GAS TURBINE ENGINE AND BLADE FOR GAS TURBINE ENGINE

One embodiment of the present invention is a unique gas turbine engine blade. Another embodiment is a unique gas turbine engine. Other embodiments include apparatuses, systems, devices, hardware, methods, and combinations for gas turbine engines and blades. Further embodiments, forms, features, aspe...

Ausführliche Beschreibung

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Bibliographische Detailangaben
1. Verfasser: SENEFF RICHARD LEX
Format: Patent
Sprache:eng
Schlagworte:
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