Invention Grant
- Patent Title: Swept combustor liner panels for gas turbine engine combustor
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Application No.: US15031070Application Date: 2014-11-18
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Publication No.: US10473330B2Publication Date: 2019-11-12
- Inventor: Seth A. Max , Kevin J. Low
- 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/US2014/066167 WO 20141118
- International Announcement: WO2015/074052 WO 20150521
- Main IPC: F23R3/04
- IPC: F23R3/04 ; F23R3/06 ; F23R3/10 ; F23R3/00 ; F23R3/58

Abstract:
A liner panel is provided for use in a combustor of a gas turbine engine. The liner panel includes a first liner panel side edge between a liner panel aft edge and a liner panel forward edge. The liner panel also includes a second liner panel side edge between the liner panel aft edge and the liner panel forward edge. The first and the second liner panel side edges are non-perpendicular to the liner panel forward and aft edge edges.
Public/Granted literature
- US20160265771A1 SWEPT COMBUSTOR LINER PANELS FOR GAS TURBINE ENGINE COMBUSTOR Public/Granted day:2016-09-15
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