发明名称 SWIRLER MOUNT INTERFACE FOR A GAS TURBINE ENGINE COMBUSTOR
摘要 A swirler for a combustor of a gas turbine engine includes a swirler outer body with a male snap component and/or female snap component of a snap-fit interface defined around a swirler central longitudinal axis. A bulkhead assembly for a combustor of a gas turbine engine includes a swirler mounted to a bulkhead support shell through a snap-fit interface.
申请公布号 EP3039344(A1) 申请公布日期 2016.07.06
申请号 EP20140839726 申请日期 2014.06.30
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 WILLIAMS, ALEXANDER W.;MAX, SETH A.;LYONS, CHRISTOPHER B.
分类号 F23R3/28;F02C7/22 主分类号 F23R3/28
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