STATOR BLADE SEGMENT OF A THERMAL TURBOMACHINE, ASSOCIATED PRODUCTION METHOD AND ALSO THERMAL TURBOMACHINE

The invention relates to a guide blade segment of a thermal turbomachine, in particular a gas turbine, comprising a number of profiled blades which are arranged on a platform. A plurality of securing elements for securing the guide blade segment to an associated guide blade support are arranged on t...

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Bibliographische Detailangaben
Hauptverfasser:	BOSTANJOGLO GEORG, MATTHEIS THORSTEN, OECHSNER MATTHIAS, BUCHAL TOBIAS, ESSER WINFRIED, PICKERT URSULA, GOLDSCHMIDT DIRK, BERGANDER KATHARINA, KUEPERKOCH RUDOLF, KOCH TORSTEN, MUESGEN RALF, VOSBERG VOLKER, MUENZER JAN
Format:	Patent
Sprache:	eng
Schlagworte:	BLASTING COMBINED OPERATIONS ENGINE PLANTS IN GENERAL HEATING LIGHTING MACHINE TOOLS MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING METAL-WORKING NOT OTHERWISE PROVIDED FOR NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES OTHER WORKING OF METAL PERFORMING OPERATIONS STEAM ENGINES TRANSPORTING UNIVERSAL MACHINE TOOLS WEAPONS
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