- Patent Title: Non-planar combustor liner panel for a gas turbine engine combustor
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Application No.: US15348619Application Date: 2016-11-10
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Publication No.: US10935236B2Publication Date: 2021-03-02
- 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: F23R3/42
- IPC: F23R3/42 ; F23R3/06 ; F23R3/50 ; F23M5/02 ; F23R3/60 ; F23M5/04 ; F23M5/08 ; F01D9/02 ; F23R3/00
Abstract:
A combustor for a gas turbine engine including a liner panel mounted to a support shell via a multiple of studs, the liner panel including a forward section and an aft section that defines an arcuate surface section therebetween in the axial profile between the forward section and the aft section.
Public/Granted literature
- US20180231249A1 NON-PLANAR COMBUSTOR LINER PANEL FOR A GAS TURBINE ENGINE COMBUSTOR Public/Granted day:2018-08-16
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