发明名称 TURBINE BLADE TIP CLEARANCE SYSTEM
摘要 A system for adjusting a clearance between blade tips of a turbine and a shroud assembly encircling the turbine in a turbine engine is disclosed herein. The system includes a first fluid passageway operable to extend from a first source of fluid at a variable pressure to a shroud assembly of a turbine engine. The first fluid passageway directs a first stream of fluid to the shroud assembly. The system also includes a first valve positioned along the first fluid passageway and moveable between open and closed configurations. The first valve is biased to the open configuration and moved to the closed configuration passively and directly by a first predetermined level of pressure of the first stream of fluid. During periods of relatively low power production of the turbine engine, the first valve is in the open configuration and moves to the closed configuration when power production of the turbine engine increases from relatively low power production.
申请公布号 US2009208321(A1) 申请公布日期 2009.08.20
申请号 US20080034408 申请日期 2008.02.20
申请人 O'LEARY MARK 发明人 O'LEARY MARK
分类号 F01D11/24;F02C7/12 主分类号 F01D11/24
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