发明授权
US06692227B2 Stationary blade shroud of a gas turbine 有权
燃气轮机的固定叶片护罩

Stationary blade shroud of a gas turbine
摘要:
A base plate and honeycomb member disposed at the inner circumference side of an inside shroud are fixed to the inside shroud, at a phase deviation in the peripheral direction, with respect to the inside shroud, so as to plug the missing range of seal member, out of gaps between adjacent inside shrouds, and therefore leakage of purge air from the missing range of seal member is prevented without adding new constituent members.
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