IT8922652A0 - Turbomotore con raffreddamento ad aria e a vapore - Google Patents

Turbomotore con raffreddamento ad aria e a vapore

Info

Publication number
IT8922652A0
IT8922652A0 IT22652A IT2265289A IT8922652A0 IT 8922652 A0 IT8922652 A0 IT 8922652A0 IT 22652 A IT22652 A IT 22652A IT 2265289 A IT2265289 A IT 2265289A IT 8922652 A0 IT8922652 A0 IT 8922652A0
Authority
IT
Italy
Prior art keywords
turboengine
air
steam cooling
steam
cooling
Prior art date
Application number
IT22652A
Other languages
English (en)
Other versions
IT1237879B (it
Inventor
William Ronald Hines
Original Assignee
Gen Electric
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 Gen Electric filed Critical Gen Electric
Publication of IT8922652A0 publication Critical patent/IT8922652A0/it
Application granted granted Critical
Publication of IT1237879B publication Critical patent/IT1237879B/it

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
    • F02C7/16Cooling of plants characterised by cooling medium
    • 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
    • F02C3/20Gas-turbine plants characterised by the use of combustion products as the working fluid using a special fuel, oxidant, or dilution fluid to generate the combustion products
    • F02C3/30Adding water, steam or other fluids for influencing combustion, e.g. to obtain cleaner exhaust gases
    • 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
    • F02C7/141Cooling of plants of fluids in the plant, e.g. lubricant or fuel of working fluid
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00Function
    • F05D2260/20Heat transfer, e.g. cooling
    • F05D2260/232Heat transfer, e.g. cooling characterized by the cooling medium
    • F05D2260/2322Heat transfer, e.g. cooling characterized by the cooling medium steam
    • 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)
  • Turbine Rotor Nozzle Sealing (AREA)
IT02265289A 1988-12-14 1989-12-11 Turbomotore con raffreddamento ad aria e a vapore IT1237879B (it)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US07/284,507 US4982564A (en) 1988-12-14 1988-12-14 Turbine engine with air and steam cooling

Publications (2)

Publication Number Publication Date
IT8922652A0 true IT8922652A0 (it) 1989-12-11
IT1237879B IT1237879B (it) 1993-06-18

Family

ID=23090460

Family Applications (1)

Application Number Title Priority Date Filing Date
IT02265289A IT1237879B (it) 1988-12-14 1989-12-11 Turbomotore con raffreddamento ad aria e a vapore

Country Status (5)

Country Link
US (1) US4982564A (it)
JP (1) JPH0635841B2 (it)
GB (1) GB2228295B (it)
IT (1) IT1237879B (it)
SE (1) SE466464B (it)

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US5177954A (en) * 1984-10-10 1993-01-12 Paul Marius A Gas turbine engine with cooled turbine blades
US5582000A (en) * 1989-02-08 1996-12-10 United Technologies Corporation Coolable rocket nozzle for a rocket engine
US5122033A (en) * 1990-11-16 1992-06-16 Paul Marius A Turbine blade unit
US5160096A (en) * 1991-10-11 1992-11-03 United Technologies Corporation Gas turbine cycle
US5340274A (en) * 1991-11-19 1994-08-23 General Electric Company Integrated steam/air cooling system for gas turbines
US5284427A (en) * 1993-05-05 1994-02-08 Wacker Roland W Preheating and cooling system for a rotary engine
US5579631A (en) * 1994-04-28 1996-12-03 Westinghouse Electric Corporation Steam cooling of gas turbine with backup air cooling
US5593274A (en) * 1995-03-31 1997-01-14 General Electric Co. Closed or open circuit cooling of turbine rotor components
US5536143A (en) * 1995-03-31 1996-07-16 General Electric Co. Closed circuit steam cooled bucket
US5819525A (en) * 1997-03-14 1998-10-13 Westinghouse Electric Corporation Cooling supply manifold assembly for cooling combustion turbine components
US6311471B1 (en) * 1999-01-08 2001-11-06 General Electric Company Steam cooled fuel injector for gas turbine
EP1293655A1 (en) 2001-09-13 2003-03-19 Mitsubishi Heavy Industries, Ltd. Gas turbine, driving method thereof and gas turbine combined electric power generation plant
JP2003083003A (ja) 2001-09-13 2003-03-19 Mitsubishi Heavy Ind Ltd ガスタービン及びガスタービン複合発電プラントの運転方法
US6779346B2 (en) 2002-12-09 2004-08-24 General Electric Company Control of gas turbine combustion temperature by compressor bleed air
US7862631B2 (en) * 2003-02-07 2011-01-04 Gm Global Technology Operations, Inc. Fuel processor primary reactor and combustor startup via electrically-heated catalyst
US7284377B2 (en) * 2004-05-28 2007-10-23 General Electric Company Method and apparatus for operating an intercooler for a gas turbine engine
EP1640586A1 (de) * 2004-09-22 2006-03-29 Siemens Aktiengesellschaft Verfahren zur Leistungssteigerung einer bestehenden, stationären Gasturbine
US20100242488A1 (en) * 2007-11-29 2010-09-30 United Technologies Corporation gas turbine engine and method of operation
US8387358B2 (en) * 2010-01-29 2013-03-05 General Electric Company Gas turbine engine steam injection manifold
RU2548245C1 (ru) * 2014-04-23 2015-04-20 Владислав Юрьевич Климов Смесительная головка парогазогенератора
RU2546372C1 (ru) * 2014-04-23 2015-04-10 Владислав Юрьевич Климов Способ получения пара в парогазогенераторе
JP6432110B2 (ja) * 2014-08-29 2018-12-05 三菱日立パワーシステムズ株式会社 ガスタービン
US10215070B2 (en) 2015-06-29 2019-02-26 General Electric Company Power generation system exhaust cooling
US9850794B2 (en) 2015-06-29 2017-12-26 General Electric Company Power generation system exhaust cooling
US9840953B2 (en) 2015-06-29 2017-12-12 General Electric Company Power generation system exhaust cooling
US9752503B2 (en) 2015-06-29 2017-09-05 General Electric Company Power generation system exhaust cooling
US9856768B2 (en) 2015-06-29 2018-01-02 General Electric Company Power generation system exhaust cooling
US9752502B2 (en) 2015-06-29 2017-09-05 General Electric Company Power generation system exhaust cooling
US10077694B2 (en) 2015-06-29 2018-09-18 General Electric Company Power generation system exhaust cooling
US10087801B2 (en) 2015-06-29 2018-10-02 General Electric Company Power generation system exhaust cooling
US9938874B2 (en) 2015-06-29 2018-04-10 General Electric Company Power generation system exhaust cooling
US9850818B2 (en) 2015-06-29 2017-12-26 General Electric Company Power generation system exhaust cooling
US10060316B2 (en) 2015-06-29 2018-08-28 General Electric Company Power generation system exhaust cooling
US10030558B2 (en) 2015-06-29 2018-07-24 General Electric Company Power generation system exhaust cooling
US11603794B2 (en) 2015-12-30 2023-03-14 Leonard Morgensen Andersen Method and apparatus for increasing useful energy/thrust of a gas turbine engine by one or more rotating fluid moving (agitator) pieces due to formation of a defined steam region
US20170306843A1 (en) * 2015-12-30 2017-10-26 Leonard Morgensen Andersen Method and apparatus for increasing useful energy/thrust of a gas turbine engine by one or more rotating fluid moving (agitator) pieces due to formation of a defined steam region
US10316759B2 (en) 2016-05-31 2019-06-11 General Electric Company Power generation system exhaust cooling

Family Cites Families (22)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB746377A (en) * 1953-04-29 1956-03-14 Allan Barker Improvements in or relating to gas turbine installations
GB759037A (en) * 1953-09-07 1956-10-10 Rolls Royce Improvements in or relating to gas turbine engines
GB774425A (en) * 1954-10-14 1957-05-08 Blackburn & Gen Aircraft Ltd Improvements in or relating to turbine engines
US3038308A (en) * 1956-07-16 1962-06-12 Nancy W N Fuller Gas turbine combustion chamber and method
US3527543A (en) * 1965-08-26 1970-09-08 Gen Electric Cooling of structural members particularly for gas turbine engines
US3359723A (en) * 1965-10-29 1967-12-26 Exxon Research Engineering Co Method of combusting a residual fuel utilizing a two-stage air injection technique and an intermediate steam injection step
US3729930A (en) * 1970-06-23 1973-05-01 Rolls Royce Gas turbine engine
US3899884A (en) * 1970-12-02 1975-08-19 Gen Electric Combustor systems
US3715170A (en) * 1970-12-11 1973-02-06 Gen Electric Cooled turbine blade
US3703808A (en) * 1970-12-18 1972-11-28 Gen Electric Turbine blade tip cooling air expander
US3747336A (en) * 1972-03-29 1973-07-24 Gen Electric Steam injection system for a gas turbine
JPS5037324B2 (it) * 1972-10-30 1975-12-02
GB1479599A (en) * 1973-11-09 1977-07-13 Secr Defence Aircraft gas turbine engine turbine blade cooling
US3965066A (en) * 1974-03-15 1976-06-22 General Electric Company Combustor-turbine nozzle interconnection
JPS5477820A (en) * 1977-12-02 1979-06-21 Hitachi Ltd Method of cooling gas turbine blade
US4384452A (en) * 1978-10-26 1983-05-24 Rice Ivan G Steam-cooled blading with steam thermal barrier for reheat gas turbine combined with steam turbine
US4314442A (en) * 1978-10-26 1982-02-09 Rice Ivan G Steam-cooled blading with steam thermal barrier for reheat gas turbine combined with steam turbine
US4296599A (en) * 1979-03-30 1981-10-27 General Electric Company Turbine cooling air modulation apparatus
JPS59160035A (ja) * 1983-03-01 1984-09-10 Agency Of Ind Science & Technol ガスタ−ビン
US4614083A (en) * 1984-04-06 1986-09-30 Agency Of Industrial Science & Technology Gas turbine
US4569195A (en) * 1984-04-27 1986-02-11 General Electric Company Fluid injection gas turbine engine and method for operating
US4631914A (en) * 1985-02-25 1986-12-30 General Electric Company Gas turbine engine of improved thermal efficiency

Also Published As

Publication number Publication date
GB8927824D0 (en) 1990-02-14
GB2228295A (en) 1990-08-22
JPH02218821A (ja) 1990-08-31
JPH0635841B2 (ja) 1994-05-11
IT1237879B (it) 1993-06-18
SE466464B (sv) 1992-02-17
SE8904209L (sv) 1990-06-15
GB2228295B (en) 1992-12-16
US4982564A (en) 1991-01-08
SE8904209D0 (sv) 1989-12-13

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Legal Events

Date Code Title Description
0001 Granted
TA Fee payment date (situation as of event date), data collected since 19931001

Effective date: 19971223