GAS TURBINE ENGINE WITH COOLING PASSAGE CIRCUIT EXTENDING THROUGH BLADE, SEAL AND CERAMIC VANE

A gas turbine engine (20) includes a rotor carrying a blade (68), a ceramic vane (70) adjacent the blade (68), a seal (80) carried on the rotor adjacent the tip of the ceramic vane (70), and a cooling passage circuit (82) extending through the blade (68), the seal (80), and the ceramic vane (70). Th...

Ausführliche Beschreibung

Bibliographische Detailangaben

1. Verfasser:	ZELESKY, Mark F
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	BLASTING ENGINE PLANTS IN GENERAL HEATING LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES STEAM ENGINES WEAPONS
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