[go: up one dir, main page]

AU2001295007A1 - Gas turbine engine having improved efficiency - Google Patents

Gas turbine engine having improved efficiency

Info

Publication number
AU2001295007A1
AU2001295007A1 AU2001295007A AU9500701A AU2001295007A1 AU 2001295007 A1 AU2001295007 A1 AU 2001295007A1 AU 2001295007 A AU2001295007 A AU 2001295007A AU 9500701 A AU9500701 A AU 9500701A AU 2001295007 A1 AU2001295007 A1 AU 2001295007A1
Authority
AU
Australia
Prior art keywords
gas turbine
turbine engine
improved efficiency
efficiency
improved
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
AU2001295007A
Inventor
Paul A. Dellenback
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.)
University of Wyoming
Original Assignee
University of Wyoming
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 University of Wyoming filed Critical University of Wyoming
Publication of AU2001295007A1 publication Critical patent/AU2001295007A1/en
Abandoned legal-status Critical Current

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
    • F02C7/08Heating air supply before combustion, e.g. by exhaust gases
    • F02C7/10Heating air supply before combustion, e.g. by exhaust gases by means of regenerative heat-exchangers
    • 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
    • F02C3/00Gas-turbine plants characterised by the use of combustion products as the working fluid
    • F02C3/04Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor
    • F02C3/10Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor with another turbine driving an output shaft but not driving the compressor
    • 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
    • F02C6/003Gas-turbine plants with heaters between turbine stages
    • 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
    • Y02EREDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E20/00Combustion technologies with mitigation potential
    • Y02E20/14Combined heat and power generation [CHP]
    • 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
    • Y02EREDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E20/00Combustion technologies with mitigation potential
    • Y02E20/16Combined cycle power plant [CCPP], or combined cycle gas turbine [CCGT]

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)
AU2001295007A 2000-08-15 2001-08-14 Gas turbine engine having improved efficiency Abandoned AU2001295007A1 (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US22535100P 2000-08-15 2000-08-15
US60225351 2000-08-15
PCT/US2001/041714 WO2002014664A1 (en) 2000-08-15 2001-08-14 Gas turbine engine having improved efficiency

Publications (1)

Publication Number Publication Date
AU2001295007A1 true AU2001295007A1 (en) 2002-02-25

Family

ID=22844526

Family Applications (1)

Application Number Title Priority Date Filing Date
AU2001295007A Abandoned AU2001295007A1 (en) 2000-08-15 2001-08-14 Gas turbine engine having improved efficiency

Country Status (2)

Country Link
AU (1) AU2001295007A1 (en)
WO (1) WO2002014664A1 (en)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8051654B2 (en) 2008-01-31 2011-11-08 General Electric Company Reheat gas and exhaust gas regenerator system for a combined cycle power plant
CN105822434B (en) * 2016-05-10 2018-04-06 中国科学院工程热物理研究所 A kind of apparatus and method for preventing the cold and hot suspension of Study On Start-up Process For Gas Turbines
FR3103218B1 (en) * 2019-11-15 2022-06-24 Psa Automobiles Sa COMBUSTION DEVICE COMPRISING A COMBUSTION CHAMBER AND AN EXCHANGER CIRCUIT AND SYSTEM COMPRISING SUCH A DEVICE

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2633707A (en) * 1946-12-16 1953-04-07 Rateau Soc Compound plant for producing mechanical power and heating steam with gas and steam turbines
US3054257A (en) * 1953-03-10 1962-09-18 Garrett Corp Gas turbine power plant for vehicles
US4506502A (en) * 1980-01-20 1985-03-26 Beit Shemesh Engines Ltd. Gas turbine engines
EP0859136A1 (en) * 1997-02-17 1998-08-19 N.V. Kema Gas turbine with energy recovering

Also Published As

Publication number Publication date
WO2002014664A1 (en) 2002-02-21

Similar Documents

Publication Publication Date Title
EP1270872A4 (en) Gas turbine engine
PL350898A1 (en) Gas turbine engine disk
AU2002235119A1 (en) Nested core gas turbine engine
GB2365078B (en) A gas turbine engine blade
GB0023293D0 (en) Gas turbine engine rotor blades
EP1291581A3 (en) Gas turbine engine combustor
GB0025878D0 (en) Gas turbine engine combustion system
GB2347221B (en) Gas turbine engine
AU2471700A (en) Gas turbine engine
AU2471500A (en) Gas turbine engine
GB2346177B (en) Gas turbine engine
GB0126371D0 (en) Gas turbine engines
GB0118077D0 (en) A gas turbine engine
GB2348675B (en) Gas turbine engine
GB9904277D0 (en) Gas turbine engine
AU2471600A (en) Gas turbine engine
AU3698500A (en) Gas turbine engine
GB2366599B (en) Gas turbine engine system
GB2356022B (en) Gas turbine engines
AU7985500A (en) Gas turbine engine
GB2355302B (en) Gas turbine engines
AU2001295007A1 (en) Gas turbine engine having improved efficiency
AU2471400A (en) Gas turbine engine
AUPR021700A0 (en) A turbine engine
GB2360836B (en) Gas turbine engine combustion system