发明名称 OIL LINE INSULATION SYSTEM FOR MID TURBINE FRAME
摘要 A gas turbine engine having a mid turbine frame comprising an annular outer case providing a portion of an engine casing; an interturbine duct (ITD) disposed within the outer case, the ITD including outer and inner rings radially spaced apart one from another and being interconnected by a plurality of radially extending and circumferentially spaced hollow strut fairings, the inner and outer rings co-operating to provide a portion of a hot gas path through the engine; a tube for delivering or discharging a lubricant fluid to or from a bearing housing, the tube extending radially through one of the hollow struts; and an insulation structure radially extending through one said hollow strut fairing, the insulation structure surrounding the tube and being spaced apart from the tube and from a hot internal surface of the one hollow strut fairing for shielding the tube from heat radiated from the hot internal surface of the one hollow strut fairing and for preventing the lubricant fluid from contacting the hot internal surface of said one hollow strut fairing when lubricant fluid leakage occurs.
申请公布号 US2010275572(A1) 申请公布日期 2010.11.04
申请号 US20090433163 申请日期 2009.04.30
申请人 PRATT & WHITNEY CANADA CORP. 发明人 DUROCHER ERIC;LEGARE PIERRE-YVES
分类号 F01D25/18;F02C7/20;F02C7/24 主分类号 F01D25/18
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