发明申请
US20120070276A1 TURBINE SHROUD THERMAL DISTORTION CONTROL 有权
涡轮机热损失控制

TURBINE SHROUD THERMAL DISTORTION CONTROL
摘要:
A shroud suitable for use in combination with an adjacent rotor blade includes a leading portion comprising a first thickness, and a trailing portion adjacent to the leading portion and comprising a second thickness, wherein the second thickness is less than the first thickness so that stiffness in the leading portion is greater than in the trailing portion and radial expansion by thermal growth of the leading portion of the shroud is constrained.
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