Gas turbine having a ring channel divided into ring sectors

The invention relates to a gas turbine (1), comprising at least one inner housing part (2) and at least one outer housing part (3), between which two housing parts (2, 3) a ring channel (4) is at least partially arranged, which ring channel circumferentially surrounds the useful flow of the working...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: KAHLSTORF UWE, HUNING MARCUS, GOSSMANN OTMAR
Format: Patent
Sprache:chi ; eng
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Beschreibung
Zusammenfassung:The invention relates to a gas turbine (1), comprising at least one inner housing part (2) and at least one outer housing part (3), between which two housing parts (2, 3) a ring channel (4) is at least partially arranged, which ring channel circumferentially surrounds the useful flow of the working fluid (5) prevailing during operation of the gas turbine (1) and circumferentially surrounds the gas turbine rotor (6), wherein the ring channel (4) is designed to conduct a cooling fluid (8), in particular compressor air, in the circumferential direction, wherein the ring channel (4) is divided into ring sectors in the circumferential direction by means of separators (7), wherein a tube (20) is at least partially provided in the ring channel (4), which tube fluidically connects individual ring sectors (10) to each other, wherein the tube (20) is designed as a distributing tube, which is fluidically connected to at least one cooling-fluid line (9) for conducting cooling fluid and has at least one outlet opening (21