FR2290574A1 - Groupe a turbines a gaz - Google Patents

Groupe a turbines a gaz

Info

Publication number
FR2290574A1
FR2290574A1 FR7436733A FR7436733A FR2290574A1 FR 2290574 A1 FR2290574 A1 FR 2290574A1 FR 7436733 A FR7436733 A FR 7436733A FR 7436733 A FR7436733 A FR 7436733A FR 2290574 A1 FR2290574 A1 FR 2290574A1
Authority
FR
France
Prior art keywords
gas turbine
turbine group
group
gas
turbine
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
FR7436733A
Other languages
English (en)
Other versions
FR2290574B1 (fr
Inventor
Sven-Olof Kronogard
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.)
United Turbine AB and Co KG
Original Assignee
United Turbine AB and Co KG
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 United Turbine AB and Co KG filed Critical United Turbine AB and Co KG
Publication of FR2290574A1 publication Critical patent/FR2290574A1/fr
Application granted granted Critical
Publication of FR2290574B1 publication Critical patent/FR2290574B1/fr
Granted 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
    • 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
    • F02C7/12—Cooling of plants
    • F02C7/16—Cooling of plants characterised by cooling medium
    • F02C7/18—Cooling of plants characterised by cooling medium the medium being gaseous, e.g. air
    • 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
    • F02C7/12—Cooling of plants
    • F02C7/16—Cooling of plants characterised by cooling medium
    • F02C7/18—Cooling of plants characterised by cooling medium the medium being gaseous, e.g. air
    • F02C7/185—Cooling means for reducing the temperature of the cooling air or gas
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F25—REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
    • F25B—REFRIGERATION MACHINES, PLANTS OR SYSTEMS; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS
    • F25B9/00—Compression machines, plants or systems, in which the refrigerant is air or other gas of low boiling point
    • F25B9/02—Compression machines, plants or systems, in which the refrigerant is air or other gas of low boiling point using Joule-Thompson effect; using vortex effect
    • F25B9/04—Compression machines, plants or systems, in which the refrigerant is air or other gas of low boiling point using Joule-Thompson effect; using vortex effect using vortex effect
    • 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
    • F05D2260/20—Heat transfer, e.g. cooling
    • F05D2260/209—Heat transfer, e.g. cooling using vortex tubes

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
FR7436733A 1974-10-16 1974-11-05 Groupe a turbines a gaz Granted FR2290574A1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US05/515,174 US3973396A (en) 1974-10-16 1974-10-16 Gas turbine power plant

Publications (2)

Publication Number Publication Date
FR2290574A1 true FR2290574A1 (fr) 1976-06-04
FR2290574B1 FR2290574B1 (fr) 1980-07-04

Family

ID=24050253

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7436733A Granted FR2290574A1 (fr) 1974-10-16 1974-11-05 Groupe a turbines a gaz

Country Status (4)

Country Link
US (1) US3973396A (fr)
DE (1) DE2451500A1 (fr)
FR (1) FR2290574A1 (fr)
GB (1) GB1451260A (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0077265A1 (fr) * 1981-10-14 1983-04-20 Societe Nationale D'etude Et De Construction De Moteurs D'aviation, "S.N.E.C.M.A." Dispositif pour contrôler les dilatations et les contraintes thermiques dans un disque de turbine à gaz

Families Citing this family (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4333754A (en) * 1979-06-27 1982-06-08 Vortec Corporation Anti-icing noise-suppressing vortex tube assembly
US4275857A (en) * 1979-11-05 1981-06-30 The United States Of America As Represented By The Secretary Of The Air Force Cooling system for ramjet engine
US4584838A (en) * 1985-01-10 1986-04-29 Johnson Service Company Apparatus for providing relatively dry, oil free compressed instrument air
DE4210541A1 (de) * 1992-03-31 1993-10-07 Asea Brown Boveri Verfahren zum Betrieb einer Gasturbogruppe
US5406786A (en) * 1993-07-16 1995-04-18 Air Products And Chemicals, Inc. Integrated air separation - gas turbine electrical generation process
US5582012A (en) * 1995-05-15 1996-12-10 Universal Vortex, Inc. Method of natural gas pressure reduction on the city gate stations
US5581996A (en) * 1995-08-16 1996-12-10 General Electric Company Method and apparatus for turbine cooling
US6276123B1 (en) * 2000-09-21 2001-08-21 Siemens Westinghouse Power Corporation Two stage expansion and single stage combustion power plant
EP1245804B1 (fr) * 2001-03-26 2006-05-24 Siemens Aktiengesellschaft Turbine à gaz
US6644012B2 (en) * 2001-11-02 2003-11-11 Alston (Switzerland) Ltd Gas turbine set
WO2005095773A1 (fr) * 2004-03-30 2005-10-13 Alstom Technology Ltd Turbine a gaz a recuperation partielle, et procede pour faire fonctionner un dispositif a turbine a gaz
US9482249B2 (en) * 2013-09-09 2016-11-01 General Electric Company Three-dimensional printing process, swirling device and thermal management process
WO2016081980A1 (fr) * 2014-11-26 2016-06-02 University Of Technology, Sydney Turbine à gaz avec système de refroidissement d'air d'entrée
CN106224035B (zh) * 2016-09-05 2018-01-05 重庆科技学院 基于垃圾气化合成气回收的湿空气透平发电系统
US10670473B2 (en) * 2017-07-25 2020-06-02 Rolls-Royce North American Technologies, Inc. Sensor with integral vortex tube for warming
US11454171B1 (en) 2019-06-27 2022-09-27 United States Of America As Represented By The Secretary Of The Air Force Turbine cooling system with energy separation

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2644315A (en) * 1949-07-04 1953-07-07 Sir George Godfrey & Partners System for the supply of conditioned air in aircraft
US2839901A (en) * 1950-05-26 1958-06-24 Garrett Corp Evaporative vortex tube refrigeration systems
US2786341A (en) * 1950-06-19 1957-03-26 Garrett Corp Direct evaporative vortex tube refrigeration system
US2839898A (en) * 1950-06-29 1958-06-24 Garrett Corp Multiple vortex tube generator cooling unit
US2839900A (en) * 1950-08-31 1958-06-24 Garrett Corp Regenerative vortex cooling systems
US2940257A (en) * 1953-03-27 1960-06-14 Daimler Benz Ag Cooling arrangement for a combustion turbine
US3123283A (en) * 1962-12-07 1964-03-03 Anti-icing valve means
US3361336A (en) * 1964-06-23 1968-01-02 Joseph V. Foa Method of energy separation and apparatus for carrying out the same
FR1548541A (fr) * 1967-10-24 1968-12-06
US3584458A (en) * 1969-11-25 1971-06-15 Gen Motors Corp Turbine cooling

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0077265A1 (fr) * 1981-10-14 1983-04-20 Societe Nationale D'etude Et De Construction De Moteurs D'aviation, "S.N.E.C.M.A." Dispositif pour contrôler les dilatations et les contraintes thermiques dans un disque de turbine à gaz
US4741153A (en) * 1981-10-14 1988-05-03 Societe Nationale D'etude Et De Construction De Moteurs D'aviation, "S.N.E.C.M.A." System for controlling heat expansion and thermal stress in a gas turbine disk

Also Published As

Publication number Publication date
US3973396A (en) 1976-08-10
DE2451500A1 (de) 1976-05-06
FR2290574B1 (fr) 1980-07-04
GB1451260A (en) 1976-09-29

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Legal Events

Date Code Title Description
ST Notification of lapse