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FR1246455A - Installation of two-shaft gas turbines - Google Patents

Installation of two-shaft gas turbines

Info

Publication number
FR1246455A
FR1246455A FR814897A FR814897A FR1246455A FR 1246455 A FR1246455 A FR 1246455A FR 814897 A FR814897 A FR 814897A FR 814897 A FR814897 A FR 814897A FR 1246455 A FR1246455 A FR 1246455A
Authority
FR
France
Prior art keywords
installation
gas turbines
shaft gas
shaft
turbines
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.)
Expired
Application number
FR814897A
Other languages
French (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.)
Sulzer AG
Original Assignee
Sulzer AG
Sulzer Freres 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 Sulzer AG, Sulzer Freres SA filed Critical Sulzer AG
Application granted granted Critical
Publication of FR1246455A publication Critical patent/FR1246455A/en
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
    • F02C3/36—Open cycles

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
FR814897A 1959-01-10 1960-01-05 Installation of two-shaft gas turbines Expired FR1246455A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CH6816959A CH363853A (en) 1959-01-10 1959-01-10 Gas turbine plant with two shafts

Publications (1)

Publication Number Publication Date
FR1246455A true FR1246455A (en) 1960-11-18

Family

ID=4528519

Family Applications (1)

Application Number Title Priority Date Filing Date
FR814897A Expired FR1246455A (en) 1959-01-10 1960-01-05 Installation of two-shaft gas turbines

Country Status (3)

Country Link
BE (1) BE586353A (en)
CH (1) CH363853A (en)
FR (1) FR1246455A (en)

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2384951A1 (en) * 1977-03-25 1978-10-20 Stal Laval Turbin Ab GAS TURBINE PLANT
EP0452642A1 (en) * 1990-03-05 1991-10-23 Rolf Jan Mowill High efficiency, twin spool, radial-high pressure, gas turbine engine
US5081832A (en) * 1990-03-05 1992-01-21 Rolf Jan Mowill High efficiency, twin spool, radial-high pressure, gas turbine engine
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
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
US6220034B1 (en) 1993-07-07 2001-04-24 R. Jan Mowill Convectively cooled, single stage, fully premixed controllable fuel/air combustor

Cited By (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2384951A1 (en) * 1977-03-25 1978-10-20 Stal Laval Turbin Ab GAS TURBINE PLANT
EP0452642A1 (en) * 1990-03-05 1991-10-23 Rolf Jan Mowill High efficiency, twin spool, radial-high pressure, gas turbine engine
US5081832A (en) * 1990-03-05 1992-01-21 Rolf Jan Mowill High efficiency, twin spool, radial-high pressure, gas turbine engine
US5377483A (en) * 1993-07-07 1995-01-03 Mowill; R. Jan Process for single stage premixed constant fuel/air ratio combustion
US5477671A (en) * 1993-07-07 1995-12-26 Mowill; R. Jan Single stage premixed constant fuel/air ratio combustor
US5481866A (en) * 1993-07-07 1996-01-09 Mowill; R. Jan Single stage premixed constant fuel/air ratio combustor
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
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
US5765363A (en) * 1993-07-07 1998-06-16 Mowill; R. Jan Convectively cooled, single stage, fully premixed controllable fuel/air combustor with tangential admission
US6220034B1 (en) 1993-07-07 2001-04-24 R. Jan Mowill Convectively cooled, single stage, fully premixed controllable fuel/air combustor

Also Published As

Publication number Publication date
CH363853A (en) 1962-08-15
BE586353A (en) 1960-07-08

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