Gas turbine engine shroud ring mounting
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United States of America Patent
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-
Jan 26, 1993
Grant Date -
N/A
app pub date -
Nov 30, 1982
filing date -
Dec 30, 1981
priority date (Note) -
Expired
status (Latency Note)
Importance
Abstract
A turbine suitable for a gas turbine engine is provided with a stage of rotary aerofoil blades which is surrounded by a shroud ring made of silicon nitride. In order to minimize load transfer between the shroud ring and the turbine casing the shroud ring is radially supported by and radially spaced apart from the turbine casing by a woven wire mesh array.
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