AU2002216768A1 - System and method for gaseous fuel control for a turbogenerator/motor - Google Patents

System and method for gaseous fuel control for a turbogenerator/motor

Info

Publication number
AU2002216768A1
AU2002216768A1 AU2002216768A AU1676802A AU2002216768A1 AU 2002216768 A1 AU2002216768 A1 AU 2002216768A1 AU 2002216768 A AU2002216768 A AU 2002216768A AU 1676802 A AU1676802 A AU 1676802A AU 2002216768 A1 AU2002216768 A1 AU 2002216768A1
Authority
AU
Australia
Prior art keywords
turbogenerator
motor
gaseous fuel
fuel control
gaseous
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.)
Abandoned
Application number
AU2002216768A
Inventor
Steven W. Lampe
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.)
Capstone Green Energy Corp
Original Assignee
Capstone Turbine Corp
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 Capstone Turbine Corp filed Critical Capstone Turbine Corp
Publication of AU2002216768A1 publication Critical patent/AU2002216768A1/en
Abandoned legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04C—ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
    • F04C28/00—Control of, monitoring of, or safety arrangements for, pumps or pumping installations specially adapted for elastic fluids
    • F04C28/08—Control of, monitoring of, or safety arrangements for, pumps or pumping installations specially adapted for elastic fluids characterised by varying the rotational speed
    • 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
    • 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
    • F02C9/26—Control of fuel supply
    • F02C9/30—Control of fuel supply characterised by variable fuel pump output
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04C—ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
    • F04C18/00—Rotary-piston pumps specially adapted for elastic fluids
    • F04C18/02—Rotary-piston pumps specially adapted for elastic fluids of arcuate-engagement type, i.e. with circular translatory movement of co-operating members, each member having the same number of teeth or tooth-equivalents
    • F04C18/0207—Rotary-piston pumps specially adapted for elastic fluids of arcuate-engagement type, i.e. with circular translatory movement of co-operating members, each member having the same number of teeth or tooth-equivalents both members having co-operating elements in spiral form
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2270/00—Control
    • F05D2270/01—Purpose of the control system
    • F05D2270/02—Purpose of the control system to control rotational speed (n)
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2270/00—Control
    • F05D2270/30—Control parameters, e.g. input parameters
    • F05D2270/301—Pressure
AU2002216768A 2000-06-29 2001-06-20 System and method for gaseous fuel control for a turbogenerator/motor Abandoned AU2002216768A1 (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US60791700A 2000-06-29 2000-06-29
US09/607917 2000-06-29
PCT/US2001/041083 WO2002002920A1 (en) 2000-06-29 2001-06-20 System and method for gaseous fuel control for a turbogenerator/motor

Publications (1)

Publication Number Publication Date
AU2002216768A1 true AU2002216768A1 (en) 2002-01-14

Family

ID=24434236

Family Applications (1)

Application Number Title Priority Date Filing Date
AU2002216768A Abandoned AU2002216768A1 (en) 2000-06-29 2001-06-20 System and method for gaseous fuel control for a turbogenerator/motor

Country Status (2)

Country Link
AU (1) AU2002216768A1 (en)
WO (1) WO2002002920A1 (en)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6616415B1 (en) * 2002-03-26 2003-09-09 Copeland Corporation Fuel gas compression system
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
US9051873B2 (en) 2011-05-20 2015-06-09 Icr Turbine Engine Corporation Ceramic-to-metal turbine shaft attachment
US10094288B2 (en) 2012-07-24 2018-10-09 Icr Turbine Engine Corporation Ceramic-to-metal turbine volute attachment for a gas turbine engine
CN105917099A (en) * 2014-07-31 2016-08-31 三菱重工业株式会社 Compressor control device, compressor control system, and compressor control method

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3596467A (en) * 1969-10-31 1971-08-03 Avco Corp Integrated fuel control system for a gas turbine engine
US3696612A (en) * 1970-12-30 1972-10-10 Westinghouse Electric Corp Fuel pump system for gas turbines
US4004412A (en) * 1974-12-20 1977-01-25 Chandler Evans Inc. Gas turbine engine fuel metering system
US4332527A (en) * 1979-08-10 1982-06-01 Lear Siegler, Inc. Variable speed centrifugal pump
US4815278A (en) * 1987-10-14 1989-03-28 Sundstrand Corporation Electrically driven fuel pump for gas turbine engines
US5274996A (en) * 1991-10-11 1994-01-04 Allied-Signal, Inc. Closed loop fuel control system
US5303545A (en) * 1992-10-05 1994-04-19 United Technologies Corporation Pressure based close loop thrust control in a turbofan engine
GB9408677D0 (en) * 1994-04-30 1994-06-22 Aisin Seiki Gaseous fuel compression and control system for gas turbine engine
US5806300A (en) * 1995-12-22 1998-09-15 United Technologies Corporation Electronic control for a variable delivery, positive displacement fuel pump
US5819524A (en) * 1996-10-16 1998-10-13 Capstone Turbine Corporation Gaseous fuel compression and control system and method
JPH11122995A (en) * 1997-09-08 1999-04-30 Capstone Turbine Corp Turbine generator-motor controller
US6066898A (en) * 1998-08-14 2000-05-23 Alliedsignal Inc. Microturbine power generating system including variable-speed gas compressor

Also Published As

Publication number Publication date
WO2002002920A1 (en) 2002-01-10

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