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GB1165537A - Improvements in Gas Turbine Systems - Google Patents

Improvements in Gas Turbine Systems

Info

Publication number
GB1165537A
GB1165537A GB1014166A GB1014166A GB1165537A GB 1165537 A GB1165537 A GB 1165537A GB 1014166 A GB1014166 A GB 1014166A GB 1014166 A GB1014166 A GB 1014166A GB 1165537 A GB1165537 A GB 1165537A
Authority
GB
United Kingdom
Prior art keywords
air
line
heat exchanger
turbine
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
Application number
GB1014166A
Inventor
Raymond Bernard Sims
James Sumner Harrison
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.)
Coal Industry Patents Ltd
Original Assignee
Coal Industry Patents 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 Coal Industry Patents Ltd filed Critical Coal Industry Patents Ltd
Publication of GB1165537A publication Critical patent/GB1165537A/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
    • F02C1/08Semi-closed cycles
    • 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
    • F02C3/205Gas-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 in a fluidised-bed combustor

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Fluidized-Bed Combustion And Resonant Combustion (AREA)
  • Engine Equipment That Uses Special Cycles (AREA)

Abstract

1,165,537. Gas turbine plant; power plant. COAL INDUSTRY (PATENTS) Ltd. Jan. 10, 1967 [Jan. 11, 1968; March 8, 19661, Nos. 1266/66 and 10141/66. Headings F1G and F1Q. A gas turbine plant comprises a hot air turbine, the air being heated by being brought into heat exchange relation with the products of combustion of a fuel in the presence of a fluidized bed of solid particles, at least some of the heated air, after expansion in the turbine, providing a source of fluidizing gas for the fluidized bed. In Fig. 1 a hot air turbine 11 drives an air compressor 12 also an electric generator 13, air from the compressor passing through line 19 to the cold pass 16A of the fluidized bed heat exchanger 16, the air after being heated passing through line 20 to the hot air turbine 11. The air discharging from the turbine passes through line 17 to the combustion chamber 16B which constitutes the hot pass of the fluidized bed heat exchanger, the combustion gases from the chamber 16B finally discharging through outlet 18. Water is passed through line 21 into the second cold pass 16C of the heat exchanger, the steam produced passing through line 22 to a steam turbine 14. In Fig. 2 two fluidized bed heat exchangers, 16 and 23 are provided, combustion gases from a separate combustion chamber 24 passing first to the heat exchanger 16 then through line 25 to the second heat exchanger 23. Air from the compressor 12 passes through line 19 to the second heat exchanger 23, the air then passing through line 26 to the first heat exchanger 16, the heated air then passing through line 20 to the air turbine 11. The air discharging from the turbine passes through line 17 to the combustion chamber 24, a portion of the air being taken off through line 17A to the fluidized bed of the heat exchanger 23, and a second portion being taken off through line 17B to the fludized bed of the heat exchanger 16.
GB1014166A 1966-01-11 1966-01-11 Improvements in Gas Turbine Systems Expired GB1165537A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB126666 1966-01-11

Publications (1)

Publication Number Publication Date
GB1165537A true GB1165537A (en) 1969-10-01

Family

ID=9718984

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1014166A Expired GB1165537A (en) 1966-01-11 1966-01-11 Improvements in Gas Turbine Systems

Country Status (1)

Country Link
GB (1) GB1165537A (en)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2412691A1 (en) * 1977-12-23 1979-07-20 Bbc Brown Boveri & Cie
EP0243801A1 (en) * 1986-04-19 1987-11-04 Asea Brown Boveri Aktiengesellschaft Combined gas and steam plant with fluidized bed
RU2480601C2 (en) * 2011-02-22 2013-04-27 Открытое акционерное общество "СТАР" Gas turbine engine start-up control method
RU2542169C1 (en) * 2013-08-15 2015-02-20 Василий Иванович Мазий Device and method for economical production of electric power and heat
RU2650452C1 (en) * 2017-01-26 2018-04-13 Общество с ограниченной ответственностью Финансово-промышленная компания "Космос-Нефть-Газ" Gas turbine plant for processing associated petroleum gas to electric power
RU2713785C1 (en) * 2019-04-29 2020-02-07 Общество с ограниченной ответственностью Финансово-промышленная компания "Космос-Нефть-Газ" Gas-turbine unit for processing associated oil and various low-pressure gases into electric energy

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2412691A1 (en) * 1977-12-23 1979-07-20 Bbc Brown Boveri & Cie
EP0243801A1 (en) * 1986-04-19 1987-11-04 Asea Brown Boveri Aktiengesellschaft Combined gas and steam plant with fluidized bed
RU2480601C2 (en) * 2011-02-22 2013-04-27 Открытое акционерное общество "СТАР" Gas turbine engine start-up control method
RU2542169C1 (en) * 2013-08-15 2015-02-20 Василий Иванович Мазий Device and method for economical production of electric power and heat
RU2650452C1 (en) * 2017-01-26 2018-04-13 Общество с ограниченной ответственностью Финансово-промышленная компания "Космос-Нефть-Газ" Gas turbine plant for processing associated petroleum gas to electric power
RU2713785C1 (en) * 2019-04-29 2020-02-07 Общество с ограниченной ответственностью Финансово-промышленная компания "Космос-Нефть-Газ" Gas-turbine unit for processing associated oil and various low-pressure gases into electric energy

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Legal Events

Date Code Title Description
PS Patent sealed
PLNP Patent lapsed through nonpayment of renewal fees