Stationary gas turbine with segmented inner ring

The stationary gas turbine has a dividing plane enclosed between a lower housing half and an upper housing half and a segmented inner ring (30) for holding guide vanes, which coaxially surrounds a rotor (3) of the gas turbine and which has multiple guide vanes at the outer periphery in same angular...

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Bibliographische Detailangaben
1. Verfasser:	TIEMANN, PETER
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	BLASTING CYLINDERS ENGINE PLANTS IN GENERAL ENGINEERING ELEMENTS AND UNITS GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS HEATING LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES PISTONS SEALINGS STEAM ENGINES TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION TECHNICAL SUBJECTS COVERED BY FORMER USPC TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS THERMAL INSULATION IN GENERAL WEAPONS
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Beschreibung
Zusammenfassung:	The stationary gas turbine has a dividing plane enclosed between a lower housing half and an upper housing half and a segmented inner ring (30) for holding guide vanes, which coaxially surrounds a rotor (3) of the gas turbine and which has multiple guide vanes at the outer periphery in same angular distances. The guide vanes form a guide vane ring, where inner ring is protected against axial displacement by a retaining ring (40). Die Erfindung betrifft ein eine stationäre Gasturbine mit einem segmentierten Innenring (30). Um eine stationäre Gasturbinen mit einer Teilungsfuge bereitzustellen, bei der der Innenring in alternativer Weise ausgestaltet ist, wird vorgeschlagen, dass der Innenring (30) mittels eines Sicherungsrings (40) gegen axiales Verschieben gesichert ist.