Platform seal strip for a gas turbine

A platform seal strip (1), in particular for use in a gas turbine blade assembly, is described. It comprises an upper side (36), a lower side (37), a first portion (31) and a second portion (32). The width (33) of the first portion (31) is smaller than the width (34) of the second portion (32). The...

Ausführliche Beschreibung

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Bibliographische Detailangaben
1. Verfasser: HEADLAND, PAUL
Format: Patent
Sprache:eng ; fre ; ger
Schlagworte:
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