COMPONENT FOR A GAS TURBINE ENGINE, CORRESPONDING GAS TURBINE ENGINE AND METHOD OF FORMING AN AIRFOIL

A component for a gas turbine engine includes an airfoil (68) that has a first end. A first platform (82) is located at the first end of the airfoil (68). A compound fillet (120) includes a first fillet portion (124) tangent to the first platform (82) and an airfoil offset (130). A second fillet por...

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Bibliographic Details
Main Authors BERGMAN, Russell J, PARKIN, Jess J
Format Patent
LanguageEnglish
French
German
Published 17.02.2021
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
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Summary:A component for a gas turbine engine includes an airfoil (68) that has a first end. A first platform (82) is located at the first end of the airfoil (68). A compound fillet (120) includes a first fillet portion (124) tangent to the first platform (82) and an airfoil offset (130). A second fillet portion (126) is tangent to a surface of the airfoil (68) and the first fillet portion (124).
Bibliography:Application Number: EP20160158144