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.