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...

Full description

Saved in:
Bibliographic Details
Main Authors BERGMAN, Russell J, DABBS, Thurman Carlo
Format Patent
LanguageEnglish
French
German
Published 18.03.2020
Subjects
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
Online AccessGet full text

Cover

More Information
Summary: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).
Bibliography:Application Number: EP20150200315