Invention Grant
- Patent Title: Combustor liner panel with non-linear circumferential edge for a gas turbine engine combustor
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Application No.: US15348639Application Date: 2016-11-10
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Publication No.: US10655853B2Publication Date: 2020-05-19
- Inventor: Steven W. Burd
- 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: Bachman & LaPointe, P.C.
- Main IPC: F23M5/04
- IPC: F23M5/04 ; F23R3/02 ; F01D9/02 ; F23M5/08 ; F23R3/06 ; F23R3/50 ; F23R3/60
Abstract:
A combustor for a gas turbine engine including a forward liner panel mounted to a support shell via a multiple of studs, the forward liner panel including an aft non-linear circumferential edge and an aft liner panel mounted to the support shell via a multiple of studs, the aft liner panel including a forward non-linear circumferential edge that is complementary to the aft non-linear circumferential edge.
Public/Granted literature
- US20180231250A1 COMBUSTOR LINER PANEL WITH NON-LINEAR CIRCUMFERENTIAL EDGE FOR A GAS TURBINE ENGINE COMBUSTOR Public/Granted day:2018-08-16
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