GAS TURBINE ENGINE AND COOLED FLOWPATH COMPONENT THEREFOR

One embodiment of the present invention is a unique gas turbine engine. Another embodiment of the present invention is a unique cooled gas turbine engine flowpath component. Other embodiments include apparatuses, systems, devices, hardware, methods, and combinations for gas turbine engines and coole...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: MOGA, CORINA, RHODES, JEFFREY, F, LAYNE, JERRY
Format: Patent
Sprache:eng ; fre
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