GB1263124A - Gas turbine installation using nuclear energy or fossil fuels as heat source - Google Patents
Gas turbine installation using nuclear energy or fossil fuels as heat sourceInfo
- Publication number
- GB1263124A GB1263124A GB21111/69A GB2111169A GB1263124A GB 1263124 A GB1263124 A GB 1263124A GB 21111/69 A GB21111/69 A GB 21111/69A GB 2111169 A GB2111169 A GB 2111169A GB 1263124 A GB1263124 A GB 1263124A
- Authority
- GB
- United Kingdom
- Prior art keywords
- heat exchanger
- ata
- compressor
- working fluid
- passing
- 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
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C1/00—Gas-turbine plants characterised by the use of hot gases or unheated pressurised gases, as the working fluid
- F02C1/04—Gas-turbine plants characterised by the use of hot gases or unheated pressurised gases, as the working fluid the working fluid being heated indirectly
- F02C1/10—Closed cycles
-
- G—PHYSICS
- G21—NUCLEAR PHYSICS; NUCLEAR ENGINEERING
- G21D—NUCLEAR POWER PLANT
- G21D5/00—Arrangements of reactor and engine in which reactor-produced heat is converted into mechanical energy
- G21D5/04—Reactor and engine not structurally combined
- G21D5/08—Reactor and engine not structurally combined with engine working medium heated in a heat exchanger by the reactor coolant
-
- Y—GENERAL 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
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E30/00—Energy generation of nuclear origin
-
- Y—GENERAL 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
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- General Engineering & Computer Science (AREA)
- Plasma & Fusion (AREA)
- High Energy & Nuclear Physics (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- Engine Equipment That Uses Special Cycles (AREA)
- Separation By Low-Temperature Treatments (AREA)
Abstract
1,263,124. Gas turbine plant - closed cycle type. SIEMENS A. G. April 24, 1969 [April 24, 1968], No.21111/69. Heading F1G. [Also in Division G6] The invention relates to a gas turbine plant of the closed circuit type comprising a first compressor and a second compressor, part only of the working fluid passing through the second compressor, which part is taken from the working fluid path downstream of the low-pressure side of a recuperative heat exchanger, the part being delivered after compression to re-join the remaining part of the working fluid at the high-pressure side of the heat exchanger at a point which is at a higher temperature than that at which the remaining part enters the heat exchanger. In Fig. 1 the working fluid, CO 2 , is heated in a heat exchanger 10 by heat exchange with a fluid heated in a nuclear reactor not shown, the CO 2 discharging at 300 ata and 500C. and passing through valves 30, 31 to a compressor-drive turbine 13 and a power turbine 14, the fluids discharging from the turbines at 57 ata and 320 C. being re-united and passing to the low-pressure side of a recuperative heat exchanger 19. The fluid then passes at 56 ata and 85 C. through a cooler 22 and thence through a compressor 16 driven by the turbine 14. The fluid then divides, the major portion (70%) passing through cooler 21, compressor 18 which is also driven by turbine 14, thence through the highpressure side 20 of the heat exchanger 19, the fluid finally discharging at 305 ata and 273 C. back to the working fluid heater 10. The remaining portion (30%) of the working fluid from the compressor 16 passes direct to the compressor 17 which is driven by the turbine 13, discharging therefrom at 308 ata and 190 C. and passing through non-return valve 32 to an intermediate point a of the high-pressure coil 20 of the heat exchanger 19. An auxiliary cooler 23 controlled by a valve 37 is provided; a by-pass valve 36 is also provided. In Fig. 2 the low-pressure working fluid discharging from the heat exchanger 19 is divided, part (70%) passing through cooler 21 to compressor 18 from which it passes to the high-pressure side 20 of the heat exchanger from which it discharges at 305 ata and 327 C. back to the working fluid heater 10. The remaining part (30%) of the working fluid passes through valve 35 to the compressor 17 and then passes through N R V 32 to re-unite with the 70% at intermediate point a of the high-pressure coil 20. In Fig. 3 the working fluid is heated, at relatively low-pressure directly in the nuclear reactor 11, the heated fluid passing to the lowpressure side of the heat exchanger 19 where it heats the high-pressure working fluid in coil 20, the working fluid discharging at 300 ata and 436 C. and dividing to pass to the two turbines 14 and 13, the fluid streams from the turbines re-uniting and passing at 120 ata and 334 C. to the nuclear reactor 11. The low-pressure fluid passes through the heat exchanger 19 and then divides, part (75%) passing through cooler 21 and thence at 110 ata and 40 C. to the compressor 16 from which it discharges at 305 ata and 73 C. to high-pressure coil 20 of the heat exchanger 19. The second part (25%) of the working fluid passes to the compressor 17 from which it discharges at 303 ata and 177 C. to an intermediate point a of the high-pressure coil 20, the re-united stream then passing to the turbines 13, 14. In Fig. 5 the working fluid is heated in a heat exchanger 121 by combustion gases from a furnace 12, the fluid at 300 ata and 500 C. dividing and passing to two turbines 13, 14, the exhaust streams from the turbines re-uniting at 93 ata and 364 C. and passing to the low-pressure side of the heat exchanger 19. The flow then divides, part (70%) passing through cooler 21 and thence through compressor 16 to the high-pressure coil 20 of the heat exchanger 19. The remaining part (30%) passes through the compressor 17 and discharges at 308 ata and 197 C. to re-unite with the 70% part at intermediate point a of the high-pressure coil 20. The re-united stream then passes through heater 121 and discharges therefrom at 300 ata and 500 C. to the turbines 13, 14. Part of the low-pressure fluid from the heat exchanger 19 is tapped off at point b and passed through air pre-heater 123, the working fluid being returned at point b of the cooler 21.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE19681751226 DE1751226C (en) | 1968-04-24 | Gas turbine plant heated by nuclear power or fossil fuels |
Publications (1)
Publication Number | Publication Date |
---|---|
GB1263124A true GB1263124A (en) | 1972-02-09 |
Family
ID=5692194
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB21111/69A Expired GB1263124A (en) | 1968-04-24 | 1969-04-24 | Gas turbine installation using nuclear energy or fossil fuels as heat source |
Country Status (5)
Country | Link |
---|---|
US (1) | US3583156A (en) |
JP (1) | JPS4820322B1 (en) |
CH (1) | CH488103A (en) |
FR (1) | FR2016741A1 (en) |
GB (1) | GB1263124A (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RU2508460C1 (en) * | 2012-07-10 | 2014-02-27 | Федеральное государственное унитарное предприятие "Государственный космический научно-производственный центр имени М.В. Хруничева" | Extra-terrestrial power plant with computer-aided energy conversion |
RU2583191C1 (en) * | 2014-12-22 | 2016-05-10 | Федеральное государственное унитарное предприятие "Государственный космический научно-производственный центр имени М.В. Хруничева" | Space power plant with machine energy conversion |
RU2716766C1 (en) * | 2019-03-11 | 2020-03-16 | Акционерное общество "Государственный космический научно-производственный центр имени М.В. Хруничева" | Power plant with machine conversion of energy |
RU2757148C1 (en) * | 2020-11-10 | 2021-10-11 | Акционерное общество "КБхиммаш им. А.М. Исаева" | Space power plant with machine energy conversion |
Families Citing this family (29)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3878683A (en) * | 1969-07-01 | 1975-04-22 | Kenji Imai | Method of cooling substance or generating power by use of liquefied gas |
FR2253254B1 (en) * | 1973-11-29 | 1977-12-16 | Rigollot Georges | |
US4003786A (en) * | 1975-09-16 | 1977-01-18 | Exxon Research And Engineering Company | Thermal energy storage and utilization system |
US4863675A (en) * | 1984-10-04 | 1989-09-05 | General Atomics | Nuclear power system |
CH682357A5 (en) * | 1991-09-05 | 1993-08-31 | Asea Brown Boveri | |
US5309492A (en) * | 1993-04-15 | 1994-05-03 | Adams Atomic Engines, Inc. | Control for a closed cycle gas turbine system |
JP3530939B2 (en) * | 2001-08-09 | 2004-05-24 | 東京工業大学長 | Reactor plant |
US20040131138A1 (en) * | 2001-05-25 | 2004-07-08 | Michael Correia | Brayton cycle nuclear power plant and a method of starting the brayton cycle |
JP3953871B2 (en) * | 2002-04-15 | 2007-08-08 | サンデン株式会社 | Refrigeration air conditioner |
JP2005233148A (en) * | 2004-02-23 | 2005-09-02 | Mitsubishi Heavy Ind Ltd | Gas turbine plant |
JP2005233149A (en) * | 2004-02-23 | 2005-09-02 | Mitsubishi Heavy Ind Ltd | Gas turbine plant |
CA2583651A1 (en) * | 2004-10-21 | 2006-05-04 | Deutsches Zentrum Fuer Luft-Und Raumfahrt E.V. | Device for generating highly compressed gas |
US20120067054A1 (en) | 2010-09-21 | 2012-03-22 | Palmer Labs, Llc | High efficiency power production methods, assemblies, and systems |
WO2012176254A1 (en) * | 2011-06-20 | 2012-12-27 | 熱技術開発株式会社 | Closed-cycle gas turbine |
WO2012176257A1 (en) * | 2011-06-20 | 2012-12-27 | 熱技術開発株式会社 | Closed-cycle gas turbine |
US8887503B2 (en) * | 2011-12-13 | 2014-11-18 | Aerojet Rocketdyne of DE, Inc | Recuperative supercritical carbon dioxide cycle |
EP2800099B1 (en) * | 2011-12-20 | 2016-07-27 | Nihon Nature Cell Co., Ltd. | Compact nuclear power generation system |
US9540999B2 (en) * | 2012-01-17 | 2017-01-10 | Peregrine Turbine Technologies, Llc | System and method for generating power using a supercritical fluid |
DE102012213614B3 (en) * | 2012-08-01 | 2014-04-03 | Areva Gmbh | Containment protection system for a nuclear installation and related operating procedure |
KR20170054411A (en) | 2014-08-22 | 2017-05-17 | 페레그린 터빈 테크놀로지스, 엘엘씨 | Power generation system and method for generating power |
WO2018231194A1 (en) * | 2017-06-12 | 2018-12-20 | General Electric Company | Counter-flow heat exchanger |
MX2020002368A (en) * | 2017-08-28 | 2020-09-14 | 8 Rivers Capital Llc | LOW-GRADE HEAT OPTIMIZATION OF RECUPERATIVE SUPERCRITICAL CO<sub>2</sub> POWER CYCLES. |
US10570783B2 (en) * | 2017-11-28 | 2020-02-25 | Hanwha Power Systems Co., Ltd | Power generation system using supercritical carbon dioxide |
US11407283B2 (en) * | 2018-04-30 | 2022-08-09 | Tiger Tool International Incorporated | Cab heating systems and methods for vehicles |
US11993130B2 (en) | 2018-11-05 | 2024-05-28 | Tiger Tool International Incorporated | Cooling systems and methods for vehicle cabs |
CN110848032B (en) * | 2019-12-05 | 2023-08-01 | 上海电气燃气轮机有限公司 | Method and adjusting system for eliminating thermal suspension precursor of gas turbine |
CN110836144B (en) * | 2019-12-05 | 2023-08-01 | 上海电气燃气轮机有限公司 | Method and adjusting system for preventing gas turbine from generating thermal suspension |
US12030368B2 (en) | 2020-07-02 | 2024-07-09 | Tiger Tool International Incorporated | Compressor systems and methods for use by vehicle heating, ventilating, and air conditioning systems |
US11492964B2 (en) | 2020-11-25 | 2022-11-08 | Michael F. Keller | Integrated supercritical CO2/multiple thermal cycles |
Family Cites Families (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2203731A (en) * | 1937-01-25 | 1940-06-11 | Ag Fuer Technische Studien | Means for regulating and starting thermal power plants |
BE665893A (en) * | 1964-07-08 | 1965-10-18 | ||
DE1564655C3 (en) * | 1966-07-09 | 1975-10-02 | Siemens Ag, 1000 Berlin Und 8000 Muenchen | Nuclear power plant with CO deep 2 cooling |
-
1969
- 1969-03-31 CH CH481569A patent/CH488103A/en not_active IP Right Cessation
- 1969-04-16 US US816520A patent/US3583156A/en not_active Expired - Lifetime
- 1969-04-23 FR FR6912866A patent/FR2016741A1/fr not_active Withdrawn
- 1969-04-24 GB GB21111/69A patent/GB1263124A/en not_active Expired
- 1969-04-24 JP JP44031336A patent/JPS4820322B1/ja active Pending
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RU2508460C1 (en) * | 2012-07-10 | 2014-02-27 | Федеральное государственное унитарное предприятие "Государственный космический научно-производственный центр имени М.В. Хруничева" | Extra-terrestrial power plant with computer-aided energy conversion |
RU2583191C1 (en) * | 2014-12-22 | 2016-05-10 | Федеральное государственное унитарное предприятие "Государственный космический научно-производственный центр имени М.В. Хруничева" | Space power plant with machine energy conversion |
RU2716766C1 (en) * | 2019-03-11 | 2020-03-16 | Акционерное общество "Государственный космический научно-производственный центр имени М.В. Хруничева" | Power plant with machine conversion of energy |
RU2757148C1 (en) * | 2020-11-10 | 2021-10-11 | Акционерное общество "КБхиммаш им. А.М. Исаева" | Space power plant with machine energy conversion |
Also Published As
Publication number | Publication date |
---|---|
JPS4820322B1 (en) | 1973-06-20 |
FR2016741A1 (en) | 1970-05-15 |
DE1751226A1 (en) | 1971-05-19 |
DE1751226B2 (en) | 1973-02-15 |
CH488103A (en) | 1970-03-31 |
US3583156A (en) | 1971-06-08 |
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