BR9714776A - "sistema gerador de eletricidade tendo um combustor anular" - Google Patents

"sistema gerador de eletricidade tendo um combustor anular"

Info

Publication number
BR9714776A
BR9714776A BR9714776-1A BR9714776A BR9714776A BR 9714776 A BR9714776 A BR 9714776A BR 9714776 A BR9714776 A BR 9714776A BR 9714776 A BR9714776 A BR 9714776A
Authority
BR
Brazil
Prior art keywords
generating system
electricity generating
annular combustor
rotor
compressor chamber
Prior art date
Application number
BR9714776-1A
Other languages
English (en)
Inventor
J Michael Teets
Jon W Teets
Original Assignee
Elliott Energy Systems Inc
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 Elliott Energy Systems Inc filed Critical Elliott Energy Systems Inc
Publication of BR9714776A publication Critical patent/BR9714776A/pt

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
    • 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
    • F02C7/12—Cooling of plants
    • F02C7/14—Cooling of plants of fluids in the plant, e.g. lubricant or fuel
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/16—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration with devices inside the flame tube or the combustion chamber to influence the air or gas flow
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D15/00—Adaptations of machines or engines for special use; Combinations of engines with devices driven thereby
    • F01D15/10—Adaptations for driving, or combinations with, electric generators
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/16—Arrangement of bearings; Supporting or mounting bearings in casings
    • 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
    • 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
    • F02C7/22—Fuel supply systems
    • F02C7/232—Fuel valves; Draining valves or systems
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23K—FEEDING FUEL TO COMBUSTION APPARATUS
    • F23K5/00—Feeding or distributing other fuel to combustion apparatus
    • F23K5/02—Liquid fuel
    • F23K5/14—Details thereof
    • F23K5/142—Fuel pumps
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • F23R3/286—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply having fuel-air premixing devices
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
    • F23R3/54—Reverse-flow combustion chambers
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23C—METHODS OR APPARATUS FOR COMBUSTION USING FLUID FUEL OR SOLID FUEL SUSPENDED IN  A CARRIER GAS OR AIR 
    • F23C2900/00—Special features of, or arrangements for combustion apparatus using fluid fuels or solid fuels suspended in air; Combustion processes therefor
    • F23C2900/03001—Miniaturized combustion devices using fluid fuels
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Engine Equipment That Uses Special Cycles (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Supercharger (AREA)
  • Connection Of Motors, Electrical Generators, Mechanical Devices, And The Like (AREA)
  • Feeding And Controlling Fuel (AREA)
  • Portable Power Tools In General (AREA)
  • Sawing (AREA)
  • Spark Plugs (AREA)

Abstract

"SISTEMA PARA A GERAçãO DE ELETRICIDADE E MéTODO PARA OPERAR UM SISTEMA PARA A GERAçãO DE ELETRICIDADE" A presente invenção se refere a um sistema para a geração de eletricidade tendo um corpo (159), um combustor anular (14), uma turbina (16), uma câmara de compressor e um compressor (102) posicionado no interior da câmara de compressor. Uma abertura de entrada está em comunicação com a câmara de compressor e uma abertura de saída está em comunicação de fluido com a turbina. Uma pluralidade de magnetos (MG) está fixada ao rotor (18) e um estator (22) feito a partir de um material atraído magneticamente tal como ferro, e tendo um enrolamento de estator proporcionado no corpo (159). O enrolamento de estator está posicionado próximo à pluralidade de magnetos montados sobre o rotor pelo que a rotação do rotor (18) induz uma corrente no enrolamento.
BR9714776-1A 1996-12-03 1997-12-03 "sistema gerador de eletricidade tendo um combustor anular" BR9714776A (pt)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US3209096P 1996-12-03 1996-12-03
PCT/US1997/022007 WO1998025082A1 (en) 1996-12-03 1997-12-03 Electricity generating system having an annular combustor

Publications (1)

Publication Number Publication Date
BR9714776A true BR9714776A (pt) 2000-10-03

Family

ID=21863050

Family Applications (1)

Application Number Title Priority Date Filing Date
BR9714776-1A BR9714776A (pt) 1996-12-03 1997-12-03 "sistema gerador de eletricidade tendo um combustor anular"

Country Status (13)

Country Link
US (1) US6314717B1 (pt)
EP (1) EP0943069B1 (pt)
JP (2) JP2002518987A (pt)
KR (1) KR20000069289A (pt)
CN (1) CN1122148C (pt)
AT (1) ATE251739T1 (pt)
AU (1) AU5689298A (pt)
BR (1) BR9714776A (pt)
CA (1) CA2273221A1 (pt)
DE (1) DE69725463D1 (pt)
ID (1) ID22740A (pt)
RU (1) RU2243383C2 (pt)
WO (1) WO1998025082A1 (pt)

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US6786049B2 (en) 2002-05-22 2004-09-07 Hamilton Sundstrand Fuel supply control for a gas turbine including multiple solenoid valves
US6819999B2 (en) * 2002-09-13 2004-11-16 Elliott Energy Systems, Inc. Multiple control loop acceleration of turboalternator previous to self-sustaining speed
US6834226B2 (en) * 2002-09-13 2004-12-21 Elliott Energy Systems, Inc. Multiple control loop acceleration of turboalternator after reaching self-sustaining speed previous to reaching synchronous speed
US6836720B2 (en) * 2002-09-13 2004-12-28 Elliott Energy Systems, Inc. Offload control of turboalternator with rich burn quick quench lean burn combustor to prevent blowout of combustor
US7574867B2 (en) * 2003-04-02 2009-08-18 Tma Power, Llc Hybrid microturbine for generating electricity
US6942451B1 (en) 2003-06-03 2005-09-13 Hamilton Sundstrand Corporation Damping system for an expendable gas turbine engine
US7194866B1 (en) 2003-06-20 2007-03-27 Hamilton Sundstrand Corporation Static structure for an expendable gas turbine engine
US8438858B1 (en) 2003-08-20 2013-05-14 Hamilton Sundstrand Corporation Rotational system for an expendable gas turbine engine
EP1528343A1 (de) * 2003-10-27 2005-05-04 Siemens Aktiengesellschaft Keramischer Hitzeschildstein mit eingebetteten Verstärkungselementen zur Auskleidung einer Gasturbinenbrennkammerwand
FR2878286B1 (fr) * 2004-11-25 2009-05-22 Snecma Moteurs Sa Turbomachine comportant un generateur de courant electrique integre
US7211906B2 (en) * 2005-04-04 2007-05-01 Tma Power, Llc Rankine—microturbine for generating electricity
US7574853B2 (en) * 2005-10-17 2009-08-18 Tma Power, Llc Microturbine with CHP system having a distillation apparatus
US7836698B2 (en) * 2005-10-20 2010-11-23 General Electric Company Combustor with staged fuel premixer
US7726112B2 (en) 2006-04-24 2010-06-01 Pratt & Whitney Canada Corp. Fuel system of gas turbine engines
US7626892B2 (en) * 2006-05-01 2009-12-01 Tai-Her Yang Timing device with power winder
US7908072B2 (en) * 2007-06-26 2011-03-15 General Electric Company Systems and methods for using a combustion dynamics tuning algorithm with a multi-can combustor
CA2762184A1 (en) 2009-05-12 2010-11-18 Icr Turbine Engine Corporation Gas turbine energy storage and conversion system
US8866334B2 (en) 2010-03-02 2014-10-21 Icr Turbine Engine Corporation Dispatchable power from a renewable energy facility
US20110265438A1 (en) * 2010-04-29 2011-11-03 Ryan William R Turbine engine with enhanced fluid flow strainer system
US8915088B2 (en) * 2010-06-11 2014-12-23 Hamilton Sundstrand Corporation Fuel control method for starting a gas turbine engine
FR2962491B1 (fr) 2010-07-07 2014-04-04 Snecma Procedure d'allumage pour une chambre de combustion de turbomachine
US8984895B2 (en) 2010-07-09 2015-03-24 Icr Turbine Engine Corporation Metallic ceramic spool for a gas turbine engine
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US8395275B2 (en) 2010-11-09 2013-03-12 Hamilton Sundstrand Corporation Integrated permanent magnet alternator and cooling fan
US9051873B2 (en) 2011-05-20 2015-06-09 Icr Turbine Engine Corporation Ceramic-to-metal turbine shaft attachment
US10634354B2 (en) 2011-08-11 2020-04-28 Beckett Gas, Inc. Combustor
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KR101232054B1 (ko) * 2011-08-12 2013-02-15 국방과학연구소 마이크로 터빈용 연소기의 성능 평가 장치 및 그 성능 평가 방법
EP2594766B1 (en) * 2011-11-18 2014-06-18 Hamilton Sundstrand Corporation A gas turbine engine comprising a permanent magnet alternator with integrated cooling fan
US10113434B2 (en) 2012-01-31 2018-10-30 United Technologies Corporation Turbine blade damper seal
US10094288B2 (en) 2012-07-24 2018-10-09 Icr Turbine Engine Corporation Ceramic-to-metal turbine volute attachment for a gas turbine engine
EP2762687A1 (en) 2013-02-01 2014-08-06 Siemens Aktiengesellschaft Method for starting a combustion system
US9958160B2 (en) 2013-02-06 2018-05-01 United Technologies Corporation Gas turbine engine component with upstream-directed cooling film holes
EP2954261B1 (en) 2013-02-08 2020-03-04 United Technologies Corporation Gas turbine engine combustor
WO2014160299A1 (en) 2013-03-14 2014-10-02 United Technologies Corporation Combustor panel with increased durability
US9347378B2 (en) * 2013-05-13 2016-05-24 Solar Turbines Incorporated Outer premix barrel vent air sweep
US20150115781A1 (en) * 2013-10-25 2015-04-30 Michael L Luparello Electrical Generator
CN104153827B (zh) * 2014-07-07 2016-03-02 桐庐福瑞太阳能科技有限公司 一种一体式风洞型汽轮发电设备
US10274201B2 (en) * 2016-01-05 2019-04-30 Solar Turbines Incorporated Fuel injector with dual main fuel injection
US20190002117A1 (en) * 2017-06-30 2019-01-03 General Electric Company Propulsion system for an aircraft
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Also Published As

Publication number Publication date
ATE251739T1 (de) 2003-10-15
JP2007170396A (ja) 2007-07-05
WO1998025082A1 (en) 1998-06-11
CN1255190A (zh) 2000-05-31
RU2243383C2 (ru) 2004-12-27
JP4465344B2 (ja) 2010-05-19
CA2273221A1 (en) 1998-06-11
ID22740A (id) 1999-12-09
CN1122148C (zh) 2003-09-24
EP0943069A4 (en) 2001-04-11
EP0943069A1 (en) 1999-09-22
US6314717B1 (en) 2001-11-13
EP0943069B1 (en) 2003-10-08
AU5689298A (en) 1998-06-29
JP2002518987A (ja) 2002-06-25
DE69725463D1 (de) 2003-11-13
KR20000069289A (ko) 2000-11-25

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Legal Events

Date Code Title Description
FA10 Dismissal: dismissal - article 33 of industrial property law
B11N Dismissal: publication cancelled [chapter 11.14 patent gazette]
B06A Patent application procedure suspended [chapter 6.1 patent gazette]
B09A Decision: intention to grant [chapter 9.1 patent gazette]
B11D Dismissal acc. art. 38, par 2 of ipl - failure to pay fee after grant in time