ANTI-ROTATION VANE

ANTI-ROTATION VANE

A vane (90) for a gas turbine engine (20) includes a radially inner platform (92) and a radially outer platform (94). At least two airfoils (80, 82) extend between the radially inner platform (92) and the radially outer platform (94). At least two anti-rotation tabs (104a, 104b) extend axially from...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: BERGMAN, Russell J, DABBS, Thurman Carlo
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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Beschreibung
Zusammenfassung:A vane (90) for a gas turbine engine (20) includes a radially inner platform (92) and a radially outer platform (94). At least two airfoils (80, 82) extend between the radially inner platform (92) and the radially outer platform (94). At least two anti-rotation tabs (104a, 104b) extend axially from the radially outer platform (94).