ID22740A - Sistem pembangkit listrik yang mempunyai suatu alat pembakaran berbentuk gelang - Google Patents

Sistem pembangkit listrik yang mempunyai suatu alat pembakaran berbentuk gelang

Info

Publication number
ID22740A
ID22740A IDW990640A ID990640A ID22740A ID 22740 A ID22740 A ID 22740A ID W990640 A IDW990640 A ID W990640A ID 990640 A ID990640 A ID 990640A ID 22740 A ID22740 A ID 22740A
Authority
ID
Indonesia
Prior art keywords
bracelet
electric power
power systems
rotor
brake tool
Prior art date
Application number
IDW990640A
Other languages
English (en)
Indonesian (id)
Inventor
Teets J Michael
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 ID22740A publication Critical patent/ID22740A/id

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00Features, 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
    • F02C7/12Cooling of plants
    • F02C7/14Cooling of plants of fluids in the plant, e.g. lubricant or fuel
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/02Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/16Continuous 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
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D15/00Adaptations of machines or engines for special use; Combinations of engines with devices driven thereby
    • F01D15/10Adaptations for driving, or combinations with, electric generators
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/16Arrangement of bearings; Supporting or mounting bearings in casings
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C6/00Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00Features, 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
    • F02C7/22Fuel supply systems
    • F02C7/232Fuel valves; Draining valves or systems
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23KFEEDING FUEL TO COMBUSTION APPARATUS
    • F23K5/00Feeding or distributing other fuel to combustion apparatus
    • F23K5/02Liquid fuel
    • F23K5/14Details thereof
    • F23K5/142Fuel pumps
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/28Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • F23R3/286Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply having fuel-air premixing devices
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/42Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
    • F23R3/54Reverse-flow combustion chambers
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23CMETHODS OR APPARATUS FOR COMBUSTION USING FLUID FUEL OR SOLID FUEL SUSPENDED IN  A CARRIER GAS OR AIR 
    • F23C2900/00Special features of, or arrangements for combustion apparatus using fluid fuels or solid fuels suspended in air; Combustion processes therefor
    • F23C2900/03001Miniaturized combustion devices using fluid fuels
    • 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/60Efficient 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)
  • Supercharger (AREA)
  • Connection Of Motors, Electrical Generators, Mechanical Devices, And The Like (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Spark Plugs (AREA)
  • Feeding And Controlling Fuel (AREA)
  • Portable Power Tools In General (AREA)
  • Sawing (AREA)
IDW990640A 1996-12-03 1997-12-03 Sistem pembangkit listrik yang mempunyai suatu alat pembakaran berbentuk gelang ID22740A (id)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US3209096P 1996-12-03 1996-12-03

Publications (1)

Publication Number Publication Date
ID22740A true ID22740A (id) 1999-12-09

Family

ID=21863050

Family Applications (1)

Application Number Title Priority Date Filing Date
IDW990640A ID22740A (id) 1996-12-03 1997-12-03 Sistem pembangkit listrik yang mempunyai suatu alat pembakaran berbentuk gelang

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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US6453658B1 (en) * 2000-02-24 2002-09-24 Capstone Turbine Corporation Multi-stage multi-plane combustion system for a gas turbine engine
WO2003018977A1 (en) 2001-08-27 2003-03-06 Elliott Energy Systems, Inc. Method for gas turbine light-off
US6786049B2 (en) 2002-05-22 2004-09-07 Hamilton Sundstrand Fuel supply control for a gas turbine including multiple solenoid valves
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
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
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
WO2011109514A1 (en) 2010-03-02 2011-09-09 Icr Turbine Engine Corporatin 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
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
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
US20140190178A1 (en) * 2011-08-11 2014-07-10 Beckett Gas, Inc. Combustor
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
WO2014123850A1 (en) 2013-02-06 2014-08-14 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
US10914470B2 (en) 2013-03-14 2021-02-09 Raytheon 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
RU182859U1 (ru) * 2018-05-28 2018-09-05 федеральное государственное бюджетное образовательное учреждение высшего образования "Уфимский государственный авиационный технический университет" Сферический генератор
US20200340409A1 (en) * 2019-04-24 2020-10-29 Viettel Group System and method for gas turbine engine control
US11788464B2 (en) 2019-05-30 2023-10-17 Joseph Michael Teets Advanced 2-spool turboprop engine
US20220332168A1 (en) * 2021-03-23 2022-10-20 Luther J. Worthington, Jr. Apparatus for cooling and/or heating the interior of an environment and methods of using same
FR3135114A1 (fr) * 2022-05-02 2023-11-03 Safran Procede d’injection de melange hydrogene-air pour bruleur de turbomachine
US11970977B2 (en) 2022-08-26 2024-04-30 Hamilton Sundstrand Corporation Variable restriction of a secondary circuit of a fuel injector
US20240271790A1 (en) * 2023-02-14 2024-08-15 Collins Engine Nozzles, Inc. Variable cooling of secondary circuit of fuel nozzles
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Also Published As

Publication number Publication date
JP4465344B2 (ja) 2010-05-19
KR20000069289A (ko) 2000-11-25
US6314717B1 (en) 2001-11-13
WO1998025082A1 (en) 1998-06-11
CN1255190A (zh) 2000-05-31
AU5689298A (en) 1998-06-29
RU2243383C2 (ru) 2004-12-27
EP0943069A4 (en) 2001-04-11
JP2007170396A (ja) 2007-07-05
DE69725463D1 (de) 2003-11-13
EP0943069B1 (en) 2003-10-08
CA2273221A1 (en) 1998-06-11
ATE251739T1 (de) 2003-10-15
JP2002518987A (ja) 2002-06-25
CN1122148C (zh) 2003-09-24
EP0943069A1 (en) 1999-09-22
BR9714776A (pt) 2000-10-03

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