GB713553A - Improvements in or relating to gas turbine installations - Google Patents

Improvements in or relating to gas turbine installations

Info

Publication number
GB713553A
GB713553A GB26820/51A GB2682051A GB713553A GB 713553 A GB713553 A GB 713553A GB 26820/51 A GB26820/51 A GB 26820/51A GB 2682051 A GB2682051 A GB 2682051A GB 713553 A GB713553 A GB 713553A
Authority
GB
United Kingdom
Prior art keywords
turbine
gas
generator
pressure
steam
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.)
Expired
Application number
GB26820/51A
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.)
MAN AG
Original Assignee
MAN Maschinenfabrik Augsburg Nuernberg AG
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 MAN Maschinenfabrik Augsburg Nuernberg AG filed Critical MAN Maschinenfabrik Augsburg Nuernberg AG
Publication of GB713553A publication Critical patent/GB713553A/en
Expired 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
    • 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
    • F02C3/26Gas-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 the fuel or oxidant being solid or pulverulent, e.g. in slurry or suspension
    • F02C3/28Gas-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 the fuel or oxidant being solid or pulverulent, e.g. in slurry or suspension using a separate gas producer for gasifying the fuel before combustion
    • 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
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/02Blade-carrying members, e.g. rotors
    • F01D5/08Heating, heat-insulating or cooling means
    • F01D5/081Cooling fluid being directed on the side of the rotor disc or at the roots of the blades
    • F01D5/084Cooling fluid being directed on the side of the rotor disc or at the roots of the blades the fluid circulating at the periphery of a multistage rotor, e.g. of drum type
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01KSTEAM ENGINE PLANTS; STEAM ACCUMULATORS; ENGINE PLANTS NOT OTHERWISE PROVIDED FOR; ENGINES USING SPECIAL WORKING FLUIDS OR CYCLES
    • F01K21/00Steam engine plants not otherwise provided for
    • F01K21/04Steam engine plants not otherwise provided for using mixtures of steam and gas; Plants generating or heating steam by bringing water or steam into direct contact with hot gas
    • F01K21/042Steam engine plants not otherwise provided for using mixtures of steam and gas; Plants generating or heating steam by bringing water or steam into direct contact with hot gas pure steam being expanded in a motor somewhere in the plant
    • 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

Abstract

713,553. Gas turbine plant. MASCHINENFABRIK AUGSBURG-NURNBERG AKT.-GES. Nov. 15, 1951 [Nov. 16,1950], No. 26820/51. Class 110(3) [Also in Group XII] A gas turbine plant fed with gaseous fuel from a liquid cooled gas generator using solid fuels, has the gas generator supplied with gasifying air taken from the circuit of the gas turbine plant bv a compressor driven by a turbine actuated by vapour from the generator cooling system and means for automatically varying the supply of vapour to this turbine in accordance with the load on the output shaft of the gas turbine. The gas turbine plant comprises compressors 1, 2 arranged in series which supply air to the combustion chamber 10 feeding gas to the turbines 4, 5 driving the compressors. The turbine 5 drives an output generator 6. An intercooler 3 is arranged between the compressors 1 and 2 and a reheat combustion chamber 11 between the turbines 4. 5. Gaseous fuel is supplied to the combustion chambers 10, 11 by a gas generator comprising a reaction chamber 12, a cooling jacket 13 to which is connected an equalising vessel 14. a coal charger 15, an ash or slag receiver 16 and a washing tower 17. The fuel gas from the generator is passed through a pressure transformer 18 and then further heated in the slag receiver 16 before being expanded down to the pressure of the combustion chambers 10, 11 in turbines 19, 20. The gasification air for the gas generator is taken from the discharge of the compressor 2 and further compressed in a compressor 21 driven by the turbines 19, 20. An intercooler may be arranged between the compressors 2, 21. Steam from the vessel 14 is supplied to a turbine 27 which assists the turbines 19, 20 to drive the compressor 21. Changes of load cause the governor 7 to actuate the fuel gas throttle valves 23. 24 to vary the fuel supply which results in a change of pressure in the pressure transformer 18. This change of pressure causes a larger change of pressure in the space below the transformer piston 26 which is connected to the equalising vessel 14. These changes of pressure cause automatic variation of the steam supply to the turbine 27. This effect may be amplified by connecting the governor 7 to a throttle valve 28 in the steam pipe leading to the turbine 27 and to a throttle valve 30 controlling a heating means 29 arranged below the accumulator 18. The feed water to the cooling jacket 13 may be preheated by the exhaust gases of the turbine 5, by the hot waste water of the washing tower 17 and by a heater burning tar separated out in the tower 17 or waste gas from the coal charging device 15. The fuel gas may pass direct to the combustion chambers 10. 11 from the generator in which case the compressor 21 is only driven by the steam turbine 27 and an electric motor. The electric motor may be used for starting. The exhaust steam from the turbine 27 may be used to cool the blade rims of the initial stages of the gas turbine 4 and additional output may be obtained by expanding steam with the combustion gases.
GB26820/51A 1950-11-16 1951-11-15 Improvements in or relating to gas turbine installations Expired GB713553A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE297551X 1950-11-16

Publications (1)

Publication Number Publication Date
GB713553A true GB713553A (en) 1954-08-11

Family

ID=6090715

Family Applications (1)

Application Number Title Priority Date Filing Date
GB26820/51A Expired GB713553A (en) 1950-11-16 1951-11-15 Improvements in or relating to gas turbine installations

Country Status (2)

Country Link
CH (1) CH297551A (en)
GB (1) GB713553A (en)

Cited By (26)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2495399A1 (en) * 1980-10-17 1982-06-04 Gen Electric CONTROL SYSTEM AND CONTROL METHOD OF POWER GENERATING PLANT
EP0319699A2 (en) * 1987-11-30 1989-06-14 General Electric Company Steam injected engine with auxillary high pressure steam turbine
WO1998038414A1 (en) * 1997-02-27 1998-09-03 Siemens Westinghouse Power Corporation Coal fuel gas turbine system
WO2001016471A1 (en) * 1999-09-01 2001-03-08 Siemens Aktiengesellschaft Method and device for increasing the pressure of a gas
WO2008076963A2 (en) * 2006-12-15 2008-06-26 Praxair Technology, Inc. Electrical power generation method
CN103205277A (en) * 2013-01-30 2013-07-17 吴江市新金城不锈钢制品有限公司 Minisize gas producer
US9452401B2 (en) 2013-10-07 2016-09-27 Praxair Technology, Inc. Ceramic oxygen transport membrane array reactor and reforming method
US9452388B2 (en) 2013-10-08 2016-09-27 Praxair Technology, Inc. System and method for air temperature control in an oxygen transport membrane based reactor
US9453644B2 (en) 2012-12-28 2016-09-27 Praxair Technology, Inc. Oxygen transport membrane based advanced power cycle with low pressure synthesis gas slip stream
US9486735B2 (en) 2011-12-15 2016-11-08 Praxair Technology, Inc. Composite oxygen transport membrane
US9492784B2 (en) 2011-12-15 2016-11-15 Praxair Technology, Inc. Composite oxygen transport membrane
US9556027B2 (en) 2013-12-02 2017-01-31 Praxair Technology, Inc. Method and system for producing hydrogen using an oxygen transport membrane based reforming system with secondary reforming
US9562472B2 (en) 2014-02-12 2017-02-07 Praxair Technology, Inc. Oxygen transport membrane reactor based method and system for generating electric power
US9561476B2 (en) 2010-12-15 2017-02-07 Praxair Technology, Inc. Catalyst containing oxygen transport membrane
US9611144B2 (en) 2013-04-26 2017-04-04 Praxair Technology, Inc. Method and system for producing a synthesis gas in an oxygen transport membrane based reforming system that is free of metal dusting corrosion
US9789445B2 (en) 2014-10-07 2017-10-17 Praxair Technology, Inc. Composite oxygen ion transport membrane
US9839899B2 (en) 2013-04-26 2017-12-12 Praxair Technology, Inc. Method and system for producing methanol using an integrated oxygen transport membrane based reforming system
US9938145B2 (en) 2013-04-26 2018-04-10 Praxair Technology, Inc. Method and system for adjusting synthesis gas module in an oxygen transport membrane based reforming system
US9938146B2 (en) 2015-12-28 2018-04-10 Praxair Technology, Inc. High aspect ratio catalytic reactor and catalyst inserts therefor
US9969645B2 (en) 2012-12-19 2018-05-15 Praxair Technology, Inc. Method for sealing an oxygen transport membrane assembly
US10005664B2 (en) 2013-04-26 2018-06-26 Praxair Technology, Inc. Method and system for producing a synthesis gas using an oxygen transport membrane based reforming system with secondary reforming and auxiliary heat source
US10118823B2 (en) 2015-12-15 2018-11-06 Praxair Technology, Inc. Method of thermally-stabilizing an oxygen transport membrane-based reforming system
US10441922B2 (en) 2015-06-29 2019-10-15 Praxair Technology, Inc. Dual function composite oxygen transport membrane
US10822234B2 (en) 2014-04-16 2020-11-03 Praxair Technology, Inc. Method and system for oxygen transport membrane enhanced integrated gasifier combined cycle (IGCC)
US11052353B2 (en) 2016-04-01 2021-07-06 Praxair Technology, Inc. Catalyst-containing oxygen transport membrane
US11136238B2 (en) 2018-05-21 2021-10-05 Praxair Technology, Inc. OTM syngas panel with gas heated reformer

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3731485A (en) * 1970-02-07 1973-05-08 Metallgesellschaft Ag Open-cycle gas turbine plant

Cited By (34)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2495399A1 (en) * 1980-10-17 1982-06-04 Gen Electric CONTROL SYSTEM AND CONTROL METHOD OF POWER GENERATING PLANT
EP0319699A2 (en) * 1987-11-30 1989-06-14 General Electric Company Steam injected engine with auxillary high pressure steam turbine
EP0319699A3 (en) * 1987-11-30 1989-09-20 General Electric Company Steam injected engine with auxillary high pressure steam turbine
WO1998038414A1 (en) * 1997-02-27 1998-09-03 Siemens Westinghouse Power Corporation Coal fuel gas turbine system
WO2001016471A1 (en) * 1999-09-01 2001-03-08 Siemens Aktiengesellschaft Method and device for increasing the pressure of a gas
WO2008076963A2 (en) * 2006-12-15 2008-06-26 Praxair Technology, Inc. Electrical power generation method
WO2008076963A3 (en) * 2006-12-15 2010-08-26 Praxair Technology, Inc. Electrical power generation method
US7856829B2 (en) 2006-12-15 2010-12-28 Praxair Technology, Inc. Electrical power generation method
AU2007333808B2 (en) * 2006-12-15 2012-05-17 Praxair Technology, Inc. Electrical power generation method
US8196387B2 (en) 2006-12-15 2012-06-12 Praxair Technology, Inc. Electrical power generation apparatus
US9561476B2 (en) 2010-12-15 2017-02-07 Praxair Technology, Inc. Catalyst containing oxygen transport membrane
US9492784B2 (en) 2011-12-15 2016-11-15 Praxair Technology, Inc. Composite oxygen transport membrane
US9486735B2 (en) 2011-12-15 2016-11-08 Praxair Technology, Inc. Composite oxygen transport membrane
US9969645B2 (en) 2012-12-19 2018-05-15 Praxair Technology, Inc. Method for sealing an oxygen transport membrane assembly
US9453644B2 (en) 2012-12-28 2016-09-27 Praxair Technology, Inc. Oxygen transport membrane based advanced power cycle with low pressure synthesis gas slip stream
CN103205277A (en) * 2013-01-30 2013-07-17 吴江市新金城不锈钢制品有限公司 Minisize gas producer
US9611144B2 (en) 2013-04-26 2017-04-04 Praxair Technology, Inc. Method and system for producing a synthesis gas in an oxygen transport membrane based reforming system that is free of metal dusting corrosion
US10005664B2 (en) 2013-04-26 2018-06-26 Praxair Technology, Inc. Method and system for producing a synthesis gas using an oxygen transport membrane based reforming system with secondary reforming and auxiliary heat source
US9938145B2 (en) 2013-04-26 2018-04-10 Praxair Technology, Inc. Method and system for adjusting synthesis gas module in an oxygen transport membrane based reforming system
US9839899B2 (en) 2013-04-26 2017-12-12 Praxair Technology, Inc. Method and system for producing methanol using an integrated oxygen transport membrane based reforming system
US9776153B2 (en) 2013-10-07 2017-10-03 Praxair Technology, Inc. Ceramic oxygen transport membrane array reactor and reforming method
US9452401B2 (en) 2013-10-07 2016-09-27 Praxair Technology, Inc. Ceramic oxygen transport membrane array reactor and reforming method
US9486765B2 (en) 2013-10-07 2016-11-08 Praxair Technology, Inc. Ceramic oxygen transport membrane array reactor and reforming method
US9452388B2 (en) 2013-10-08 2016-09-27 Praxair Technology, Inc. System and method for air temperature control in an oxygen transport membrane based reactor
US9573094B2 (en) 2013-10-08 2017-02-21 Praxair Technology, Inc. System and method for temperature control in an oxygen transport membrane based reactor
US9556027B2 (en) 2013-12-02 2017-01-31 Praxair Technology, Inc. Method and system for producing hydrogen using an oxygen transport membrane based reforming system with secondary reforming
US9562472B2 (en) 2014-02-12 2017-02-07 Praxair Technology, Inc. Oxygen transport membrane reactor based method and system for generating electric power
US10822234B2 (en) 2014-04-16 2020-11-03 Praxair Technology, Inc. Method and system for oxygen transport membrane enhanced integrated gasifier combined cycle (IGCC)
US9789445B2 (en) 2014-10-07 2017-10-17 Praxair Technology, Inc. Composite oxygen ion transport membrane
US10441922B2 (en) 2015-06-29 2019-10-15 Praxair Technology, Inc. Dual function composite oxygen transport membrane
US10118823B2 (en) 2015-12-15 2018-11-06 Praxair Technology, Inc. Method of thermally-stabilizing an oxygen transport membrane-based reforming system
US9938146B2 (en) 2015-12-28 2018-04-10 Praxair Technology, Inc. High aspect ratio catalytic reactor and catalyst inserts therefor
US11052353B2 (en) 2016-04-01 2021-07-06 Praxair Technology, Inc. Catalyst-containing oxygen transport membrane
US11136238B2 (en) 2018-05-21 2021-10-05 Praxair Technology, Inc. OTM syngas panel with gas heated reformer

Also Published As

Publication number Publication date
CH297551A (en) 1954-03-31

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