GB642118A - Improvements in power plant - Google Patents

Improvements in power plant

Info

Publication number
GB642118A
GB642118A GB784547A GB784547A GB642118A GB 642118 A GB642118 A GB 642118A GB 784547 A GB784547 A GB 784547A GB 784547 A GB784547 A GB 784547A GB 642118 A GB642118 A GB 642118A
Authority
GB
United Kingdom
Prior art keywords
steam
pressure
furnace
generator
vapour
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
GB784547A
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.)
RONALD ERNEST ZOLLER
Babcock International Ltd
Original Assignee
RONALD ERNEST ZOLLER
Babcock and Wilcox Ltd
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 RONALD ERNEST ZOLLER, Babcock and Wilcox Ltd filed Critical RONALD ERNEST ZOLLER
Priority to GB784547A priority Critical patent/GB642118A/en
Publication of GB642118A publication Critical patent/GB642118A/en
Expired legal-status Critical Current

Links

Classifications

    • 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
    • F01K23/00Plants characterised by more than one engine delivering power external to the plant, the engines being driven by different fluids
    • F01K23/02Plants characterised by more than one engine delivering power external to the plant, the engines being driven by different fluids the engine cycles being thermally coupled
    • F01K23/06Plants characterised by more than one engine delivering power external to the plant, the engines being driven by different fluids the engine cycles being thermally coupled combustion heat from one cycle heating the fluid in another cycle
    • F01K23/10Plants characterised by more than one engine delivering power external to the plant, the engines being driven by different fluids the engine cycles being thermally coupled combustion heat from one cycle heating the fluid in another cycle with exhaust fluid of one cycle heating the fluid in another cycle
    • F01K23/106Plants characterised by more than one engine delivering power external to the plant, the engines being driven by different fluids the engine cycles being thermally coupled combustion heat from one cycle heating the fluid in another cycle with exhaust fluid of one cycle heating the fluid in another cycle with water evaporated or preheated at different pressures in exhaust boiler

Abstract

642,118. Gas turbine plant. BABCOCK & WILCOX, Ltd., and ZOLLER, R. E. March 21, 1947, No. 7845. [Class 110(iii)] In a gas turbine plant having a furnace fired by a vapour atomizing liquid burner the vapour for the burner is supplied by a vapour generator heated by the turbine exhaust gases. The gas turbine plant shown comprises a high pressure gas turbine 1 driven by gases supplied by a high pressure furnace 2 and a low pressure turbine 5 supplied by a low pressure furnace 4 which re-heats the exhaust gases from the turbine 1. The high pressure furnace 2 is supplied with combustion air by the compressors 6, 7 arranged in series, the low pressure compressor 6 being driven by the turbine 5 and the high pressure compressor 7 by the turbine 1. The combustion air for the high pressure furnace is heated in a heat exchanger 9 by the exhaust gases from the turbine 5. A conduit 10 supplies combustion air to the furnace 4. The furnaces 2, 4 are preferably of the type described in Specification 622,537, [Group XII]. and the burners 12, 13 of the whirlless type described in Specification 579,591, [Group XII]. Oil is supplied to the burners through pipes 14, 15 and steam through the pipes 18, 19 connected through pipes 24, 29 to steam generators 25, 30 heated by the exhaust gases from the low pressure turbine 5. Steam in excess of that required by the burners is passed through pipes 22, 23 and mixed with the furnace gases before they enter the respective turbines. The steam generator 25 is designed to generate steam at a higher pressure than that of the generator 30. The steam pressure in these two generators may be constant above that of the atmosphere or a pressure exceeding by a constant amount the gas pressure within the furnace or the liquid fuel pressure at the burner to which they are respectively connected. The generators 25, 30 are provided with steam and water drums 27, 32 and forced circulation pumps 28, 33. Feed water for the steam generators is heated in an economizer 34. The generating tube banks and economizer may be formed of finned and studded tubes as described in Specification 569,573. [Group XIII]. The valves 35, 36 controlling the amount of steam admixed with the gases may be used to automatically increase the steam pressure in the steam generators with increase of pressure in the furnaces 2, 4. A steam pipe 37 provided with an overflow valve 38 may be arranged to automatically control the pressure in the steam generator 30. Excess steam from the generator 25 may be passed through a connecting pipe 39 to the generator 30. Mechanical or air atomizing oil burners 41 are provided adjacent the generator 25 and are fired during starting up. According to the Provisional Specification, three vapour generators may be provided, the high pressure vapour generator supplies vapour to the burner of the high pressure furnace, the burner of the low pressure furnace may be supplied from the high or medium pressure vapour generator, and the medium and low pressure generators are arranged to supply vapour to the hollow jackets surrounding the combustion spaces of the furnaces as described in Specification 642,117. Specification 512,919, [Group XI], also is referred to.
GB784547A 1947-03-21 1947-03-21 Improvements in power plant Expired GB642118A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB784547A GB642118A (en) 1947-03-21 1947-03-21 Improvements in power plant

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB784547A GB642118A (en) 1947-03-21 1947-03-21 Improvements in power plant

Publications (1)

Publication Number Publication Date
GB642118A true GB642118A (en) 1950-08-30

Family

ID=9840886

Family Applications (1)

Application Number Title Priority Date Filing Date
GB784547A Expired GB642118A (en) 1947-03-21 1947-03-21 Improvements in power plant

Country Status (1)

Country Link
GB (1) GB642118A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2869323A (en) * 1957-01-02 1959-01-20 Gen Electric Gas turbine power plant with steam injection
US3353360A (en) * 1966-02-18 1967-11-21 Foster Wheeler Corp Power plant with steam injection
US6234984B1 (en) 1995-12-15 2001-05-22 Deca-Medics, Inc. Chest compression apparatus for cardiac arrest
AT501554A1 (en) * 2005-03-11 2006-09-15 Nagel Siegfried COMBUSTION ENGINE WITH INJECTOR, AND METHOD FOR OPERATING A COMBUSTION ENGINE WITH INJECTOR

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2869323A (en) * 1957-01-02 1959-01-20 Gen Electric Gas turbine power plant with steam injection
US3353360A (en) * 1966-02-18 1967-11-21 Foster Wheeler Corp Power plant with steam injection
US6234984B1 (en) 1995-12-15 2001-05-22 Deca-Medics, Inc. Chest compression apparatus for cardiac arrest
AT501554A1 (en) * 2005-03-11 2006-09-15 Nagel Siegfried COMBUSTION ENGINE WITH INJECTOR, AND METHOD FOR OPERATING A COMBUSTION ENGINE WITH INJECTOR
AT501554B1 (en) * 2005-03-11 2008-09-15 Delunamagma Ind Gmbh COMBUSTION ENGINE WITH A MEDIUM OR HIGH PRESSURE EXHAUST GAS TURBINE AND METHOD OF OPERATING THEREOF

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