GB631069A - Improvements in thermal power plants - Google Patents

Improvements in thermal power plants

Info

Publication number
GB631069A
GB631069A GB27155/47A GB2715547A GB631069A GB 631069 A GB631069 A GB 631069A GB 27155/47 A GB27155/47 A GB 27155/47A GB 2715547 A GB2715547 A GB 2715547A GB 631069 A GB631069 A GB 631069A
Authority
GB
United Kingdom
Prior art keywords
heat
working medium
turbine
fluid
compressor
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
GB27155/47A
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.)
Aktiengesellschaft fuer Technische Studien
Original Assignee
Aktiengesellschaft fuer Technische Studien
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 Aktiengesellschaft fuer Technische Studien filed Critical Aktiengesellschaft fuer Technische Studien
Publication of GB631069A publication Critical patent/GB631069A/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
    • F02C1/00Gas-turbine plants characterised by the use of hot gases or unheated pressurised gases, as the working fluid
    • F02C1/04Gas-turbine plants characterised by the use of hot gases or unheated pressurised gases, as the working fluid the working fluid being heated indirectly
    • F02C1/05Gas-turbine plants characterised by the use of hot gases or unheated pressurised gases, as the working fluid the working fluid being heated indirectly characterised by the type or source of heat, e.g. using nuclear or solar energy
    • GPHYSICS
    • G21NUCLEAR PHYSICS; NUCLEAR ENGINEERING
    • G21CNUCLEAR REACTORS
    • G21C1/00Reactor types
    • G21C1/04Thermal reactors ; Epithermal reactors
    • 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
    • Y02E30/00Energy generation of nuclear origin
    • Y02E30/30Nuclear fission reactors

Abstract

631,069. Fluid-pressure servomotor-control systems. AKT.-GES. FUR TECHNISCHE STUDIEN. Oct. 9, 1947, No. 27155. Convention date, Nov. 2, 1946. - [Class 135] [Also in Group XXVI] A gas-turbine plant in which a gaseous working medium describes a closed circuit including at least one compressor and at least one turbine and receives heat in a heater from an intermediate heat convector fluid circulating in an auxiliary circuit containing a nuclear reaction pile, has means for regulating the velocity of circulation of the heat convector fluid so that it is substantially proportional to the quantity of heat to be transmitted to the gaseous working medium. In the gas-turbine plant shown the gaseous working medium flows through a closed circuit including a compressor 1, a heat exchanger 2, a heater 3 in which heat is supplied to the working medium from an external source, a turbine 4 which drives the compressor 1 and a generator 5 and a cooler 71. The heat supplied to the heater 3 is obtained from a nuclear reaction pile 50 through which and the heat exchanger 3, a heat convector fluid is circulated by a blower 52. A decrease in load on the generator 5 causes the governor weights to fly out and turn the lever 9 counterclockwise thus lowering the valve 11. This allows servo fluid to pass into the space above the piston 13 which then moves downwards and through the collar 17 opens the valve 19. At the same time the lever 24 is moved in a counterclockwise direction which causes the collar 26 to open the valve 27 and the lever 49 to switch on the driving motor 45 of the charging compressor 44. Working medium is then extracted from the circuit at the point 38 and flows through pipe 37, valve 27 and pipe 41 into the suction 43 of the compressor 44 from which it is discharged through the pipe 46, valve 19 and pipe 34 into the storage vessel 35. The pressure at the point 59 then falls and the piston 56 is moved to the right by the spring 57. This causes the contact arm 59<SP>1</SP> to move over the variable resistance 60 and thus slow down the motor 61 of the blower 52 which circulates the heat convector fluid. When the load on the generator 5 is increased the valves are so operated that working medium is pumped from the storage vessel 35 into the circuit and the speed of the motor 61 increased. If the output power plant is controlled by means of a byepass pipe around the turbine or by throttling the current of working medium in the main circuit, the velocity at which the heat convector fluid is circulated may be regulated by the difference of inlet and exhaust pressures of the turbine.
GB27155/47A 1946-11-02 1947-10-09 Improvements in thermal power plants Expired GB631069A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CH631069X 1946-11-02

Publications (1)

Publication Number Publication Date
GB631069A true GB631069A (en) 1949-10-26

Family

ID=4524748

Family Applications (1)

Application Number Title Priority Date Filing Date
GB27155/47A Expired GB631069A (en) 1946-11-02 1947-10-09 Improvements in thermal power plants

Country Status (1)

Country Link
GB (1) GB631069A (en)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1114362B (en) * 1958-02-14 1961-09-28 Parsons & Marine Eng Turbine Closed circuit gas turbine plant
US3042600A (en) * 1956-11-28 1962-07-03 Gen Electric Reactor control
US3045895A (en) * 1957-01-30 1962-07-24 Parsons C A & Co Ltd Gas circulatory means
US3065162A (en) * 1957-07-22 1962-11-20 Internuclear Company Nuclear reactor control system
US3109781A (en) * 1958-11-06 1963-11-05 Richfield Oil Corp Combined apparatus of a retort, fractionator and heater for treating hydrocarboniferous material
US3166479A (en) * 1961-05-26 1965-01-19 Asea Ab Method for pressure relief in gas containers and means for carrying out the method

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3042600A (en) * 1956-11-28 1962-07-03 Gen Electric Reactor control
US3045895A (en) * 1957-01-30 1962-07-24 Parsons C A & Co Ltd Gas circulatory means
US3065162A (en) * 1957-07-22 1962-11-20 Internuclear Company Nuclear reactor control system
DE1114362B (en) * 1958-02-14 1961-09-28 Parsons & Marine Eng Turbine Closed circuit gas turbine plant
US3109781A (en) * 1958-11-06 1963-11-05 Richfield Oil Corp Combined apparatus of a retort, fractionator and heater for treating hydrocarboniferous material
US3166479A (en) * 1961-05-26 1965-01-19 Asea Ab Method for pressure relief in gas containers and means for carrying out the method

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