STATOR VANE ASSEMBLY FOR A GAS TURBINE ENGINE AND METHOD OF ASSEMBLING THE SAME

A gas turbine engine (20) has a stator vane assembly (200). The stator vane assembly (200) includes an inner diameter shroud (202), an outer diameter shroud (240) located radially outward from the inner diameter shroud (202), a vane (204) extending radially outward from the first inner diameter shro...

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Bibliographic Details
Main Authors BARAINCA, Brian, BAUMANN, Paul W
Format Patent
LanguageEnglish
French
German
Published 16.01.2019
Subjects
BLASTING
ENGINE PLANTS IN GENERAL
HEATING
LIGHTING
MACHINES OR ENGINES IN GENERAL
MECHANICAL ENGINEERING
NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES
NON-POSITIVE DISPLACEMENT PUMPS
POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS
PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
STEAM ENGINES
WEAPONS
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Summary:A gas turbine engine (20) has a stator vane assembly (200). The stator vane assembly (200) includes an inner diameter shroud (202), an outer diameter shroud (240) located radially outward from the inner diameter shroud (202), a vane (204) extending radially outward from the first inner diameter shroud (202) to the outer diameter shroud (240). The wedge clip (206) is positioned horizontally through the vane (204) to prevent the vane (204) from being dislodged from the stator vane assembly (200).
Bibliography:Application Number: EP20180179562