SPLINE SEAL FOR A GAS TURBINE ENGINE

Embodiments of the invention relate to a turbine assembly 100 including a shroud assembly 102 and a nozzle assembly 106 axially adjacent to each other which both include confronting radial sides 112, 113, 212, 213 and confronting axial ends 110, 210. A spline connector 116, 116a, 116b having a circu...

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Bibliographic Details
Main Authors FELDMANN, Kevin Robert, SMITH, Aaron Ezekiel
Format Patent
LanguageEnglish
French
German
Published 17.01.2018
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:Embodiments of the invention relate to a turbine assembly 100 including a shroud assembly 102 and a nozzle assembly 106 axially adjacent to each other which both include confronting radial sides 112, 113, 212, 213 and confronting axial ends 110, 210. A spline connector 116, 116a, 116b having a circumferential portion 122, 222 and an axial portion such that the circumferential portion 122, 222 of the spline connector 116, 116a, 116b extends across the axial ends 110, 210 and the axial portion of the spline connector 116, 116a, 116b extends across the confronting radial sides 112, 113, 212, 213.
Bibliography:Application Number: EP20170153876