Method of starting a turbo machine

The method involves operating a fluid-flow machine (101) during exceeding a threshold value characterized for temperature in a preset region of a rotor. The temperature is continuously measured in the preset region of the rotor. A turbine unit (106) and a compressor (102) are arranged on a common tu...

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Hauptverfasser: FLOHR, PATRICK RONALD, HOELL, HARALD, WODITSCHKA, FRANK, BALKOWSKI, INGO, VEITSMAN, VYACHESLAV, AHAUS, GUIDO, LYKO, CHRISTIAN, RICKEN, OLIVER, HECKEL, WALDEMAR, SIEBER, UWE, STOCK, SEBASTIAN
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Sprache:eng ; fre ; ger
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creator FLOHR, PATRICK RONALD
HOELL, HARALD
WODITSCHKA, FRANK
BALKOWSKI, INGO
VEITSMAN, VYACHESLAV
AHAUS, GUIDO
LYKO, CHRISTIAN
RICKEN, OLIVER
HECKEL, WALDEMAR
SIEBER, UWE
STOCK, SEBASTIAN
description The method involves operating a fluid-flow machine (101) during exceeding a threshold value characterized for temperature in a preset region of a rotor. The temperature is continuously measured in the preset region of the rotor. A turbine unit (106) and a compressor (102) are arranged on a common turbine shaft (108). A generator and/or a working machine are supported with the turbine shaft. A set of rotary blades (112) is connected with the turbine shaft. Fixed guide vanes (114) are formed as annular under formation of the guide vanes at a guide vane carrier (116) of the turbine unit. An independent claim is also included for a fluid-flow machine. Ein Verfahren zum Anfahren einer Strömungsmaschine (101) mit einem Rotor soll angegeben werden, welches ein schnelleres Anfahren erlaubt, ohne dabei die Lebensdauer des Rotors zu reduzieren. Dazu wird bei Überschreitung eines für die Temperatur in einem vorgegebenen Bereich des Rotors charakteristischen Grenzwertes die Strömungsmaschine (101) in Betrieb genommen, wobei die Temperatur in dem vorgegebenen Bereich des Rotors gemessen wird.
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The temperature is continuously measured in the preset region of the rotor. A turbine unit (106) and a compressor (102) are arranged on a common turbine shaft (108). A generator and/or a working machine are supported with the turbine shaft. A set of rotary blades (112) is connected with the turbine shaft. Fixed guide vanes (114) are formed as annular under formation of the guide vanes at a guide vane carrier (116) of the turbine unit. An independent claim is also included for a fluid-flow machine. Ein Verfahren zum Anfahren einer Strömungsmaschine (101) mit einem Rotor soll angegeben werden, welches ein schnelleres Anfahren erlaubt, ohne dabei die Lebensdauer des Rotors zu reduzieren. Dazu wird bei Überschreitung eines für die Temperatur in einem vorgegebenen Bereich des Rotors charakteristischen Grenzwertes die Strömungsmaschine (101) in Betrieb genommen, wobei die Temperatur in dem vorgegebenen Bereich des Rotors gemessen wird.</abstract><oa>free_for_read</oa></addata></record>
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language eng ; fre ; ger
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subjects AIR INTAKES FOR JET-PROPULSION PLANTS
BLASTING
CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TOTRANSPORTATION
COMBUSTION ENGINES
CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
ENGINE PLANTS IN GENERAL
GAS-TURBINE PLANTS
GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS
HEATING
HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
INDEXING SCHEME FOR ASPECTS RELATING TONON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES ORJET-PROPULSION PLANTS
INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUSSUBCLASSES OF CLASSES F01-F04
LIGHTING
MACHINES OR ENGINES IN GENERAL
MECHANICAL ENGINEERING
NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES
STEAM ENGINES
TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINSTCLIMATE CHANGE
WEAPONS
title Method of starting a turbo machine
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