Invention Grant
- Patent Title: Swirler for a turbine engine combustor
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Application No.: US15025685Application Date: 2014-10-01
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Publication No.: US10830441B2Publication Date: 2020-11-10
- Inventor: Andreas Sadil , Steven W. Trinks , Jonathan M. Jause
- Applicant: United Technologies Corporation
- Applicant Address: US CT Farmington
- Assignee: Raytheon Technologies Corporation
- Current Assignee: Raytheon Technologies Corporation
- Current Assignee Address: US CT Farmington
- Agency: Getz Balich LLC
- International Application: PCT/US2014/058616 WO 20141001
- International Announcement: WO2015/050986 WO 20150409
- Main IPC: F23R3/28
- IPC: F23R3/28 ; F23R3/14 ; F02C7/236

Abstract:
A swirler is provided for a turbine engine. The swirler includes a swirler housing and a swirler nozzle that is attached to the housing. The housing defines a first inlet and a second inlet. The housing and the nozzle form an inner passage and an outer passage. The inner passage is radially within the nozzle and coupled with the first inlet. The outer passage is radially between the housing and the nozzle and coupled with the second inlet.
Public/Granted literature
- US20160231000A1 SWIRLER FOR A TURBINE ENGINE COMBUSTOR Public/Granted day:2016-08-11
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