Turbine shroud engagement arrangement and method

A turbine shroud engagement (10) arrangement includes an outer shroud (14) and an inner shroud (18) operably connectable to the outer shroud (14). The outer shroud (14) has at least one of a channel (22) formed in and a protruding member (34) extending from an inner radial surface (28) thereof. The...

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Bibliographic Details
Main Authors Kulkarni, Shruti, Hemadribhotla, Venkata Ramana Murthy, Patil, Ajay Gangadhar
Format Patent
LanguageEnglish
French
German
Published 18.07.2018
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:A turbine shroud engagement (10) arrangement includes an outer shroud (14) and an inner shroud (18) operably connectable to the outer shroud (14). The outer shroud (14) has at least one of a channel (22) formed in and a protruding member (34) extending from an inner radial surface (28) thereof. The inner shroud (18) has at least one of a protruding member (34) extending from an outer radial surface (26) thereof that is complementary to the at least one channel (22) of the outer shroud (14) or a channel (22) formed in the outer radial surface (26) that is complementary to the at least one protruding member (34) of the outer shroud (14). The turbine shroud engagement arrangement (10) is primarily axially slidably engagable and configured to radially support the inner shroud (18) relative to the outer shroud (14).
Bibliography:Application Number: EP20130196018