FR2630498B1 - Systeme pour regler la position des aubes orientables des tuyeres d'une turbine a gaz - Google Patents

Systeme pour regler la position des aubes orientables des tuyeres d'une turbine a gaz

Info

Publication number
FR2630498B1
FR2630498B1 FR8905308A FR8905308A FR2630498B1 FR 2630498 B1 FR2630498 B1 FR 2630498B1 FR 8905308 A FR8905308 A FR 8905308A FR 8905308 A FR8905308 A FR 8905308A FR 2630498 B1 FR2630498 B1 FR 2630498B1
Authority
FR
France
Prior art keywords
nozzles
adjusting
gas turbine
adjustable vanes
vanes
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 - Lifetime
Application number
FR8905308A
Other languages
English (en)
Other versions
FR2630498A1 (fr
Inventor
Mezzedimi Vasco
Frosini Franco
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.)
Nuovo Pignone Holding SpA
Original Assignee
Nuovopignone Industrie Meccaniche e Fonderia SpA
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 Nuovopignone Industrie Meccaniche e Fonderia SpA filed Critical Nuovopignone Industrie Meccaniche e Fonderia SpA
Publication of FR2630498A1 publication Critical patent/FR2630498A1/fr
Application granted granted Critical
Publication of FR2630498B1 publication Critical patent/FR2630498B1/fr
Anticipated expiration legal-status Critical
Expired - Lifetime 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
    • F01D17/00—Regulating or controlling by varying flow
    • F01D17/10—Final actuators
    • F01D17/12—Final actuators arranged in stator parts
    • F01D17/14—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits
    • F01D17/16—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of nozzle vanes
    • F01D17/162—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of nozzle vanes for axial flow, i.e. the vanes turning around axes which are essentially perpendicular to the rotor centre line

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Control Of Turbines (AREA)
  • Support Of The Bearing (AREA)
FR8905308A 1988-04-21 1989-04-21 Systeme pour regler la position des aubes orientables des tuyeres d'une turbine a gaz Expired - Lifetime FR2630498B1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
IT20272/88A IT1217437B (it) 1988-04-21 1988-04-21 Sistema perfezionato di registrazione in posizione degli ugelli orientabili di una turbina a gas

Publications (2)

Publication Number Publication Date
FR2630498A1 FR2630498A1 (fr) 1989-10-27
FR2630498B1 true FR2630498B1 (fr) 1993-12-24

Family

ID=11165325

Family Applications (1)

Application Number Title Priority Date Filing Date
FR8905308A Expired - Lifetime FR2630498B1 (fr) 1988-04-21 1989-04-21 Systeme pour regler la position des aubes orientables des tuyeres d'une turbine a gaz

Country Status (7)

Country Link
JP (1) JP2864127B2 (fr)
CA (1) CA1333695C (fr)
CH (1) CH675748A5 (fr)
DE (1) DE3913195A1 (fr)
FR (1) FR2630498B1 (fr)
GB (1) GB2217790B (fr)
IT (1) IT1217437B (fr)

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP3771765B2 (ja) * 2000-01-24 2006-04-26 三菱重工業株式会社 可変ターボチャージャ
DE10035762A1 (de) * 2000-07-22 2002-01-31 Daimler Chrysler Ag Abgasturbolader für eine Brennkraftmaschine und Verfahren zum Betrieb eines Abgasturboladers
DE10238413A1 (de) * 2002-08-22 2004-03-04 Volkswagen Ag Turbolader mit variabler Turbinengeometrie
FR2879695B1 (fr) * 2004-12-16 2007-04-06 Snecma Moteurs Sa Dispositif de liaison, de longueur ajustable, entre deux pieces
US7594794B2 (en) * 2006-08-24 2009-09-29 United Technologies Corporation Leaned high pressure compressor inlet guide vane
GB2470586A (en) * 2009-05-29 2010-12-01 Rolls Royce Plc Eccentric joint for actuator connection rod.
US8714916B2 (en) * 2010-09-28 2014-05-06 General Electric Company Variable vane assembly for a turbine compressor
US8668444B2 (en) * 2010-09-28 2014-03-11 General Electric Company Attachment stud for a variable vane assembly of a turbine compressor
EP2594743A1 (fr) * 2011-11-21 2013-05-22 Siemens Aktiengesellschaft Broches d'ajustement de diaphragme excentrique pour un moteur à turbine à gaz
DE102012206755B4 (de) * 2012-04-25 2022-11-24 Zf Friedrichshafen Ag Steuerstangenanordnung
DE102015213321A1 (de) * 2015-07-16 2017-01-19 Bosch Mahle Turbo Systems Gmbh & Co. Kg Variable Turbinen- oder Verdichtergeometrie für einen Abgasturbolader
US11486304B2 (en) * 2017-11-03 2022-11-01 Borgwarner Inc. Lever with pre-attached self locking nut for a variable turbine geometry turbocharger

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1060663A (fr) * 1952-07-29 1954-04-05 Ventilateur hélicoïde à haute pression
US2933235A (en) * 1955-01-11 1960-04-19 Gen Electric Variable stator compressor
GB1276720A (en) * 1969-12-19 1972-06-07 English Electric Co Ltd Drives to adjustable stator blades for turbomachinery
US3949550A (en) * 1975-03-05 1976-04-13 United Technologies Corporation Engine exhaust flow diverter
US4139329A (en) * 1977-05-16 1979-02-13 Westinghouse Canada Limited Vane tip motion transfer device
JPS55134704A (en) * 1979-04-07 1980-10-20 Mitsui Eng & Shipbuild Co Ltd Structure for fine adjustment of setting angle of stator blade for furnace-top pressure turbine
JPS6052840A (ja) * 1983-09-01 1985-03-26 Fuji Xerox Co Ltd 複写機用原稿照明装置
JPS6137441A (ja) * 1984-07-31 1986-02-22 Toshiba Corp ドツトプリンタの高速印字処理方式

Also Published As

Publication number Publication date
DE3913195C2 (fr) 1991-05-23
GB2217790A (en) 1989-11-01
JPH01305134A (ja) 1989-12-08
DE3913195A1 (de) 1989-11-02
GB2217790B (en) 1992-07-01
CA1333695C (fr) 1994-12-27
IT8820272A0 (it) 1988-04-21
JP2864127B2 (ja) 1999-03-03
IT1217437B (it) 1990-03-22
FR2630498A1 (fr) 1989-10-27
GB8908878D0 (en) 1989-06-07
CH675748A5 (fr) 1990-10-31

Similar Documents

Publication Publication Date Title
FR2619868B1 (fr) Systeme d'aubes de compresseurs pour turbine a gaz
FR2585407B1 (fr) Dispositif pour commander la circulation de l'air de refroidissement d'une turbine a gaz
FR2483523B1 (fr) Tuyere d'ejection pour moteur a turbine a gaz
GB9302020D0 (en) Guide vanes for gas turbine engines
FR2631656B1 (fr) Dispositif d'etancheite pour interieur de turbine a gaz
ITMI922517A0 (it) Struttura d'anello perfezionata per turbina a gas
FR2638206B1 (fr) Dispositif d'amenee d'air de refroidissement pour les aubes de rotor de turbines a gaz
FR2630498B1 (fr) Systeme pour regler la position des aubes orientables des tuyeres d'une turbine a gaz
IT9021363A0 (it) Apparato di controllo di gioco di sommita' di pale per turbomotore a gas
GB9027986D0 (en) Gas turbine engine clearance control
FR2672636B1 (fr) Machine tournante du type compresseur ou turbine pour la compression ou la detente d'un gaz dangereux.
FR2636678B1 (fr) Generateur d'allumage haute energie notamment pour turbine a gaz
GB9225762D0 (en) Societe a structural arm for the casing of a turbomachine
GB8811657D0 (en) Nozzle guide vane for gas turbine engine
FR2463859B1 (fr) Tuyere d'ejection a flux de gaz ejectes orientable
FR2632015B1 (fr) Syste me d'injecteurs pour moteur a turbine a gaz
YU32188A (en) Device for fastening blades for preventing relative move of blades at steam turbines
FR2569232B1 (fr) Tuyere d'echappement orientable pour turbomachine a gaz
FR2630162B1 (fr) Systeme d'antigivrage de cone d'entree pour turbomoteurs a gaz
FR2604215B1 (fr) Tuyere de propulsion pour turbomoteur a gaz.
FR2629891B1 (fr) Raccord d'assemblage de canalisations notamment pour gaz
BE892325A (fr) Structure d'aube refroidie par air pour turbine a gaz
FR2637031B1 (fr) Accouplement d'arbres pour moteur a turbine a gaz
FR2524937B1 (fr) Tuyere d'ejection a geometrie variable pour turbomachines
GB9115670D0 (en) Gas turbine combustion system