GAS TURBINE WITH WELDED COMBUSTOR SHELL

The gas turbine has an annular combustion chamber (3), which is formed on a ring shaped inner and outer shell (8,7), and comprises a parting plane in the inner and outer shell. The inner and outer shell closes the annular combustion chamber in the parting plane by a parting plane weld seam and is fi...

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Bibliographische Detailangaben
Hauptverfasser: HAEHNLE, HARTMUT, MARKOVIC, ALEN, TSCHUOR, REMIGI, SCHNEIDER, LOTHAR
Format: Patent
Sprache:eng ; fre ; ger
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Zusammenfassung:The gas turbine has an annular combustion chamber (3), which is formed on a ring shaped inner and outer shell (8,7), and comprises a parting plane in the inner and outer shell. The inner and outer shell closes the annular combustion chamber in the parting plane by a parting plane weld seam and is film cooling the parting plane weld seam or a part of the parting plane weld seam. An independent claim is included for a method for fixing or replacing of an inner and outer shell of a gas turbine.