FR2351249A1 - Perfectionnement a un dispositif d'admission du fluide moteur dans une turbine de grande puissance - Google Patents

Perfectionnement a un dispositif d'admission du fluide moteur dans une turbine de grande puissance

Info

Publication number
FR2351249A1
FR2351249A1 FR7614597A FR7614597A FR2351249A1 FR 2351249 A1 FR2351249 A1 FR 2351249A1 FR 7614597 A FR7614597 A FR 7614597A FR 7614597 A FR7614597 A FR 7614597A FR 2351249 A1 FR2351249 A1 FR 2351249A1
Authority
FR
France
Prior art keywords
steam turbine
inlet guide
guide blades
steam
nozzles
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
FR7614597A
Other languages
English (en)
Other versions
FR2351249B1 (fr
Inventor
Gilbert Riollet
Jean-Pierre Gros
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.)
EUROP TURB VAPEUR
Original Assignee
EUROP TURB VAPEUR
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 EUROP TURB VAPEUR filed Critical EUROP TURB VAPEUR
Priority to FR7614597A priority Critical patent/FR2351249A1/fr
Publication of FR2351249A1 publication Critical patent/FR2351249A1/fr
Application granted granted Critical
Publication of FR2351249B1 publication Critical patent/FR2351249B1/fr
Granted legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D9/00—Stators
    • F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
    • F01D9/04—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
    • F01D9/047—Nozzle boxes

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Control Of Turbines (AREA)
FR7614597A 1976-05-14 1976-05-14 Perfectionnement a un dispositif d'admission du fluide moteur dans une turbine de grande puissance Granted FR2351249A1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR7614597A FR2351249A1 (fr) 1976-05-14 1976-05-14 Perfectionnement a un dispositif d'admission du fluide moteur dans une turbine de grande puissance

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR7614597A FR2351249A1 (fr) 1976-05-14 1976-05-14 Perfectionnement a un dispositif d'admission du fluide moteur dans une turbine de grande puissance

Publications (2)

Publication Number Publication Date
FR2351249A1 true FR2351249A1 (fr) 1977-12-09
FR2351249B1 FR2351249B1 (fr) 1978-08-25

Family

ID=9173161

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7614597A Granted FR2351249A1 (fr) 1976-05-14 1976-05-14 Perfectionnement a un dispositif d'admission du fluide moteur dans une turbine de grande puissance

Country Status (1)

Country Link
FR (1) FR2351249A1 (fr)

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3242713A1 (de) * 1981-11-30 1983-06-01 BBC Aktiengesellschaft Brown, Boveri & Cie., 5401 Baden, Aargau Einlassgehaeuse fuer dampfturbine
EP0191380A1 (fr) * 1985-02-20 1986-08-20 BBC Brown Boveri AG Turbine pour une turbosoufflante
EP0491134A1 (fr) * 1990-12-18 1992-06-24 Asea Brown Boveri Ag Enveloppe d'admission pour turbine à gaz
EP0575659A1 (fr) * 1992-06-26 1993-12-29 Asea Brown Boveri Ag Enveloppe d'admission pour turbine à gaz
ITMI20091740A1 (it) * 2009-10-12 2011-04-13 Alstom Technology Ltd Turbina a vapore assiale alimentata radialmente ad alta temperatura
DE102011089242A1 (de) * 2011-12-20 2013-06-20 Siemens Aktiengesellschaft Verbrennungssystem mit zwei Ringbrennkammern
EP2693018A4 (fr) * 2011-03-31 2015-03-18 Mitsubishi Heavy Ind Ltd Turbocompresseur

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3242713A1 (de) * 1981-11-30 1983-06-01 BBC Aktiengesellschaft Brown, Boveri & Cie., 5401 Baden, Aargau Einlassgehaeuse fuer dampfturbine
EP0191380A1 (fr) * 1985-02-20 1986-08-20 BBC Brown Boveri AG Turbine pour une turbosoufflante
EP0491134A1 (fr) * 1990-12-18 1992-06-24 Asea Brown Boveri Ag Enveloppe d'admission pour turbine à gaz
US5215436A (en) * 1990-12-18 1993-06-01 Asea Brown Boveri Ltd. Inlet casing for steam turbine
EP0575659A1 (fr) * 1992-06-26 1993-12-29 Asea Brown Boveri Ag Enveloppe d'admission pour turbine à gaz
ITMI20091740A1 (it) * 2009-10-12 2011-04-13 Alstom Technology Ltd Turbina a vapore assiale alimentata radialmente ad alta temperatura
US8702376B2 (en) 2009-10-12 2014-04-22 Alstom Technology Ltd. High temperature radially fed axial steam turbine
EP2693018A4 (fr) * 2011-03-31 2015-03-18 Mitsubishi Heavy Ind Ltd Turbocompresseur
DE102011089242A1 (de) * 2011-12-20 2013-06-20 Siemens Aktiengesellschaft Verbrennungssystem mit zwei Ringbrennkammern

Also Published As

Publication number Publication date
FR2351249B1 (fr) 1978-08-25

Similar Documents

Publication Publication Date Title
ES8205932A1 (es) Una turbina de flujo radial hacia dentro
ES483420A1 (es) Perfeccionamientos en los aparatos de distribucion de gases en zonas de atomizacion
GB1317992A (en) Gas turbine power plant
GB1457634A (en) Converging-diverging supersonic nozzles
GB1149513A (en) Bearing assembly
FR2351249A1 (fr) Perfectionnement a un dispositif d'admission du fluide moteur dans une turbine de grande puissance
GB847084A (en) Combustion chamber for a gas turbine or rocket motor
FR2274788A1 (fr) Perfectionnement aux installations motrices a turbine a gaz comprenant deux grilles d'aubes superposees
GB622384A (en) Improvements relating to gas turbine engines
GB847242A (en) Improvements in or relating to radial flow gas turbines
GB1524956A (en) Gas tubine engine
GB1435083A (en) Gas turbine engine combustion equipment
GB733646A (en) Improvements in or relating to diffusers
GB891278A (en) A gas turbine power unit
GB834800A (en) Turbine-driven fans
GB1138941A (en) Improvements in and relating to radial flow turbines
GB1193587A (en) Nozzle Guide Vanes for Gas Turbine Engines.
GB1070480A (en) Aerofoil shaped blade for a fluid flow machine such as a gas turbine engine
FR2233511A1 (en) Ejector type jet pump - has hyperboloid walls with spiral inlet and centre jets
GB1524259A (en) Turbines
FR2375440A1 (fr) Rotor de turbine axiale
GB989581A (en) High power steam turbine
JPS5793607A (en) Guide for fluid inlet port
GB881816A (en) Improved gas turbine engine
JPS5465203A (en) Nozzle cut-out governor for steam turbine

Legal Events

Date Code Title Description
ST Notification of lapse