FR2384951A1 - Centrale a turbine a gaz - Google Patents

Centrale a turbine a gaz

Info

Publication number
FR2384951A1
FR2384951A1 FR7807972A FR7807972A FR2384951A1 FR 2384951 A1 FR2384951 A1 FR 2384951A1 FR 7807972 A FR7807972 A FR 7807972A FR 7807972 A FR7807972 A FR 7807972A FR 2384951 A1 FR2384951 A1 FR 2384951A1
Authority
FR
France
Prior art keywords
high pressure
low pressure
pressure turbine
pressure compressor
low
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.)
Withdrawn
Application number
FR7807972A
Other languages
English (en)
Inventor
Thorolf Ingman
Ben Kyrklund
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.)
ABB Stal AB
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
Publication of FR2384951A1 publication Critical patent/FR2384951A1/fr
Withdrawn legal-status Critical Current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
    • F02C3/00Gas-turbine plants characterised by the use of combustion products as the working fluid
    • F02C3/04Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor
    • 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
    • F02C3/04Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor
    • F02C3/10Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor with another turbine driving an output shaft but not driving the compressor
    • 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
    • F02C3/36Open 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
    • F02C9/00Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
    • F02C9/16Control of working fluid flow
    • F02C9/20Control of working fluid flow by throttling; by adjusting vanes
    • F02C9/22Control of working fluid flow by throttling; by adjusting vanes by adjusting turbine vanes

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Control Of Positive-Displacement Air Blowers (AREA)
  • Supercharger (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

Centrale à turbine à gaz. Cette centrale comprend un compresseur LK basse pression et un compresseur HK haute pression entraînant respectivement une turbine HT haute pression et une turbine LT basse pression. La turbine haute pression entraîne un générateur. Une chambre B de combustion est interposée entre le compresseur HK haute pression et la turbine HT haute pression. Production d'énergie.
FR7807972A 1977-03-25 1978-03-20 Centrale a turbine a gaz Withdrawn FR2384951A1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SE7703422A SE404948B (sv) 1977-03-25 1977-03-25 Tvaaxlig gasturbinanleggning

Publications (1)

Publication Number Publication Date
FR2384951A1 true FR2384951A1 (fr) 1978-10-20

Family

ID=20330836

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7807972A Withdrawn FR2384951A1 (fr) 1977-03-25 1978-03-20 Centrale a turbine a gaz

Country Status (4)

Country Link
CH (1) CH626425A5 (fr)
DE (1) DE2812237A1 (fr)
FR (1) FR2384951A1 (fr)
SE (1) SE404948B (fr)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1993008391A1 (fr) * 1991-10-15 1993-04-29 United Technologies Corporation Systeme de turbo-moteur a combustion
WO1999061767A1 (fr) * 1998-05-29 1999-12-02 Pratt & Whitney Canada Corp Recuperateur pour moteur a turbine a gaz

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
ZA835029B (en) * 1982-09-27 1984-03-28 English Electric Co Ltd Power-generation plant and method
US5081832A (en) * 1990-03-05 1992-01-21 Rolf Jan Mowill High efficiency, twin spool, radial-high pressure, gas turbine engine
SE469039B (sv) * 1991-09-13 1993-05-03 Abb Carbon Ab Foerfarande vid luftfloedesreglering i en pfbc-anlaeggning samt anordning foer genomfoerande av foerfarandet.
US5628182A (en) * 1993-07-07 1997-05-13 Mowill; R. Jan Star combustor with dilution ports in can portions
US5638674A (en) * 1993-07-07 1997-06-17 Mowill; R. Jan Convectively cooled, single stage, fully premixed controllable fuel/air combustor with tangential admission
US5377483A (en) * 1993-07-07 1995-01-03 Mowill; R. Jan Process for single stage premixed constant fuel/air ratio combustion
US5572862A (en) * 1993-07-07 1996-11-12 Mowill Rolf Jan Convectively cooled, single stage, fully premixed fuel/air combustor for gas turbine engine modules
US5613357A (en) * 1993-07-07 1997-03-25 Mowill; R. Jan Star-shaped single stage low emission combustor system
US6220034B1 (en) 1993-07-07 2001-04-24 R. Jan Mowill Convectively cooled, single stage, fully premixed controllable fuel/air combustor
RU2525041C1 (ru) * 2013-05-07 2014-08-10 Федеральное государственное бюджетное образовательное учреждение высшего профессионального образования "Казанский государственный энергетический университет" (ФГБОУ ВПО "КГЭУ") Способ работы газораспределительной станции
CN104791128A (zh) * 2014-02-12 2015-07-22 摩尔动力(北京)技术股份有限公司 高低压轴变界机构发动机
RU2636643C1 (ru) * 2016-09-20 2017-11-24 Михаил Аркадьевич Верткин Утилизационная турбоустановка

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CH210657A (de) * 1938-12-24 1940-07-31 Sulzer Ag Gasturbinenanlage.
FR998209A (fr) * 1948-11-02 1952-01-16 Power Jets Res & Dev Ltd Perfectionnements apportés aux installations avec turbines à gaz
FR1043051A (fr) * 1950-06-01 1953-11-05 Oerlikon Maschf Procédé de réglage des installations de turbines à gaz
FR1246455A (fr) * 1959-01-10 1960-11-18 Sulzer Ag Installation de turbines à gaz à deux arbres
FR2062652A5 (fr) * 1969-09-25 1971-06-25 Garrett Corp
FR2124253A1 (fr) * 1971-02-01 1972-09-22 Stal Laval Turbin Ab

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CH210657A (de) * 1938-12-24 1940-07-31 Sulzer Ag Gasturbinenanlage.
FR998209A (fr) * 1948-11-02 1952-01-16 Power Jets Res & Dev Ltd Perfectionnements apportés aux installations avec turbines à gaz
FR1043051A (fr) * 1950-06-01 1953-11-05 Oerlikon Maschf Procédé de réglage des installations de turbines à gaz
FR1246455A (fr) * 1959-01-10 1960-11-18 Sulzer Ag Installation de turbines à gaz à deux arbres
FR2062652A5 (fr) * 1969-09-25 1971-06-25 Garrett Corp
FR2124253A1 (fr) * 1971-02-01 1972-09-22 Stal Laval Turbin Ab

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1993008391A1 (fr) * 1991-10-15 1993-04-29 United Technologies Corporation Systeme de turbo-moteur a combustion
WO1999061767A1 (fr) * 1998-05-29 1999-12-02 Pratt & Whitney Canada Corp Recuperateur pour moteur a turbine a gaz
US6092361A (en) * 1998-05-29 2000-07-25 Pratt & Whitney Canada Corp. Recuperator for gas turbine engine

Also Published As

Publication number Publication date
DE2812237A1 (de) 1978-10-05
CH626425A5 (en) 1981-11-13
SE7703422L (sv) 1978-09-26
SE404948B (sv) 1978-11-06

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Legal Events

Date Code Title Description
RE Withdrawal of published application