发明名称 Low profile attachment hanger system for a cooling liner within a gas turbine engine swivel exhaust duct
摘要 An exhaust duct assembly includes a cooling liner spaced apart from an exhaust duct case that articulate for use in a short take off vertical landing (STOVL) type of aircraft. The cooling liner assembly is attached to the exhaust duct case through a foldable attachment hanger system. The foldable attachment hanger system provides a low profile (foldable up/down) for a limited access installation envelope typical of a three bearing swivel duct (3BSD) which rotates about three bearing planes to permit transition between a cruise configuration and a hover configuration. In this way, each cooling liner segment may be formed as a complete cylindrical member requiring joints only between the swivelable duct sections.
申请公布号 US2008022689(A1) 申请公布日期 2008.01.31
申请号 US20060492412 申请日期 2006.07.25
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 FARAH JORGE L.;HOOP WILLIAM G.
分类号 F02K1/00 主分类号 F02K1/00
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