Invention Grant
- Patent Title: Gas turbine engine combustor liner assembly with convergent hyperbolic profile
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Application No.: US14765227Application Date: 2014-02-05
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Publication No.: US10174949B2Publication Date: 2019-01-08
- Inventor: Frank J. Cunha , Nurhak Erbas-Sen
- 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/US2014/014819 WO 20140205
- International Announcement: WO2014/189556 WO 20141127
- Main IPC: F23R3/50
- IPC: F23R3/50 ; F23R3/00 ; F23R3/60
Abstract:
A heat shield for a combustor of a gas turbine engine includes a first edge with a first set of cantilevered members and a second edge with a second set of cantilevered members.
Public/Granted literature
- US20150369490A1 GAS TURBINE ENGINE COMBUSTOR LINER ASSEMBLY WITH CONVERGENT HYPERBOLIC PROFILE Public/Granted day:2015-12-24
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