Invention Grant
- Patent Title: Swirler mount interface for gas turbine engine combustor
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Application No.: US14911205Application Date: 2014-06-30
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Publication No.: US10101031B2Publication Date: 2018-10-16
- Inventor: Alexander W. Williams , Seth A. Max , Christopher B. Lyons
- Applicant: United Technologies Corporation
- Applicant Address: US CT Farmington
- Assignee: United Technologies Corporation
- Current Assignee: United Technologies Corporation
- Current Assignee Address: US CT Farmington
- Agency: O'Shea Getz P.C.
- International Application: PCT/US2014/044904 WO 20140630
- International Announcement: WO2015/030928 WO 20150305
- Main IPC: F23R3/60
- IPC: F23R3/60 ; F23R3/12 ; F23R3/14 ; F23R3/28
Abstract:
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.
Public/Granted literature
- US20160201915A1 SWIRLER MOUNT INTERFACE FOR GAS TURBINE ENGINE COMBUSTOR Public/Granted day:2016-07-14
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