SE7802285L - GAS TURBIN VALVE DEVICE - Google Patents

GAS TURBIN VALVE DEVICE

Info

Publication number
SE7802285L
SE7802285L SE7802285A SE7802285A SE7802285L SE 7802285 L SE7802285 L SE 7802285L SE 7802285 A SE7802285 A SE 7802285A SE 7802285 A SE7802285 A SE 7802285A SE 7802285 L SE7802285 L SE 7802285L
Authority
SE
Sweden
Prior art keywords
turbine
valve
valves
chamber
compressor
Prior art date
Application number
SE7802285A
Other languages
Unknown language ( )
Swedish (sv)
Other versions
SE410641B (en
Inventor
B Johansson
J Wikner
Original Assignee
Stal Laval Turbin Ab
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 Stal Laval Turbin Ab filed Critical Stal Laval Turbin Ab
Priority to SE7802285A priority Critical patent/SE410641B/en
Priority to CH73379A priority patent/CH634633A5/en
Priority to DE19792906393 priority patent/DE2906393A1/en
Priority to GB7906992A priority patent/GB2017219B/en
Publication of SE7802285L publication Critical patent/SE7802285L/en
Publication of SE410641B publication Critical patent/SE410641B/en

Links

Classifications

    • 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
    • F01D21/00Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for
    • F01D21/04Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for responsive to undesired position of rotor relative to stator or to breaking-off of a part of the rotor, e.g. indicating such position
    • F01D21/06Shutting-down
    • 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
    • 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
    • F02C9/00Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
    • F02C9/16Control of working fluid flow
    • F02C9/18Control of working fluid flow by bleeding, bypassing or acting on variable working fluid interconnections between turbines or compressors or their stages

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Fluidized-Bed Combustion And Resonant Combustion (AREA)
  • Engine Equipment That Uses Special Cycles (AREA)
  • Control Of Turbines (AREA)

Abstract

The plant comprises a combustion chamber 3, which may be a fluidised bed combustion chamber, an air compressor 1 having its outlet side connected to the chamber 3 by a pipe 5, and a pipe 6 for conveying combustion products from the chamber 3 to the inlet side of a gas turbine 2. For the purpose of stopping the turbine rapidly, in the event of a sudden loss of load or damage to the plant, valves 7 and 8 are provided in the pipes 5 and 6, respectively, and a third valve 9 is provided between the pipes 5 and 6. Normally the valves 7, 8 are open and the valve 9 shut, but when it is required to stop the turbine, the valve 9 is opened and the valves 7, 8 are closed. This has the effect of by- passing the combustion chamber 3 so that cool air flows from the compressor 1 directly to the turbine 2. The load of the compressor rapidly slows down the turbine. <IMAGE>
SE7802285A 1978-03-01 1978-03-01 GAS TURBIN VALVE DEVICE SE410641B (en)

Priority Applications (4)

Application Number Priority Date Filing Date Title
SE7802285A SE410641B (en) 1978-03-01 1978-03-01 GAS TURBIN VALVE DEVICE
CH73379A CH634633A5 (en) 1978-03-01 1979-01-25 VALVE ASSEMBLY FOR SHIFTING A COMBUSTOR IN A GAS TURBINE PLANT.
DE19792906393 DE2906393A1 (en) 1978-03-01 1979-02-20 VALVE ARRANGEMENT FOR SHUNTING A COMBUSTION CHAMBER IN A GAS TURBINE SYSTEM
GB7906992A GB2017219B (en) 1978-03-01 1979-02-28 Gas turbine plant

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SE7802285A SE410641B (en) 1978-03-01 1978-03-01 GAS TURBIN VALVE DEVICE

Publications (2)

Publication Number Publication Date
SE7802285L true SE7802285L (en) 1979-09-02
SE410641B SE410641B (en) 1979-10-22

Family

ID=20334131

Family Applications (1)

Application Number Title Priority Date Filing Date
SE7802285A SE410641B (en) 1978-03-01 1978-03-01 GAS TURBIN VALVE DEVICE

Country Status (4)

Country Link
CH (1) CH634633A5 (en)
DE (1) DE2906393A1 (en)
GB (1) GB2017219B (en)
SE (1) SE410641B (en)

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5058373A (en) * 1989-01-26 1991-10-22 General Electric Company Overspeed protection for a gas turbine/steam turbine combined cycle
US5069030A (en) * 1989-01-26 1991-12-03 General Electric Company Overspeed protection for a gas turbine/steam turbine combined cycle
US5199256A (en) * 1989-01-26 1993-04-06 General Electric Company Overspeed protection for a gas turbine/steam turbine combined cycle
EP0379930B1 (en) * 1989-01-26 1993-05-26 General Electric Company Overspeed protection for a gas turbine/steam turbine combined cycle
US5099643A (en) * 1989-01-26 1992-03-31 General Electric Company Overspeed protection for a gas turbine/steam turbine combined cycle
US5042247A (en) * 1989-01-26 1991-08-27 General Electric Company Overspeed protection method for a gas turbine/steam turbine combined cycle
US5042246A (en) * 1989-11-06 1991-08-27 General Electric Company Control system for single shaft combined cycle gas and steam turbine unit
US5301499A (en) * 1990-06-28 1994-04-12 General Electric Company Overspeed anticipation and control system for single shaft combined cycle gas and steam turbine unit
DE4339724C1 (en) * 1993-11-22 1995-01-19 Siemens Ag Gas fitting
DE4446395C2 (en) * 1994-12-23 1999-05-06 Janich Gmbh & Co Swing flap for hot gas pipelines
DE19541889A1 (en) * 1995-11-10 1997-05-15 Asea Brown Boveri Power plant
DE19741197C1 (en) 1997-09-18 1999-01-28 Siemens Ag Adaptor fitting for stationary gas turbine plant

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2040048A1 (en) * 1970-08-12 1972-02-17 Plessey Co Ltd Loaders for internal combustion engines
SE364756B (en) * 1972-07-07 1974-03-04 Stal Laval Turbin Ab
DE7418534U (en) * 1973-06-08 1974-10-24 Brown Boveri Sulzer Turbomaschinen Ag Closed gas turbine compressor arrangement with a relief device
DE2421708A1 (en) * 1974-05-04 1975-11-20 Robert Von Dipl Ing Linde Gas feed to an engine with external combustion - has regulated air by pass, and fuel metering unit
SE402797B (en) * 1975-09-12 1978-07-17 Stal Laval Turbin Ab COMBINED ENGINE AND GAS TURBINE SYSTEM

Also Published As

Publication number Publication date
GB2017219A (en) 1979-10-03
DE2906393A1 (en) 1979-09-06
GB2017219B (en) 1982-07-14
SE410641B (en) 1979-10-22
DE2906393C2 (en) 1991-02-28
CH634633A5 (en) 1983-02-15

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