MX9306959A - METHOD AND APPARATUS TO INCREASE THE POWER PRODUCED BY GAS TURBINES. - Google Patents

METHOD AND APPARATUS TO INCREASE THE POWER PRODUCED BY GAS TURBINES.

Info

Publication number
MX9306959A
MX9306959A MX9306959A MX9306959A MX9306959A MX 9306959 A MX9306959 A MX 9306959A MX 9306959 A MX9306959 A MX 9306959A MX 9306959 A MX9306959 A MX 9306959A MX 9306959 A MX9306959 A MX 9306959A
Authority
MX
Mexico
Prior art keywords
supplied
main compressor
air
power produced
turbine
Prior art date
Application number
MX9306959A
Other languages
Spanish (es)
Inventor
Lucien Y Bronicki
Yoel Gilin
Original Assignee
Ormat Ind 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 Ormat Ind Ltd filed Critical Ormat Ind Ltd
Publication of MX9306959A publication Critical patent/MX9306959A/en

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
    • F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants

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)
  • Separation By Low-Temperature Treatments (AREA)

Abstract

La potencia producida por un sistema de turbina de gas se aumenta mediante un dispositivo precompresor que comprime el aire ambiental suministrado al compresor principal del sistema, con lo cual introduce temperatura y sube la presión en el aire suministrado. Se enfría el aire suministrado al compresor principal usando un sistema de refrigeración mecánica para disminuir la temperatura del aire suministrado en la entrada al compresor principal de una turbina de gas. El aire comprimido por el compresor principal se suministra a una cámara de combustión para calentar el aire comprimido y producir gases calientes que se suministran a una turbina que suministra una carga e impulsa al compresor principal. Los gases calientes descargados se suministran a una caldera que produce vapor que se aplica a una turbina de vapor que suministra una carga. El uso de un enfriador en lugar de un enfriamiento evaporativo del comprimido es conveniente por que le da al aparato insensibilidad a las condiciones húmedas del aire ambiental.The power produced by a gas turbine system is increased by a precompressor device that compresses the ambient air supplied to the main compressor of the system, thereby introducing temperature and increasing the pressure in the supplied air. The air supplied to the main compressor is cooled using a mechanical refrigeration system to lower the temperature of the air supplied at the inlet to the main compressor of a gas turbine. The compressed air from the main compressor is supplied to a combustion chamber to heat the compressed air and produce hot gases that are supplied to a turbine that supplies a load and drives the main compressor. The discharged hot gases are supplied to a steam producing boiler which is applied to a steam turbine which supplies a charge. The use of a cooler instead of evaporative cooling of the tablet is convenient because it makes the device insensitive to humid ambient air conditions.

MX9306959A 1992-11-09 1993-11-08 METHOD AND APPARATUS TO INCREASE THE POWER PRODUCED BY GAS TURBINES. MX9306959A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US97361292A 1992-11-09 1992-11-09

Publications (1)

Publication Number Publication Date
MX9306959A true MX9306959A (en) 1994-05-31

Family

ID=25521059

Family Applications (1)

Application Number Title Priority Date Filing Date
MX9306959A MX9306959A (en) 1992-11-09 1993-11-08 METHOD AND APPARATUS TO INCREASE THE POWER PRODUCED BY GAS TURBINES.

Country Status (8)

Country Link
KR (1) KR940011780A (en)
CN (1) CN1092136A (en)
BR (1) BR9304471A (en)
ES (1) ES2068781B1 (en)
IL (1) IL107530A (en)
IT (1) IT1273629B (en)
MX (1) MX9306959A (en)
RU (1) RU2123610C1 (en)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
ES2115487B1 (en) * 1994-12-29 1999-02-16 Sener Ing & Sist SYSTEM AND INSTALLATION TO IMPROVE THE PERFORMANCE OF GAS TURBINES LOCATED IN AREAS WITH LOW ATMOSPHERIC PRESSURE.
EP2105887A1 (en) 2008-03-28 2009-09-30 Siemens Aktiengesellschaft Method for diagnosing a gas turbine
US9441542B2 (en) 2011-09-20 2016-09-13 General Electric Company Ultrasonic water atomization system for gas turbine inlet cooling and wet compression
JP2013092053A (en) * 2011-10-24 2013-05-16 Mitsubishi Heavy Ind Ltd Liquefied gas processing system, control method thereof, liquefied gas carrying vessel including the same, and liquefied gas storage facility including the same
US20180171877A1 (en) * 2016-12-15 2018-06-21 General Electric Company Power Generation System and Method for Operating Same

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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
NL7800077A (en) * 1978-01-03 1979-07-05 Thomassen Holland Bv GASTURBINE INSTALLATION.
GB2051238B (en) * 1979-06-08 1983-09-14 Sadek R M Fluid operated power plant
US4751814A (en) * 1985-06-21 1988-06-21 General Electric Company Air cycle thermodynamic conversion system
AU7196091A (en) * 1990-02-27 1991-08-29 Turbine Developments Aktiengesellschaft A gas turbine
DE4030332A1 (en) * 1990-06-20 1992-01-09 Zimmermann & Jansen Gmbh Process and plant for energy recovery from blast furnace gas - comprises pressure recovery turbine with generator and by=pass with gas compressor, combustion chamber with fuel enrichment

Also Published As

Publication number Publication date
IT1273629B (en) 1997-07-08
KR940011780A (en) 1994-06-22
ITMI932374A1 (en) 1995-05-09
RU2123610C1 (en) 1998-12-20
ES2068781R (en) 1997-04-16
BR9304471A (en) 1994-05-17
IL107530A0 (en) 1994-02-27
ITMI932374A0 (en) 1993-11-09
IL107530A (en) 1999-06-20
ES2068781B1 (en) 1997-12-01
CN1092136A (en) 1994-09-14
ES2068781A2 (en) 1995-04-16

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Legal Events

Date Code Title Description
FG Grant or registration
MM Annulment or lapse due to non-payment of fees