Movatterモバイル変換

[0]ホーム
URL:

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

Installation of two-shaft gas turbines

Info

Publication number
FR1246455A
FR1246455AFR814897AFR814897AFR1246455AFR 1246455 AFR1246455 AFR 1246455AFR 814897 AFR814897 AFR 814897AFR 814897 AFR814897 AFR 814897AFR 1246455 AFR1246455 AFR 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 SAfiledCriticalSulzer AG
Application grantedgrantedCritical
Publication of FR1246455ApublicationCriticalpatent/FR1246455A/en
Expiredlegal-statusCriticalCurrent

Links

Classifications

Landscapes

FR814897A1959-01-101960-01-05 Installation of two-shaft gas turbinesExpiredFR1246455A (en)

Applications Claiming Priority (1)

Application NumberPriority DateFiling DateTitle
CH6816959ACH363853A (en)1959-01-101959-01-10 Gas turbine plant with two shafts

Publications (1)

Publication NumberPublication Date
FR1246455Atrue FR1246455A (en)1960-11-18

Family

ID=4528519

Family Applications (1)

Application NumberTitlePriority DateFiling Date
FR814897AExpiredFR1246455A (en)1959-01-101960-01-05 Installation of two-shaft gas turbines

Country Status (3)

CountryLink
BE (1)BE586353A (en)
CH (1)CH363853A (en)
FR (1)FR1246455A (en)

Cited By (9)

* Cited by examiner, † Cited by third party
Publication numberPriority datePublication dateAssigneeTitle
FR2384951A1 (en)*1977-03-251978-10-20Stal Laval Turbin Ab GAS TURBINE PLANT
EP0452642A1 (en)*1990-03-051991-10-23Rolf Jan MowillHigh efficiency, twin spool, radial-high pressure, gas turbine engine
US5081832A (en)*1990-03-051992-01-21Rolf Jan MowillHigh efficiency, twin spool, radial-high pressure, gas turbine engine
US5377483A (en)*1993-07-071995-01-03Mowill; R. JanProcess for single stage premixed constant fuel/air ratio combustion
US5572862A (en)*1993-07-071996-11-12Mowill Rolf JanConvectively cooled, single stage, fully premixed fuel/air combustor for gas turbine engine modules
US5613357A (en)*1993-07-071997-03-25Mowill; R. JanStar-shaped single stage low emission combustor system
US5628182A (en)*1993-07-071997-05-13Mowill; R. JanStar combustor with dilution ports in can portions
US5638674A (en)*1993-07-071997-06-17Mowill; R. JanConvectively cooled, single stage, fully premixed controllable fuel/air combustor with tangential admission
US6220034B1 (en)1993-07-072001-04-24R. Jan MowillConvectively cooled, single stage, fully premixed controllable fuel/air combustor

Cited By (12)

* Cited by examiner, † Cited by third party
Publication numberPriority datePublication dateAssigneeTitle
FR2384951A1 (en)*1977-03-251978-10-20Stal Laval Turbin Ab GAS TURBINE PLANT
EP0452642A1 (en)*1990-03-051991-10-23Rolf Jan MowillHigh efficiency, twin spool, radial-high pressure, gas turbine engine
US5081832A (en)*1990-03-051992-01-21Rolf Jan MowillHigh efficiency, twin spool, radial-high pressure, gas turbine engine
US5377483A (en)*1993-07-071995-01-03Mowill; R. JanProcess for single stage premixed constant fuel/air ratio combustion
US5477671A (en)*1993-07-071995-12-26Mowill; R. JanSingle stage premixed constant fuel/air ratio combustor
US5481866A (en)*1993-07-071996-01-09Mowill; R. JanSingle stage premixed constant fuel/air ratio combustor
US5572862A (en)*1993-07-071996-11-12Mowill Rolf JanConvectively cooled, single stage, fully premixed fuel/air combustor for gas turbine engine modules
US5613357A (en)*1993-07-071997-03-25Mowill; R. JanStar-shaped single stage low emission combustor system
US5628182A (en)*1993-07-071997-05-13Mowill; R. JanStar combustor with dilution ports in can portions
US5638674A (en)*1993-07-071997-06-17Mowill; R. JanConvectively cooled, single stage, fully premixed controllable fuel/air combustor with tangential admission
US5765363A (en)*1993-07-071998-06-16Mowill; R. JanConvectively cooled, single stage, fully premixed controllable fuel/air combustor with tangential admission
US6220034B1 (en)1993-07-072001-04-24R. Jan MowillConvectively cooled, single stage, fully premixed controllable fuel/air combustor

Also Published As

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

Similar Documents

PublicationPublication DateTitle
FR1262452A (en) Gas turbine thruster unit
FR1205480A (en) Gas turbine power unit
BE589863A (en) Improvements to gas turbo-engines
FR1246455A (en) Installation of two-shaft gas turbines
CH367662A (en) Gas turbine group
FR1247159A (en) Gas burner
FR1165074A (en) Gas turbine
BE589882A (en) Gas compressor
FR1276261A (en) Gas turbine
FR1242634A (en) Gas turbojet
FR1254871A (en) Gas connection plug-valve
FR1308962A (en) Installation of combustion gas turbines
FR1226960A (en) Gas turbine
CH386773A (en) Power plant comprising a gas turbine
FR1205792A (en) Gas turbine installation
FR1245571A (en) Gas turbine installation
FR1233698A (en) Gas burner
FR1246033A (en) Gas turbine generator set
FR1228090A (en) Gas turbine compressor
FR1138344A (en) Two-shaft gas turbine installation
FR1254186A (en) Gas turbine
FR1220926A (en) Gas bearing
FR1249469A (en) Advanced gas burner
BE590200A (en) Gas connection plug-valve
FR1200284A (en) Improvements to gas turbine installations
[8]ページ先頭
©2009-2025 Movatter.jp