Axially segmented guide vane mount for a gas turbine

A stator blade carrier for a gas turbine is provided. The stator blade carrier includes a plurality of axial segments. At least one axial segment is designed as a tubular lattice structure. This allows a simpler design technically and a more flexible adaptation to the temperature profile present on...

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Bibliographische Detailangaben
Hauptverfasser:	SCHNEIDER OLIVER, KAHLSTORF UWE, SIMON GERHARD, KLEIN KARL, SHEVCHENKO VADIM, BRYK RODERICH, SHENG SHILUN, THAMM NORBERT, SAVILIUS NICOLAS, HARTMANN MARTIN, LUESEBRINK OLIVER, DUNGS SASCHA, MILAZAR MIRKO
Format:	Patent
Sprache:	eng
Schlagworte:	BLASTING ENGINE PLANTS IN GENERAL HEATING LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES NON-POSITIVE DISPLACEMENT PUMPS POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC FLUIDS STEAM ENGINES WEAPONS
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Beschreibung
Zusammenfassung:	A stator blade carrier for a gas turbine is provided. The stator blade carrier includes a plurality of axial segments. At least one axial segment is designed as a tubular lattice structure. This allows a simpler design technically and a more flexible adaptation to the temperature profile present on the stator blade carrier to maintain operational safety.