Invention Grant
- Patent Title: Swirler mount interface for gas turbine engine combustor
-
Application No.: US14904490Application Date: 2014-05-15
-
Publication No.: US10088166B2Publication Date: 2018-10-02
- Inventor: Christopher Drake , Seth A. Max , Meggan Harris
- 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/US2014/038198 WO 20140515
- International Announcement: WO2015/017002 WO 20150205
- Main IPC: F23R3/28
- IPC: F23R3/28 ; F23R3/10 ; F23R3/60 ; F02C7/236 ; F23R3/14 ; B23P19/04 ; F02C7/22
Abstract:
A swirler is provided for a gas turbine engine. The swirler includes a swirler body with a threaded section and a multiple of circumferentially arranged tabs operable to flex radially outward. The multiple of circumferentially arranged tabs are radially displaced from the threaded section.
Public/Granted literature
- US20160169521A1 SWIRLER MOUNT INTERFACE FOR GAS TURBINE ENGINE COMBUSTOR Public/Granted day:2016-06-16
Information query
