发明申请
US20110229301A1 ACTIVE TIP CLEARANCE CONTROL FOR SHROUDED GAS TURBINE BLADES AND RELATED METHOD 有权
用于气体涡轮叶片的主动提升间隙控制及相关方法

ACTIVE TIP CLEARANCE CONTROL FOR SHROUDED GAS TURBINE BLADES AND RELATED METHOD
摘要:
A turbine bucket tip clearance control system includes a rotor assembly having a rotor supporting a plurality of axially spaced wheels, each wheel mounting an annular row of buckets, the annular row of buckets on at least one of the plurality of axially-spaced wheels having a radially outer tip shroud provided with at least one seal tooth. A stator assembly includes a radially inwardly facing, axially-stepped surface, formed with radially inner and outer seal surfaces connected by a shoulder. The stator assembly and rotor assembly are moveable axially relative to each other, enabling selective positioning of the at least one seal tooth radially opposite one of the radially inner and outer seal surfaces to thereby selectively alter a clearance gap between the at least one seal tooth and the radially inward facing axially-stepped surface.
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