FR2413551A1 - Installation de turbine a gaz - Google Patents

Installation de turbine a gaz

Info

Publication number
FR2413551A1
FR2413551A1 FR7836848A FR7836848A FR2413551A1 FR 2413551 A1 FR2413551 A1 FR 2413551A1 FR 7836848 A FR7836848 A FR 7836848A FR 7836848 A FR7836848 A FR 7836848A FR 2413551 A1 FR2413551 A1 FR 2413551A1
Authority
FR
France
Prior art keywords
turbine
compressor
gas turbine
turbine installation
section
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.)
Granted
Application number
FR7836848A
Other languages
English (en)
Other versions
FR2413551B1 (fr
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.)
Thomassen Holland BV
Original Assignee
Thomassen Holland BV
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 Thomassen Holland BV filed Critical Thomassen Holland BV
Publication of FR2413551A1 publication Critical patent/FR2413551A1/fr
Application granted granted Critical
Publication of FR2413551B1 publication Critical patent/FR2413551B1/fr
Expired legal-status Critical Current

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
    • F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
    • F02C3/04—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor
    • F02C3/10—Gas-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
    • F02C3/103—Gas-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 the compressor being of the centrifugal type
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01K—STEAM ENGINE PLANTS; STEAM ACCUMULATORS; ENGINE PLANTS NOT OTHERWISE PROVIDED FOR; ENGINES USING SPECIAL WORKING FLUIDS OR CYCLES
    • F01K23/00—Plants characterised by more than one engine delivering power external to the plant, the engines being driven by different fluids
    • F01K23/02—Plants characterised by more than one engine delivering power external to the plant, the engines being driven by different fluids the engine cycles being thermally coupled
    • F01K23/06—Plants characterised by more than one engine delivering power external to the plant, the engines being driven by different fluids the engine cycles being thermally coupled combustion heat from one cycle heating the fluid in another cycle
    • F01K23/10—Plants characterised by more than one engine delivering power external to the plant, the engines being driven by different fluids the engine cycles being thermally coupled combustion heat from one cycle heating the fluid in another cycle with exhaust fluid of one cycle heating the fluid in another cycle
    • 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
    • F02C6/00—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use
    • F02C6/18—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use using the waste heat of gas-turbine plants outside the plants themselves, e.g. gas-turbine power heat plants
    • 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
    • F02C7/00—Features, 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
    • F02C7/08—Heating air supply before combustion, e.g. by exhaust gases
    • F02C7/10—Heating air supply before combustion, e.g. by exhaust gases by means of regenerative heat-exchangers

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Engine Equipment That Uses Special Cycles (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

INSTALLATION DE TURBINE A GAZ COMPRENANT UNE SECTION DE COMPRESSEUR ET UNE SECTION DE TURBINE, LOGEES A L'INTERIEUR D'UN CARTER A PARTIES MULTIPLES, ET DANS LEQUEL LES ARBRES DES DIFFERENTES SECTIONS SONT CO-AXIAUX. LA SECTION DE COMPRESSEUR COMPREND UN COMPRESSEUR RADIAL BASSE PRESSION A DOUBLE FACE, UN COMPRESSEUR RADIAL A HAUTE PRESSION ET UN REFRIGERANT INTERMEDIAIRE TANDIS QUE L'ETAGE TURBINE COMPREND UNE PREMIERE TURBINE AXIALE MONTEE SUR LE MEME ARBRE QUE LE COMPRESSEUR ET AU MOINS UN ETAGE DE TURBINE SUPPLEMENTAIRE, UN ECHANGEUR DE CHALEUR OU REGENERATEUR ETANT INCORPORE DANS L'ECHAPPEMENT DE LA TURBINE.
FR787836848A 1978-01-03 1978-12-29 Installation de turbine a gaz Expired FR2413551B1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
NL7800077A NL7800077A (nl) 1978-01-03 1978-01-03 Gasturbine-installatie.

Publications (2)

Publication Number Publication Date
FR2413551A1 true FR2413551A1 (fr) 1979-07-27
FR2413551B1 FR2413551B1 (fr) 1985-07-26

Family

ID=19830084

Family Applications (1)

Application Number Title Priority Date Filing Date
FR787836848A Expired FR2413551B1 (fr) 1978-01-03 1978-12-29 Installation de turbine a gaz

Country Status (20)

Country Link
US (1) US4244191A (fr)
JP (1) JPS5498411A (fr)
AT (1) AT366786B (fr)
AU (1) AU523328B2 (fr)
BE (1) BE872865A (fr)
BR (1) BR7900016A (fr)
CA (1) CA1123618A (fr)
CH (1) CH627233A5 (fr)
CS (1) CS235074B2 (fr)
DD (1) DD141049A5 (fr)
DE (1) DE2900014A1 (fr)
ES (1) ES476461A1 (fr)
FR (1) FR2413551B1 (fr)
GB (1) GB2011543B (fr)
IT (1) IT1148701B (fr)
MX (1) MX150266A (fr)
NL (1) NL7800077A (fr)
NO (1) NO157115C (fr)
PL (1) PL120655B1 (fr)
SE (1) SE438709B (fr)

Families Citing this family (23)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3435382A1 (de) * 1984-09-27 1986-04-03 Hermann Dipl.-Ing. 5401 Kobern-Gondorf Bongers Gas-/dampf-verbundturbine mit erhoehtem temperaturniveau
DE3444433A1 (de) * 1984-12-06 1986-06-12 Hermann Dipl.-Ing. 5401 Kobern-Gondorf Bongers Gas/dampf-verbundturbine mit zweistufiger abwaermenutzung
JPH0776535B2 (ja) * 1985-02-05 1995-08-16 ウルステイン ターバイン エイ／エス 複式導入ラジアルタ−ビンガスゼネレ−タ
US4751814A (en) * 1985-06-21 1988-06-21 General Electric Company Air cycle thermodynamic conversion system
WO1990001624A1 (fr) * 1988-08-09 1990-02-22 Sundstrand Corporation Moteur de turbine avec refroidisseur intermediaire a haute pression
US4949544A (en) * 1988-12-06 1990-08-21 General Electric Company Series intercooler
CA2093683C (fr) * 1992-05-14 2002-10-15 William Miller Farrell Turbine a gaz a refroidissement intermediaire
RU2123610C1 (ru) * 1992-11-09 1998-12-20 ОРМАТ, Инк. Способ увеличения энергии, вырабатываемой системой газовой турбины
WO1995011376A1 (fr) * 1993-10-19 1995-04-27 State Of California Energy Resources Conservation And Development Commission Centrale thermique a turbine a gaz a performances ameliorees
US5937633A (en) * 1996-05-31 1999-08-17 Wang; Lin-Shu High-pressure intercooled gas turbine
US6363706B1 (en) 1998-12-24 2002-04-02 Alliedsignal Apparatus and method to increase turbine power
US6318065B1 (en) 1999-08-06 2001-11-20 Tom L. Pierson System for chilling inlet air for gas turbines
US6769258B2 (en) 1999-08-06 2004-08-03 Tom L. Pierson System for staged chilling of inlet air for gas turbines
US20050121532A1 (en) * 2003-12-05 2005-06-09 Reale Michael J. System and method for district heating with intercooled gas turbine engine
DE10358953A1 (de) 2003-12-15 2005-07-28 Man Turbo Ag Lagerung des Rotors einer Gasturbine
US7121906B2 (en) * 2004-11-30 2006-10-17 Carrier Corporation Method and apparatus for decreasing marine vessel power plant exhaust temperature
US20060112693A1 (en) * 2004-11-30 2006-06-01 Sundel Timothy N Method and apparatus for power generation using waste heat
US7665304B2 (en) * 2004-11-30 2010-02-23 Carrier Corporation Rankine cycle device having multiple turbo-generators
GB0608859D0 (en) * 2006-05-05 2006-06-14 Rolls Royce Plc A gas turbine engine
US20080047276A1 (en) * 2006-08-25 2008-02-28 Siemens Power Generation, Inc. Combustion turbine having a single compressor with inter-cooling between stages
CN102865139A (zh) * 2011-09-08 2013-01-09 摩尔动力(北京)技术股份有限公司 径流射流热动力系统
US10767561B2 (en) 2014-10-10 2020-09-08 Stellar Energy Americas, Inc. Method and apparatus for cooling the ambient air at the inlet of gas combustion turbine generators
US10808615B2 (en) 2015-09-04 2020-10-20 Stellar Energy Americas, Inc. Modular chiller plant

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB461887A (en) * 1935-07-25 1937-02-25 Frank Whittle Improvements relating to internal combustion turbines
GB653285A (en) * 1948-07-16 1951-05-09 Rolls Royce Improvements in or relating to gas-turbine power-plants
US2695499A (en) * 1949-08-22 1954-11-30 Power Jets Res & Dev Ltd Gas turbine power unit
US2960825A (en) * 1955-10-19 1960-11-22 Thompson Ramo Wooldridge Inc Reexpansion gas turbine engine with differential compressor drive
FR1284515A (fr) * 1957-10-16 1962-02-16 Perfectionnements apportés aux installations à turbines à gaz, notamment à celles pour la propulsion de véhicules
FR2292185A1 (fr) * 1974-11-22 1976-06-18 Sulzer Ag Procede et installation de vaporisation et de rechauffage de gaz naturel liquefie

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2575683A (en) * 1947-01-13 1951-11-20 Lockheed Aircraft Corp Intercooler and control system for turbo power plants
GB770563A (en) * 1953-12-28 1957-03-20 Garrett Corp Improvements in or relating to compressor output pressure control valve
US3209539A (en) * 1963-07-17 1965-10-05 Stanley Works G M B H Pump and motor transmission
FR1566271A (fr) * 1968-01-19 1969-05-09
US3796045A (en) * 1971-07-15 1974-03-12 Turbo Dev Inc Method and apparatus for increasing power output and/or thermal efficiency of a gas turbine power plant
US4003204A (en) * 1974-04-01 1977-01-18 Bradley Curtis E Fuel regenerated non-polluting internal combustion engine
US4030288A (en) * 1975-11-10 1977-06-21 Caterpillar Tractor Co. Modular gas turbine engine assembly

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB461887A (en) * 1935-07-25 1937-02-25 Frank Whittle Improvements relating to internal combustion turbines
GB653285A (en) * 1948-07-16 1951-05-09 Rolls Royce Improvements in or relating to gas-turbine power-plants
US2695499A (en) * 1949-08-22 1954-11-30 Power Jets Res & Dev Ltd Gas turbine power unit
US2960825A (en) * 1955-10-19 1960-11-22 Thompson Ramo Wooldridge Inc Reexpansion gas turbine engine with differential compressor drive
FR1284515A (fr) * 1957-10-16 1962-02-16 Perfectionnements apportés aux installations à turbines à gaz, notamment à celles pour la propulsion de véhicules
FR2292185A1 (fr) * 1974-11-22 1976-06-18 Sulzer Ag Procede et installation de vaporisation et de rechauffage de gaz naturel liquefie

Also Published As

Publication number Publication date
NO157115C (no) 1988-01-20
FR2413551B1 (fr) 1985-07-26
NO157115B (no) 1987-10-12
DE2900014A1 (de) 1979-07-12
GB2011543A (en) 1979-07-11
PL212218A1 (pl) 1979-09-10
AU523328B2 (en) 1982-07-22
BR7900016A (pt) 1979-08-07
DD141049A5 (de) 1980-04-09
JPS5498411A (en) 1979-08-03
CS235074B2 (en) 1985-04-16
MX150266A (es) 1984-04-06
CA1123618A (fr) 1982-05-18
ES476461A1 (es) 1979-05-01
AT366786B (de) 1982-05-10
ATA179A (de) 1981-09-15
CH627233A5 (fr) 1981-12-31
PL120655B1 (en) 1982-03-31
GB2011543B (en) 1982-07-21
SE438709B (sv) 1985-04-29
NO784413L (no) 1979-07-04
US4244191A (en) 1981-01-13
BE872865A (nl) 1979-06-19
NL7800077A (nl) 1979-07-05
AU4294378A (en) 1979-07-12
IT1148701B (it) 1986-12-03
IT7919025A0 (it) 1979-01-03
SE7813386L (sv) 1979-07-04

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Legal Events

Date Code Title Description
TP Transmission of property
ST Notification of lapse