 | 2004-10-26 | HYBRID ENGINE ACCESSORIES DRIVE SYSTEM |
JP2006538178A JP4664304B2 (en) | 2003-10-27 | 2004-10-26 | Hybrid engine auxiliary power system |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US10/694,645 US7975465B2 (en) | 2003-10-27 | 2003-10-27 | Hybrid engine accessory power system |
US10/694,645 | 2003-10-27 |
Publications (1)
Publication Number | Publication Date |
---|---|
WO2005045215A1 true WO2005045215A1 (en) | 2005-05-19 |
Family
ID=34573206
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/US2004/035489 WO2005045215A1 (en) | 2003-10-27 | 2004-10-26 | Hybrid engine accessory power system |
Country Status (9)
Country | Link |
---|---|
US (2) | US7975465B2 (en) |
EP (1) | EP1682758B1 (en) |
JP (1) | JP4664304B2 (en) |
CN (1) | CN100507239C (en) |
AT (1) | ATE491876T1 (en) |
DE (1) | DE602004030611D1 (en) |
RU (1) | RU2352800C2 (en) |
UA (1) | UA91184C2 (en) |
WO (1) | WO2005045215A1 (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP1617053A3 (en) * | 2004-07-16 | 2008-01-23 | Honeywell International Inc. | Gas turbine engine bleed air power assist system and method |
US9765861B2 (en) | 2011-04-07 | 2017-09-19 | Kawasaki Jukogyo Kabushiki Kaisha | Sealing arrangement of accessory to aircraft engine |
US10711702B2 (en) | 2015-08-18 | 2020-07-14 | General Electric Company | Mixed flow turbocore |
Families Citing this family (82)
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US7811050B2 (en) * | 2006-12-28 | 2010-10-12 | General Electric Company | Operating line control of a compression system with flow recirculation |
FR2912782B1 (en) * | 2007-02-19 | 2009-05-22 | Snecma Sa | METHOD FOR COLLECTING AUXILIARY ENERGY ON AN AIRCRAFT TURBOJET AND TURBOJET ENGINE EQUIPPED TO IMPLEMENT SUCH A METHOD |
DE102007013345B4 (en) * | 2007-03-20 | 2022-07-07 | Airbus Operations Gmbh | Energy control device for an aircraft |
US8213136B2 (en) * | 2007-08-16 | 2012-07-03 | Pratt & Whitney Canada Corp. | Engine having power bus fault short circuit control with a disconnection switch |
US9719428B2 (en) * | 2007-11-30 | 2017-08-01 | United Technologies Corporation | Gas turbine engine with pylon mounted accessory drive |
FR2928696B1 (en) * | 2008-03-14 | 2013-09-27 | Hispano Suiza Sa | ASSEMBLY FOR DRIVING ACCESSORIES OF A GAS TURBINE |
ES2358650B1 (en) * | 2008-05-30 | 2012-03-23 | Airbus Operations, S.L. | CONFIGURATION OF THE PNEUMATIC INSTALLATION IN THE COLA ZONE OF AN AIRCRAFT. |
DE102008031185A1 (en) * | 2008-07-03 | 2010-01-07 | Rolls-Royce Deutschland Ltd & Co Kg | Turbofan engine with at least one device for driving at least one generator |
US20100005657A1 (en) * | 2008-07-10 | 2010-01-14 | Van Vactor David R | Methods and systems to facilitate over-speed protection |
US8224552B2 (en) * | 2008-07-10 | 2012-07-17 | General Electric Company | Methods and systems to facilitate over-speed protection |
US8321119B2 (en) * | 2008-07-10 | 2012-11-27 | General Electric Company | Methods and systems to facilitate over-speed protection |
FR2934321B1 (en) * | 2008-07-25 | 2013-09-27 | Hispano Suiza Sa | CONTROL OF FUEL FLOW DRAINED IN A FUEL SYSTEM OF AN AIRCRAFT PROPELLED BY AN ENGINE. |
ES2363897B1 (en) * | 2008-10-24 | 2012-07-04 | Airbus Operations, S.L. | AUXILIARY POWER UNIT (APU) OF AN AIRCRAFT |
FR2941743B1 (en) * | 2009-02-05 | 2011-03-04 | Microturbo | AIR STARTER FOR TURBOMACHINE. |
WO2010132439A1 (en) | 2009-05-12 | 2010-11-18 | Icr Turbine Engine Corporation | Gas turbine energy storage and conversion system |
GB0912340D0 (en) * | 2009-07-16 | 2009-08-26 | Rolls Royce Plc | Aircraft power management system |
FR2948151B1 (en) * | 2009-07-17 | 2011-11-25 | Snecma | METHOD AND SYSTEM FOR CONTROLLING AN AIRCRAFT ENGINE STARTER-GENERATOR |
US9175605B2 (en) * | 2009-12-29 | 2015-11-03 | Rolls-Royce Corporation | Gas turbine engine surge margin bleed power recuperation |
US8794902B1 (en) * | 2010-01-26 | 2014-08-05 | II Daniel K. Van Ness | System and method to improve the exhaust pressure across a RAM air turbine through secondary flow mixing |
US8866334B2 (en) | 2010-03-02 | 2014-10-21 | Icr Turbine Engine Corporation | Dispatchable power from a renewable energy facility |
US8984895B2 (en) | 2010-07-09 | 2015-03-24 | Icr Turbine Engine Corporation | Metallic ceramic spool for a gas turbine engine |
US8672637B2 (en) * | 2010-08-17 | 2014-03-18 | Hamilton Sundstrand Corporation | Air turbine starter turbine blade airfoil |
US8672638B2 (en) * | 2010-08-17 | 2014-03-18 | Hamilton Sundstrand Corporation | Air turbine starter |
US9028208B2 (en) * | 2010-08-17 | 2015-05-12 | Hamilton Sundstrand Corporation | Air turbine starter turbine nozzle airfoil |
FR2964087B1 (en) * | 2010-08-25 | 2013-06-14 | Turbomeca | METHOD FOR OPTIMIZING THE ENGINE OPERABILITY OF AN AIRCRAFT AND INDEPENDENT POWER UNIT FOR IMPLEMENTING THE SAME |
CA2813680A1 (en) | 2010-09-03 | 2012-03-08 | Icr Turbine Engine Corporation | Gas turbine engine configurations |
US8395275B2 (en) | 2010-11-09 | 2013-03-12 | Hamilton Sundstrand Corporation | Integrated permanent magnet alternator and cooling fan |
US9035802B2 (en) * | 2010-12-22 | 2015-05-19 | Textron Innovations Inc. | Power safety instrument system |
DE102011013746A1 (en) * | 2011-03-12 | 2012-09-13 | Man Truck & Bus Ag | Via hybrid drive connected hybrid drive |
DE102011101197B4 (en) * | 2011-05-11 | 2021-01-28 | Rolls-Royce Deutschland Ltd & Co Kg | Aircraft gas turbine with hydraulic or pneumatic auxiliary unit drive |
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US9051873B2 (en) | 2011-05-20 | 2015-06-09 | Icr Turbine Engine Corporation | Ceramic-to-metal turbine shaft attachment |
US9926849B2 (en) * | 2011-06-14 | 2018-03-27 | Honeywell International Inc. | Transverse mounted accessory gearbox |
US9068515B2 (en) * | 2011-12-07 | 2015-06-30 | United Technologies Corporation | Accessory gearbox with tower shaft removal capability |
US9097186B2 (en) | 2012-01-29 | 2015-08-04 | United Technologies Corporation | Bevel gear arrangement for axial accessory gearbox |
US9206775B2 (en) | 2012-02-01 | 2015-12-08 | United Technologies Corporation | Fuel preheating using electric pump |
EP2870351B1 (en) * | 2012-07-05 | 2018-04-25 | United Technologies Corporation | Fuel preheating using electric pump |
US9382010B2 (en) * | 2012-07-12 | 2016-07-05 | Pratt & Whitney Canada Corp. | Aircraft power outtake management |
US10094288B2 (en) | 2012-07-24 | 2018-10-09 | Icr Turbine Engine Corporation | Ceramic-to-metal turbine volute attachment for a gas turbine engine |
CN103661922B (en) * | 2012-08-31 | 2016-08-31 | 北京精密机电控制设备研究所 | A kind of servo control mechanism electricity consumption combustion gas mixing power set |
FR2997467B1 (en) * | 2012-10-26 | 2016-07-29 | Hispano Suiza Sa | TURBOMACHINE MOVEMENT GEAR BOX, COMPOSED OF ASSEMBLED CASING |
US9045996B2 (en) | 2012-11-20 | 2015-06-02 | Honeywell International Inc. | Gas turbine engine optimization by electric power transfer |
US9500133B2 (en) | 2012-12-23 | 2016-11-22 | United Technologies Corporation | Mount with an axial upstream linkage for connecting a gearbox to a turbine engine case |
US9777639B2 (en) | 2012-12-23 | 2017-10-03 | United Technologies Corporation | Turbine engine gearbox mount with multiple fuse joints |
WO2014143187A1 (en) | 2013-03-15 | 2014-09-18 | Michael Armstrong | Lifing and performance optimization limit management for turbine engine |
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EP2887536B1 (en) | 2013-12-23 | 2019-02-27 | Rolls-Royce Corporation | Control system for a dual redundant motor/generator and engine |
US9771932B2 (en) * | 2014-02-14 | 2017-09-26 | The Boeing Company | Apparatus, controller and method for controlling the cool down of an aircraft engine rotor |
US9458770B2 (en) | 2014-04-01 | 2016-10-04 | Honeywell International Inc. | Optimized engine control using secondary power system horsepower extraction information |
FR3026452B1 (en) * | 2014-09-30 | 2016-10-28 | Hispano Suiza Sa | SPEED REDUCER WITH TWO INTERMEDIATE TRANSMISSION LINES |
GB201420444D0 (en) * | 2014-11-18 | 2014-12-31 | Rolls Royce Plc | A method of starting a gas turbine engine |
CN105298685A (en) * | 2014-12-23 | 2016-02-03 | 丁义存 | Turbofan type vehicle engine |
CN104608933B (en) * | 2015-01-26 | 2017-09-15 | 哈尔滨飞机工业集团有限责任公司 | A kind of engine inertia separator control system and its control method |
US20160230843A1 (en) * | 2015-02-09 | 2016-08-11 | United Technologies Corporation | Gearbox for gas turbine engine |
US20170044989A1 (en) * | 2015-08-14 | 2017-02-16 | General Electric Company | Gas turbine engine stall margin management |
US10578028B2 (en) | 2015-08-18 | 2020-03-03 | General Electric Company | Compressor bleed auxiliary turbine |
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US20170175646A1 (en) * | 2015-12-22 | 2017-06-22 | General Electric Company | Method and system for stall margin modulation as a function of engine health |
US10836505B2 (en) | 2016-06-23 | 2020-11-17 | Raytheon Technologies Corporation | Operating auxiliary power unit during off-nominal propulsion system operation |
US11073085B2 (en) * | 2016-11-08 | 2021-07-27 | Raytheon Technologies Corporation | Intercooled cooling air heat exchanger arrangement |
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US10502142B2 (en) * | 2017-04-11 | 2019-12-10 | United Technologies Corporation | Turbine engine gearbox assembly with sets of inline gears |
US10762726B2 (en) | 2017-06-13 | 2020-09-01 | General Electric Company | Hybrid-electric propulsion system for an aircraft |
DE102017211117A1 (en) * | 2017-06-30 | 2019-01-03 | Siemens Aktiengesellschaft | An engine assembly and method for providing propulsion power to an electrical device for providing electrical energy |
US11333076B2 (en) | 2017-12-21 | 2022-05-17 | Raytheon Technologies Corporation | Power takeoff transmission |
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US10479525B2 (en) | 2018-04-03 | 2019-11-19 | Kidde Technologies, Inc. | Utilization of engine bleed air to provide extended duration emergency aircraft power |
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US11015480B2 (en) | 2018-08-21 | 2021-05-25 | General Electric Company | Feed forward load sensing for hybrid electric systems |
US11097849B2 (en) | 2018-09-10 | 2021-08-24 | General Electric Company | Aircraft having an aft engine |
US20200086998A1 (en) * | 2018-09-13 | 2020-03-19 | Hamilton Sundstrand Corporation | Two-turbine environmental control system |
US11015532B2 (en) | 2018-10-18 | 2021-05-25 | Rolls-Royce North American Technologies, Inc. | Parallel starter/generator and air turbine starter |
US11261795B2 (en) | 2018-10-18 | 2022-03-01 | Rolls-Royce North American Technologies, Inc. | Dual mode starter generator |
EP3693571B1 (en) * | 2019-02-05 | 2022-11-02 | Raytheon Technologies Corporation | Transient operation control of a hybrid gas turbine engine |
US11333077B2 (en) * | 2019-05-06 | 2022-05-17 | The Boeing Company | Systems and methods for transferring mechanical power in a turbine engine |
CN110273758B (en) * | 2019-06-04 | 2020-12-08 | 湖南航翔燃气轮机有限公司 | Micro gas turbine generator set |
US11428171B2 (en) | 2019-12-06 | 2022-08-30 | General Electric Company | Electric machine assistance for multi-spool turbomachine operation and control |
US11713719B2 (en) * | 2020-05-07 | 2023-08-01 | The Boeing Company | Engine bleed power recovery systems and related methods |
CN113217195A (en) * | 2021-06-28 | 2021-08-06 | 中科航星科技有限公司 | Aircraft engine fuel system |
RU209929U1 (en) * | 2021-11-24 | 2022-03-23 | Публичное Акционерное Общество "Одк-Сатурн" | Auxiliary gas turbine engine with auxiliary power unit function |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
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US3514945A (en) * | 1968-10-04 | 1970-06-02 | Avco Corp | Gas turbine accessory power drive unit |
GB2063188A (en) * | 1979-11-16 | 1981-06-03 | Messerschmitt Boelkow Blohm | Flexible power take-off system for the gas turbine engine of an aircraft |
GB2074654A (en) * | 1980-04-16 | 1981-11-04 | Rolls Royce | Remote power system for aircraft |
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-
2003
- 2003-10-27 US US10/694,645 patent/US7975465B2/en not_active Expired - Fee Related
-
2004
- 2004-10-26 RU RU2006117061/06A patent/RU2352800C2/en not_active IP Right Cessation
- 2004-10-26 UA UAA200605417A patent/UA91184C2/en unknown
- 2004-10-26 WO PCT/US2004/035489 patent/WO2005045215A1/en active Application Filing
- 2004-10-26 AT AT04796461T patent/ATE491876T1/en not_active IP Right Cessation
- 2004-10-26 EP EP04796461A patent/EP1682758B1/en not_active Not-in-force
- 2004-10-26 DE DE602004030611T patent/DE602004030611D1/en active Active
- 2004-10-26 JP JP2006538178A patent/JP4664304B2/en not_active Expired - Fee Related
- 2004-10-26 CN CNB2004800392163A patent/CN100507239C/en not_active Expired - Fee Related
-
2009
- 2009-03-30 US US12/413,617 patent/US8800918B2/en not_active Expired - Fee Related
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US3514945A (en) * | 1968-10-04 | 1970-06-02 | Avco Corp | Gas turbine accessory power drive unit |
GB2063188A (en) * | 1979-11-16 | 1981-06-03 | Messerschmitt Boelkow Blohm | Flexible power take-off system for the gas turbine engine of an aircraft |
GB2074654A (en) * | 1980-04-16 | 1981-11-04 | Rolls Royce | Remote power system for aircraft |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP1617053A3 (en) * | 2004-07-16 | 2008-01-23 | Honeywell International Inc. | Gas turbine engine bleed air power assist system and method |
US9765861B2 (en) | 2011-04-07 | 2017-09-19 | Kawasaki Jukogyo Kabushiki Kaisha | Sealing arrangement of accessory to aircraft engine |
US9890839B2 (en) | 2011-04-07 | 2018-02-13 | Kawasaki Jukogyo Kabushiki Kaisha | Generating device for aircraft |
US10711702B2 (en) | 2015-08-18 | 2020-07-14 | General Electric Company | Mixed flow turbocore |
Also Published As
Publication number | Publication date |
---|---|
CN100507239C (en) | 2009-07-01 |
US8800918B2 (en) | 2014-08-12 |
EP1682758B1 (en) | 2010-12-15 |
RU2352800C2 (en) | 2009-04-20 |
RU2006117061A (en) | 2007-12-10 |
UA91184C2 (en) | 2010-07-12 |
JP2007510091A (en) | 2007-04-19 |
US7975465B2 (en) | 2011-07-12 |
JP4664304B2 (en) | 2011-04-06 |
US20050103931A1 (en) | 2005-05-19 |
US20090271086A1 (en) | 2009-10-29 |
CN1902389A (en) | 2007-01-24 |
EP1682758A1 (en) | 2006-07-26 |
DE602004030611D1 (en) | 2011-01-27 |
ATE491876T1 (en) | 2011-01-15 |
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