发明名称 HEAT SHIELD ASSEMBLY WITH DOUBLE LAP JOINT FOR A GAS TURBINE ENGINE
摘要 A heat shield assembly for a gas turbine engine includes a first heat shield segment defined about an axis and a second heat shield segment defined about the axis. A double circumferential lap joint is defined between the first heat shield segment and the second heat shield segment.
申请公布号 EP3008312(A4) 申请公布日期 2016.08.03
申请号 EP20140811460 申请日期 2014.06.12
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 LESLIE, NICHOLAS R.;TATMAN, NEIL L.
分类号 F02C7/24;F01D25/08 主分类号 F02C7/24
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