DE3000614A1 - Turbomaschine - Google Patents

Turbomaschine

Info

Publication number
DE3000614A1
DE3000614A1 DE19803000614 DE3000614A DE3000614A1 DE 3000614 A1 DE3000614 A1 DE 3000614A1 DE 19803000614 DE19803000614 DE 19803000614 DE 3000614 A DE3000614 A DE 3000614A DE 3000614 A1 DE3000614 A1 DE 3000614A1
Authority
DE
Germany
Prior art keywords
compressor
turbine
connecting surface
turbo machine
turbomachine
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.)
Withdrawn
Application number
DE19803000614
Other languages
German (de)
English (en)
Inventor
Jean Michel Simon
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Publication of DE3000614A1 publication Critical patent/DE3000614A1/de
Withdrawn legal-status Critical Current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
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/02—Blade-carrying members, e.g. rotors
    • F01D5/03—Annular blade-carrying members having blades on the inner periphery of the annulus and extending inwardly radially, i.e. inverted rotors
    • 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
    • F01D21/00—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for
    • F01D21/04—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for responsive to undesired position of rotor relative to stator or to breaking-off of a part of the rotor, e.g. indicating such position
    • F01D21/045—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for responsive to undesired position of rotor relative to stator or to breaking-off of a part of the rotor, e.g. indicating such position special arrangements in stators or in rotors dealing with breaking-off of part of rotor
    • 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
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12—Blades
    • F01D5/28—Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
    • F01D5/282—Selecting composite materials, e.g. blades with reinforcing filaments
    • 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
    • F02C3/04—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor
    • F02C3/045—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor having compressor and turbine passages in a single rotor-module
    • 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
    • F02C3/14—Gas-turbine plants characterised by the use of combustion products as the working fluid characterised by the arrangement of the combustion chamber in the plant
    • 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
    • F02C3/14—Gas-turbine plants characterised by the use of combustion products as the working fluid characterised by the arrangement of the combustion chamber in the plant
    • F02C3/16—Gas-turbine plants characterised by the use of combustion products as the working fluid characterised by the arrangement of the combustion chamber in the plant the combustion chambers being formed at least partly in the turbine rotor or in an other rotating part of the plant
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Materials Engineering (AREA)
  • Composite Materials (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Connection Of Motors, Electrical Generators, Mechanical Devices, And The Like (AREA)
DE19803000614 1979-01-15 1980-01-09 Turbomaschine Withdrawn DE3000614A1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR7900836A FR2446384A1 (fr) 1979-01-15 1979-01-15 Turbomachine

Publications (1)

Publication Number Publication Date
DE3000614A1 true DE3000614A1 (de) 1980-07-17

Family

ID=9220728

Family Applications (1)

Application Number Title Priority Date Filing Date
DE19803000614 Withdrawn DE3000614A1 (de) 1979-01-15 1980-01-09 Turbomaschine

Country Status (4)

Country Link
JP (1) JPS55117035A (US20030220297A1-20031127-C00009.png)
DE (1) DE3000614A1 (US20030220297A1-20031127-C00009.png)
FR (1) FR2446384A1 (US20030220297A1-20031127-C00009.png)
GB (1) GB2040359B (US20030220297A1-20031127-C00009.png)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0383862A1 (de) * 1988-08-01 1990-08-29 TOBLER, Max Rotierender brennraum mit wasserinjektion- und kühlung für eine turbine
DE4232383A1 (de) * 1992-09-26 1994-03-31 Asea Brown Boveri Gasturbogruppe
GB2349671A (en) * 1999-04-26 2000-11-08 Andrew David James Sampson Gas turbine having rotating mixing chambers and helical flow
FR2842246A1 (fr) * 2002-07-15 2004-01-16 Remy Eric Patrick Mercier Moteur thermique a effet centrifuge
NL1030744C2 (nl) * 2005-12-22 2007-06-25 Micro Turbine Technology B V Reactieturbine.
CN113279857B (zh) * 2021-05-27 2022-03-15 中国科学院工程热物理研究所 一种适用于无人飞行器的高推重比燃气涡轮发生器

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2704645A (en) * 1955-03-22 colvin
GB598774A (en) * 1945-09-10 1948-02-26 Wolfgang Bial Improvements in or relating to internal combustion jet and power units
FR383966A (fr) * 1907-09-26 1908-03-25 Armand Ferrier Turbine à combustion interne
FR980201A (fr) * 1949-02-07 1951-05-09 Moteur à combustion
DE821736C (de) * 1950-02-04 1951-11-19 Hardy Radermacher Strahltriebwerk
US2748563A (en) * 1953-08-21 1956-06-05 Wiktor Dominik Single burner turbojet engine
US3015524A (en) * 1958-11-19 1962-01-02 Owens Corning Fiberglass Corp Inverted turbine
FR1466403A (fr) * 1965-11-24 1967-01-20 Dispositif et procédé pour augmenter le rendement du réacteur
FR1594147A (US20030220297A1-20031127-C00009.png) * 1968-12-05 1970-06-01
DE2116654A1 (de) * 1971-04-06 1972-11-02 Kuske, Albrecht, Prof. Dr.-Ing., 3392 Clausthal-Zellerfeld Gasturbine
DE2122782A1 (de) * 1971-05-08 1972-11-16 Unbehaun, Dieter, 8500 Nürnberg Gasturbine mit rotierender Brennkammer
DE2419972A1 (de) * 1974-04-25 1975-11-06 Lothar Strach Gasturbinen - beschaufelung

Also Published As

Publication number Publication date
JPS55117035A (en) 1980-09-09
FR2446384A1 (fr) 1980-08-08
GB2040359A (en) 1980-08-28
FR2446384B1 (US20030220297A1-20031127-C00009.png) 1982-06-25
GB2040359B (en) 1982-12-08

Similar Documents

Publication Publication Date Title
DE3305170C2 (de) Turbomaschinengehäuse
EP0592803B1 (de) Getriebe-Mehrwellenturbokompressor
DE3814971C2 (de) Gasturbinentriebwerk
DE1551183A1 (de) Zusammengesetzter Dichtungsbauteil fuer ein Turbinentriebwerk
DE2622234A1 (de) Brennkammerverkleidung
DE2242219A1 (de) Geraeuscharmer antriebsventilator
DE4015732C2 (de) Verfahren zum Umwandeln eines Flugzeug-Turbofan-Triebwerks in ein Triebwerk für einen nicht-flugtechnischen Zweck und Vorrichtung zur Durchführung des Verfahrens
DE3942203A1 (de) Turbinenanordnung mit heckseitig angebrachten ausstroemleitschaufeln
DE2616031A1 (de) Turbinenummantelungsgebilde
DE2728190C3 (de) Gasturbine
CH704935B1 (de) Stator-Rotor-Anordnung, Strömungsmaschine und Verfahren zum Herstellen einer Struktur aus umgekehrten Turbulatoren
DE2925941A1 (de) Diffusor fuer ein fluidantriebsgeraet
DE4110244A1 (de) Zwischenstufendichtungsanordnung fuer schaufelstufen von gegenlaeufigen turbinentriebwerksrotoren
DE69001284T2 (de) Gegenlaeufiges blaesertriebwerk.
WO1998013584A1 (de) Kompensation des druckverlustes einer kühlluftführung in einer gasturbinenanlage
DE3000614A1 (de) Turbomaschine
DE833879C (de) Abgas-Turbolader fuer Brennkraftmaschinen
DE1133184B (de) Gasturbinentriebwerk mit koaxial angeordneten und gegenlaeufig rotierenden Laeufern eines Zentripetal-verdichters und einer Zentrifugalturbine und mit einer Brennkammer
DE4117362A1 (de) Gasturbinentriebwerksstator und verfahren zum steuern des radialen spiels zwischen stator und rotor
DE3728436A1 (de) Gegenlaeufiges turbofantriebwerk mit hohem bypass-verhaeltnis
DE3235585C2 (de) Hochleistungsgebläse oder -verdichter für aggressive und/oder heiße Medien
DE102011053929A1 (de) Turbinenblattspitzenabdeckung zur Verwendung bei einem Spitzenabstandssteuerungssystem
DE19920524A1 (de) Radialverdichter mit Wandschlitzen
DE102019109056A1 (de) Verbrennungsmotor mit turbolader
CH266474A (de) Strahltriebwerk.

Legal Events

Date Code Title Description
8141 Disposal/no request for examination