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ES382862A1 - Combustion control system for gas turbines - Google Patents

Combustion control system for gas turbines

Info

Publication number
ES382862A1
ES382862A1 ES382862A ES382862A ES382862A1 ES 382862 A1 ES382862 A1 ES 382862A1 ES 382862 A ES382862 A ES 382862A ES 382862 A ES382862 A ES 382862A ES 382862 A1 ES382862 A1 ES 382862A1
Authority
ES
Spain
Prior art keywords
compressor
turbine
valve
combustion chamber
outlet pressure
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
ES382862A
Other languages
Spanish (es)
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.)
CAV Ltd
Original Assignee
CAV 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 CAV Ltd filed Critical CAV Ltd
Publication of ES382862A1 publication Critical patent/ES382862A1/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
    • F02C7/00Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/26Starting; Ignition
    • F02C7/262Restarting after flame-out
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2270/00Control
    • F05D2270/30Control parameters, e.g. input parameters
    • F05D2270/301Pressure

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Control Of Combustion (AREA)
  • Regulation And Control Of Combustion (AREA)
  • Feeding And Controlling Fuel (AREA)

Abstract

Improvements in the flame sensor systems, for use with combustion systems of the kind that comprise a combustion chamber, a turbine moved by heated gases that leave the combustion chamber, a compressor moved by said turbine to supply air under pressure to the chamber combustion, a valve to control the passage of fuel to the combustion chamber, means to rotate the compressors and the turbine for start-up and means to ignite the air/fuel mixture in the combustion chamber, characterized in that the system comprises in combination pressure-actuated switching means that respond to the outlet pressure of the compressor, said switching means being arranged so that they are actuated when the outlet pressure of the compressor reaches a predetermined value greater than the maximum outlet pressure that may occur when the means to rotate the compressor and the turbine are working ndo, said switch means serving when operated to keep said valve in the open position, and timer means operable for a limited period of time to effect opening of said valve for start-up, such arrangement being that in the case of If the compressor outlet pressure does not reach said predetermined value within the time allowed by said timing means, the valve will close to prevent the additional passage of fuel. (Machine-translation by Google Translate, not legally binding)
ES382862A 1969-08-07 1970-08-04 Combustion control system for gas turbines Expired ES382862A1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB3952169 1969-08-07

Publications (1)

Publication Number Publication Date
ES382862A1 true ES382862A1 (en) 1972-12-16

Family

ID=10410011

Family Applications (1)

Application Number Title Priority Date Filing Date
ES382862A Expired ES382862A1 (en) 1969-08-07 1970-08-04 Combustion control system for gas turbines

Country Status (9)

Country Link
AU (1) AU1855770A (en)
BE (1) BE754490A (en)
DE (1) DE2038088A1 (en)
ES (1) ES382862A1 (en)
FR (1) FR2056755A5 (en)
GB (1) GB1314516A (en)
NL (1) NL7011396A (en)
RO (1) RO54542A (en)
ZA (1) ZA705185B (en)

Also Published As

Publication number Publication date
AU1855770A (en) 1972-02-10
NL7011396A (en) 1971-02-09
RO54542A (en) 1974-01-03
FR2056755A5 (en) 1971-05-14
ZA705185B (en) 1971-04-28
GB1314516A (en) 1973-04-26
BE754490A (en) 1971-01-18
DE2038088A1 (en) 1971-02-18

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