STATOR VANE DAMPENING SYSTEM USABLE WITHIN A TURBINE ENGINE

A stator assembly (10) usable in a gas turbine engine (12) and configured to restrain inner and outer endwalls (14, 16) to limit deflection, provide mechanical dampening and prevent clearance loss relative to adjacent blade rotor disks is disclosed. The stator assembly (10) may be formed from a plur...

Ausführliche Beschreibung

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Bibliographische Detailangaben
1. Verfasser: GRIFFIN, Elliot G
Format: Patent
Sprache:eng ; fre
Schlagworte:
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