ENGINE AIR SEALING BY SEALS IN SERIES

A gas turbine engine (20) includes a stator vane (72). A blade outer air seal may be adjacent to the stator vane (72). A seal assembly may be disposed between the blade outer air seal and the stator vane (72). The seal assembly may include a first seal (102) disposed between a first airflow path (S)...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	DAVIS, Timothy M, SCHWEITZER, Jaimie, DRAKE, Jeremy, PAULINO, Jose R, TYLER, Jr., Terence P
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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