FR2342397A1 - Disque de recouvrement pour rotor radial de turbo-machine, notamment de moteur a reaction a turbine a gaz - Google Patents

Disque de recouvrement pour rotor radial de turbo-machine, notamment de moteur a reaction a turbine a gaz

Info

Publication number
FR2342397A1
FR2342397A1 FR7705754A FR7705754A FR2342397A1 FR 2342397 A1 FR2342397 A1 FR 2342397A1 FR 7705754 A FR7705754 A FR 7705754A FR 7705754 A FR7705754 A FR 7705754A FR 2342397 A1 FR2342397 A1 FR 2342397A1
Authority
FR
France
Prior art keywords
turbo
machine
gas turbine
radial rotor
covering disk
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
FR7705754A
Other languages
English (en)
French (fr)
Other versions
FR2342397B3 (enExample
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.)
MTU Aero Engines AG
Original Assignee
MTU Motoren und Turbinen Union Muenchen GmbH
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 MTU Motoren und Turbinen Union Muenchen GmbH filed Critical MTU Motoren und Turbinen Union Muenchen GmbH
Publication of FR2342397A1 publication Critical patent/FR2342397A1/fr
Application granted granted Critical
Publication of FR2342397B3 publication Critical patent/FR2342397B3/fr
Granted legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D11/00Preventing or minimising internal leakage of working-fluid, e.g. between stages
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/40Casings; Connections of working fluid
    • F04D29/42Casings; Connections of working fluid for radial or helico-centrifugal pumps
    • F04D29/4206Casings; Connections of working fluid for radial or helico-centrifugal pumps especially adapted for elastic fluid pumps

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
FR7705754A 1976-02-26 1977-02-28 Disque de recouvrement pour rotor radial de turbo-machine, notamment de moteur a reaction a turbine a gaz Granted FR2342397A1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE2607776A DE2607776C2 (de) 1976-02-26 1976-02-26 In der Meridianebene geteilte Deckscheibe für Radiallaufräder von Strömungsmaschinen, insbesondere Gasturbinentriebwerken

Publications (2)

Publication Number Publication Date
FR2342397A1 true FR2342397A1 (fr) 1977-09-23
FR2342397B3 FR2342397B3 (enExample) 1980-01-04

Family

ID=5970903

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7705754A Granted FR2342397A1 (fr) 1976-02-26 1977-02-28 Disque de recouvrement pour rotor radial de turbo-machine, notamment de moteur a reaction a turbine a gaz

Country Status (3)

Country Link
US (1) US4153387A (enExample)
DE (1) DE2607776C2 (enExample)
FR (1) FR2342397A1 (enExample)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2216516A1 (de) * 2009-02-04 2010-08-11 ABB Turbo Systems AG Berstschutzvorrichtung für Radialverdichter

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2607776C2 (de) * 1976-02-26 1982-05-27 MTU Motoren- und Turbinen-Union München GmbH, 8000 München In der Meridianebene geteilte Deckscheibe für Radiallaufräder von Strömungsmaschinen, insbesondere Gasturbinentriebwerken
US5685693A (en) * 1995-03-31 1997-11-11 General Electric Co. Removable inner turbine shell with bucket tip clearance control
US5803709A (en) * 1995-12-06 1998-09-08 Canarm Limited Axial flow fan
JP3294491B2 (ja) * 1995-12-20 2002-06-24 株式会社日立製作所 内燃機関の過給機
DE10050931C5 (de) * 2000-10-13 2007-03-29 Man Diesel Se Turbomaschine mit radial durchströmten Laufrad
DE102006060125A1 (de) * 2006-12-20 2008-06-26 Mahle International Gmbh Ladeeinrichtung
DE102008057878A1 (de) * 2008-11-18 2010-05-20 Bosch Mahle Turbo Systems Gmbh & Co. Kg Ladeeinrichtung
US20250237154A1 (en) * 2024-01-23 2025-07-24 Pratt & Whitney Canada Corp. Impeller containment system

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2404609A (en) * 1940-03-02 1946-07-23 Power Jets Res & Dev Ltd Centrifugal compressor
US2312422A (en) * 1941-08-20 1943-03-02 Meckum Engineering Inc Dredge pump
US3043559A (en) * 1954-10-22 1962-07-10 Maschf Augsburg Nuernberg Ag Gas turbine
US3498727A (en) * 1968-01-24 1970-03-03 Westinghouse Electric Corp Blade ring support
US3628884A (en) * 1970-06-26 1971-12-21 Westinghouse Electric Corp Method and apparatus for supporting an inner casing structure
DE2607776C2 (de) * 1976-02-26 1982-05-27 MTU Motoren- und Turbinen-Union München GmbH, 8000 München In der Meridianebene geteilte Deckscheibe für Radiallaufräder von Strömungsmaschinen, insbesondere Gasturbinentriebwerken

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2216516A1 (de) * 2009-02-04 2010-08-11 ABB Turbo Systems AG Berstschutzvorrichtung für Radialverdichter
EP2216517A1 (de) * 2009-02-04 2010-08-11 ABB Turbo Systems AG Berstschutzvorrichtung für Radialverdichter
US8393851B2 (en) 2009-02-04 2013-03-12 Abb Turbo Systems Ag Bursting protection

Also Published As

Publication number Publication date
DE2607776A1 (de) 1977-09-01
US4153387A (en) 1979-05-08
DE2607776C2 (de) 1982-05-27
FR2342397B3 (enExample) 1980-01-04

Similar Documents

Publication Publication Date Title
BE854751A (fr) Assemblage de pales de rotor en ceramique pour moteur a turbine a gaz
FR2333954A1 (fr) Mecanisme moteur de turbines a gaz
CA1031975A (en) Combustion chamber liner for a gas turbine engine
JPS5395414A (en) Rotor stage of gas turbine engine
CA1031974A (en) Combustion chamber liner for a gas turbine engine
BR7708281A (pt) Registrador integrado de historico para motores de turbina a gas
DE3064862D1 (en) Stator vane assembly for a gas turbine engine
IL51008A0 (en) Clearance control for gas turbine engine
JPS51141912A (en) Combustor liner for gas turbine engine and method of manufacture thereof
FR2351250A1 (fr) Dispositif d'etancheite de circulation de fluide pour turbo-machine, notamment pour moteurs a reaction a turbine a gaz
IT8020482A0 (it) Rotore palettato per motore a turbina a gas.
AR213401A1 (es) Compresor centrifugo para un motor de turbina de gas
IL52915A (en) Means for calculating turbine inlet temperature of a gas turbine engine
CA1031580A (en) Catalytic combustor having a variable temperature profile for a gas turbine engine
BE777521A (fr) Rotor pour turbomachine, notamment pour moteur a turbine a gaz
FR2315611A1 (fr) Moteur-turbine a gaz
FR2315612A1 (fr) Moteur a turbine a gaz
JPS5274713A (en) Gas turbine engine combustor
IT1132977B (it) Turbina di un turbocompressore dei gas di scarico per motori endotermici
FR2335701A1 (fr) Rotor en ceramique pour moteur a turbine a gaz
FR2334818A1 (fr) Rotor pour turbomachines, notamment pour moteurs a reaction a turbines a gaz
FR2342397A1 (fr) Disque de recouvrement pour rotor radial de turbo-machine, notamment de moteur a reaction a turbine a gaz
IT1031830B (it) Paletta raffreddata per motori a turbina a gas
FR2314361A1 (fr) Moteur a turbine a gaz
GB2049069B (en) Rotor assembly for a gas turbine engine