Turbine vane segment and impingement insert configuration for fail-safe impingement insert retention

The present invention relates generally to cooling gas turbines that are used, for example, for electrical power generation and, more particularly, to the impingement insert to nozzle connection in such gas turbines. An impingement insert sleeve is provided that is adapted to be disposed in a coolan...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: Burdgick, Steven Sebastian, Kellock, Iain Robertson
Format: Patent
Sprache:eng
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