- Patent Title: Cooling flow for leading panel in a gas turbine engine combustor
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Application No.: US15108107Application Date: 2015-01-09
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Publication No.: US10344979B2Publication Date: 2019-07-09
- Inventor: Frank J. Cunha , Timothy S. Snyder
- 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: Carlson, Gaskey & Olds, P.C.
- International Application: PCT/US2015/010716 WO 20150109
- International Announcement: WO2015/116360 WO 20150806
- Main IPC: F23R3/06
- IPC: F23R3/06 ; F23R3/00 ; F02C3/14 ; F23M5/08 ; F23R3/14 ; F23R3/58

Abstract:
A heat resistant panel has a bulkhead and a swirler adjacent a combustion chamber. The heat resistant panel comprises an inner panel for facing the combustion chamber and defining a first exit port at an upstream end thereof configured to direct cooling air into the combustor chamber in a first direction adjacent the bulkhead. A second exit port at a downstream end thereof is configured to direct cooling air into the combustor chamber in a second direction with an axial direction defined between the upstream and downstream ends. The first and second directions have opposed axial components. A heat resistant structure and a combustor are also disclosed.
Public/Granted literature
- US20160327273A1 Cooling Flow for Leading Panel in a Gas Turbine Engine Combustor Public/Granted day:2016-11-10
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