FR2592683A1 - Installation de turbine a gaz a cycle ameliore. - Google Patents

Installation de turbine a gaz a cycle ameliore.

Info

Publication number
FR2592683A1
FR2592683A1 FR8600222A FR8600222A FR2592683A1 FR 2592683 A1 FR2592683 A1 FR 2592683A1 FR 8600222 A FR8600222 A FR 8600222A FR 8600222 A FR8600222 A FR 8600222A FR 2592683 A1 FR2592683 A1 FR 2592683A1
Authority
FR
France
Prior art keywords
turbine
inlet
gas
gas turbine
outlet
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
FR8600222A
Other languages
English (en)
Other versions
FR2592683B1 (fr
Inventor
Jean Poulain
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.)
Alstom SA
Original Assignee
Alstom SA
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 Alstom SA filed Critical Alstom SA
Priority to FR8600222A priority Critical patent/FR2592683B1/fr
Publication of FR2592683A1 publication Critical patent/FR2592683A1/fr
Application granted granted Critical
Publication of FR2592683B1 publication Critical patent/FR2592683B1/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
    • F02C6/00—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use
    • F02C6/006—Open cycle gas-turbine in which the working fluid is expanded to a pressure below the atmospheric pressure and then compressed to atmospheric pressure
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00—Function
    • F05D2260/60—Fluid transfer
    • F05D2260/601—Fluid transfer using an ejector or a jet pump

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)

Abstract

Installation de turbine à gaz à cycle amélioré comprenant un compresseur 1, une turbine à gaz 6 et une chambre de combustion 5 recevant en entrée de l'air comprimé sortant du compresseur et alimentant en sortie l'entrée de ladite turbine, ladite chambre de combustion étant alimentée en combustible 7, la turbine et le compresseur étant liés mécaniquement en rotation et la turbine entraînant une machine utilisatrice 9, l'échappement 11 de la turbine étant relié à une entrée gaz 12 d'un évaporateur surchauffeur 13 alimenté en fluide liquide par une entrée liquide 15, ledit évaporateur surchauffeur comportant en outre une sortie gaz 14 et une sortie vapeur 16, caractérisé en ce que la sortie gaz 14 de l'évaporateur surchauffeur est reliée à une entrée d'un dispositif 17 provoquant la dépression, par rapport à la pression atmosphérique, de l'échappement 11 de ladite turbine à gaz, ledit dispositif comprenant un moyen moteur alimenté par ladite sortie vapeur 16 dudit évaporateur surchauffeur. (CF DESSIN DANS BOPI)
FR8600222A 1986-01-09 1986-01-09 Installation de turbine a gaz a cycle ameliore. Expired FR2592683B1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR8600222A FR2592683B1 (fr) 1986-01-09 1986-01-09 Installation de turbine a gaz a cycle ameliore.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR8600222A FR2592683B1 (fr) 1986-01-09 1986-01-09 Installation de turbine a gaz a cycle ameliore.

Publications (2)

Publication Number Publication Date
FR2592683A1 true FR2592683A1 (fr) 1987-07-10
FR2592683B1 FR2592683B1 (fr) 1989-10-06

Family

ID=9330936

Family Applications (1)

Application Number Title Priority Date Filing Date
FR8600222A Expired FR2592683B1 (fr) 1986-01-09 1986-01-09 Installation de turbine a gaz a cycle ameliore.

Country Status (1)

Country Link
FR (1) FR2592683B1 (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1830052A1 (fr) * 2006-03-03 2007-09-05 Hubert Antoine Cycle combiné à air

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR912055A (fr) * 1944-03-18 1946-07-30 Sulzer Ag Installation de turbines à gaz pour la propulsion de véhicules
DE1149573B (de) * 1959-06-01 1963-05-30 Havilland Engine Company De Waermekraftanlage mit einer aus Verdichter, Brennkammer und Gasturbine bestehenden Gasturbinenanlage
FR2321091A1 (fr) * 1975-08-13 1977-03-11 Inst Gornospasatelnogo Dela Generateur de gaz inertes
US4308718A (en) * 1978-01-02 1982-01-05 Jan Mowill Bleedoff of gas from diffusers in fluid flow machines
US4414805A (en) * 1981-11-27 1983-11-15 General Motors Corporation Hybrid gas turbine engine and flywheel propulsion system

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR912055A (fr) * 1944-03-18 1946-07-30 Sulzer Ag Installation de turbines à gaz pour la propulsion de véhicules
DE1149573B (de) * 1959-06-01 1963-05-30 Havilland Engine Company De Waermekraftanlage mit einer aus Verdichter, Brennkammer und Gasturbine bestehenden Gasturbinenanlage
FR2321091A1 (fr) * 1975-08-13 1977-03-11 Inst Gornospasatelnogo Dela Generateur de gaz inertes
US4308718A (en) * 1978-01-02 1982-01-05 Jan Mowill Bleedoff of gas from diffusers in fluid flow machines
US4414805A (en) * 1981-11-27 1983-11-15 General Motors Corporation Hybrid gas turbine engine and flywheel propulsion system

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
NAVAL ENGINEERS JOURNAL, vol. 86, no. 6, décembre 1974, pages 81-90, Washington, US; N. GASPAROVIC: "Gas turbine cycle operating partly at sub-atmospheric pressure" *

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1830052A1 (fr) * 2006-03-03 2007-09-05 Hubert Antoine Cycle combiné à air

Also Published As

Publication number Publication date
FR2592683B1 (fr) 1989-10-06

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